US3589833A

US3589833A - Marine propeller attachment and assembly

Info

Publication number: US3589833A
Application number: US876523A
Authority: US
Inventors: Diore Louis Lancioni
Original assignee: MICHIGAN WHEEL CO
Current assignee: Michigan Wheel Corp; MICHIGAN WHEEL CO
Priority date: 1969-11-13
Filing date: 1969-11-13
Publication date: 1971-06-29
Anticipated expiration: 1988-06-29

Abstract

Anticavitation, flow-through propeller attachment and combination employing inner and outer concentric but axially displaced rings, the inner being forwardly of the outer and attachable at the mounting of the propeller hub to the drive shaft. The outer ring is connected to the inner ring by radially and rearwardly extending spokes that form generally V-shaped recesses with the outer ring to receive the rear edge of the hub. The outer ring extends forwardly around the hub rear edge, terminating in a waterflow-controlling forward face and shearing edge.

Description

United States Patent Inventor Diore Louis Lancioni Grand Rapids, Mich.

A pl. No. 876,523

Filed Nov. 13, 1969 Patented June 29, 1971 Assignee Michigan Wheel Company Grand Rapids, Mich.

MARINE PROPELLER ATTACHMENT AND ASSEMBLY 9 Claims, 6 Drawing Figs.

U.S. Cl 416/62,

416/93, 416/193 Int. Cl B63h 1/18 Field of Search 416/62, 93, 193

[56] References Cited UNITED STATES PATENTS 2,458,785 l/l949 Kottke 416/62 3,102,506 9/1963 Kiekhaefer. 416/193 3,246,698 4/1966 Kiekhaefer.... 416/93 (M) 3,356,151 12/1967 Strang 416/93 (M) Primary Examiner-Everette A. Powell, Jr.

Attorney-Price, Heneveld, Huizenga & Cooper ABSTRACT: Anticavitation, flow-through propeller attachment and combination employing inner and outer concentric but axially displaced rings, the inner being forwardly of the outer and attachable at the mounting of the propeller hub to the drive shaft. The outerring is connected to the inner ring by radially and rearwardly extending spokes that form generally V-shaped recesses with the outer ring to receive the rear edge of the hub. The outer ring extends forwardly around the hub rear edge, terminating in a waterflow-controlling forward face and shearing edge.

MARINE PROPELLER ATTACHMENT AND ASSEMBLY BACKGROUND OF THE INVENTION This invention relates to flow-through propeller apparatus and more particularly to an anticavitation attachment for a flow-through propeller, and the combination thereof.

The substantial power output of marine, pleasure craft engines in recent times has accentuated the age-old problem of cavitation-ventilation around the propeller blades. This includes flow-through propellers. Several different and specialized propeller constructions have been devised by a few of the manufacturers in efforts to lessen cavitation. Some of these seem to be somewhat effective. However, purchasers frequently do not purchase these specialized units, probably because of unawareness of the problem, or because of high cost, or because of conflicting claims made for the specialized units, or other reasons. Further, once a conventional propeller is purchased, the cost of another specialized one is quite prohibitive.

SUMMARY OF THE INVENTION It is an object of this invention to provide a unique anticavitation attachment to a flow-through propeller, whereby a ring extending around the periphery of the propeller hub governs waterflow characteristics for anticavitation purposes. The novel ring attachment has a special relationship between .the outer ring and axially and radially extending spokes, t fit onto the rear end portion of the flow-through hub.

The novel attachment unit is relatively inexpensive in comparison to a special propeller. It can be attached in a minute or two, simply by removing the nut that retains the propeller in place, positioning the attachment, and replacing the nut. It operates in combination with the hub, forming a part of the assembly. It can be purchased as part of a new propeller assembly, or can be purchased for combination with a used propeller. The unit has proven in tests to have desirable anticavitation action.

These and other objects, features, and advantages will be apparent upon studying the following specification in conjunction with the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view of the combination flowthrough propeller and anticavitation attachment;

FIG. 2 is an enlarged side elevational view of the anticavitation attachment;

FIG. 3 is a rear end elevational view of the combination in FIG. 1, with the securement nut removed;

FIG. 4 is a sectional, fragmentary, side elevational view of the rear end portion of the flow-through propeller and attachment combination;

FIG. 5 is a perspective view showing a'modified form of the attachment in combination with a flow-through propeller; and

FIG. 6 is a side elevational enlarged view'of the modified attachment in FIG. 5.

DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now specifically to the drawings, the combination 10 there illustrated includes the subcombination flow-through propeller l2 and the subcombination anticavitation attachment l4.

Flow-through propeller subassembly 12, in operation, is attached to the conventional depending underwater power assembly (not shown) of a conventional marine engine apparatus (not shown). The flow-through propeller subassembly is normally attached to a splined drive shaft (not shown) which extends through the center of the hollow hub. One typical attachment of the propeller assembly to the drive shaft employs the illustrated resilient, cooperably configurated bushing 16, as of rubber, which is housed by and secured to a surrounding collar 18. The rearward end of collar 18 projects radially inwardly-behind bushing 16 to'form a rear mounting surface 18' and to retain bushing 16. Shaft-receiving openings 16a and 18a in the bushing and collar are aligned when assembled. Collar 18 is in turn secured to an outer sleeve 20 by a plurality, here three, of struts 22, defining arcuate exhaust flow-through passages 24 therebetween (FIG. 3). Outer sleeve 20 extends rearwardly considerably further than the mounting means formed by

elements

16 and 18 to define a cylindrical passage communicating with the arcuate passages 22 for flow of the exhaust gases therethrough and out the open rear end of the sleeve into the water.

A plurality of propeller blades 26 project radially from the outer periphery of sleeve 20.

The rear cylindrical end of outer sleeve 20 of the hub assembly preferably has a taper on its inner surface, such taper being rearwardly-outwardly at an angle of about l5-20 to the axis.

Anticavitation subassemably 14 cooperates with the rear of the flow-through propeller. Specifically, subassembly 14 includes an outer ring 30, an inner ring 32, and a plurality of spokes 34 therebetweenflnner ring 32 is considerably forwardly offset, axially, with respect to outer ring 30, is smaller,

and is concentric therewith. The forward face of inner ring 32 is an abutment surface to engage the rear surface 18' of the mounting means for the hub subassembly. It includes a cylindrical passage 32a that aligns with passages 16a and 18a for extension of the drive shaft therethrough, so that the threaded securement nut 36 can mount subassembly 14 as well as subassembly 12 on the drive shaft. Spokes 34 extend from inner mounting ring 32 radially outwardly and rearwardly back to outer ring 30. These spokes join with outer ring 30 rearwardly of the forward portion of ring 30, for example at the rear end portion of ring 30, defining a plurality of generally V-shaped recesses or pockets 40 between the spokes and the outer ring. These pockets are radially positioned and oriented to receive the rear terminal edge portion of sleeve 20 of the hub subassembly as shown in FIG. 4. Outer ring 30 extends forwardly of the rear edge of sleeve 20, over a portion of. the outer periphery of the hub subassembly, fitting tightly against surface portions, e.g. 20a, of this hub to prevent waterflow between the hub and the attachment.

The forward portion of outer ring 30 is a radially extending face 30a around the periphery of the hub and projecting radially outwardly therefrom, and terminating at the outer peripheral edge in a water-shearing edge 30b. Surface 30a is preferably substantially normal to the hub axis, or forwardly at a small acute angle of about l020 to the normal. Preferably, the peripheral surface of outer ring 30 slopes radially inwardly-rearwardly away from this shearing edge 30b. In other words, this edge 32b should be at an acute angle.

It is intended that a stagnant water zone be created immediately forwardly of face 30a, with the water flowing over the stagnant zone causing a shearing action over the edge 30b at the juncture of front face 30a with the peripheral surface of ring 30, altering the velocity gradients and therefore the pressure gradient. The exhaust gases that flow out the rear end of the hub tend to curl around the hub edge and follow forwardly along the low-pressure zone that occurs along the hub periphery. The attachment ring shears OK the gases as they reach the shearing edge 30b and hence before they reach the vicinity of the propeller blades.

A less preferred form of the device is illustrated in FIGS. 5 and 6 to include the same subassembly 12 and a slightly modified attachment subassembly 140. In this modified device, the forward inner smaller mounting ring 132 is thinner, the rearwardly radially outwardly extending spokes 134 are straight rather than curvilinear, and the rearward outward ring is basically cylindrical in configuration, rather than frustoconical as in the preferred previously described form.

It is conceivable that certain minor deviations in construction may be made in the apparatus illustrated without departing from the concept presented.

The embodiments of the invention in which an exclusive property or privilege I claim are defined as follows.

1. A fluid flow control, anticavitation ring unit attachment to the annular rear edge of a flow-through propeller hub comprising: an outer peripheral ring, an inner attachment ring, and a plurality of spokes connecting said rings; said outer ring having a forward waterflow control edge portion and a rearward edge portion; said inner ring being concentric of said outer ring and forwardly of said outer ring forward edge; said spokes extending from said inner ring, radially outwardly and rearwardly to the rearward edge portion of said outer ring, forming a plurality of annularly correlated recesses to receive the rear edge of a flow-through propeller hub.

2. The fluid flow control ring unit in claim 1 wherein sai forward waterflow control edge portion has awater-shearing edge.

3. The fluid flow control ring unit in claim 2 wherein said shearing edge has an angle of no greater than about 90.

4. The fluid flow control ring unit in claim 1 wherein said outer ring forward edge portion has a front water-stagnating surface.

5. The fluid control ring unit in claim 1 wherein said outer ring is tapered radially outwardly from said rear edge portion toward said forward edge portion.

6. A combination flow-through propeller unit and fluid flow control, anticavitation ring attachment comprising: a propeller unit having a forward end and having a rearward end with a peripheral rear edge, propeller blades extending radially outwardly from said hub, and mounting means centrally within said hub for attachment of said propeller unit to a shaft, a control ring attachment at said propeller unit rearward end, including an outer ring, an inner attachment ring forwardly of said outer ring, and a plurality of spokes extending rearwardly from said inner ring to said outer ring forming generally V- shaped recesses between said spokes and said outer ring; said inner ring being adjacent said mounting means, said propeller unit peripheral rear edge extending into said generally V- shaped recesses, with said outer ring having a waterflow-controlling surface area radially outwardly of said hub.

7. The combination in claim 6 wherein said outer ring extends forwardly beyond said peripheral rear edge, and has a forwardly facing waterflow-directing surface.

8. The fluid flow control ring unit in claim 6 wherein said forward waterflow control edge portion has a water-shearing edge.

9, The fluid flow control ring unit in claim 6 wherein said shearing edge has an angle of no greater than about

Claims

1. A fluid flow control, anticavitation ring unit attachment to the annular rear edge of a flow-through propeller hub comprising: an outer peripheral ring, an inner attachment ring, and a plurality of spokes connecting said rings; said outer ring having a forward waterflow control edge portion and a rearward edge portion; said inner ring being concentric of said outer ring and forwardly of said outer ring forward edge; said spokes extending from said inner ring, radially outwardly and rearwardly to the rearward edge portion of said outer ring, forming a plurality of annularly correlated recesses to receive the rear edge of a flowthrough propeller hub.

2. The fluid flow control ring unit in claim 1 wherein said forward waterflow control edge portion has a water-shearing edge.

3. The fluid flow control ring unit in claim 2 wherein said shearing edge has an angle of no greater than about 90*.

6. A combination flow-through propeller unit and fluid flow control, anticavitation ring attachment comprising: a propeller unit having a forward end and having a rearward end with a peripheral rear edge, propeller blades extending radially outwardly from said hub, and mounting means centrally within said hub for attachment of said propeller unit to a shaft, a control ring attachment at said propeller unit rearward end, including an outer ring, an inner attachment ring forwardly of said outer ring, and a plurality of spokes extending rearwardly from said inner ring to said outer ring forming generally V-shaped recesses between said spokes and said outer ring; said inner ring being adjacent said mounting means, said propeller unit peripheral rear edge extending into said generally V-shaped recesses, with said outer ring having a waterflow-controlling surface area radially outwardly of said hub.

9. The fluid flow control ring unit in claim 6 wherein said shearing edge has an angle of no greater than about 90*.