US20060029491A1 - Roto-dynamic fluidic systems - Google Patents
Roto-dynamic fluidic systems Download PDFInfo
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- US20060029491A1 US20060029491A1 US11/249,553 US24955305A US2006029491A1 US 20060029491 A1 US20060029491 A1 US 20060029491A1 US 24955305 A US24955305 A US 24955305A US 2006029491 A1 US2006029491 A1 US 2006029491A1
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- fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
Definitions
- Hydrodynamic cavitation is a physical phenomenon that involves the formation and collapse of cavities within a liquid.
- the cavities are often filled with a vapor-gas mixture and are typically created by reducing a fluid's local pressure.
- the vapor bubbles once formed, cannot hold their shape, being formed by fluid walls, and their rapid collapse creates mixing, emulsification, dispersion, and kinetic effects which may be useful.
- the fluid is typically near its particular phase transformation at the inception of cavitation, the process can be used for particle dispersion, atomization, and emulsion formation. Sufficient agitation can be imparted such that full vaporization can be accomplished, if so desired.
- the cavitation of certain substances create desired chemical reactions. For example, the cavitation of water produces OH radicals and peroxides which serve to attack any biological contaminants within the water, providing a level of disinfection of the water through the occurrence of cavitation.
- venturi may be formed by a fixed diameter throat that is smaller in diameter than an upstream inlet, smoothly transitioned from the inlet and onward to the outlet, or it may be formed by a simple restriction placed inside a fluid flow field which has a similar effect of raising the fluid's velocity and thus lowering its pressure. This occurs in accordance with Bernoulli's principle which states that for steady flow of an incompressible fluid the pressure will decrease if the velocity increases, and visa versa.
- Embodiments, among others, of the present invention provide an apparatus and method for facilitating cavitation in a fluid.
- the apparatus includes a housing that has a generally hollow interior for receiving a rotor.
- a rotor having an exterior surface is disposed in the housing, and the rotor defines a first opening disposed on the exterior surface and a second opening with a fluid passage extending therebetween.
- the fluid passage facilitates cavitation in a fluid.
- FIG. 1A is an isometric view of a roto-dynamic fluidic system.
- FIG. 1B is an exploded view of a roto-dynamic fluidic system.
- FIG. 2A is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 2B is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 3B is an cross sectional view of a rotor.
- FIG. 3C is an cross sectional view of a rotor.
- FIG. 3D is an cross sectional view of a rotor.
- FIG. 4B is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 4C is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 5 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 6 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 7 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 8 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 9 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 10A is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 10B is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 10C is a perspective view of a rotor.
- FIG. 11 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 12 is an cross sectional view of a roto-dynamic fluidic device.
- FIG. 13 is an cut away/cross sectional view of a rotor.
- a roto-dynamic system 1 includes a roto-dynamic fluidic device 2 and motor 6 .
- the roto-dynamic system 1 is shown in perspective view
- the roto-dynamic fluidic device 2 is shown in exploded from the motor 6 .
- FIG. 2A the roto-dynamic fluidic device 2 is shown and a portion of a shaft 16 in longitudinal cross section
- the roto-dynamic fluidic device is shown in cross section as viewed from line A-A of FIG. 2A .
- the roto-dynamic fluidic device 2 includes a housing 2 , and the housing 2 is coupled to the motor 6 via bolts.
- the housing 4 includes a front plate 8 , which is bolted onto a base portion 10 .
- the base portion 10 defines a cavity 12 , which is generally cylindrical.
- Disposed within the cavity 12 is a rotor 14 , which is held by the shaft 16 .
- the solid line 91 passing through the roto-dynamic fluidic device 2 denotes the center of rotation of the rotor 14 .
- the shaft 16 is longitudinally rotatable and driven by the motive source 6 .
- a sealing element 18 abuts the shaft 16 and prevents fluid from escaping rearward from the cavity 12 .
- the sealing element includes a rubber ring member 113 held in place by tension from a ring member 115 of metal nature.
- other embodiments include other types of seals as would be understood by those skilled in the art.
- a support bearing 20 supports the shaft 16 .
- the rotor 14 is approximately cylindrical in shape having a front face 22 and a rear face 24 and a longitudinal exterior 26 extending therebetween.
- a center void 28 extends from the front 22 of the rotor rearward.
- the region between the center void 28 and the rear face 24 is a boss 105 , and the boss 105 defines an opening 29 that extends between the center void 28 and the rear face 24 .
- a threaded bolt 30 extends from the center void 28 rearward through the opening 29 to the shaft 16 .
- the shaft 16 defines a threaded opening 31 , for engaging the bolt 30 .
- the bolt 30 and shaft 16 are threaded such that during operation, when the rotor 14 is spun, the bolt 30 is tightened.
- the opening 29 is threaded and the shaft 16 has threads on its exterior surface so that the shaft 16 can be threadably received by the rotor 14 .
- the shaft 16 may be formed as part of the rotor, and all such ways of coupling are intended to be within the scope of the invention.
- the rotor 14 can be spherical or have an exterior surface of any other predetermined shape.
- the boss 105 has an exterior 107 that is generally cylindrical shape that tapers inward to a flat head 109 for abutting against the bolt 30 .
- the interior 111 of the boss 105 is adapted to receive the shaft 16 such that when the shaft 16 is beveled or tapered the interior 111 of the boss 105 is complementary configured.
- the rotor 14 is plastic and is formed using injection molding known to those skilled in the art.
- the rotor 14 can also be made from, but is not limited to, metal, which may be made using manufacturing methods such as, but not limited to, die-cast methods, or machining methods, among others known to those skilled in the art.
- the rotor 14 can also be made from ceramics using known methods or from other rigid materials.
- the rotor 14 defines fluid passages 32 having walls 34 .
- the fluid passages 32 extend outward from a first opening 36 to a second opening 38 , which are disposed along the longitudinal exterior 26 of the rotor 14 .
- the rotor 14 is illustrated as having multiple fluid passages 32 with second openings 38 approximately longitudinally aligned.
- the rotor may more, fewer, or no sets of approximately longitudinally aligned second openings 38 or third openings.
- the base portion 10 defines an exterior surface 50 and an interior surface 52 having an opening 54 formed therethrough.
- An outlet/inlet pipe 56 extends outward from the opening 54 and is in communication with the cavity 12 . When fluid flows into the cavity 12 from an inlet/outlet pipe 48 , the fluid flows out the outlet/inlet pipe 56 .
- the base portion 10 also includes a rear wall 11 and a longitudinal wall 101 having an inner surface 103 .
- the rear wall 11 defines an opening 19 , which extends through the rear wall 11 .
- the opening 19 is adapted to receive the shaft 16 so that the shaft 16 can extend from the motive source 6 to the rotor 14 .
- the rotor 14 and cavitation housing 4 have an interstitial clearance 40 that is typically greater than (including magnitudes greater than, in some embodiments) approximately 0.005 inches.
- the interstitial clearance is defined as the distance between the longitudinal exterior surface 26 of the rotor 14 and the inner surface 103 of the longitudinal wall 101 of the base portion 14 .
- the interstitial clearance 40 is typically large enough so that there is no fluid flow restriction, which might reduce the cavitation effect within the fluid passages 32 .
- the interstitial clearance 40 is on the order of multiple feet.
- a roto-dynamic fluidic system for treating municipal waste waster may have interstitial clearances in the range of multiple feet.
- the interstitial clearance is typically large enough so that fluid disposed between the rotor 14 and the housing 4 is not generally cavitated by shear forces induced by spinning the rotor 14 .
- the distance between the front and rear faces of the rotor is approximately the same as the interstitial distance 40 .
- the front plate 8 defines an exterior face 42 and an interior face 44 having an opening 46 formed therethrough.
- a fluid inlet/outlet pipe 48 extends outward from the opening 46 and partially into the cavity 12 .
- the fluid inlet/outlet pipe 48 threadably mates with the opening 46 .
- a fluid flows from a reservoir (not shown) through a hose or pipe, etc. (not shown) into the cavity 12 .
- the inlet/outlet pipe 48 and the center void 28 are operationally aligned such that fluid flowing through the inlet/outlet pipe 48 flows into the center void 28 and, from there, through the fluid passages 32 .
- the front face 22 defines a notch 115 that circumscribes the center void 28 .
- a sealing element 58 is pressed into the notch 115 and extends thereform to the inlet/outlet pipe 48 .
- the sealing element 58 provides an essentially fluid tight seal between the front plate 8 and the rotor 14 so that fluid flowing from the inlet/outlet pipe 48 is directed into the center void 28 .
- sealing elements 18 and 58 include, but are not limited to, lip seals, carbon-element spring loaded seals, packing elements, labyrinth seals, etc.
- the roto-dynamic fluidic device 2 will include three fluid regions: a central region (I); a peripheral region (II); and an intermediate region (III).
- the central region is defined by the inlet/outlet pipe 48 , the sealing element 58 , and the void 28 .
- the peripheral region is the region between the interior surfaces 44 and 52 and the exterior of the rotor 14 .
- the intermediate region is defined as the regions that fluidically connect the central region (I) with the peripheral region (II). If not for the passages 32 , the sealing element 58 would essentially prevent proper fluidic communication between the central region (I) and the peripheral region (II).
- the roto-dynamic fluidic device 2 can be operated such that there is a pressure differential between the pressure of the fluid flowing through the inlet/outlet pipe 48 and the pressure of the fluid flowing out of the outlet/inlet pipe 56 .
- the pressure of the fluid in the inlet/outlet pipe 48 is beneath a given value, the given value depending upon the fluid, the fluid entering the roto-dynamic fluidic device 2 experiences tensile stress induced by the pressure “stretching” the fluid.
- the fluid is not “stretched” to the point that vapor bubbles will form in the fluid prior to the fluid beginning to flow through the passages 32 .
- the pressure at the inlet/outlet pipe 48 is typically within the range of 0 to 100 psi.
- the rotor 14 is spun at rpm levels typically ranging from 70 to 65,000 rpm depending on the dimensional parameters of the rotor 14 itself and the fluid being cavitated.
- fluid flows into the passages 32 through the first openings 36 as the rotor 14 is being spun, and the fluid in the passages 32 experiences centrifugal force induced by the rotation of the rotor 14 .
- the fluid within the passages 32 experience centrifugal force, which results in tensile stresses being developed in the fluid column present within the passage 32 .
- the tensile stress serves as the primary or one of many components that cause vapor bubbles to form within the fluid.
- the fluid exits the passages 32 , and generally the vapor bubbles collapse within the interstitial clearance 40 .
- some or all of the vapor bubbles may collapse within the passages 32 prior to their exiting the passages 32 . It should be also understood that, in other embodiments, when fluid flows radially inward (from the second openings 38 to the first openings 36 ) through the rotor 14 , the fluid undergoes centripetal acceleration which creates a low pressure field proximate to the center of rotation, thereby promoting cavitation in the fluid.
- first opening 36 and the second opening 38 of the passages 32 within the rotor 14 have been shown as being circular in cross section, this is simply in accordance with at least one embodiment.
- the cross section of the first openings 36 , the second openings 38 , and the passages 32 may be, but are not limited to, a circular, or square, or rectangular, or oval, or irregular shape.
- the passages 32 are defined by walls 34 that may be diverging or converging or a combination of both, among others.
- the motive source 6 is illustrated as being proximal to the cavitation housing 4 , this is for illustrative purposes only and is a non-limiting example.
- the shaft 16 having the rotor 14 coupled thereto can be powered by other sources such as, but not limited to, a belt, chain, gear, hydraulic, air, or similar drive means.
- the motive force for the rotor 14 is provided through the provision within the rotor for it to also act as an armature for a brush-type or inductive electric motor with the corresponding components being provided within the housing 4 .
- water pressure from an outside source is used as the motive force for the rotor 14 through the use of a water driven turbine connected rotationally to the rotor 14 of the roto-dynamic fluidic device 2 .
- a magnetic bearing it is advantageous to use a magnetic bearing to reduce the frictional losses within the roto-dynamic fluidic device 2 .
- the rotor 14 is supported by the fluid within the housing 4 by a hydrodynamic bearing through the dimensional configurations of the rotor and housing construction.
- the roto-dynamic fluidic device 2 may act as both a turbine and a cavitation facilitator.
- the roto-dynamic fluidic device 2 includes a hollow rotatable shaft (not shown) that extends through the opening 46 .
- the hollow shaft is supported by a support bearing (not shown), and a sealing element (not shown) abuts the hollow shaft and the interior face 44 of the front plate 8 .
- the hollow shaft is coupled to the rotor 14 pressing the hollow shaft into the void 28 .
- Those skilled in the art are familiar with other ways of coupling the hollow shaft to the rotor 14 , and the other ways are included within the scope of the invention.
- the shaft 16 is a through shaft that extends through the rotor 14 .
- the front plate 8 may also include a support bearing for supporting the through shaft.
- a through shaft can also have a hollow interior, and if the through shaft defines a hollow interior for communicating fluid into (or out of) the roto-dynamic fluidic device 2 , then the through shaft includes ports for communicating fluid.
- a through shaft may be used to communicate a first fluid from one end of the through shaft into the roto-dynamic fluidic device 2 and a second fluid or gas or gaseous-fluid mix into the roto-dynamic fluidic device 2 .
- the ports in the through shaft may be located such that one of the fluids is communicated between the center void 28 and the through shaft and the second fluid is communicated between the region that is exterior to the rotor 14 and the through shaft such that the fluids mix after cavitation.
- the ports can be disposed on the through shaft such that the two fluids mix prior to or during cavitation.
- the inlet/outlet pipe 48 can include a plurality of tubes such that multiple fluids, gases, types of particulate matter, etc. can be injected into the roto-dynamic fluidic device 2 .
- the tubes can be co-axial, and the tubes can be used to inject the substances into different regions of the roto-dynamic fluidic device 2 such that mixture can occur before, during, or after cavitation.
- the roto-dynamic fluidic device 2 preferably provides for controlled cavitation such that when vapor bubbles collapse, the vapor bubbles collapse in predetermined zones such that the mechanical components of the roto-dynamic fluidic device 2 are not harmed. Typically, this is accomplished by providing for substantial laminar flow between the first opening 34 and the second opening 38 or the passage 32 .
- the passages 32 are narrow or any portion of a passage is narrow, then the walls 34 of that portion are smooth so as to facilitate laminar fluid flow.
- the walls can be rough. Fluid flowing in a wide passage having a rough wall can form a turbulent boundary layer proximal to the rough wall, which promotes vapor bubble travel within the flow field region away from the walls.
- FIG. 3A shows a perspective cutaway view of a rotor 14 A having an inducer 60 , which is disposed within a center void 28
- FIG. 3B shows the rotor 14 A in cross section as seen from line B-B.
- the inducer 60 aids the transition of the fluid flow from longitudinal to radial.
- the inducer 60 includes vanes 61 that extend outward from the center of the inducer 60 .
- the inducer 60 and rotor 14 spin as one element on the shaft 16 (not shown, but the shaft is connectable to the rear of the rotor 14 A, as with the boss 105 illustrated in FIG.
- the vanes 61 impart rotational momentum to the fluid in the center void 28 , which enhances fluid flow from the center void 28 into the first openings 36 of the passages 32 .
- the passages 32 extend non-radially from the center void 28 to the exterior surface 26 . However, the passages 32 could also extend radially from the center void 28 to the exterior surface 26 . In various embodiments, passages 32 are preferably circular cylindrical but could be otherwise in other embodiments. In other embodiments, an inducer may be formed by passages formed to impart rotational momentum to the fluid.
- FIG. 3C which is cross sectional view of another embodiment of a rotor 14 B
- the rotor 14 B defines passages 32 that are formed along a curved or irregular path.
- the curvature of the passages 32 is such that when fluid flows through the passages 32 , the fluid helps rotate the rotor 14 c.
- the rotor 14 c defines a plurality of fluid passages 62 having walls 64 .
- Each of the fluid passages 62 includes a feed passage 66 having an inlet opening 67 and a cavitation passage 68 having an outlet opening 69 .
- the feed passage 66 is formed at an angle with respect to the normal of the outer surface 26 of the rotor 14 and extends partially inward towards the center of the rotor 14 .
- the feed passage 66 communicates with the cavitation passage 68 .
- the cavitation passage 68 extends from the inner most portion 70 to the exterior surface 26 of the rotor 14 c .
- the spinning rotor 14 c allows fluid to flow from the interstitial clearance 40 down the feed passage 66 and out the cavitation passage 68 back to the interstitial clearance 40 .
- the cavitation passage 68 can extend radially or non-radially from the inner most portion 70 to the surface 26 .
- the minimum distance (d 1 ) between the inner most portion 70 and a given point 71 on the exterior surface 26 be less than the minimum distance (d 2 ) between the center of rotation 73 of the rotator 14 c and the given point on the exterior surface 26 , where the given point 71 lies upon the shortest line on the surface (d 3 ) extending between the inlet opening 67 and the outlet opening 69 .
- the fluid passages 62 can include a longitudinal component.
- the feed passage 66 could extend tangentially inward (toward the shaft 16 ) and rearward (toward the rear face 24 ) to the inner most portion 70 , and the cavitation passage 68 would extend outward from the inner most portion 70 back to the exterior surface 26 .
- the cavitation passage 68 could also include a longitudinal component such that the cavitation passage 68 could extend both outward from the inner most portion 70 and toward either the front face 22 or the rear face 24 .
- FIG. 4A and FIG. 4B in FIG. 4A the housing 4 and a rotor 14 D are shown in cross section, and in FIG. 4B the housing 4 and the rotor 14 D are shown in cross section as viewed from line C-C.
- the rotor 14 D comprises a hub 74 and a plurality of hollow tubes 72 that extend outward from the hub 74 .
- Each of the tubes 74 is defined by a proximal end 76 and a distal end 78 , relative to the hub 74 .
- the hub 74 defines a generally hollow interior 80 for receiving a fluid via the inlet/outlet pipe 48 .
- the inlet/outlet pipe 48 extends partially into the cavity 12
- the sealing element 58 extends from a notch 82 formed in the hub 74 to the inlet/outlet pipe 48 .
- the peripheral region (II) includes all of the volume of the cavity 12 outside of the rotor 14 and the inlet/outlet pipe 48 .
- the central region (I) is defined by the volume of the inlet/outlet pipe 48 and the hollow interior 80 of the hub 74 .
- the front face 22 defines a discharge port 84 that extends from the interior face 44 to the exterior face 42 .
- the discharge ports 84 enable excess fluid to be discharged from the roto-dynamic fluidic device 2 .
- the front face 22 also defines an opening for receiving an outlet/inlet pipe 56 .
- a fluid 86 A flows into the hollow interior 80 of the hub 74 via the inlet/outlet pipe 48 and through the tubes 72 into the cavity 12 .
- the spinning of the rotor 14 d causes the fluid 86 b in the cavity 12 to spin in conjunction with the rotor 14 d .
- the spinning fluid 86 b experiences centrifugal force, which causes it to push against the interior face 52 of the base portion 10 away from the center of rotation, which for the present embodiment is shaft 16 .
- Fluid that cannot move proximal to the interior face 52 is drained from the cavity 12 via the discharge ports 84 . Due to the centrifugal force experienced by the spinning fluid 86 b , a pressure gradient develops across the spinning fluid.
- the spinning liquid 86 b defines a liquid ring that extends from a fluid-vapor boundary 88 to the interior face 52 .
- the rotational speed of the rotor 14 and the locations of the discharge ports 84 are such that the pressure acting on the fluid at the fluid-vapor boundary 88 is approximately the vapor pressure of the fluid.
- the distal ends 78 are immersed in the fluid ring 86 b , and fluid 86 c in the tubes 72 experiences tensile stress as the rotor 14 d is rotated, thereby causing the formation of vapor bubbles in the fluid in the tubes 72 .
- the vapor bubbles formed by tensile stresses acting on the fluid within the tubes 72 are exposed to the high pressure fluid 86 b when the fluid 86 c exits the distal end 78 of the tubes 72 .
- the high pressure fluid 86 b enhances the collapsing of the vapor bubbles.
- the housing 4 defines a longitudinal center 90 , and the shaft 16 is offset from the longitudinal center 90 .
- the shaft 16 defines a center of rotation 91 that is offset to the left from the longitudinal center 90 , and consequently, the tubes 72 a that are currently in the left half of the housing 4 extend deeper into the fluid ring 86 b than do the tubes 72 b that are currently in the right half of the housing 4 .
- the fluidic pressure exerted on a vapor bubble exiting the distal end 78 of a tube 72 depends upon the instantaneous position of the distal end 78 .
- the rotor 14 E includes a plurality of passages 32 having first openings 36 disposed front face 22 of the rotor 14 E and second openings 38 disposed on the longitudinal surface 26 .
- the interior surface 52 of the base portion 10 defines a notch 93 that extends circumferentially around the rotor 14 E.
- a sealing element 95 extends from the base portion 10 to the longitudinal surface 26 .
- region I is defined to include the inlet/outlet pipe 48 and the volume of space between the interior face 42 of the front plate 16 and the sealing element 58 and the front face 22 of the rotor 14 E.
- Region III is defined as the volume behind the sealing element 95 .
- the passages 32 define region II, and the passages 32 include both straight and curved passages.
- fluid flows into Region I of the roto-dynamic fluidic device 2 , through region II into region III, and from region III out of the roto-dynamic fluidic device 2 .
- the fluid flow is reversed.
- the spinning of the rotor 14 E induces tensile stress in fluid within the region II, thereby causing vapor bubble formation in the fluid therein.
- FIG. 6A shows the housing 4 and a rotor 14 F in cross section.
- the rotor 14 F defines passages 32 A- 32 C, each of the passages 32 have a restrictive section 94 A- 94 C, respectively, where a restrictive section is defined as a region having a relatively narrow cross section or having an obstruction therein.
- the restrictive section 94 is the narrowest region along the length of the passage 32 and is typically narrower than the cross sections of the first opening 36 and the second opening 38 .
- the flow area for the fluid is reduced at the restrictive section 94 which results in an increase in the velocity of the fluid in the restrictive section 94 .
- the fluid experiences a drop in local fluid pressure.
- the region upstream from the restrictive section 94 is defined as the converging section 114
- the region downstream from the restrictive section is defined as the diverging section 116 .
- the restrictive section 94 may be placed anywhere along the passages 32 , but it is preferably located proximal to the second opening 38 .
- the diverging section 116 may be eliminated and the passage 32 can discharge directly into the interstitial region 40 .
- the vapor bubbles typically collapse because the pressure partially recovers after the restrictive section 94 as the fluid enters the diverging section 116 .
- the restrictive section 94 A is defined by a pin 97 A that extends from the front face 22 through a hole 99 into the passage 32 A.
- the pin 97 A is pressed into the hole 99 , but the pin 97 A can also be welded, threaded, glued or otherwise affixed to the rotor 14 F.
- the restrictive section 94 B is defined by the walls 34 tapering inward in a converging section 114 to a minimum clearance section 95 a and then tapering outward as the diverging section 116 .
- the passage 32 C is hexagonal in cross section, and the restrictive section 94 C is defined by a triangularly shaped pin 97 B.
- the pin 97 B extends from the rear face 24 through a hole (not shown) into the passage 32 C.
- the pin 97 C is pressed into the hole, but the pin 97 B can also be welded, threaded, glued or otherwise affixed to the rotor 14 F.
- restrictive sections 94 placed in succession to one another to process the working fluid multiple times. Ports and passageways can be provided for the introduction or removal of elements at given points in the process to affect chemical and physical reactions.
- the multiple restrictive sections 94 are placed linearly one after the other inside the passageways 32 which are used to direct the fluid from one pressure reduction section to the next.
- the restrictive section 94 c is defined by one or more restrictive elements 94 placed in the passage 32 c .
- restrictive elements 94 include a cylinder and other geometrical objects whose cross-sectional area is smaller than the passageway's flow area at the point of insertion such that the fluid is forced through a narrower passage as it passes the restrictive element.
- a moveable restrictive element 94 placed at a chosen location within the fluid passage and held in place by the flow field acting on the exterior surfaces of the moveable restrictive element.
- the moveable restrictive elements 94 may be acted upon by centrifugal or centripetal force which serve to close off the passageway but are prevented from totally shutting off the flow due to the external geometry of the restrictive element 94 , thus providing a changeable means of decreasing the fluid flow area at a chosen point in the passageway and increasing the fluid velocity in this region.
- the moveable restrictive element 94 may be affixed to a spring or springing medium such that the force of the spring acting on the restrictive element acts to maintain a near-constant pressure or flow within the passageway, such as is known to those skilled in the art.
- the moveable restrictive element 94 may be vibrated at a chosen frequency to impart cyclic pressure fluctuations in the fluid, such as is known to those skilled in the art.
- the front 22 of the rotor 14 defines a notch 97 that circumscribes the center void 28 and has the sealing element 58 affixed thereto.
- the sealing element 58 extends from the notch 82 to the inlet/outlet pipe 48 , which extends partially into the cavity 12 and partially past the front 22 of the rotor 14 .
- region I is defined to include the inlet/outlet pipe 48 and the center void 28 .
- Region III is defined as the volume between interior of the housing 4 and the rotor 14 f and the inlet/outlet pipe 48 .
- the passages 32 define region II, and the passages 32 include both straight and curved passages.
- the fluid flow is reversed.
- the spinning of the rotor 14 F induces tensile stress in fluid within the region II, thereby causing vapor bubble formation in the fluid therein.
- the interior face 52 of the housing 2 defines multiple circumferential troughs 96 .
- the design of the circumferential troughs 96 is such that the fluid exiting the rotor 14 G fills the troughs 96 and is brought into rotation around the inside of the cavitation housing 4 by the motion of the rotor 14 .
- a rotating fluid ring 86 forms within the circumferential trough 96 and fluid pressure builds up within the trough 96 in relation to the speed of the rotor.
- the pressure of the fluid within the trough 96 is higher than the pressure of the fluid in the passages 32 , and the higher pressure facilitates the violent collapse of vapor bubbles.
- the liquid ring 86 is driven into rotation by the shearing action of the rotor against the fluid within the housing, and the whirling effect of the fluid exiting the passageways.
- the rotor 14 H includes passages 32 , which have a restrictive section 94 .
- the width between the walls 34 of the passages 32 abruptly narrows in a step like manner at the beginning of the restrictive section 94 , and the restrictive section 94 ends at the exterior surface 26 .
- the interstitial region 40 is a diverging section where cavitation occurs.
- the diverging section 116 may be provided within the passage 32 .
- FIG. 9 which shows a cross sectional view of the housing 2 , a hollow shaft 102 , and a rotor 14 I
- the rear 24 of the rotor 14 I defines an opening 100 for receiving the hollow shaft 102 .
- the opening 100 is configured to receive the hollow shaft 102 such that when the shaft 102 is pressed onto the rotor 14 I, the hollow shaft 102 and rotor 14 move as one element.
- the rotor 14 I includes a plurality of channels 104 that extend outward from a cavity 106 , which is in fluidic communication with the hollow shaft 102 . Each one of the channels 104 intersects and is in fluidic communication with one of the passages 32 at an intersection point 108 .
- the center void 28 receives a first fluid 86 d via the inlet/outlet pipe 48 , which then flows towards the interstitial region 40 via the passages 32 .
- the hollow shaft 102 communicates a second fluid 86 e into the cavity 106 , and the second fluid then flows through the channels 104 to the intersection points 108 .
- the first fluid 86 d and the second fluid 86 e mix together and the resultant fluid 86 f discharges into the interstitial region 40 .
- having the intersection point 108 in proximity to the restrictive section 94 enhances mixing because of the energitics of the destruction of the vapor bubbles formed in the restrictive section 94 .
- the intersection point 108 may be before or after the restrictive section 94 .
- the rotor 14 J is comprised of a front section 110 and a rear section 112 whose cross sections form a converging section 114 and diverging section 116 in passage 32 .
- the interstitial clearance 40 between rotor front section 110 and rotor rear section 112 is typically greater than 0.010 inches to prevent fluid friction from “choking” the device.
- the front section 110 and rear section 112 each define a plurality of aligned pairs holes 118 and 120 , respectively, and each pair of aligned holes is for receiving a connecting member 122 .
- the connecting members 122 extend rigidly between the front section 110 and the rear section 112 such that the front section 110 x and rear section 112 rotate as essentially one element.
- the connecting members 122 are formed in a manner such that they do not substantially block fluid flowing from region I to region II.
- Non-limiting examples of connecting members 122 include rods, pins, bolts, and the like.
- a first fluid 86 d is passed into the cavity 124 of the rotor 14 J via the inlet/outlet pipe 48 .
- Another fluid 86 e is passed into the cavity 124 of the rotor 14 J via the hollow shaft 102 , and the two fluids are mixed in the passage 32 .
- the mixed fluid 86 f exits the passages 32 into the cavity 12 .
- the rear section 112 is attached to the shaft 102 by aligning the opening 100 with the shaft 102 and pressing the rear section 112 onto the shaft 102 .
- Those skilled in the art will recognize other ways of coupling the shaft 102 and the rear section 112 such as, but not limited to, the ways previously described hereinabove, all of which are included within the scope of the invention.
- the fluid experiences centrifugal force as the rotor is spun because the fluid in the rotor spins in conjunction with the rotor.
- the rotational movement of the fluid results in tensile stresses being developed in the fluid.
- the converging section 114 leads to a minimal clearance section 126 which results in an increase in the velocity of the fluid, thereby reducing the local fluid pressure.
- This pressure reduction in cooperation with the tensile stresses already present in the liquid act to cause the fluid to form vapor bubbles which collapse in the diverging section 116 of the passage 32 downstream of minimal clearance section 126 , wherein the pressure partially recovers, completing the cavitation process.
- the same process applies when two fluids are mixed.
- the base portion 10 also defines a single circumferential trough 96 .
- the fluid 86 f in the trough 96 experiences centrifugal force as the rotor 14 J is spun.
- the pressure on the fluid 86 f in the trough 96 is higher than the pressure on the fluid in the diverging section 116 of the rotor 14 J, and the pressure on the fluid in the diverging section 116 is less than the pressure on the fluid in the converging section 14 J.
- FIG. 10B shows a cross sectional view of the housing 2 , the hollow shaft 102 , the rotor 14 J, and a volute ring 128
- FIG. 10C shows an isometric view of the rotor 14 J
- the volute ring 128 is attached to the front section 110 and rear section 112 and spins in conjunction with the front section 110 and rear section 112
- the volute ring 128 includes opposed ends 130 and a peak region 132 that is approximately half-way between the opposed ends 130 .
- the opposed ends 130 are attached to the front section 110 and rear section 112 such that the peak region 132 is approximately aligned with the passage 32 .
- the opposed ends 130 are attached by fasteners and/or adhesives such as, but not limited to, screws, bolts, rivets, welds, and spot welds to the longitudinal surface 26 .
- the volute ring 128 defines a plurality of bleed-off ports 134 for communicating fluid from the region between the volute ring 128 and the rotor 14 J to the exterior of the volute ring 128 .
- the bleed-off ports 134 are configured to drain the volute ring 128 at a chosen rate that maintains a desired pressure within the cavity 12 and maintains a desired pressure gradient in the fluid 86 F trapped by the volute ring 128 .
- one or both of the opposed ends 130 may be raised from the longitudinal exterior 26 by spacers (not shown) or the like such that fluid can escape from the volute ring element 128 by flowing between the volute ring element 128 and the rotor 14 J.
- the volute ring element 128 has the same rotational speed as the front section 110 and rear section 112 , thereby reducing the fluidic shear present in the embodiment shown in FIG. 7 and FIG. 10 a .
- the pressure within the circumferential ring of fluid 86 f formed inside the volute ring element will be greater, which facilitates more violent bubble collapse.
- volute element 128 driven at a speed higher than that of the rotor 14 J to increase the pressure within the fluid 86 f trapped by the volute ring 128 ; the increased pressured caused by the increased rotational speed of the volute ring element 128 .
- the volute ring 128 is not attached to the rotor 14 J and is driven by an outside motive force.
- the volute ring 128 is supported by a bearing element (not shown) surrounding the main input shaft 16 of the roto-dynamic fluidic device 2 , and the volute ring 128 is driven by a planetary gear transmission (not shown) to spin at a chosen rpm higher than that of the rotor 14 J.
- the center gear of the planetary gear transmission being affixed to the input shaft 16 of the device.
- the volute ring element 128 may have a sequence of peaks and valleys between the opposed ends 130 ; the number of peaks related to the type of rotor 14 that the volute ring element 128 is used with.
- the rotor 14 (see FIG. 2A ) includes three sets of fluid passages 32 , each set of passages having second openings 38 that are approximately longitudinally aligned on the longitudinal exterior 26 .
- a volute ring element 128 for use with the rotor 14 a would preferably include three peaks so that each of the peaks is aligned with one of the sets of openings.
- the volute ring element 128 could also include fewer or more peaks because even though it is preferable to coincide the peaks with the sets of openings, it is not is required that the peaks and sets of openings coincide, and a single peak could be wide enough to traverse more than one set of openings.
- the rotor 14 a was described as having sets of openings that are approximately longitudinally aligned. However, it should be remembered that the second openings 38 disposed on the longitudinal exterior 26 need not be disposed such that they are approximately longitudinally aligned. The second openings 38 in any of the non-limiting rotors 14 described hereinabove may disposed in any predetermined configuration or random configuration.
- front section 112 and rear section 1110 may spin at different speeds to each other, or the two elements may counter-rotate with respect to one another through known means, all of which will serve to create small vortices within the minimal clearance 126 , thereby aiding bubble formation.
- the input shaft 102 is connected to the volute element 128 and the rotor 14 J is supported by a bearing mounted on the shaft 102 and allowed to freewheel such that the motive force for the rotor becomes the shearing effect of the fluid between the volute element and the rotor's external surfaces.
- a control means such as a brake (not shown) actuated by control means known to those skilled in the art of speed control.
- the brake is provided to maintain the rotor at a chosen rotational speed, such speed being advantageous for creating the level of cavitation desired within the device, said speed alterations being able to be performed without interfering with the rotation of the volute element and the established circumferential liquid ring therein.
- the rotor 14 K includes a plurality of cavities 136 that extend inward from the exterior surface 26 of the rotor 14 K.
- the cavity 12 of the roto-dynamic fluidic device 2 is essentially filled by both the rotor 14 K and fluid, which enters via inlet/outlet port 48 , and exits via outlet/inlet port 56 .
- tension is created in the fluid due to centripetal force and a vapor bubble is created within cavity 136 .
- the fluid contained within the now filled cavity 136 is propelled in an outwardly radial direction, carrying the recently formed vapor bubble with the fluid flow. In this way the vapor bubble is ejected from cavity 126 and sent into interstitial clearance region 40 .
- the expelled bubbles experience a high pressure field due to the centrifugal force acting on the total fluid mass, which facilitates the implosion of the vapor bubble upon itself, thus completing the cavitation cycle.
- the vapor bubbles may collapse within the cavity 136 prior to their reaching the interstitial clearance 40 . It should be understood that cavities 136 within the rotor may have any predetermined shape.
- Non-limiting examples of cross sections for cavity 126 include circular, or square, or rectangular, or an irregular shape.
- the cavities may have diverging or converging walls which facilitate the creation of tensile stress within the fluid to enhance the formation of vapor bubbles.
- the cavities 136 are disposed on the exterior surface 26 in a irregular/quasi-random or random manner. The irregularity or randomness of the cavities 136 promotes cavitation over regularly spaced cavities 136 because the fluid between the rotor 14 K and the housing 4 is more turbulent than when the cavities 136 are evenly/regularly spaced.
- it is preferred that the opening for a cavity 136 have an abrupt wide edge, instead of a curved round edge, at the upstream portion of the cavity 136 .
- the cavities 136 are defined by inner walls 138 , which is coated with a lining material 140 .
- the lining material 140 can be rough, or smooth, or threaded, or have ridges, or include one or more materials that are different than the rotor material to enhance or hinder reactions that occur when cavitation is present, or have magnetic properties.
- the material 140 includes one or more permanent or electrical magnets that affect chemical processes within the roto-dynamic fluidic device 2 .
- the magnets can be placed upstream or downstream from where vapor bubbles are formed or from where the vapor bubbles collapse.
- electrical magnets are controllable such that their magnet fields can be controlled for strength for the purpose of, among other things, affecting chemical processes within the device.
- the housing may be fitted with such permanent and/or electric magnets in the fluid flow between the surface of the rotor and inner surface of the housing to affect the chemical processes within the device.
- the material 140 includes a membrane.
- the membrane may be located upstream or downstream from where vapor bubbles are formed or from where the vapor bubbles collapse.
- the material 140 includes metal alloys that affect specific chemical reactions or physical elements within the fluid as it passes through the cavity, with or without cavitation occurring.
- one or more cavity(ies) may include a chemical process tube such as disclosed in U.S. Pat. No. 5,048,499; 5,197,446; 5,482,629; or 6,106,787 which are incorporated herein by reference.
- the units or transducers are activated at frequencies that will intensify the cavitation of fluid within one or more selected cavities.
- the inner walls 136 are not lined by material 140 , but are instead themselves rough, or smooth, or threaded, or have ridges, or include one or more materials that are different than the rotor material to enhance or hinder reactions that occur when cavitation is present, or have magnetic properties.
- the rotor 14 L defines undulating passages 32 .
- the passage 32 extends radially outward from the central void 28 to a point of inflection 119 where the passage 32 then extends inward to a second point of inflection 121 . From the second point of inflection 121 , the passage 32 extends to the surface 26 .
- the passage 32 can define more than two points of inflection.
- the rotor 14 L acts as a pump as a fluid is flowing from the center void 28 to the first point of inflection, and the formation of vapor bubbles typically occurs in the region of the second point of inflection. If the passage 32 defines more than one pair of points of inflection, then cavitation may occur in the regions where the flow of the fluid changes from inward to outward.
- the rotor 14 M is used for, among other things, vaporizing a fluid.
- the rotor 14 M defines a passage 32 having a first restrictive element 119 such as for example a nozzle.
- the passage 32 in non-uniformly shaped within the rotor, and preferably, the restrictive element 119 is located at the exterior surface 26 .
- the passage 32 defines a second restrictive element 94 and a diverging section 116 that is down stream from the second restrictive element 94 .
- fluid flows through the second restrictive element 94 , and consequently, the fluid cavitates in the diverging section 116 .
- the fluid is chosen such that the cavitation process creates a phase change in the fluid, or facilitates the combustion of a monopropellant, or of a fuel when air or oxygen is added by additional passages (not shown), such that high pressure is created, whereupon the partially or fully affected fluid is exhausted from the rotor 14 M via the first restrictive element 119 .
- Combustion may be precipitated by known ignition or catalysis means.
- the fluid or gases exiting through the surface of the rotor are directed such that a jet is formed and a force vector that is generally tangential to the surface of the rotor is formed.
- the second restrictive element 119 can be disposed inside of the rotor 14 M
- the rotor 14 M can include secondary channels that intersect with the passage 32 .
- the secondary passages can be used for, among other things, introducing a second fluid, or gas, or exhausting the combusted fluid.
- a fluid can include gases such as, but not limited to, argon, which can be premixed with the fluid before the fluid is received by the roto-dynamic fluidic device or the gas(es) can be mixed with a fluid in the roto-dynamic fluidic device prior to or after the formation of vapor bubbles.
- gases are mixed with the fluid to facilitate (or hinder) certain chemical reactions.
- particulate matter can also be mixed with the fluid. The particulate matter may be introduced to facilitate (or hinder) certain chemical reactions.
- the roto-dynamic fluidic device 2 may include mechanical components such as a ratchet and pawl assembly for, among other things, vibrating the rotor 14 .
- the roto-dynamic fluidic system 1 can be used for, among other things, modifying or aerating fuels, sonochemical reactions, production of nano-materials or nano-fluids, separation/mixing of gases or fluids or particulates, steam production, purification of water, combustion of fuels, and creating special alloys.
Abstract
An apparatus and method for generating cavitation in fluids is disclosed. The apparatus includes a housing for receiving a rotor, which is driven by a motive force. Multiple embodiments of the rotors are disclosed including, but not limited to, centrally feed, centrally drained, face feed, and face drained rotors. In one preferred embodiment, cavitation is enhanced by inducing tensile stress in the fluid by subjecting the fluid centrifugal force or centripital force depending upon the flow of the fluid.
Description
- The present application claims the benefit of the following U.S. Provisional Patent Applications: Ser. No. 60/414,238, filed Sep. 26, 2002; Ser. No. 60/419,751, filed Oct. 18, 2002; Ser. No. 60/428,073, filed Nov. 21, 2002; Ser. No. 60/441,623, filed Jan. 21, 2003; Ser. No. 60/463,689, filed Apr. 16, 2003; Ser. No. 60/448,017, filed Feb. 18, 2003; Ser. No. 60/453,139, filed Mar. 10, 2003; Ser. No. 60/478,881, filed Jun. 16, 2003; and Ser. No. 60/482,707, filed Jun. 20, 2003, all of which are hereby incorporated by reference.
- Hydrodynamic cavitation is a physical phenomenon that involves the formation and collapse of cavities within a liquid. The cavities (bubbles) are often filled with a vapor-gas mixture and are typically created by reducing a fluid's local pressure. The vapor bubbles, once formed, cannot hold their shape, being formed by fluid walls, and their rapid collapse creates mixing, emulsification, dispersion, and kinetic effects which may be useful. Since the fluid is typically near its particular phase transformation at the inception of cavitation, the process can be used for particle dispersion, atomization, and emulsion formation. Sufficient agitation can be imparted such that full vaporization can be accomplished, if so desired. In addition, the cavitation of certain substances create desired chemical reactions. For example, the cavitation of water produces OH radicals and peroxides which serve to attack any biological contaminants within the water, providing a level of disinfection of the water through the occurrence of cavitation.
- The mechanism of the bubble collapse, as described in the field, is that a “finger” of fluid is pulled through the surface of the bubble, which has lower pressure than the surrounding fluid, from a single point (or a small local region) of the bubble's surface. This finger forms a micro-jet of fluid, which strikes the opposing surface of the bubble with great force and speed (measured as being supersonic). This collision creates forces that can be disruptive to the chemical structure of the fluid. Sonochemistry involves the studying of such forces to facilitate various chemical reactions and efforts, including atomization.
- Traditionally, hydrodynamic cavitation is created by pumping a fluid through a venturi of some sort. The restrictive portion of the venturi creates the necessary local velocity increase and corresponding pressure drop, which precipitates cavitation. A venturi may be formed by a fixed diameter throat that is smaller in diameter than an upstream inlet, smoothly transitioned from the inlet and onward to the outlet, or it may be formed by a simple restriction placed inside a fluid flow field which has a similar effect of raising the fluid's velocity and thus lowering its pressure. This occurs in accordance with Bernoulli's principle which states that for steady flow of an incompressible fluid the pressure will decrease if the velocity increases, and visa versa. In the case of a venturi, the restriction causes an increase in the fluid's local velocity and thus lowers its pressure. This can be accomplished through the use of a simple restrictive element as well, although flow losses will be greater. Conventional ventrui systems are held fixed and a fluid is passed through them.
- The pressure reduction created by venturis (or restrictive elements in passages) has been utilized to create cavitation in fluids by reducing a fluid's local pressure to a level below its vaporization pressure, causing vapor bubbles to form in the fluid. These bubbles collapse, in the case of a venturi, once the pressure of the fluid recovers downstream of the venturi throat, the higher relative fluid pressure causing the vapor bubble to implode upon itself with great force.
- It is also observed in experiments that do no involve centrifugal or centripetal forces such as experiments involving stretching a fluid using a piston and cylinder or by cooling a fluid in a fixed volume that vapor bubbles may be created within a fluid through the application of tensile stresses to the fluid. Due to the weak molecular bonds existing within a fluid, once the tensile strength of the fluid is exceeded, the fluid “fractures” and forms a vapor bubble. If the tensile stress within the fluid is removed in a sufficiently rapid fashion, the bubble will collapse, completing the cavitation cycle.
- Embodiments, among others, of the present invention provide an apparatus and method for facilitating cavitation in a fluid.
- Briefly described, in architecture, one embodiment of the apparatus, among others, can be implemented as follows. The apparatus includes a housing that has a generally hollow interior for receiving a rotor. A rotor having an exterior surface is disposed in the housing, and the rotor defines a first opening disposed on the exterior surface and a second opening with a fluid passage extending therebetween. The fluid passage facilitates cavitation in a fluid.
- In another embodiment, an apparatus includes a rotor having a front face, an opposed rear face, and an exterior surface extending therebetween. The exterior surface of the rotor defines an plurality of irregularly spaced cavities disposed thereon.
- Embodiment of the present invention can also be viewed as providing methods for inducing cavitation. In this regard, one embodiment of such a method, among others, can be broadly summarized by the following steps: providing a fluid; and inducing tensile stress in the fluid for facilitating controlled cavitation through rotation.
- Other systems, methods, features, and advantages of the present invention will be or become apparent to one with skill in the art upon examination of the following drawings and detailed description. It is intended that all such additional systems, methods, features, and advantages be included within this description, be within the scope of the present invention, and be protected by the accompanying claims.
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FIG. 1A is an isometric view of a roto-dynamic fluidic system. -
FIG. 1B is an exploded view of a roto-dynamic fluidic system. -
FIG. 2A is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 2B is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 3A is an perspective view with a partial cut away of a rotor. -
FIG. 3B is an cross sectional view of a rotor. -
FIG. 3C is an cross sectional view of a rotor. -
FIG. 3D is an cross sectional view of a rotor. -
FIG. 4A is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 4B is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 4C is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 5 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 6 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 7 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 8 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 9 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 10A is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 10B is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 10C is a perspective view of a rotor. -
FIG. 11 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 12 is an cross sectional view of a roto-dynamic fluidic device. -
FIG. 13 is an cut away/cross sectional view of a rotor. - Many aspects of the preferred embodiments, among others, of the invention can be better understood with reference to the following drawings. The components in the drawings are not necessarily to scale, emphasis instead being placed upon clearly illustrating the principles of the present invention. Moreover, in the drawings, like reference numerals designate corresponding parts throughout the several views. Except for some embodiments in which like numbers denote elements having at least one structural or functional similarity.
- For the purposes of this disclosure the following definitions are provided:
- Vaporization: the formation of vapor bubbles within a fluid at a temperature lower in value than its normal boiling point for a given pressure.
- Cavitation: the formation and subsequent collapse of vapor bubbles within a fluid at a temperature that is below its normal boiling point for a given pressure.
- Centrifugal force: the component of apparent force on a element in curvilinear motion, as observed in the non-inertial reference frame of the element, that is directed away from the axis of rotation in a direct radial vector.
- Centripetal force: the component of force acting on a body in curvilinear motion that is directed toward the center of the axis of rotation as viewed from an inertial reference frame.
- Inertia: the tendency of an element in motion to remain in motion, or for an element at rest to remain at rest, or for an element traveling in one direction to remain traveling along that vector or direction.
- Sonochemistry: the use of the high levels of acoustic energy created within a cavitation bubble collapse event to affect chemical reactions, and applies to cavitation caused by any process, be it ultrasonic excitation of a fluid, or the hydrodynamic manipulation of a fluid to induce cavitation in same, or any other means of creating cavitation within fluids.
- Refer now in more detail to the drawings, in which like numerals indicate corresponding parts throughout the several views. Referring to
FIGS. 1A and 1B andFIGS. 2A and 2B , a roto-dynamic system 1 includes a roto-dynamic fluidic device 2 andmotor 6. InFIG. 1A the roto-dynamic system 1 is shown in perspective view, and inFIG. 1B the roto-dynamic fluidic device 2 is shown in exploded from themotor 6. InFIG. 2A the roto-dynamic fluidic device 2 is shown and a portion of ashaft 16 in longitudinal cross section, and inFIG. 2B the roto-dynamic fluidic device is shown in cross section as viewed from line A-A ofFIG. 2A . The roto-dynamic fluidic device 2 includes ahousing 2, and thehousing 2 is coupled to themotor 6 via bolts. Thehousing 4 includes afront plate 8, which is bolted onto abase portion 10. Thebase portion 10 defines acavity 12, which is generally cylindrical. Disposed within thecavity 12 is arotor 14, which is held by theshaft 16. Thesolid line 91 passing through the roto-dynamic fluidic device 2 denotes the center of rotation of therotor 14. - The
shaft 16 is longitudinally rotatable and driven by themotive source 6. A sealingelement 18 abuts theshaft 16 and prevents fluid from escaping rearward from thecavity 12. Preferably, the sealing element includes a rubber ring member 113 held in place by tension from aring member 115 of metal nature. Of course, other embodiments include other types of seals as would be understood by those skilled in the art. A support bearing 20 supports theshaft 16. - The
rotor 14 is approximately cylindrical in shape having afront face 22 and arear face 24 and alongitudinal exterior 26 extending therebetween. Acenter void 28 extends from thefront 22 of the rotor rearward. The region between thecenter void 28 and therear face 24 is aboss 105, and theboss 105 defines anopening 29 that extends between thecenter void 28 and therear face 24. Typically, a threadedbolt 30 extends from thecenter void 28 rearward through theopening 29 to theshaft 16. Theshaft 16 defines a threadedopening 31, for engaging thebolt 30. Typically, thebolt 30 andshaft 16 are threaded such that during operation, when therotor 14 is spun, thebolt 30 is tightened. In another embodiment, theopening 29 is threaded and theshaft 16 has threads on its exterior surface so that theshaft 16 can be threadably received by therotor 14. Those skilled in the art will recognize other ways of coupling therotor 14 to theshaft 16, such as, but not limited to, pressing, brazing, welding, press-fit, using keys and keyways, splines, geometrically shaped shaft, set screws, clamping elements, bonded, and in addition, the shaft may be formed as part of the rotor, and all such ways of coupling are intended to be within the scope of the invention. - In alternative embodiments, the
rotor 14 can be spherical or have an exterior surface of any other predetermined shape. - Typically, the
boss 105 has an exterior 107 that is generally cylindrical shape that tapers inward to aflat head 109 for abutting against thebolt 30. Theinterior 111 of theboss 105 is adapted to receive theshaft 16 such that when theshaft 16 is beveled or tapered theinterior 111 of theboss 105 is complementary configured. - In one embodiment, the
rotor 14 is plastic and is formed using injection molding known to those skilled in the art. Therotor 14 can also be made from, but is not limited to, metal, which may be made using manufacturing methods such as, but not limited to, die-cast methods, or machining methods, among others known to those skilled in the art. Therotor 14 can also be made from ceramics using known methods or from other rigid materials. - The
rotor 14 definesfluid passages 32 havingwalls 34. Thefluid passages 32 extend outward from afirst opening 36 to asecond opening 38, which are disposed along thelongitudinal exterior 26 of therotor 14. Therotor 14 is illustrated as having multiplefluid passages 32 withsecond openings 38 approximately longitudinally aligned. A first set offluid passages 32 proximal to thefront face 22; a second set offluid passages 32 proximal to therear face 24; and a third set offluid passages 32 interposing the first and second set of fluid passages. However, this is merely one embodiment, and in alternative embodiments, the rotor may more, fewer, or no sets of approximately longitudinally alignedsecond openings 38 or third openings. - The
base portion 10 defines anexterior surface 50 and aninterior surface 52 having an opening 54 formed therethrough. An outlet/inlet pipe 56 extends outward from the opening 54 and is in communication with thecavity 12. When fluid flows into thecavity 12 from an inlet/outlet pipe 48, the fluid flows out the outlet/inlet pipe 56. - The
base portion 10 also includes arear wall 11 and alongitudinal wall 101 having an inner surface 103. Therear wall 11 defines anopening 19, which extends through therear wall 11. Theopening 19 is adapted to receive theshaft 16 so that theshaft 16 can extend from themotive source 6 to therotor 14. - The
rotor 14 andcavitation housing 4 have aninterstitial clearance 40 that is typically greater than (including magnitudes greater than, in some embodiments) approximately 0.005 inches. For the purposes of this disclosure, the interstitial clearance is defined as the distance between thelongitudinal exterior surface 26 of therotor 14 and the inner surface 103 of thelongitudinal wall 101 of thebase portion 14. Theinterstitial clearance 40 is typically large enough so that there is no fluid flow restriction, which might reduce the cavitation effect within thefluid passages 32. In some embodiments, theinterstitial clearance 40 is on the order of multiple feet. For example, a roto-dynamic fluidic system for treating municipal waste waster may have interstitial clearances in the range of multiple feet. In addition, the interstitial clearance is typically large enough so that fluid disposed between therotor 14 and thehousing 4 is not generally cavitated by shear forces induced by spinning therotor 14. Typically, the distance between the front and rear faces of the rotor is approximately the same as theinterstitial distance 40. - The
front plate 8 defines anexterior face 42 and aninterior face 44 having anopening 46 formed therethrough. A fluid inlet/outlet pipe 48 extends outward from theopening 46 and partially into thecavity 12. Typically, the fluid inlet/outlet pipe 48 threadably mates with theopening 46. A fluid flows from a reservoir (not shown) through a hose or pipe, etc. (not shown) into thecavity 12. The inlet/outlet pipe 48 and thecenter void 28 are operationally aligned such that fluid flowing through the inlet/outlet pipe 48 flows into thecenter void 28 and, from there, through thefluid passages 32. - The
front face 22 defines anotch 115 that circumscribes thecenter void 28. A sealingelement 58 is pressed into thenotch 115 and extends thereform to the inlet/outlet pipe 48. The sealingelement 58 provides an essentially fluid tight seal between thefront plate 8 and therotor 14 so that fluid flowing from the inlet/outlet pipe 48 is directed into thecenter void 28. Examples of sealingelements - For the purposes of this disclosure, the roto-
dynamic fluidic device 2 will include three fluid regions: a central region (I); a peripheral region (II); and an intermediate region (III). In the embodiment illustrated inFIG. 1 , the central region is defined by the inlet/outlet pipe 48, the sealingelement 58, and the void 28. The peripheral region is the region between theinterior surfaces rotor 14. The intermediate region is defined as the regions that fluidically connect the central region (I) with the peripheral region (II). If not for thepassages 32, the sealingelement 58 would essentially prevent proper fluidic communication between the central region (I) and the peripheral region (II). - In operation the roto-
dynamic fluidic device 2 can be operated such that there is a pressure differential between the pressure of the fluid flowing through the inlet/outlet pipe 48 and the pressure of the fluid flowing out of the outlet/inlet pipe 56. When the pressure of the fluid in the inlet/outlet pipe 48 is beneath a given value, the given value depending upon the fluid, the fluid entering the roto-dynamic fluidic device 2 experiences tensile stress induced by the pressure “stretching” the fluid. Typically, the fluid is not “stretched” to the point that vapor bubbles will form in the fluid prior to the fluid beginning to flow through thepassages 32. For a fluid such as water, the pressure at the inlet/outlet pipe 48 is typically within the range of 0 to 100 psi. - It should be noted that although the fluid flow into the roto-
dynamic fluidic device 2 has been described as flowing from the inlet/outlet pipe 48, through therotor 14, and out the outlet/inlet pipe 56 that this was done for exemplary purposes only. In another preferred embodiment, the fluid flow is reversed such that fluid flows into the roto-dynamic fluidic device 2 from the outlet/inlet pipe 56 and out the inlet/outlet pipe 48. - The
rotor 14 is spun at rpm levels typically ranging from 70 to 65,000 rpm depending on the dimensional parameters of therotor 14 itself and the fluid being cavitated. In operation, fluid flows into thepassages 32 through thefirst openings 36 as therotor 14 is being spun, and the fluid in thepassages 32 experiences centrifugal force induced by the rotation of therotor 14. The fluid within thepassages 32 experience centrifugal force, which results in tensile stresses being developed in the fluid column present within thepassage 32. Generally, the tensile stress serves as the primary or one of many components that cause vapor bubbles to form within the fluid. The fluid exits thepassages 32, and generally the vapor bubbles collapse within theinterstitial clearance 40. However, in some modes of operation, some or all of the vapor bubbles may collapse within thepassages 32 prior to their exiting thepassages 32. It should be also understood that, in other embodiments, when fluid flows radially inward (from thesecond openings 38 to the first openings 36) through therotor 14, the fluid undergoes centripetal acceleration which creates a low pressure field proximate to the center of rotation, thereby promoting cavitation in the fluid. - Furthermore, it should be understood that although the
first opening 36 and thesecond opening 38 of thepassages 32 within therotor 14 have been shown as being circular in cross section, this is simply in accordance with at least one embodiment. In alternative preferred embodiments, the cross section of thefirst openings 36, thesecond openings 38, and thepassages 32 may be, but are not limited to, a circular, or square, or rectangular, or oval, or irregular shape. Furthermore, alternative preferred embodiments, thepassages 32 are defined bywalls 34 that may be diverging or converging or a combination of both, among others. - Although the
motive source 6 is illustrated as being proximal to thecavitation housing 4, this is for illustrative purposes only and is a non-limiting example. In other embodiments, theshaft 16 having therotor 14 coupled thereto can be powered by other sources such as, but not limited to, a belt, chain, gear, hydraulic, air, or similar drive means. In other embodiments of the invention, the motive force for therotor 14 is provided through the provision within the rotor for it to also act as an armature for a brush-type or inductive electric motor with the corresponding components being provided within thehousing 4. In other preferred embodiments of the invention, water pressure from an outside source is used as the motive force for therotor 14 through the use of a water driven turbine connected rotationally to therotor 14 of the roto-dynamic fluidic device 2. In some implementations of the invention, it is advantageous to use a magnetic bearing to reduce the frictional losses within the roto-dynamic fluidic device 2. In other implementations of the invention, therotor 14 is supported by the fluid within thehousing 4 by a hydrodynamic bearing through the dimensional configurations of the rotor and housing construction. Furthermore, in other implementations, the roto-dynamic fluidic device 2 may act as both a turbine and a cavitation facilitator. - In an alternative embodiment, the roto-
dynamic fluidic device 2 includes a hollow rotatable shaft (not shown) that extends through theopening 46. The hollow shaft is supported by a support bearing (not shown), and a sealing element (not shown) abuts the hollow shaft and theinterior face 44 of thefront plate 8. The hollow shaft is coupled to therotor 14 pressing the hollow shaft into the void 28. Those skilled in the art are familiar with other ways of coupling the hollow shaft to therotor 14, and the other ways are included within the scope of the invention. - In yet another embodiment, the
shaft 16 is a through shaft that extends through therotor 14. In this case, thefront plate 8 may also include a support bearing for supporting the through shaft. As those skilled in the art will recognize, a through shaft can also have a hollow interior, and if the through shaft defines a hollow interior for communicating fluid into (or out of) the roto-dynamic fluidic device 2, then the through shaft includes ports for communicating fluid. In some embodiments, a through shaft may be used to communicate a first fluid from one end of the through shaft into the roto-dynamic fluidic device 2 and a second fluid or gas or gaseous-fluid mix into the roto-dynamic fluidic device 2. The ports in the through shaft may be located such that one of the fluids is communicated between thecenter void 28 and the through shaft and the second fluid is communicated between the region that is exterior to therotor 14 and the through shaft such that the fluids mix after cavitation. Alternatively, the ports can be disposed on the through shaft such that the two fluids mix prior to or during cavitation. - In yet another embodiment, the inlet/
outlet pipe 48 can include a plurality of tubes such that multiple fluids, gases, types of particulate matter, etc. can be injected into the roto-dynamic fluidic device 2. The tubes can be co-axial, and the tubes can be used to inject the substances into different regions of the roto-dynamic fluidic device 2 such that mixture can occur before, during, or after cavitation. - In some embodiments of the invention, the
cavitation housing 4 is an open structure presented to therotor 14 such that fluid can flow into and out of theinterior cavity 12 of thecavitation housing 4. In some implementations of this embodiment, therotor 14 is immersed in an open reservoir, wherein the fluid enters thecenter void 28 of the rotor and exits thepassages 32 via thesecond opening 38. - The roto-
dynamic fluidic device 2 preferably provides for controlled cavitation such that when vapor bubbles collapse, the vapor bubbles collapse in predetermined zones such that the mechanical components of the roto-dynamic fluidic device 2 are not harmed. Typically, this is accomplished by providing for substantial laminar flow between thefirst opening 34 and thesecond opening 38 or thepassage 32. Generally, in some embodiments, if thepassages 32 are narrow or any portion of a passage is narrow, then thewalls 34 of that portion are smooth so as to facilitate laminar fluid flow. Alternatively, in portions of thepassages 32 that are wide, the walls can be rough. Fluid flowing in a wide passage having a rough wall can form a turbulent boundary layer proximal to the rough wall, which promotes vapor bubble travel within the flow field region away from the walls. - The following figures illustrate, alternative embodiments, among others, of the
rotor 14. The following embodiments are intended to be non-limiting and are provided for, among other things, exemplary purposes. -
FIG. 3A shows a perspective cutaway view of arotor 14A having aninducer 60, which is disposed within acenter void 28, andFIG. 3B shows therotor 14A in cross section as seen from line B-B. Theinducer 60 aids the transition of the fluid flow from longitudinal to radial. Theinducer 60 includesvanes 61 that extend outward from the center of theinducer 60. Theinducer 60 androtor 14 spin as one element on the shaft 16 (not shown, but the shaft is connectable to the rear of therotor 14A, as with theboss 105 illustrated inFIG. 2A ), and thevanes 61 impart rotational momentum to the fluid in thecenter void 28, which enhances fluid flow from thecenter void 28 into thefirst openings 36 of thepassages 32. Thepassages 32 extend non-radially from thecenter void 28 to theexterior surface 26. However, thepassages 32 could also extend radially from thecenter void 28 to theexterior surface 26. In various embodiments,passages 32 are preferably circular cylindrical but could be otherwise in other embodiments. In other embodiments, an inducer may be formed by passages formed to impart rotational momentum to the fluid. - Refer to
FIG. 3C , which is cross sectional view of another embodiment of arotor 14B, therotor 14B definespassages 32 that are formed along a curved or irregular path. Preferably, the curvature of thepassages 32 is such that when fluid flows through thepassages 32, the fluid helps rotate the rotor 14 c. - Refer to
FIG. 3 d, which is cross sectional view of another embodiment of arotor 14C, the rotor 14 c defines a plurality offluid passages 62 havingwalls 64. Each of thefluid passages 62 includes afeed passage 66 having aninlet opening 67 and acavitation passage 68 having anoutlet opening 69. Thefeed passage 66 is formed at an angle with respect to the normal of theouter surface 26 of therotor 14 and extends partially inward towards the center of therotor 14. At the innermost portion 70 of thefluid passage 62, thefeed passage 66 communicates with thecavitation passage 68. Thecavitation passage 68 extends from the innermost portion 70 to theexterior surface 26 of the rotor 14 c. In operation, the spinning rotor 14 c allows fluid to flow from theinterstitial clearance 40 down thefeed passage 66 and out thecavitation passage 68 back to theinterstitial clearance 40. As fluid flows through thecavitation passages 68, the fluid experiences tension, thereby producing cavitation in the fluid. Thecavitation passage 68 can extend radially or non-radially from the innermost portion 70 to thesurface 26. In addition, it is preferable that the minimum distance (d1) between the innermost portion 70 and a givenpoint 71 on theexterior surface 26 be less than the minimum distance (d2) between the center of rotation 73 of the rotator 14 c and the given point on theexterior surface 26, where the givenpoint 71 lies upon the shortest line on the surface (d3) extending between theinlet opening 67 and theoutlet opening 69. - In alternative embodiments, the
fluid passages 62 can include a longitudinal component. For example, for a givenfluid passage 62, thefeed passage 66 could extend tangentially inward (toward the shaft 16) and rearward (toward the rear face 24) to the innermost portion 70, and thecavitation passage 68 would extend outward from the innermost portion 70 back to theexterior surface 26. Thecavitation passage 68 could also include a longitudinal component such that thecavitation passage 68 could extend both outward from the innermost portion 70 and toward either thefront face 22 or therear face 24. - Refer to
FIG. 4A andFIG. 4B , inFIG. 4A thehousing 4 and arotor 14D are shown in cross section, and inFIG. 4B thehousing 4 and therotor 14D are shown in cross section as viewed from line C-C. Therotor 14D comprises ahub 74 and a plurality ofhollow tubes 72 that extend outward from thehub 74. Each of thetubes 74 is defined by aproximal end 76 and adistal end 78, relative to thehub 74. Thehub 74 defines a generallyhollow interior 80 for receiving a fluid via the inlet/outlet pipe 48. In this embodiment, the inlet/outlet pipe 48 extends partially into thecavity 12, and the sealingelement 58 extends from anotch 82 formed in thehub 74 to the inlet/outlet pipe 48. In this embodiment, the peripheral region (II) includes all of the volume of thecavity 12 outside of therotor 14 and the inlet/outlet pipe 48. The central region (I) is defined by the volume of the inlet/outlet pipe 48 and thehollow interior 80 of thehub 74. - The
front face 22 defines adischarge port 84 that extends from theinterior face 44 to theexterior face 42. Thedischarge ports 84 enable excess fluid to be discharged from the roto-dynamic fluidic device 2. In this embodiment, thefront face 22 also defines an opening for receiving an outlet/inlet pipe 56. - Refer to
FIG. 4B , a fluid 86A flows into thehollow interior 80 of thehub 74 via the inlet/outlet pipe 48 and through thetubes 72 into thecavity 12. The spinning of therotor 14 d causes the fluid 86 b in thecavity 12 to spin in conjunction with therotor 14 d. Thus, the spinningfluid 86 b experiences centrifugal force, which causes it to push against theinterior face 52 of thebase portion 10 away from the center of rotation, which for the present embodiment isshaft 16. Fluid that cannot move proximal to theinterior face 52 is drained from thecavity 12 via thedischarge ports 84. Due to the centrifugal force experienced by the spinningfluid 86 b, a pressure gradient develops across the spinning fluid. Maximum pressure is experienced at theinterior face 52 of thebase portion 10 and decreases radially inward toward the axis of rotation. The spinningliquid 86 b defines a liquid ring that extends from a fluid-vapor boundary 88 to theinterior face 52. Typically, the rotational speed of therotor 14 and the locations of thedischarge ports 84 are such that the pressure acting on the fluid at the fluid-vapor boundary 88 is approximately the vapor pressure of the fluid. - In operation, the distal ends 78 are immersed in the
fluid ring 86 b, and fluid 86 c in thetubes 72 experiences tensile stress as therotor 14 d is rotated, thereby causing the formation of vapor bubbles in the fluid in thetubes 72. The vapor bubbles formed by tensile stresses acting on the fluid within thetubes 72 are exposed to thehigh pressure fluid 86 b when the fluid 86 c exits thedistal end 78 of thetubes 72. Thehigh pressure fluid 86 b enhances the collapsing of the vapor bubbles. - Refer to
FIG. 4C , in this embodiment, thehousing 4 defines alongitudinal center 90, and theshaft 16 is offset from thelongitudinal center 90. Theshaft 16 defines a center ofrotation 91 that is offset to the left from thelongitudinal center 90, and consequently, thetubes 72 a that are currently in the left half of thehousing 4 extend deeper into thefluid ring 86 b than do thetubes 72 b that are currently in the right half of thehousing 4. In this embodiment, the fluidic pressure exerted on a vapor bubble exiting thedistal end 78 of atube 72 depends upon the instantaneous position of thedistal end 78. - Refer to
FIG. 5 , which shows thehousing 4 and arotor 14E in cross sectional view, therotor 14E includes a plurality ofpassages 32 havingfirst openings 36 disposedfront face 22 of therotor 14E andsecond openings 38 disposed on thelongitudinal surface 26. Theinterior surface 52 of thebase portion 10 defines anotch 93 that extends circumferentially around therotor 14E. A sealingelement 95 extends from thebase portion 10 to thelongitudinal surface 26. Here, region I is defined to include the inlet/outlet pipe 48 and the volume of space between theinterior face 42 of thefront plate 16 and the sealingelement 58 and thefront face 22 of therotor 14E. Region III is defined as the volume behind the sealingelement 95. Thepassages 32 define region II, and thepassages 32 include both straight and curved passages. In one preferred implementation, fluid flows into Region I of the roto-dynamic fluidic device 2, through region II into region III, and from region III out of the roto-dynamic fluidic device 2. In another implementation, the fluid flow is reversed. The spinning of therotor 14E induces tensile stress in fluid within the region II, thereby causing vapor bubble formation in the fluid therein. - Refer to
FIG. 6 ,FIG. 6A shows thehousing 4 and arotor 14F in cross section. Therotor 14F definespassages 32A-32C, each of thepassages 32 have arestrictive section 94A-94C, respectively, where a restrictive section is defined as a region having a relatively narrow cross section or having an obstruction therein. Typically, therestrictive section 94 is the narrowest region along the length of thepassage 32 and is typically narrower than the cross sections of thefirst opening 36 and thesecond opening 38. The flow area for the fluid is reduced at therestrictive section 94 which results in an increase in the velocity of the fluid in therestrictive section 94. As the fluid has passes through therestrictive section 94, the fluid experiences a drop in local fluid pressure. This pressure reduction in cooperation with the tensile stresses already present in the liquid act to cause the fluid to form vapor bubbles which typically collapse after passing through therestrictive section 94, thereby completing the cavitation process. The region upstream from therestrictive section 94 is defined as the convergingsection 114, and the region downstream from the restrictive section is defined as the divergingsection 116. Therestrictive section 94 may be placed anywhere along thepassages 32, but it is preferably located proximal to thesecond opening 38. In some embodiments, the divergingsection 116 may be eliminated and thepassage 32 can discharge directly into theinterstitial region 40. The vapor bubbles typically collapse because the pressure partially recovers after therestrictive section 94 as the fluid enters the divergingsection 116. - In
passage 32A, therestrictive section 94A is defined by apin 97A that extends from thefront face 22 through ahole 99 into thepassage 32A. Typically, thepin 97A is pressed into thehole 99, but thepin 97A can also be welded, threaded, glued or otherwise affixed to therotor 14F. - In
passage 32B, therestrictive section 94B is defined by thewalls 34 tapering inward in a convergingsection 114 to a minimum clearance section 95 a and then tapering outward as the divergingsection 116. - The
passage 32C is hexagonal in cross section, and therestrictive section 94C is defined by a triangularly shapedpin 97B. Thepin 97B extends from therear face 24 through a hole (not shown) into thepassage 32C. The pin 97C is pressed into the hole, but thepin 97B can also be welded, threaded, glued or otherwise affixed to therotor 14F. - In one preferred implementation, there are a series of
restrictive sections 94 placed in succession to one another to process the working fluid multiple times. Ports and passageways can be provided for the introduction or removal of elements at given points in the process to affect chemical and physical reactions. The multiplerestrictive sections 94 are placed linearly one after the other inside thepassageways 32 which are used to direct the fluid from one pressure reduction section to the next. - In passage 32 c, the restrictive section 94 c is defined by one or more
restrictive elements 94 placed in the passage 32 c. Non-limiting examples of arestrictive element 94 include a cylinder and other geometrical objects whose cross-sectional area is smaller than the passageway's flow area at the point of insertion such that the fluid is forced through a narrower passage as it passes the restrictive element. - In some preferred implementations there may be provided a moveable
restrictive element 94 placed at a chosen location within the fluid passage and held in place by the flow field acting on the exterior surfaces of the moveable restrictive element. In other implementations of the invention the moveablerestrictive elements 94 may be acted upon by centrifugal or centripetal force which serve to close off the passageway but are prevented from totally shutting off the flow due to the external geometry of therestrictive element 94, thus providing a changeable means of decreasing the fluid flow area at a chosen point in the passageway and increasing the fluid velocity in this region. In other preferred embodiments the moveablerestrictive element 94 may be affixed to a spring or springing medium such that the force of the spring acting on the restrictive element acts to maintain a near-constant pressure or flow within the passageway, such as is known to those skilled in the art. In other preferred embodiments the moveablerestrictive element 94 may be vibrated at a chosen frequency to impart cyclic pressure fluctuations in the fluid, such as is known to those skilled in the art. - In this embodiment, the
front 22 of therotor 14 defines a notch 97 that circumscribes thecenter void 28 and has the sealingelement 58 affixed thereto. The sealingelement 58 extends from thenotch 82 to the inlet/outlet pipe 48, which extends partially into thecavity 12 and partially past thefront 22 of therotor 14. - Here, region I is defined to include the inlet/
outlet pipe 48 and thecenter void 28. Region III is defined as the volume between interior of thehousing 4 and the rotor 14 f and the inlet/outlet pipe 48. Thepassages 32 define region II, and thepassages 32 include both straight and curved passages. In one preferred implementation, fluid flows into Region I of the roto-dynamic fluidic device 2, through region II into region III, and from region III out of the roto-dynamic fluidic device 2. In another implementation, the fluid flow is reversed. The spinning of therotor 14F induces tensile stress in fluid within the region II, thereby causing vapor bubble formation in the fluid therein. - Refer to
FIG. 7 , which shows thehousing 4 and arotor 14G in cross section, theinterior face 52 of thehousing 2 defines multiplecircumferential troughs 96. The design of thecircumferential troughs 96 is such that the fluid exiting therotor 14G fills thetroughs 96 and is brought into rotation around the inside of thecavitation housing 4 by the motion of therotor 14. A rotatingfluid ring 86 forms within thecircumferential trough 96 and fluid pressure builds up within thetrough 96 in relation to the speed of the rotor. The pressure of the fluid within thetrough 96 is higher than the pressure of the fluid in thepassages 32, and the higher pressure facilitates the violent collapse of vapor bubbles. Theliquid ring 86 is driven into rotation by the shearing action of the rotor against the fluid within the housing, and the whirling effect of the fluid exiting the passageways. - Refer to
FIG. 8 , which shows thehousing 4 and arotor 14H in cross section, therotor 14H includespassages 32, which have arestrictive section 94. In this embodiment, the width between thewalls 34 of thepassages 32 abruptly narrows in a step like manner at the beginning of therestrictive section 94, and therestrictive section 94 ends at theexterior surface 26. Thus, as the fluid flows out of thepassages 32, the fluid is no longer confined by therestrictive section 94. In other words, theinterstitial region 40 is a diverging section where cavitation occurs. In other implementations, the divergingsection 116 may be provided within thepassage 32. - Refer to
FIG. 9 , which shows a cross sectional view of thehousing 2, ahollow shaft 102, and a rotor 14I, the rear 24 of the rotor 14I defines anopening 100 for receiving thehollow shaft 102. Typically, theopening 100 is configured to receive thehollow shaft 102 such that when theshaft 102 is pressed onto the rotor 14I, thehollow shaft 102 androtor 14 move as one element. The rotor 14I includes a plurality ofchannels 104 that extend outward from a cavity 106, which is in fluidic communication with thehollow shaft 102. Each one of thechannels 104 intersects and is in fluidic communication with one of thepassages 32 at anintersection point 108. - In operation, the
center void 28 receives a first fluid 86 d via the inlet/outlet pipe 48, which then flows towards theinterstitial region 40 via thepassages 32. Thehollow shaft 102 communicates a second fluid 86 e into the cavity 106, and the second fluid then flows through thechannels 104 to the intersection points 108. At eachintersection point 108, the first fluid 86 d and the second fluid 86 e mix together and the resultant fluid 86 f discharges into theinterstitial region 40. It should be noted that having theintersection point 108 in proximity to therestrictive section 94 enhances mixing because of the energitics of the destruction of the vapor bubbles formed in therestrictive section 94. However, in alternative embodiments, theintersection point 108 may be before or after therestrictive section 94. - Refer to
FIG. 10A , which shows a cross sectional view of thehousing 2, thehollow shaft 102, and arotor 14J, therotor 14J is comprised of afront section 110 and arear section 112 whose cross sections form a convergingsection 114 and divergingsection 116 inpassage 32. Theinterstitial clearance 40 between rotorfront section 110 and rotorrear section 112 is typically greater than 0.010 inches to prevent fluid friction from “choking” the device. Thefront section 110 andrear section 112 each define a plurality of aligned pairs holes 118 and 120, respectively, and each pair of aligned holes is for receiving a connectingmember 122. The connectingmembers 122 extend rigidly between thefront section 110 and therear section 112 such that the front section 110 x andrear section 112 rotate as essentially one element. The connectingmembers 122 are formed in a manner such that they do not substantially block fluid flowing from region I to region II. Non-limiting examples of connectingmembers 122 include rods, pins, bolts, and the like. - Together the
front section 110 and therear section 112 define acavity 124 that is in fluid communication with the inlet/outlet pipe 48 and thehollow shaft 102. A first fluid 86 d is passed into thecavity 124 of therotor 14J via the inlet/outlet pipe 48. Another fluid 86 e is passed into thecavity 124 of therotor 14J via thehollow shaft 102, and the two fluids are mixed in thepassage 32. The mixed fluid 86 f exits thepassages 32 into thecavity 12. - In this embodiment, the
rear section 112 is attached to theshaft 102 by aligning theopening 100 with theshaft 102 and pressing therear section 112 onto theshaft 102. Those skilled in the art will recognize other ways of coupling theshaft 102 and therear section 112 such as, but not limited to, the ways previously described hereinabove, all of which are included within the scope of the invention. - For operation with a single fluid, the fluid experiences centrifugal force as the rotor is spun because the fluid in the rotor spins in conjunction with the rotor. The rotational movement of the fluid results in tensile stresses being developed in the fluid. The converging
section 114 leads to aminimal clearance section 126 which results in an increase in the velocity of the fluid, thereby reducing the local fluid pressure. This pressure reduction in cooperation with the tensile stresses already present in the liquid act to cause the fluid to form vapor bubbles which collapse in the divergingsection 116 of thepassage 32 downstream ofminimal clearance section 126, wherein the pressure partially recovers, completing the cavitation process. The same process applies when two fluids are mixed. - In this embodiment, the
base portion 10 also defines a singlecircumferential trough 96. In operation, the fluid 86 f in thetrough 96 experiences centrifugal force as therotor 14J is spun. As previously described hereinabove, the pressure on the fluid 86 f in thetrough 96 is higher than the pressure on the fluid in the divergingsection 116 of therotor 14J, and the pressure on the fluid in the divergingsection 116 is less than the pressure on the fluid in the convergingsection 14J. The local pressure reduction in the divergingsection 116 along with the tensile stresses already present in the fluid (the tensile stresses being due to the fluid's rotational movement imparted by the rotor) act to cause the fluid to form vapor bubbles. Some of the vapor bubbles collapse in the divergingsection 116 of thepassage 32 downstream ofminimal clearance section 126. Bubbles that do not collapse in therotor 14J are directed by fluid flow and radial momentum into the relatively higher pressure zone of thecircumferential trough 96, and the increase in pressure as the bubbles move from the lowerpressure diverging section 116 into the higher pressurecircumferential trough 96 enhances the destruction of the bubbles in thetrough 96. - Refer to
FIGS. 10B and 10C ,FIG. 10B shows a cross sectional view of thehousing 2, thehollow shaft 102, therotor 14J, and avolute ring 128, andFIG. 10C shows an isometric view of therotor 14J. Thevolute ring 128 is attached to thefront section 110 andrear section 112 and spins in conjunction with thefront section 110 andrear section 112. In cross section, thevolute ring 128 includes opposed ends 130 and apeak region 132 that is approximately half-way between the opposed ends 130. The opposed ends 130 are attached to thefront section 110 andrear section 112 such that thepeak region 132 is approximately aligned with thepassage 32. Typically, the opposed ends 130 are attached by fasteners and/or adhesives such as, but not limited to, screws, bolts, rivets, welds, and spot welds to thelongitudinal surface 26. Thevolute ring 128 defines a plurality of bleed-offports 134 for communicating fluid from the region between thevolute ring 128 and therotor 14J to the exterior of thevolute ring 128. The bleed-offports 134 are configured to drain thevolute ring 128 at a chosen rate that maintains a desired pressure within thecavity 12 and maintains a desired pressure gradient in the fluid 86F trapped by thevolute ring 128. In an alternative embodiment, one or both of the opposed ends 130 may be raised from thelongitudinal exterior 26 by spacers (not shown) or the like such that fluid can escape from thevolute ring element 128 by flowing between thevolute ring element 128 and therotor 14J. - In this implementation, the
volute ring element 128 has the same rotational speed as thefront section 110 andrear section 112, thereby reducing the fluidic shear present in the embodiment shown inFIG. 7 andFIG. 10 a. With the reduction in fluidic shear provided by the volute ring element inFIG. 10 b, the pressure within the circumferential ring of fluid 86 f formed inside the volute ring element will be greater, which facilitates more violent bubble collapse. In some implementations of the invention it may be desirable to have thevolute element 128 driven at a speed higher than that of therotor 14J to increase the pressure within the fluid 86 f trapped by thevolute ring 128; the increased pressured caused by the increased rotational speed of thevolute ring element 128. In that case, thevolute ring 128 is not attached to therotor 14J and is driven by an outside motive force. In a preferred implementation of the invention, thevolute ring 128 is supported by a bearing element (not shown) surrounding themain input shaft 16 of the roto-dynamic fluidic device 2, and thevolute ring 128 is driven by a planetary gear transmission (not shown) to spin at a chosen rpm higher than that of therotor 14J. The center gear of the planetary gear transmission being affixed to theinput shaft 16 of the device. - In alternative embodiments, the
volute ring element 128 may have a sequence of peaks and valleys between the opposed ends 130; the number of peaks related to the type ofrotor 14 that thevolute ring element 128 is used with. For example, in one non-limiting embodiment, the rotor 14 (seeFIG. 2A ) includes three sets offluid passages 32, each set of passages havingsecond openings 38 that are approximately longitudinally aligned on thelongitudinal exterior 26. (A first set proximal to thefront face 22; a second set proximal to therear face 24; and a third set between the first and second set.) In this case, avolute ring element 128 for use with the rotor 14 a would preferably include three peaks so that each of the peaks is aligned with one of the sets of openings. However, in this embodiment, thevolute ring element 128 could also include fewer or more peaks because even though it is preferable to coincide the peaks with the sets of openings, it is not is required that the peaks and sets of openings coincide, and a single peak could be wide enough to traverse more than one set of openings. For the purposes of discussing a non-limiting embodiment of thevolute ring element 128, the rotor 14 a was described as having sets of openings that are approximately longitudinally aligned. However, it should be remembered that thesecond openings 38 disposed on thelongitudinal exterior 26 need not be disposed such that they are approximately longitudinally aligned. Thesecond openings 38 in any of thenon-limiting rotors 14 described hereinabove may disposed in any predetermined configuration or random configuration. - In another embodiment, the
front section 112 and rear section 1110 may spin at different speeds to each other, or the two elements may counter-rotate with respect to one another through known means, all of which will serve to create small vortices within theminimal clearance 126, thereby aiding bubble formation. - In yet another preferred implementation of the invention, the
input shaft 102 is connected to thevolute element 128 and therotor 14J is supported by a bearing mounted on theshaft 102 and allowed to freewheel such that the motive force for the rotor becomes the shearing effect of the fluid between the volute element and the rotor's external surfaces. In this manner, the speed of the volute element will always be higher than the speed of the rotor and a control means such as a brake (not shown) actuated by control means known to those skilled in the art of speed control. The brake is provided to maintain the rotor at a chosen rotational speed, such speed being advantageous for creating the level of cavitation desired within the device, said speed alterations being able to be performed without interfering with the rotation of the volute element and the established circumferential liquid ring therein. - Refer to
FIG. 11 , which shows a cross sectional view of thehousing 2 and a partial cut away view of arotor 14K, therotor 14K includes a plurality ofcavities 136 that extend inward from theexterior surface 26 of therotor 14K. Thecavity 12 of the roto-dynamic fluidic device 2 is essentially filled by both therotor 14K and fluid, which enters via inlet/outlet port 48, and exits via outlet/inlet port 56. In operation, as the fluid fills anindividual cavity 136 within the spinningrotor 14K, tension is created in the fluid due to centripetal force and a vapor bubble is created withincavity 136. Due to centrifugal forces acting on the fluid, the fluid contained within the now filledcavity 136 is propelled in an outwardly radial direction, carrying the recently formed vapor bubble with the fluid flow. In this way the vapor bubble is ejected fromcavity 126 and sent intointerstitial clearance region 40. Typically, the expelled bubbles experience a high pressure field due to the centrifugal force acting on the total fluid mass, which facilitates the implosion of the vapor bubble upon itself, thus completing the cavitation cycle. In some modes of operation, the vapor bubbles may collapse within thecavity 136 prior to their reaching theinterstitial clearance 40. It should be understood thatcavities 136 within the rotor may have any predetermined shape. Non-limiting examples of cross sections forcavity 126 include circular, or square, or rectangular, or an irregular shape. Furthermore, the cavities may have diverging or converging walls which facilitate the creation of tensile stress within the fluid to enhance the formation of vapor bubbles. Typically, thecavities 136 are disposed on theexterior surface 26 in a irregular/quasi-random or random manner. The irregularity or randomness of thecavities 136 promotes cavitation over regularly spacedcavities 136 because the fluid between therotor 14K and thehousing 4 is more turbulent than when thecavities 136 are evenly/regularly spaced. Furthermore, it is preferred that the opening for acavity 136 have an abrupt wide edge, instead of a curved round edge, at the upstream portion of thecavity 136. - The
cavities 136 are defined byinner walls 138, which is coated with a lining material 140. The lining material 140 can be rough, or smooth, or threaded, or have ridges, or include one or more materials that are different than the rotor material to enhance or hinder reactions that occur when cavitation is present, or have magnetic properties. In one preferred embodiment, the material 140 includes one or more permanent or electrical magnets that affect chemical processes within the roto-dynamic fluidic device 2. The magnets can be placed upstream or downstream from where vapor bubbles are formed or from where the vapor bubbles collapse. Typically, electrical magnets are controllable such that their magnet fields can be controlled for strength for the purpose of, among other things, affecting chemical processes within the device. - Further, the housing may be fitted with such permanent and/or electric magnets in the fluid flow between the surface of the rotor and inner surface of the housing to affect the chemical processes within the device.
- In addition, in one embodiment, the material 140 includes a membrane. The membrane may be located upstream or downstream from where vapor bubbles are formed or from where the vapor bubbles collapse.
- Furthermore, in one embodiment, the material 140 includes metal alloys that affect specific chemical reactions or physical elements within the fluid as it passes through the cavity, with or without cavitation occurring. Further, in these embodiments, one or more cavity(ies) may include a chemical process tube such as disclosed in U.S. Pat. No. 5,048,499; 5,197,446; 5,482,629; or 6,106,787 which are incorporated herein by reference.
- In other preferred embodiments of the invention, there are mechanical or pizeo-electric or electrical ultrasonic transducers placed proximate to the cavities, either within the cavities themselves or in the housing's inner wall, and the transducers enhance or hinder reactions that occur when cavitation is present. Typically, the units or transducers are activated at frequencies that will intensify the cavitation of fluid within one or more selected cavities.
- In yet in another embodiment, the
inner walls 136 are not lined by material 140, but are instead themselves rough, or smooth, or threaded, or have ridges, or include one or more materials that are different than the rotor material to enhance or hinder reactions that occur when cavitation is present, or have magnetic properties. - Refer to
FIG. 12 , which shows arotor 14L and thehousing 2 in cross section, therotor 14L defines undulatingpassages 32. For each one of the passages, thepassage 32 extends radially outward from thecentral void 28 to a point ofinflection 119 where thepassage 32 then extends inward to a second point ofinflection 121. From the second point ofinflection 121, thepassage 32 extends to thesurface 26. In alternative embodiments, thepassage 32 can define more than two points of inflection. Typically, therotor 14L acts as a pump as a fluid is flowing from thecenter void 28 to the first point of inflection, and the formation of vapor bubbles typically occurs in the region of the second point of inflection. If thepassage 32 defines more than one pair of points of inflection, then cavitation may occur in the regions where the flow of the fluid changes from inward to outward. - Refer to
FIG. 13 , which shows a portion of arotor 14M in cross section, therotor 14M is used for, among other things, vaporizing a fluid. Therotor 14M defines apassage 32 having a firstrestrictive element 119 such as for example a nozzle. Preferably, thepassage 32 in non-uniformly shaped within the rotor, and preferably, therestrictive element 119 is located at theexterior surface 26. Thepassage 32 defines a secondrestrictive element 94 and a divergingsection 116 that is down stream from the secondrestrictive element 94. In the preferred embodiment, fluid flows through the secondrestrictive element 94, and consequently, the fluid cavitates in the divergingsection 116. The fluid is chosen such that the cavitation process creates a phase change in the fluid, or facilitates the combustion of a monopropellant, or of a fuel when air or oxygen is added by additional passages (not shown), such that high pressure is created, whereupon the partially or fully affected fluid is exhausted from therotor 14M via the firstrestrictive element 119. Combustion may be precipitated by known ignition or catalysis means. Preferably, the fluid or gases exiting through the surface of the rotor are directed such that a jet is formed and a force vector that is generally tangential to the surface of the rotor is formed. In alternative embodiments, the secondrestrictive element 119 can be disposed inside of therotor 14M Furthermore, in alternative embodiments, therotor 14M can include secondary channels that intersect with thepassage 32. The secondary passages can be used for, among other things, introducing a second fluid, or gas, or exhausting the combusted fluid. - It should be emphasized that a fluid can include gases such as, but not limited to, argon, which can be premixed with the fluid before the fluid is received by the roto-dynamic fluidic device or the gas(es) can be mixed with a fluid in the roto-dynamic fluidic device prior to or after the formation of vapor bubbles. Typically, gases are mixed with the fluid to facilitate (or hinder) certain chemical reactions. In addition, particulate matter can also be mixed with the fluid. The particulate matter may be introduced to facilitate (or hinder) certain chemical reactions.
- In yet another alternative embodiment, the roto-
dynamic fluidic device 2 may include mechanical components such as a ratchet and pawl assembly for, among other things, vibrating therotor 14. - The roto-
dynamic fluidic system 1 can be used for, among other things, modifying or aerating fuels, sonochemical reactions, production of nano-materials or nano-fluids, separation/mixing of gases or fluids or particulates, steam production, purification of water, combustion of fuels, and creating special alloys. - It should be emphasized that the above-described embodiments of the present invention, particularly, any “preferred” embodiments, are merely possible examples of implementations, merely set forth for a clear understanding of the principles of the invention and that the embodiments disclosed hereinabove are non-limiting embodiments. Many variations and modifications may be made to the above-described embodiment(s) of the invention without departing substantially from the spirit and principles of the invention. Alternative embodiments may include more or fewer elements than were illustrated in the various non-limiting described embodiments. For example, the
inducer 60 could be included in any one or none of the described embodiments. Similarly, it should be remembered that in the interest of brevity and clarity fluid flow was normally described in one direction, but the fluid flow can be reversed in each of the embodiments described hereinabove with appropriate modification where necessary. For example, if the fluid flow were reversed in rotor 14 f, then the passage 32 b would also be reversed such that thewalls 34 would taper inward from thesecond opening 38 to the minimum clearance 95 b and then expand in a step like manner. All such modifications and variations are intended to be included herein within the scope of this disclosure and the present invention and protected by the following claims.
Claims (20)
1. An apparatus for facilitating cavitation in fluids, the apparatus comprising:
a housing having a generally hollow interior, the housing defining a first opening for receiving a shaft;
a rotor disposed within the hollow interior of the housing, the rotor adapted to couple with a shaft, the rotor having an exterior surface, the rotor defining a first opening disposed on the exterior surface and a second opening with a fluid passage extending therebetween, wherein the fluid passage facilitates cavitation in a fluid.
2. The apparatus of claim 1 , wherein the housing defines a fluid ingress opening and a fluid egress opening, and the rotor includes a front face and an opposed rear face with a longitudinal exterior surface extending therebetween, wherein the front face defines a void extending rearward toward the rear face, the rotor defining a fluid passage extending generally outward from the void to the longitudinal exterior surface, wherein responsive to rotation of the rotor and fluid flowing through fluid passage in the rotor, cavitation occurs in the fluid.
3. The apparatus of claim 2 , wherein the fluid ingress opening is aligned with the void of the rotor such that fluid flowing from the fluid ingress opening is received by the void.
4. The apparatus of claim 2 , wherein the fluid engress opening is aligned with the void of the rotor such that fluid flowing from the void is received by the fluid egress.
5. The apparatus of claim 2 , wherein a given opening selected from a set of openings consisting of the fluid ingress opening and the fluid egress opening is generally aligned with the void, and further including:
a fluid seal abutting the rotor, the fluid seal generally aligned with the void and the given opening, wherein the fluid seal substantially communicates direct fluid flow between the given opening and the void.
6. The apparatus of claim 5 , further including:
a pipe received by the given opening, the pipe extending at least partially into the hollow interior of the housing.
7. The apparatus of claim 6 , wherein the front face of the rotor defines a notch extending around the circumference of the void, wherein the fluid seal fixedly abuts the notch and extends therefrom to the pipe.
8. The apparatus of claim 2 , wherein the fluid passage includes a point of minimal clearance such that on one side of the point fluid in the fluid passage is at a higher pressure than fluid on the opposite side of the point.
9. The apparatus of claim 2 , wherein the housing includes a front face having the fluid ingress and egress openings formed therein.
10. The apparatus of claim 2 , further including:
a shaft defining a hollow interior in communication with the void, wherein a non-fluid flows either into or out of the housing via the hollow shaft.
11. The apparatus of claim 2 , wherein the housing includes a face plate and a base portion, wherein the face plate defines only one opening for providing fluid flow, the one opening being either the fluid ingress or the fluid egress opening.
12. The apparatus of claim 2 , wherein the housing includes a face plate and a base portion, wherein the face plate defines multiple openings for providing fluid flow, the multiple openings including the fluid ingress opening and the fluid egress opening.
13. The apparatus of claim 2 , further including:
a restrictive element disposed in the fluid passage, wherein fluid in the fluid pressure on one side of the restrictive element is at a higher pressure than fluid on the opposite side of the restrictive element.
14. The apparatus of claim 13 , further including:
a second restrictive element disposed in the fluid passage, wherein fluid in the fluid passage on one side of the second restrictive element is at a higher pressure than fluid on the opposite side of the second restrictive element.
15. The apparatus of claim 13 , further including:
a restrictive element biaser adapted to bias the restrictive element such that fluid flow past the restrictive element is approximately at a predetermined value.
16. The apparatus of claim 2 , wherein the housing includes a base portion and a face plate, the base portion having an inner wall defining the hollow interior of the housing, and the inner wall defines a circumferential trough about the rotor.
17. The apparatus of claim 2 , wherein fluid flows into the void of the rotor, through the passage of the rotor, and into the circumferential trough, wherein responsive to spinning of the rotor and fluid flowing through the apparatus, the fluid in the circumferential trough spins about an axis defined by the rotor, the spinning fluid having a pressure gradient with maximum pressure distal from the rotor.
18. The apparatus of claim 2 , further including:
a transducer disposed within the housing, the transducer adapted to emit ultrasonic energy into the cavity.
19. The apparatus of claim 18 , wherein the transducer is affixed to the rotor.
20. The apparatus of claim 2 , further including:
a volute ring circumferentially disposed around the rotor, the volute ring adapted to spin about an axis and receive fluid from the rotor, wherein responsive to the volute ring spinning about the axis and having a fluid therein, the fluid develops a pressure gradient with maximum pressure distal from the axis.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/249,553 US20060029491A1 (en) | 2002-09-26 | 2005-10-13 | Roto-dynamic fluidic systems |
Applications Claiming Priority (11)
Application Number | Priority Date | Filing Date | Title |
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US41423802P | 2002-09-26 | 2002-09-26 | |
US41975102P | 2002-10-18 | 2002-10-18 | |
US42807302P | 2002-11-21 | 2002-11-21 | |
US44162303P | 2003-01-21 | 2003-01-21 | |
US44801703P | 2003-02-18 | 2003-02-18 | |
US45313903P | 2003-03-10 | 2003-03-10 | |
US46368903P | 2003-04-16 | 2003-04-16 | |
US47888103P | 2003-06-16 | 2003-06-16 | |
US48270703P | 2003-06-26 | 2003-06-26 | |
US10/672,509 US6974305B2 (en) | 2002-09-26 | 2003-09-26 | Roto-dynamic fluidic systems |
US11/249,553 US20060029491A1 (en) | 2002-09-26 | 2005-10-13 | Roto-dynamic fluidic systems |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US10/672,509 Continuation-In-Part US6974305B2 (en) | 2002-09-26 | 2003-09-26 | Roto-dynamic fluidic systems |
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US20060029491A1 true US20060029491A1 (en) | 2006-02-09 |
Family
ID=32034568
Family Applications (1)
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US11/249,553 Abandoned US20060029491A1 (en) | 2002-09-26 | 2005-10-13 | Roto-dynamic fluidic systems |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080228205A1 (en) * | 2004-01-09 | 2008-09-18 | Cardiokinetix, Inc. | Ventricular partitioning device |
ITAN20100123A1 (en) * | 2010-07-22 | 2012-01-23 | Ernesto Panti | CENTRIPETA IMPELLER IMPROVED AND CENTRIPETA TURBINE EQUIPPED WITH THIS IMPELLER. |
RU2599454C2 (en) * | 2015-01-29 | 2016-10-10 | Федеральное агентство научных организаций Федеральное Государственное Бюджетное Научное Учреждение Всероссийский научно-исследовательский институт электрификации сельского хозяйства (ФГБНУ ВИЭСХ) | Free power radial turbine with cylindrical rotor |
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ITAN20100123A1 (en) * | 2010-07-22 | 2012-01-23 | Ernesto Panti | CENTRIPETA IMPELLER IMPROVED AND CENTRIPETA TURBINE EQUIPPED WITH THIS IMPELLER. |
RU2599454C2 (en) * | 2015-01-29 | 2016-10-10 | Федеральное агентство научных организаций Федеральное Государственное Бюджетное Научное Учреждение Всероссийский научно-исследовательский институт электрификации сельского хозяйства (ФГБНУ ВИЭСХ) | Free power radial turbine with cylindrical rotor |
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