US3892832A - Method of compressing and rolling powder - Google Patents

Method of compressing and rolling powder Download PDF

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US3892832A
US3892832A US369885A US36988573A US3892832A US 3892832 A US3892832 A US 3892832A US 369885 A US369885 A US 369885A US 36988573 A US36988573 A US 36988573A US 3892832 A US3892832 A US 3892832A
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rolls
rolling
pair
edge cracking
compaction
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US369885A
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John A Schey
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Priority to DE19661527652 priority Critical patent/DE1527652A1/en
Priority to SE4343/66A priority patent/SE307117B/xx
Priority to BE678865D priority patent/BE678865A/en
Priority to NL6604426A priority patent/NL6604426A/xx
Priority to GB14437/66A priority patent/GB1147326A/en
Priority to US691109A priority patent/US3561240A/en
Priority to US00067910A priority patent/US3746071A/en
Application filed by Individual filed Critical Individual
Priority to US369885A priority patent/US3892832A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/22Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B39/00Arrangements for moving, supporting, or positioning work, or controlling its movement, combined with or arranged in, or specially adapted for use in connection with, metal-rolling mills
    • B21B39/14Guiding, positioning or aligning work
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B39/00Arrangements for moving, supporting, or positioning work, or controlling its movement, combined with or arranged in, or specially adapted for use in connection with, metal-rolling mills
    • B21B39/14Guiding, positioning or aligning work
    • B21B39/16Guiding, positioning or aligning work immediately before entering or after leaving the pass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H7/00Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons
    • B21H7/16Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons turbine blades; compressor blades; propeller blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H8/00Rolling metal of indefinite length in repetitive shapes specially designed for the manufacture of particular objects, e.g. checkered sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • B22D11/0637Accessories therefor
    • B22D11/0648Casting surfaces
    • B22D11/066Side dams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/18Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal

Definitions

  • ABSTRACT A method of preventing edge cracking when continuously rolling and compressing powdered material comprising the steps of feeding the powdered material between a pair of rotating rolls, reducing the thickness of the powdered material by compacting as it passes between the rolls, engaging the lateral edges of the compacted material with a pair of inflexible, compressible elongated restraint members throughout a zone of compaction, traveling the restraint members rectilinearly at a velocity substantially equal to the velocity of said rolls, restraining the lateral edges of the com pacted material by said restraint members during said compaction to prevent lateral deformation of the compacted material while reducing the thickness thereof.
  • the tensile forces along the lateral edges of the compacted material are sufficiently reduced to prevent edge cracking.
  • the present invention relates to a novel process useful therewith for the rolling or casting of various materials and more particularly is directed to a relatively simple means of preventing edge cracking in the rolling aspect hereof. While my invention may be used with a number of materials which are subject to edge cracking upon rolling it has special applicability for the treatment of metals and furthermore my invention is useful in the continuous casting of metal ingots.
  • My invention is useful not only in the rolling and casting of materials such as metal sheets, slabs and plates, but also may readily be employed in the consolidation of metal powders into an integral body.
  • the essential feature of the rolling aspect of my invention involves rolling under complete lateral restraint with the lateral restraining members moving with the rolls and by employing such restraint l have discovered that I can readily and conveniently roll without producing edge cracking in those materials which hithertofore, to the best of my knowledge, have never been rolled without edge cracking. The utility and importance of such discovery will be immediately apparent to those skilled in this particular art.
  • Another aspect of this invention is directed to the continuous casting of molten metal or the like into solid ingots by use of only slightly modified apparatus from that which is used in the edge restraint rolling embodiment hereof.
  • molds which have previously been used in the continuous casting of materials, particularly metals, are usually made in the form of a cooled frame which is oscillated and/or critically lubricated to provide the means for separating the cast ingot from the mold.
  • the mold moves; in others water cooled drums or rolls are used to cast thin bands; another process employs a grooved wheel with a cover band for casting wire bars.
  • a primary object of my invention is to provide a method of preventing .edge cracking during the rolling of metal structures which process includes as its most important step edge restraint at the sides of the material being rolled and which edge restraint members are movable with the rolling mechanisms.
  • Another object of my invention is to provide a material rolling process whereby edge cracking is markedly reduced or eliminated.
  • FIG. 1 schematically illustrates a roll element for use in the present process
  • FIG. 2 is a view taken along lines 2-2 of FIG. I in partial section and also schematically illustrates the practice of the present process and the equipment re quired herewith;
  • FIG. 3 schematically illustrates another embodiment of the process and apparatus of the present invention.
  • FIG. 4 schematically illustrates still another embodiment hereof especially useful in the rolling of powder materials.
  • FIG. 5 illustrates another embodiment of the present invention in partial cross section as in FIG. 2;
  • FIG. 6 shows a product produced by the apparatus of FIG. 5.
  • FIG. 7 is an enlarged cross section taken along line 7-7 of FIG. 6.
  • edge cracking problems encountered in the rolling of metal bodies as taught by the practices of the art prior to my invention.
  • the rolling of flat slabs or sheets of metal has been carried out for a long time.
  • Present industrial practices are a culmination of almost a century of effort and development in metal rolling and metal rolling techniques, but to the best of my knowledge until the present invention was made one of the most vexing problems faced by those operating in this area of technology, namely edge cracking. had not really been solved.
  • Efforts directed to the elimination of edge cracking have been made but I know of no comparable process which either completely eliminates edge cracking or so markedly reduces such phenomena as results from the practice of edge restraint rolling as is taught in the present specification.
  • edge cracking is self explanatory l merely wish to say at this point that it alludes to the cracking, splitting, breaking of a metal structure during rolling at the uncovered lateral sides thereof.
  • the term also refers to similar detrimental phenomena occurring in materials other than metals. It appears that edge cracking is caused by secondary tensile stresses which are inevitable whenever metal or other material spread occurs as in rolling. The result has been with many materials that either they can not be rolled at all or there was a considerable loss involved in trimming the cracked portions off of the central body of the rolled material. The economic loss has been significant.
  • edge cracking can be prevented only by the complete elimination of spread in the roll gap but prior to my present invention no workable solutions for this problem existed.
  • the most widely practiced partial remedy is rolling in closed passes. Such passes are closed by interlocking annular projections (i.e. shoulders or the like) of the rolls.
  • Such solution suffers from several limitation: the slab may be entered into the closed pass only at a substantially narrower width for otherwise the spreading material will firmly wedge between the shoulders of the roll and instead of being released at the exit side it will be wound around the roll. It is therefore common prac tice to allow almost free spread in the closed pass with consequent edge cracking of sensitive materials.
  • edge restraint in closed passes can be provided only if the shoulders of the rolls are big enough to cover the entire zone of deformation: the requisite large shoulders produce a substantial annular velocity difference between the rolled material and various parts of the closed pass with a resulting undesirable distortion and wear. Furthermore, it is impossible to re-introduce the material rolled in a closed pass into the same pass for further reduction and the heavy total reduction normally sought for can be achieved only in a succession of closed passes which for the reasons noted above must be successively widened thus opening the way for further edge cracking.
  • edge cracking problems in rolling are eliminated by the practice of my invention.
  • edge cracking is substantiallly or completely eliminated in the rolling of most metals and other materials subject to edge cracking. It is important in the practice of such edge restraint that the lateral restraining members be movable with the rolls and with the materials being rolled.
  • FIGS. 1 and 2 hereof Here is illustrated a twohigh rolling mill having a top roll 11 and a bottom roll l2.
  • a metal slab 13 being rolled is interposed between the rolls in the usual manner.
  • Grooves I4 are provided in the rolls, said grooves being in register for both the top and bottom roll and as shown in the drawing, are lateral to the central part of the roll.
  • a pair of restraining bars 16 It is such restraining bars 16 in this embodiment of my invention which provide the edge restraint of the material being rolled.
  • the restraining bars are made of various strong materials, e.g., alloys similar to those of which the rolls are fabricated. Therefore, as in the case of the rolls, they are relatively incompressible compared to the material being rolled.
  • the rolled slab I3 is now rolled in a tightly closed. i.e., vertically and horizontally closed. chamber which not only provides the usual rolling but also tight and strong edge restraint.
  • FIGS. 1 and 2 While a solid metal slab is illustrated in FIGS. 1 and 2 it will of course be apparent that metal powders may be substituted therefor and compacted and consolidated in the present process. Various other materials subject to edge cracking upon rolling may be similarly treated.
  • the restraining bars 16 closely but movably fit in the grooves 14 of the upper and lower rollers and thus their movement laterally is restrained. As shown in FIG. 1 each such restraining bar rests in the bottom of the groove provided in the lower roll and there is a space 15 left for clearance purposes between the top of the restraining bar and the top of the groove of the top roll 11. But because of such grooving the restraining bars 16 are held in close restraint to prevent lateral movement. The clearance 15 permits repeated thickness reductions of the slab being rolled by closing the rolls in the usual manner.
  • the restraining bars are posi tioned on table rollers 17 and are assisted in being maintained in operative position by guide rollers 18.
  • Aluminum alloy slabs containing 8 magnesium were prepared and subjected to rolling both with and without edge restraint as herein taught. All slabs of this material rolled without such restraint invariably cracked at the edges whereby the restrained ones gave perfect parallel edges absolutely free of cracking.
  • Powder bodies of iron powders were made by ramming them into shape and then rolling at 2400F both with and without edge restraint as herein taught.
  • the non-restrained bodies cracked severely; their density was approximately percent of theoretical density of iron after 70 to percent reduction in thickness.
  • Similar powder bodies rolled with edge restraint as herein taught gave dense bodies free of edge cracks and with mechanical properties similar to those of typical hot rolled slabs.
  • an appropriate protective atmosphere should be employed.
  • Metal powder bodies were made by ramming them into a mild steel sheath. When rolling without edge restraint the sheath broke open and much of the powder escaped. By using the restraining bars the rolled body was free of edge cracking and yielded a much superior compacted product with a density approaching theoretical after only 70 percent reduction in thickness.
  • the process is primarily suited for operation in reversing mills where a succession of passes may be taken on one and the same slab without need of separating the slab from the restraining elements.
  • the restraining elements are in the form of endless belts 21.
  • belts fit into lateral grooves 22 on the rolls.
  • the thickness of such belts is of necessity limited by the requirement to maintain their flexibility adequate strength can be obtained for edge restraint purposes in view of the support that such belts receive from the portion of the rolls which form the outer wall of the grooves 22.
  • the clearance between belts 2i and grooves 22 is greatly exaggerated in the schematic illustration of FIG. 3.
  • the present process can also be employed for cladding.
  • a cladding material may be fed through the input side of the roll pair onto the base metal or other material being rolled with edge restraint.
  • the present process may also be employed in the rolling of materials other than metals.
  • materials other than metals.
  • ceramics which are sheathed or canned in a metal may be rolled with edge restraint to prevent edge cracking of the composite structure.
  • the present process may be used for the continuous casting of metals and the like.
  • the preferred apparatus is disclosed in FIG. 3 but for casting both the rolls (numbers II and 12 of FIGS. 1 and 2) are cooled and the two endless, flexible belts 21 and 22 are also cooled.
  • the rolls are driven and the belts may be driven or dragged by the rolls.
  • Such belts are fully supported in the grooves of the rolls.
  • the two rolls and the two belts fully enclose and define a mold of rectangular cross section. All four walls of this mold move together with the solidifying ingot at a rate selected for the material being cast. Friction is completely eliminated and separation of the ingot from the mold is automatically accomplished. Pouring rates are so adjusted that the porosity is eliminated in the converging section of the mold.
  • FIG. 5 A modified form of the present invention is shown in FIG. 5, wherein parts similar to those shown in FIGS. 1 and 2 are indicated with the same reference numeral and the subscript a.”
  • the apparatus includes a top roll 11a and a bottom roll 12a.
  • the top roll has a central barrel portion 26 corresponding to the area between the grooves in FIG. 1 which is of a non-circular configuration.
  • the central barrel portion is provided with four recesses equally spaced around the circumference.
  • the resultant raised sections 29 and the recessed sections 28 correspond to the top surface of the shapes to be rolled.
  • the bottom roll 12a also has a central barrel portion 27 made up of similar recessed sections 30 and raised sections 31.
  • each of the recessed sections 28 and 30 and each of the raised sections 29 and 31 is geometrically symmetrical.
  • the top roll lla and the bottom roll 12a are rotated in opposite directions to cause the opposing faces to move the workpiece 13a in the same direction in conventional rolling fashion.
  • the respective raised sections 29 and 31 oppose each other as do the recessed sections 28 and 30 during the rolling operation.
  • This coordination is accomplished by conventional means such as gears.
  • the workpiece 13a which enters the rolls as a bar of uniform cross section is transformed by the central barrel portions of the rolls 11a and 12a into a periodic configuration of thick and thin section in uniformly repeating patterns.
  • the lateral restraint is again accomplished by movable bars 160.
  • the remainder of the apparatus is essentially the same as that shown in FIGS. 1 and 2.
  • the flexible belts of FIG. 3 could again be substituted for the rigid bars shown in FIG. 5.
  • the workpiece 13a is transformed by rolling from its initial cross sectional shape into the desired configuration. The reduction is accomplished without edge cracking due to the presence of the restraining bars 16a. Reductions in thickness up to 84 percent have been achieved without edge cracking or the formation of flash.
  • the only limitation on use of the apparatus for periodic rolling is that the transitional surface of the rolls connecting the raised sections and the recessed sections should not be undercut. Undercutting of this transitional surface results in the pulling or tearing of the workpiece as the roller attempts to free itself.
  • FIGS. 6 and 7 Typical turbine blades formed by the process of this invention are shown in FIGS. 6 and 7.
  • FIG. 6 shows a continuous section of the workpiece after rolling and before cutting.
  • the thick section defines root portions 32 of two blades disposed end to end.
  • the thin section defines airfoil portions 33 of two blades disposed end to end. After cutting at the points indicated each turbine blade has the form shown in FIG. 7 or its mirror image.
  • the airfoil portion 33 shown in FIG. 7 is laterally curved and tapered, however, it is not disposed at an angle to the root portion.
  • the airfoil cross section 33 shown in H0. 7 is formed by one raised section 29 rolling in coordination with one raised section 31 in FIG. 5.
  • the raised section 29 of the upper roll lla is of a shape identical to the top boundary of airfoil 33.
  • Mating raised section 31 is of a shape identical to the bottom boundary of airfoil 33.
  • the shape of the airfoil 33 and its angle to the root section 32 is wholly a function of the shapes of the respective raised and recessed sections of the central barrel portions of the rolls. If no mirror image blades are desired, the rolls can be designed to make only duplicate blades connected root to foil to root. Application of the present invention to the rolling of turbine blades will be more clearly understood with reference to the following specific examples.
  • Turbine blades have been rolled with apparatus similar to that shown in FIG. 5.
  • the width of the turbine blade and of the workpiece inserted is three quarters of an inch. This width is maintained by spacing the restraining bars at three quarters of an inch and having the width of the central barrel portion of the top and bottom rolls also of three quarters of an inch width.
  • Each turbine blade is 2 inches in total length.
  • the air foil section is one and three quarters inches long and the root section A: inch long.
  • the starting material is fed into the roll at a thickness of three fourths of an inch.
  • the material is passed through the rollers in a single pass which produces turbine blades having an air foil thickness of 0.125 inches and a root thickness of 0.525 inches.
  • the raised portions of the rolls are correspondingly cut at a thirty degree angle to the roll axis resulting in an airfoil portion which is also at a thirty degree angle to the sides of the root portion.
  • the materials employed for this turbine blade configuration were 7075 aluminum alloy rolled at 800F and Ti-6Al- 4V alloy rolled at l800F.
  • a larger turbine blade has been made from 7075 aluminum alloy rolled at 800F.
  • the finished blade is one and fifteen sixteenths inches wide and 3.! inches long.
  • the airfoil section is 2.6 inches long.
  • the root thickness is 0.430 inches with the airfoil being again 0.125 inches. This airfoil is laterally curved and is rolled with no angle relative to the root section,
  • Turbine blades have been employed merely by way of example.
  • the central barrel portions of the rolls may be designed to yield one or several repetitions per revolution.
  • One roll may be cylindrical and one irregular in shape. The variations in geometry are almost unlimited.
  • the apparatus for carrying out the method may be used for making preforms or for making end items.
  • the tolerances of the roller parts depend on whether the product is to be subjected to one final forging step or used as rolled. In either case the process saves from 4 to 6 steps needed for current forming methods.
  • a method of preventing edge cracking when continuously rolling and compressing powder material between at least one pair of spaced, parallel aligned rolls comprising:
  • a method in accordance with claim 1 including the further step of: compacting loose particulate powder prior to step a) between a pair of converging belts defining a feeding throat tapering to said rolls and said zone of compaction therebetween.

Abstract

A method of preventing edge cracking when continuously rolling and compressing powdered material comprising the steps of feeding the powdered material between a pair of rotating rolls, reducing the thickness of the powdered material by compacting as it passes between the rolls, engaging the lateral edges of the compacted material with a pair of inflexible, compressible elongated restraint members throughout a zone of compaction, traveling the restraint members rectilinearly at a velocity substantially equal to the velocity of said rolls, restraining the lateral edges of the compacted material by said restraint members during said compaction to prevent lateral deformation of the compacted material while reducing the thickness thereof. By such a method, the tensile forces along the lateral edges of the compacted material are sufficiently reduced to prevent edge cracking.

Description

[4 1 July 1, 1975 i 1 METHOD OF COMPRESSING AND ROLLING POWDER {76] Inventor: John A. Schey, 7l6 S. Bruner St.,
Hinsdale, lll. 60521 [22] Filed: June 14, 1973 [21 1 Appl. No.: 369,885
Related US. Application Data [60] Division of Ser. No. 67,9l0. Aug. 28, 1970, Pat. No. 3,746,701, which is a division of Ser. No. 691,109, Dec. 7, 1967, Pat. No. 3,56l,240, which is a continuation-impart of Ser. No. 587,358. Sept. 16, 1966, which is a continuation-in-part of Ser. No. 444,637, April 1, 1965, abandoned.
Primary Examiner-Robert F. White Assistant Examiner.l R. Hall Attorney, Agent, or FirmFitch, Even, Tabin & Luedeka [57] ABSTRACT A method of preventing edge cracking when continuously rolling and compressing powdered material comprising the steps of feeding the powdered material between a pair of rotating rolls, reducing the thickness of the powdered material by compacting as it passes between the rolls, engaging the lateral edges of the compacted material with a pair of inflexible, compressible elongated restraint members throughout a zone of compaction, traveling the restraint members rectilinearly at a velocity substantially equal to the velocity of said rolls, restraining the lateral edges of the com pacted material by said restraint members during said compaction to prevent lateral deformation of the compacted material while reducing the thickness thereof. By such a method, the tensile forces along the lateral edges of the compacted material are sufficiently reduced to prevent edge cracking.
2 Claims, 7 Drawing Figures wwswmm. 1 ms SHEET 1 METHOD OF COMPRESSING AND ROLLING POWDER This is a divisional application of co-pending application Ser. No. 67.910, filed Aug. 28, 1970, entitled Method For Treating Materials," now US. Pat. No. 3,746,071, which, in turn, was co-pending with and a divisional application of application Ser. No. 691,109, filed Dec. 7, 1967, entitled Method and Apparatus for Treating Materials, now US. Pat. No. 3,561,240.
Application Ser. No. 691,109 is a continuation-inpart of my co-pending application Ser. No. 587,358, filed Sept. 16, 1966. which application is a continuation-in-part of my application Ser. No. 444,637 filed Apr. 1, 1965, and now abandoned.
The present invention relates to a novel process useful therewith for the rolling or casting of various materials and more particularly is directed to a relatively simple means of preventing edge cracking in the rolling aspect hereof. While my invention may be used with a number of materials which are subject to edge cracking upon rolling it has special applicability for the treatment of metals and furthermore my invention is useful in the continuous casting of metal ingots.
My invention is useful not only in the rolling and casting of materials such as metal sheets, slabs and plates, but also may readily be employed in the consolidation of metal powders into an integral body.
The essential feature of the rolling aspect of my invention involves rolling under complete lateral restraint with the lateral restraining members moving with the rolls and by employing such restraint l have discovered that I can readily and conveniently roll without producing edge cracking in those materials which hithertofore, to the best of my knowledge, have never been rolled without edge cracking. The utility and importance of such discovery will be immediately apparent to those skilled in this particular art.
Another aspect of this invention is directed to the continuous casting of molten metal or the like into solid ingots by use of only slightly modified apparatus from that which is used in the edge restraint rolling embodiment hereof. As is well known to those skilled in this art molds which have previously been used in the continuous casting of materials, particularly metals, are usually made in the form of a cooled frame which is oscillated and/or critically lubricated to provide the means for separating the cast ingot from the mold. In some prior art processes the mold moves; in others water cooled drums or rolls are used to cast thin bands; another process employs a grooved wheel with a cover band for casting wire bars.
All of such prior art continuous casting processes suffer a number of disadvantages. Internal porosity and surface defects are common in all of the resulting cast materials except those made with the water cooled drums and the latter process yields materials of limited thickness due primarily to the failure to enclose the roll gap from the sides.
In distinction to these problems encountered in prior art continuous casting methods, the present process provides excellent continuously cast ingots without any severe size limitations. All of this will be set out in greater detail as the description proceeds.
Accordingly. a primary object of my invention is to provide a method of preventing .edge cracking during the rolling of metal structures which process includes as its most important step edge restraint at the sides of the material being rolled and which edge restraint members are movable with the rolling mechanisms.
Another object of my invention is to provide a material rolling process whereby edge cracking is markedly reduced or eliminated.
These and other objects, features and advantages of my invention will become apparent to those skilled in this particular art from the following detailed disclosure thereof and the accompanying drawings in which:
FIG. 1 schematically illustrates a roll element for use in the present process;
FIG. 2 is a view taken along lines 2-2 of FIG. I in partial section and also schematically illustrates the practice of the present process and the equipment re quired herewith;
FIG. 3 schematically illustrates another embodiment of the process and apparatus of the present invention; and
FIG. 4 schematically illustrates still another embodiment hereof especially useful in the rolling of powder materials; and
FIG. 5 illustrates another embodiment of the present invention in partial cross section as in FIG. 2; and
FIG. 6 shows a product produced by the apparatus of FIG. 5; and
FIG. 7 is an enlarged cross section taken along line 7-7 of FIG. 6.
Before considering the present invention, reference should first be briefly had to the edge cracking problems encountered in the rolling of metal bodies as taught by the practices of the art prior to my invention. Obviously the rolling of flat slabs or sheets of metal has been carried out for a long time. Present industrial practices are a culmination of almost a century of effort and development in metal rolling and metal rolling techniques, but to the best of my knowledge until the present invention was made one of the most vexing problems faced by those operating in this area of technology, namely edge cracking. had not really been solved. Efforts directed to the elimination of edge cracking have been made but I know of no comparable process which either completely eliminates edge cracking or so markedly reduces such phenomena as results from the practice of edge restraint rolling as is taught in the present specification.
Others have attempted to alleviate this problem by, for example, rolling in grooved rolls or by the employment of vertical edge rollers. Neither of these processes have brought about any degree of improvement akin to my findings in the process herein described. As a result, edge cracking in crack-sensitive materials remains a serious problem and scrap losses due to edge cracking account for a substantial portion of the present production costs of some of the never so-called exotic materials. In fact many materials with desirable mechanical properties have had to be somewhat abandoned because of their uncontrollable edge cracking or in the alternative, had to be produced by expensive methods in order to break down their cast structure. A similar situation has existed in the compaction of metal powders.
While the term edge cracking" is self explanatory l merely wish to say at this point that it alludes to the cracking, splitting, breaking of a metal structure during rolling at the uncovered lateral sides thereof. As used in the present specification and claims the term also refers to similar detrimental phenomena occurring in materials other than metals. It appears that edge cracking is caused by secondary tensile stresses which are inevitable whenever metal or other material spread occurs as in rolling. The result has been with many materials that either they can not be rolled at all or there was a considerable loss involved in trimming the cracked portions off of the central body of the rolled material. The economic loss has been significant.
It has been perhaps recognized that edge cracking can be prevented only by the complete elimination of spread in the roll gap but prior to my present invention no workable solutions for this problem existed. The most widely practiced partial remedy is rolling in closed passes. Such passes are closed by interlocking annular projections (i.e. shoulders or the like) of the rolls. Such solution suffers from several limitation: the slab may be entered into the closed pass only at a substantially narrower width for otherwise the spreading material will firmly wedge between the shoulders of the roll and instead of being released at the exit side it will be wound around the roll. It is therefore common prac tice to allow almost free spread in the closed pass with consequent edge cracking of sensitive materials. In the rolling of powders the problem may be somewhat alleviated by placing one shoulder on each of the opposite rolls as disclosed in the patent to Naeser, US. Pat. No. 3,0l9,487 and Dasher, et al. US. Pat. No. 3,017,665 thereby imparting a twist on the exiting strip product and freeing it from the confines of the roll gap. Such solution, however, is obviously unworkable with solid material having full density especially when such material has a substantial thickness. Furthermore, a three dimensional consideration of the problem will show that edge restraint in closed passes can be provided only if the shoulders of the rolls are big enough to cover the entire zone of deformation: the requisite large shoulders produce a substantial annular velocity difference between the rolled material and various parts of the closed pass with a resulting undesirable distortion and wear. Furthermore, it is impossible to re-introduce the material rolled in a closed pass into the same pass for further reduction and the heavy total reduction normally sought for can be achieved only in a succession of closed passes which for the reasons noted above must be successively widened thus opening the way for further edge cracking.
The edge cracking problems in rolling are eliminated by the practice of my invention. By complete edge restraint laterally at right angles to the material being rolled edge cracking is substantiallly or completely eliminated in the rolling of most metals and other materials subject to edge cracking. It is important in the practice of such edge restraint that the lateral restraining members be movable with the rolls and with the materials being rolled.
To understand my invention reference should next be had to FIGS. 1 and 2 hereof. Here is illustrated a twohigh rolling mill having a top roll 11 and a bottom roll l2. A metal slab 13 being rolled is interposed between the rolls in the usual manner. Grooves I4 are provided in the rolls, said grooves being in register for both the top and bottom roll and as shown in the drawing, are lateral to the central part of the roll. In the two lateral grooves I insert a pair of restraining bars 16. It is such restraining bars 16 in this embodiment of my invention which provide the edge restraint of the material being rolled. The restraining bars are made of various strong materials, e.g., alloys similar to those of which the rolls are fabricated. Therefore, as in the case of the rolls, they are relatively incompressible compared to the material being rolled.
As clearly shown in FIG. l the rolled slab I3 is now rolled in a tightly closed. i.e., vertically and horizontally closed. chamber which not only provides the usual rolling but also tight and strong edge restraint.
Parenthetically. while a solid metal slab is illustrated in FIGS. 1 and 2 it will of course be apparent that metal powders may be substituted therefor and compacted and consolidated in the present process. Various other materials subject to edge cracking upon rolling may be similarly treated.
The restraining bars 16 closely but movably fit in the grooves 14 of the upper and lower rollers and thus their movement laterally is restrained. As shown in FIG. 1 each such restraining bar rests in the bottom of the groove provided in the lower roll and there is a space 15 left for clearance purposes between the top of the restraining bar and the top of the groove of the top roll 11. But because of such grooving the restraining bars 16 are held in close restraint to prevent lateral movement. The clearance 15 permits repeated thickness reductions of the slab being rolled by closing the rolls in the usual manner.
As shown in FIG. 2 the restraining bars are posi tioned on table rollers 17 and are assisted in being maintained in operative position by guide rollers 18.
It will be apparent that the grooved rolls permit the closing of the rolls and thus its operation is substantially as flexible as that with a conventional two-high rolling mill, except of course the width of the rolled slab now remains constant. By such configuration I obtain the marked reduction in edge cracking previously alluded to. The restraining elements prevent side spread and rolling is carried out under plane strain conditions. Thus the development of harmful secondary tensile stresses is entirely suppressed.
By employing edge restraint through elements that do not form part of the rolls my invention solves all of the earlier mentioned problems associated with the elimination of edge cracking. The material is laterally supported in the entire zone of deformation. Velocity differences between the rolled material and the restraining elements are reduced to a minimum and the material may be re-entered into the same pair of rolls for succession of passes with Zero spread. The rolled product is readily removed from the roll gap without twisting or scraping.
A number of materials were rolled with edge restraint as herein taught to clearly point up the edge cracking prevention resulting from my process. For example:
Aluminum alloy slabs containing 8 magnesium were prepared and subjected to rolling both with and without edge restraint as herein taught. All slabs of this material rolled without such restraint invariably cracked at the edges whereby the restrained ones gave perfect parallel edges absolutely free of cracking.
Powder bodies of iron powders were made by ramming them into shape and then rolling at 2400F both with and without edge restraint as herein taught. The non-restrained bodies cracked severely; their density was approximately percent of theoretical density of iron after 70 to percent reduction in thickness. Similar powder bodies rolled with edge restraint as herein taught gave dense bodies free of edge cracks and with mechanical properties similar to those of typical hot rolled slabs. In this particular aspect of my invention an appropriate protective atmosphere should be employed.
Metal powder bodies were made by ramming them into a mild steel sheath. When rolling without edge restraint the sheath broke open and much of the powder escaped. By using the restraining bars the rolled body was free of edge cracking and yielded a much superior compacted product with a density approaching theoretical after only 70 percent reduction in thickness.
In the foregoing embodiment of my invention the process is primarily suited for operation in reversing mills where a succession of passes may be taken on one and the same slab without need of separating the slab from the restraining elements. In another embodiment hereof as illustrated in FIG. 3 the restraining elements are in the form of endless belts 21. Here such belts fit into lateral grooves 22 on the rolls. While the thickness of such belts is of necessity limited by the requirement to maintain their flexibility adequate strength can be obtained for edge restraint purposes in view of the support that such belts receive from the portion of the rolls which form the outer wall of the grooves 22. The clearance between belts 2i and grooves 22 is greatly exaggerated in the schematic illustration of FIG. 3.
The present process can also be employed for cladding. For this purpose a cladding material may be fed through the input side of the roll pair onto the base metal or other material being rolled with edge restraint.
The present process may also be employed in the rolling of materials other than metals. For example ceramics which are sheathed or canned in a metal may be rolled with edge restraint to prevent edge cracking of the composite structure.
It should also be evident to those skilled in this particular art that the present process may be employed in the rolling of complex shapes rather than mere plates or sheets as hereinabove described. As is more clearly described hereinafter with reference to FIG. 5 my process will likewise prevent edge cracking in such shapes which hithertofore were subject to such detrimental phenomena.
In the compaction and rolling of loose particulate matter as herein taught, a variety of known means can be employed to bring such matter into position in the roll gap. I prefer, however, that a pair of converging belts be used to convey, for example powders 40 into the gap. This is illustrated schematically in FIG. 4. Here again there is an upper and lower roll 41 and 42 respec' tively and edge restraint is provided by belts or rings 23. To bring the powders 40 in endless belts 24 and 25 are mounted on rollers and positioned as shown. The belts 24 and 25 together with the restraining elements 23 define a feeding throat which tapers into the roll gap. By virtue of the movement of all four sides of the feeding throat powder 40 is drawn and thickness reductions far in excess of those normally obtained may be accomplished. Obviously this structure may be employed in either a vertical or horizontal plane or configuration.
As noted above, the present process, with very slight modification, may be used for the continuous casting of metals and the like. In this embodiment the preferred apparatus is disclosed in FIG. 3 but for casting both the rolls (numbers II and 12 of FIGS. 1 and 2) are cooled and the two endless, flexible belts 21 and 22 are also cooled. As noted above as regards FIG. 3 the rolls are driven and the belts may be driven or dragged by the rolls. Such belts are fully supported in the grooves of the rolls. The two rolls and the two belts fully enclose and define a mold of rectangular cross section. All four walls of this mold move together with the solidifying ingot at a rate selected for the material being cast. Friction is completely eliminated and separation of the ingot from the mold is automatically accomplished. Pouring rates are so adjusted that the porosity is eliminated in the converging section of the mold.
A modified form of the present invention is shown in FIG. 5, wherein parts similar to those shown in FIGS. 1 and 2 are indicated with the same reference numeral and the subscript a." The apparatus includes a top roll 11a and a bottom roll 12a. The top roll has a central barrel portion 26 corresponding to the area between the grooves in FIG. 1 which is of a non-circular configuration. In the embodiment shown the central barrel portion is provided with four recesses equally spaced around the circumference. The resultant raised sections 29 and the recessed sections 28 correspond to the top surface of the shapes to be rolled. In like manner the bottom roll 12a also has a central barrel portion 27 made up of similar recessed sections 30 and raised sections 31. In this embodiment each of the recessed sections 28 and 30 and each of the raised sections 29 and 31 is geometrically symmetrical. The top roll lla and the bottom roll 12a are rotated in opposite directions to cause the opposing faces to move the workpiece 13a in the same direction in conventional rolling fashion. The respective raised sections 29 and 31 oppose each other as do the recessed sections 28 and 30 during the rolling operation. This coordination is accomplished by conventional means such as gears. The workpiece 13a which enters the rolls as a bar of uniform cross section is transformed by the central barrel portions of the rolls 11a and 12a into a periodic configuration of thick and thin section in uniformly repeating patterns.
The lateral restraint is again accomplished by movable bars 160. The remainder of the apparatus is essentially the same as that shown in FIGS. 1 and 2. The flexible belts of FIG. 3 could again be substituted for the rigid bars shown in FIG. 5. The workpiece 13a is transformed by rolling from its initial cross sectional shape into the desired configuration. The reduction is accomplished without edge cracking due to the presence of the restraining bars 16a. Reductions in thickness up to 84 percent have been achieved without edge cracking or the formation of flash. The only limitation on use of the apparatus for periodic rolling is that the transitional surface of the rolls connecting the raised sections and the recessed sections should not be undercut. Undercutting of this transitional surface results in the pulling or tearing of the workpiece as the roller attempts to free itself.
While the modification shown in FIG. 5 lends itself readily to the one step rolling of any non-uniform shape the invention finds particular application in the field of rolling turbine blades.
Typical turbine blades formed by the process of this invention are shown in FIGS. 6 and 7. FIG. 6 shows a continuous section of the workpiece after rolling and before cutting. The thick section defines root portions 32 of two blades disposed end to end. The thin section defines airfoil portions 33 of two blades disposed end to end. After cutting at the points indicated each turbine blade has the form shown in FIG. 7 or its mirror image. The airfoil portion 33 shown in FIG. 7 is laterally curved and tapered, however, it is not disposed at an angle to the root portion.
The airfoil cross section 33 shown in H0. 7 is formed by one raised section 29 rolling in coordination with one raised section 31 in FIG. 5. For this particular application the raised section 29 of the upper roll lla is of a shape identical to the top boundary of airfoil 33. Mating raised section 31 is of a shape identical to the bottom boundary of airfoil 33. The shape of the airfoil 33 and its angle to the root section 32 is wholly a function of the shapes of the respective raised and recessed sections of the central barrel portions of the rolls. If no mirror image blades are desired, the rolls can be designed to make only duplicate blades connected root to foil to root. Application of the present invention to the rolling of turbine blades will be more clearly understood with reference to the following specific examples.
Turbine blades have been rolled with apparatus similar to that shown in FIG. 5. The width of the turbine blade and of the workpiece inserted is three quarters of an inch. This width is maintained by spacing the restraining bars at three quarters of an inch and having the width of the central barrel portion of the top and bottom rolls also of three quarters of an inch width. Each turbine blade is 2 inches in total length. The air foil section is one and three quarters inches long and the root section A: inch long. The starting material is fed into the roll at a thickness of three fourths of an inch. The material is passed through the rollers in a single pass which produces turbine blades having an air foil thickness of 0.125 inches and a root thickness of 0.525 inches. The raised portions of the rolls are correspondingly cut at a thirty degree angle to the roll axis resulting in an airfoil portion which is also at a thirty degree angle to the sides of the root portion. The materials employed for this turbine blade configuration were 7075 aluminum alloy rolled at 800F and Ti-6Al- 4V alloy rolled at l800F.
A larger turbine blade has been made from 7075 aluminum alloy rolled at 800F. The finished blade is one and fifteen sixteenths inches wide and 3.! inches long. The airfoil section is 2.6 inches long. The root thickness is 0.430 inches with the airfoil being again 0.125 inches. This airfoil is laterally curved and is rolled with no angle relative to the root section,
It will be evident to one skilled in the art that many other complex shapes can be rolled without departing from the scope of this invention. Turbine blades have been employed merely by way of example. The central barrel portions of the rolls may be designed to yield one or several repetitions per revolution. One roll may be cylindrical and one irregular in shape. The variations in geometry are almost unlimited.
The apparatus for carrying out the method may be used for making preforms or for making end items. The tolerances of the roller parts depend on whether the product is to be subjected to one final forging step or used as rolled. In either case the process saves from 4 to 6 steps needed for current forming methods.
It will be understood that various modifications and variations may be affected without departing from the spirit or scope of the novel concepts of my invention.
What is claimed is:
l. A method of preventing edge cracking when continuously rolling and compressing powder material between at least one pair of spaced, parallel aligned rolls comprising:
a. feeding the powder material between a pair of rotating rolls,
b. reducing the thickness of the powder material by compacting as it passes between the rolls,
c. engaging the lateral edges of said compacted material with a pair of substantially incompressible elongated restraint members being substantially inflexible throughout a zone of compaction with said rolls,
d. restraining the lateral edges of the compacted material during said compaction, and
e. moving said restraint members rectilinearly at a velocity substantially equal to the peripheral velocities of said rolls with the compact material to pre' vent lateral deformation of compacted material while reducing the thickness thereof, whereby the tensile forces along the lateral edges of the compacted material are sufficiently reduced to prevent edge cracking.
2. A method in accordance with claim 1 including the further step of: compacting loose particulate powder prior to step a) between a pair of converging belts defining a feeding throat tapering to said rolls and said zone of compaction therebetween. i i i

Claims (2)

1. A METHOD OF PREVENTING EDGE CRACKING WHEN CONTINUOUSLY ROLLING AND COMPRESSING POWDER MATERIAL BETWEEN AT LEAST ONE PAIR OF SPACED, PARALLEL ALIGNED ROOLS COMPRISING: A. FEEDING THE POWDER MATERIAL BETWEEN A PAIR OF ROTATING ROLLS, B. REDUCING THE THICKNESS OF THE POWDER MATERIAL BY COMPACTING AS IT PASSES BETWEEN THE ROLLS, C. ENGAGING THE LATERAL EDGES OF SAID COMPACTED MATERIAL WITH A PAIR OF SUBSTANTIALLY INCOMPRESSIBLE ELONGATED RESTRAINT MEMBERS BEING SUBSTANTIALLY INFLEXIBLE THROUGHOUT A ZONE OF COMPACTION WITH SAID ROLLS, D. RESTRAINING THE LATERAL EDGES OF THE COMPACTED MATERIAL DURING SAID COMPACTION, AND E. MOVING SAID RESTRAINT MEMBERS RECTILINEARLY AT A VELOCITY SUBSTANTIALLY EQUAL TO THE PERPHERAL VELOCITIES OF SAID ROLLS WITH THE COMPACT MATERIAL TO PREVENT LATERAL DEFORMATION OF COMPACTED MATERIAL WHILE REDUCING THE THICKNESS THEREOF, WHEREBY THE TENSILE FORCES ALONG THE LATERAL EDGES OF THE COMPACTED MATERIAL ARE SUFFICIENTLY REDUCED TO PREVENT EDGE CRACKING.
2. A method in accordance with claim 1 including the further step of: compacting loose particulate powder prior to step a) between a pair of converging belts defining a feeding throat tapering to said rolls and said zone of compaction therebetween.
US369885A 1965-04-01 1973-06-14 Method of compressing and rolling powder Expired - Lifetime US3892832A (en)

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DE19661527652 DE1527652A1 (en) 1965-04-01 1966-03-31 Method and device for rolling
SE4343/66A SE307117B (en) 1965-04-01 1966-03-31
NL6604426A NL6604426A (en) 1965-04-01 1966-04-01
GB14437/66A GB1147326A (en) 1965-04-01 1966-04-01 Method and apparatus for rolling
BE678865D BE678865A (en) 1965-04-01 1966-04-01 Arrangement of a rolling mill for irons, especially small gauges, and method for its operation
US691109A US3561240A (en) 1965-04-01 1967-12-07 Method and apparatus for treating materials
US00067910A US3746071A (en) 1965-04-01 1970-08-28 Method for treating materials
US369885A US3892832A (en) 1965-04-01 1973-06-14 Method of compressing and rolling powder

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US44463765A 1965-04-01 1965-04-01
US69110967A 1967-12-07 1967-12-07
US6791070A 1970-08-28 1970-08-28
US369885A US3892832A (en) 1965-04-01 1973-06-14 Method of compressing and rolling powder

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US4172111A (en) * 1976-03-10 1979-10-23 Davy-Loewy Limited Trimming of compacted metal powder strip
US4743512A (en) * 1987-06-30 1988-05-10 Carpenter Technology Corporation Method of manufacturing flat forms from metal powder and product formed therefrom
US5160470A (en) * 1992-05-20 1992-11-03 Dow Corning Corporation Method for compacting silica fume
US20130032343A1 (en) * 2011-08-05 2013-02-07 Baker Hughes Incorporated Permeable material compacting method and apparatus
US8664318B2 (en) 2011-02-17 2014-03-04 Baker Hughes Incorporated Conformable screen, shape memory structure and method of making the same
US8684075B2 (en) 2011-02-17 2014-04-01 Baker Hughes Incorporated Sand screen, expandable screen and method of making
US8721958B2 (en) 2011-08-05 2014-05-13 Baker Hughes Incorporated Permeable material compacting method and apparatus
US9017501B2 (en) 2011-02-17 2015-04-28 Baker Hughes Incorporated Polymeric component and method of making
US9044914B2 (en) 2011-06-28 2015-06-02 Baker Hughes Incorporated Permeable material compacting method and apparatus

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US4172111A (en) * 1976-03-10 1979-10-23 Davy-Loewy Limited Trimming of compacted metal powder strip
US4743512A (en) * 1987-06-30 1988-05-10 Carpenter Technology Corporation Method of manufacturing flat forms from metal powder and product formed therefrom
US5160470A (en) * 1992-05-20 1992-11-03 Dow Corning Corporation Method for compacting silica fume
US8664318B2 (en) 2011-02-17 2014-03-04 Baker Hughes Incorporated Conformable screen, shape memory structure and method of making the same
US8684075B2 (en) 2011-02-17 2014-04-01 Baker Hughes Incorporated Sand screen, expandable screen and method of making
US9017501B2 (en) 2011-02-17 2015-04-28 Baker Hughes Incorporated Polymeric component and method of making
US9155983B2 (en) 2011-02-17 2015-10-13 Baker Hughes Incorporated Method of making a shape memory structure
US9044914B2 (en) 2011-06-28 2015-06-02 Baker Hughes Incorporated Permeable material compacting method and apparatus
US20130032343A1 (en) * 2011-08-05 2013-02-07 Baker Hughes Incorporated Permeable material compacting method and apparatus
US8720590B2 (en) * 2011-08-05 2014-05-13 Baker Hughes Incorporated Permeable material compacting method and apparatus
US8721958B2 (en) 2011-08-05 2014-05-13 Baker Hughes Incorporated Permeable material compacting method and apparatus

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DE1527652A1 (en) 1970-01-22
GB1147326A (en) 1969-04-02
NL6604426A (en) 1966-10-03
BE678865A (en) 1966-10-03
SE307117B (en) 1968-12-23
US3746071A (en) 1973-07-17
US3561240A (en) 1971-02-09

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