US1766865A - Alloy structure - Google Patents

Alloy structure Download PDF

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US1766865A
US1766865A US630414A US63041423A US1766865A US 1766865 A US1766865 A US 1766865A US 630414 A US630414 A US 630414A US 63041423 A US63041423 A US 63041423A US 1766865 A US1766865 A US 1766865A
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alloy
metal
porous
bearing
pressure
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US630414A
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Harry M Williams
Alfred L Boegehold
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General Motors Research Corp
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General Motors Research Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/122Multilayer structures of sleeves, washers or liners
    • 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
    • B22F7/002Manufacture 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 porous nature
    • B22F7/004Manufacture 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 porous nature comprising at least one non-porous part
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/103Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/103Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing
    • F16C33/104Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing in a porous body, e.g. oil impregnated sintered sleeve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/14Special methods of manufacture; Running-in
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2204/00Metallic materials; Alloys
    • F16C2204/10Alloys based on copper
    • F16C2204/12Alloys based on copper with tin as the next major constituent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00Shaping
    • F16C2220/20Shaping by sintering pulverised material, e.g. powder metallurgy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/30Coating surfaces
    • F16C2223/32Coating surfaces by attaching pre-existing layers, e.g. resin sheets or foils by adhesion to a substrate; Laminating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/30Coating surfaces
    • F16C2223/40Coating surfaces by dipping in molten material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/30Material joints
    • F16C2226/32Material joints by soldering
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/30Material joints
    • F16C2226/36Material joints by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50Positive connections
    • F16C2226/70Positive connections with complementary interlocking parts
    • F16C2226/76Positive connections with complementary interlocking parts with tongue and groove or key and slot
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S76/00Metal tools and implements, making
    • Y10S76/05Electric welding
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49636Process for making bearing or component thereof
    • Y10T29/49643Rotary bearing
    • Y10T29/49647Plain bearing
    • Y10T29/49668Sleeve or bushing making
    • Y10T29/49677Sleeve or bushing making having liner
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • Y10T428/12042Porous component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • Y10T428/12063Nonparticulate metal component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12903Cu-base component
    • Y10T428/12917Next to Fe-base component
    • Y10T428/12924Fe-base has 0.01-1.7% carbon [i.e., steel]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12972Containing 0.01-1.7% carbon [i.e., steel]

Definitions

  • Another object. is to enable suchporous alloy structures to be fixed securely to shafts, etc., so asto, avoid radial displacement.
  • Fig. 1 is an elevation partly in section on line l-1 of Fig. 2, of a laminated bearing sleeve or bushing made according to the present invention.
  • Fig. 2 is an endview of the same.
  • Fig. 3 is a plan of a partially cut gear blank made in accordance with the invention, with part of the blank broken away.
  • porous metallic materials capable of absorbing a relatively large proportion of liquid lubricant have been used for'plain bearings with a large measure of success.
  • These materials consist of'a porous alloy, preferably bronze, having uniformly distributed tlierethrough a finely divided
  • Various materials have been used for the latter purpose and among these may be mentioned graphite, mica, magnesia,-alumina, talc, etc.
  • Porous alloy structures do not have sufiicient strength to withstand the extreme heavy loads and shocks to which the articles would be subjected if used without reinforcement in some of the places where their properties would make them highly desirable. Accordingly the articles which are subject of the appended claims, have been devised to take care of this particular difficulty, which is overcome by reenforcing the bearing material with a ring or portion of non-porous ALLOY STRUCTURE 192s. seri l No. 630,414.
  • the present invention relates to porous .Y relatively strong metal, for example, steel.
  • the gear is shown as being made of the porous alloy 10 carried upon a steel 'collar 15 which latter has been slotted as at 16' for the purpose of permitting the use of a key to fix the gear upon a'shaft.
  • the formed article is then allowed to cool without access of air and when cooled is slized by forcing through a suitable shaping
  • the process which is the subject of this application differs from that just' described in that the amount of pressure applied in the second step is chosen with a diflerent end in view.
  • the pressure is so chosen that in the subsequent sintering or alloying process the article will neither swell nor shrink an objectionable amount, so that the die is substantially the size of the finished body.
  • Another method of producing articles such as shown in Fig. 3 consists in compressing the alloyable materials between a steel core or liner prepared as indicated below, and an outside'steel sleeve, using a compression of about 80,000 lbs. per square inch so as to cause an expansion or swelling in the heating operation.
  • the compressed material will tend to expand more than the encasing steel sleeve and as the latter is sufiiciently strong to resist the pressure, the alloying composition will be forced against the liner.
  • the reenforcing ring is first tinned upon the surface to be in contact with the alloy and then placed in the die and the operations carried out as described.
  • the tinning step is carried out to facilitate a cohesive bonding of the alloy and steel or other metal.
  • the junction therefore, is not merely a pressure contact, but is also a welded or soldered oint. It is obvious that, when using other metals than those mentioned, the tinning may be done with something other than tin so as to facilitate the bonding of the layers or laminations.
  • a new article of manufacture consisting of a body comprising porous metal bonded cohesively to a reinforcing body of relatively strong non-porous metal by a metallic alloy bond.
  • a process of producing laminated structures of porous. alloy and non-porous stronger metal laminae which comprises inlow cylinder of peripherally laminated structure, one of the laminations of which timately mixing finely divided alloy con-' stituents; compressing said constituents in a die of which the said metal lamina suitably prepared constitutes a portion; removing the so formed laminated article-from the die and heating under non-oxidizing conditions to cause alloying of the said constituents and bonding of the laminae.
  • a process of producing laminated structures of porous alloy and non-porous stronger metal laminae which comprises intimately mixing finely divided alloy constituents; compressing said constituents in a die of which the said metal laminasuitably prepared constitutes a portion; adjusting the pressure'to such an amount that, in the subsequent heating, the alloy in formation will exert pressure against the said metal lamina.
  • a process of making reinforced members adapted to be used with one surface in rubbing contact with another member which consists in mixing finely divided particles of metal, compressing and thereby molding a quantity of the metallic particles in contact with a reinforceing body of solid metal, and highly heating the so combined molded metallic particles and solid metal until coherence is effected between the molded particles and between said molded particles and the said solid metal.
  • said pressure being of such degree as to cause the metals to exert pressure a ainst the back during the heating operation or facilitating the union.
  • a bearing element comprising a bearing lining of porous metallic structure capable of absorbing lubricant, a relatively strong metal back therefor, and an interposed metal stratum alloyed with both said lining and backing.
  • a bearing element comprising a bearing lining of porous metallic structure capable of absorbing a considerable amount of lubricant, a ferrous metal back for said lining having a metal coating on its surface adjacent said lining, said coating being alloyed with the metal of said lining to give an alloy bond.
  • the method of making a" bearing I member which consists in providing a bearing back, tinning the back, placing a quantity of finely powdered metal in the back and applying heavy pressure to the powdered metal to cause it to adhere to the back.
  • a bearing element comprising a bearing lining of porous metallic structure

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Sliding-Contact Bearings (AREA)

Description

' and June 24, 1930. H. M. WILLIAMS ET L 1,766,855
ALLOY STRUCTURE Filed April 6, 1923 y W I ZZ M MM 5 supporting filling material.
' e ew 24; 1.9%07:
.uNITnnf s'i-AT s PATENT OFFICE HARRY u. wunrams AND ALE'RED L. BOEGEHOLD, 0E DAYTON, omo, nssmnons TO.
GENERAL MOTORS RESEARCH CORPORATION, OI DAYTON, OHIO, A CORPORATION 0 DELAWARE Application filed Apr-1T6,
structures adapted to be used in conjunction with other arrangements where there 5 is rubbing or sliding contact.
Among the objects of the invention is to furnish a substantial support for the porous alloy, which latter isrelatively low in resistance to bendingand shearing stresses.
Another object. is to enable suchporous alloy structures to be fixed securely to shafts, etc., so asto, avoid radial displacement.
Further objects and advantages of the presentinvention will be apparent from the followingdescription, reference being had to the accompanying drawings, where-' in a preferredform ofiembodiment of the present invention is clearly shown.
' In the drawings:
Fig. 1 is an elevation partly in section on line l-1 of Fig. 2, of a laminated bearing sleeve or bushing made according to the present invention.
Fig. 2 is an endview of the same.
' Fig. 3 is a plan of a partially cut gear blank made in accordance with the invention, with part of the blank broken away.
Bearings of porous metallic materials capable of absorbing a relatively large proportion of liquid lubricant have been used for'plain bearings with a large measure of success. These materials consist of'a porous alloy, preferably bronze, having uniformly distributed tlierethrough a finely divided Various materials have been used for the latter purpose and among these may be mentioned graphite, mica, magnesia,-alumina, talc, etc.
Porous alloy structures, however, of the kind described, do not have sufiicient strength to withstand the extreme heavy loads and shocks to which the articles would be subjected if used without reinforcement in some of the places where their properties would make them highly desirable. Accordingly the articles which are subject of the appended claims, have been devised to take care of this particular difficulty, which is overcome by reenforcing the bearing material with a ring or portion of non-porous ALLOY STRUCTURE 192s. seri l No. 630,414. The present invention relates to porous .Y relatively strong metal, for example, steel.
alloy structures and particularly to"such- Other materials such as malleable or cast iron and even brass and copper may be used with advantage .but steel has been found preferable in most instancesi In the drawings, there'fhave been illus trated a bushing constructed according to the present invention and also a gear.
In Figs. 1 and 2 the porous alloy portion is indicated at 10 and the reenforcing ma-' terial at 11.-
In. Fig. 3 the gear is shown as being made of the porous alloy 10 carried upon a steel 'collar 15 which latter has been slotted as at 16' for the purpose of permitting the use of a key to fix the gear upon a'shaft.
The process preferably followed in male, ing plain porous metallic bearings which are not reinforced, is fully described in the patent to Harry M. Williams, No. 1,642,347, issued September 13, 1927, and consists in mixing together finely divided particles of alloy constituents, for example, copper 90 parts and tin 10 parts, together with the supporting filler material (from 2' to 8 parts) also in a finelydivided condition. l/Vhen these materials have been thoroughly mixed, a suitable amount of the mixture is placed in a die and put under a'compression of about 75,000 to 80,000 lbs. per sq. inch. After having been compressed,-the formed article is placed in a furnace and heated to a temperature of about 1350 F. for about five hours, under non-oxidizing conditions.
.The formed article is then allowed to cool without access of air and when cooled is slized by forcing through a suitable shaping The process which is the subject of this application differs from that just' described in that the amount of pressure applied in the second step is chosen with a diflerent end in view.
In the process of making unreinforced bearings the pressure is so chosen that in the subsequent sintering or alloying process the article will neither swell nor shrink an objectionable amount, so that the die is substantially the size of the finished body.
In the process of this application, however,
to 90,000 lbs. per sq. inch is used.
when producing an article such as is shown in Fig. 1 of the drawings, in which the reinforcement is on the outside, such a pressure is used that, in the sintering operation, a certain amount of swelling tends to take place. In such cases a pressure of 85,200
11 the other hand, when an article of the type indicated, in Fig. 3 is in prospect, the pressure is regulated so .as to permit a small amount of shrinkage in the sintering operation, and insuch cases a pressure of 65,000 to? 0,000 lbs. is used. The reason for this will readily be seen as it is designed to give a better junction between the reenforcs ing ring and the alloy portion.
Another method of producing articles such as shown in Fig. 3 consists in compressing the alloyable materials between a steel core or liner prepared as indicated below, and an outside'steel sleeve, using a compression of about 80,000 lbs. per square inch so as to cause an expansion or swelling in the heating operation. Upon heating this assembly, the compressed material will tend to expand more than the encasing steel sleeve and as the latter is sufiiciently strong to resist the pressure, the alloying composition will be forced against the liner.
or core and exert great pressure against it. This procedure causes an effective bonding of the composition material with the liner or core, while the encasing sleeve may be comparatively easily removed.
It should be added that in producing the articles mentioned herein the reenforcing ring is first tinned upon the surface to be in contact with the alloy and then placed in the die and the operations carried out as described.
The tinning step is carried out to facilitate a cohesive bonding of the alloy and steel or other metal. The junction, therefore, is not merely a pressure contact, but is also a welded or soldered oint. It is obvious that, when using other metals than those mentioned, the tinning may be done with something other than tin so as to facilitate the bonding of the layers or laminations.
While the forms of embodiments of the invention as herein disclosed, constitute preferred forms, it is to be understood that other forms might be adopted, all coming within the scope of the claims which follow.
\Vhat we claim is as follows:
1. A new article of manufacture consisting of a body comprising porous metal bonded cohesively to a reinforcing body of relatively strong non-porous metal by a metallic alloy bond.
2. As a new article of manufacture a hollow cylinder of peripherally laminated structure, one of the laminations of which is of a non-porous relatively strong metal and another-of which comprises a porous alloy, said metal and alloy beingsecured together by a metallic alloy bond.
3. As a new article of manufacture a' holis of non-porous relatively strong metal and another of which comprises porous bronze, saidmetal and alloy being secured together by a metallic alloy bond.
4.. As a new article of manufacture a hollow cylinder of peripherally laminated structure, one of the' laminations of which is of a non-porous relatively strong metal and another of which is a porous alloy containing uniformly distributed therethrough a supporting fillingmaterial, said metal and alloy being secured together by a metallic alloy bond.
5. As a new article of manufacture a hollow cylinder of peripherally laminated structure, one of the laminations of which is a non-porous relatively strong metal and another of which is porous bronze, containing uniformly distributed therethrough. a supporting filling material, said metal and alloy being secured together by a metallic alloy bond. a
6. As a new article of manufacture a hollow cylinder of steel having secured therein a lining of a porous alloy, bonded to the steel by a metallic alloy bond. I
7. As a new article of manufacture a hollow cylinder of steel having secured therein a lining of a porous alloy, containing uniformly distributed therethrough a supporting filling material and bonded to the steel by a metallic alloy bond.
8. A process of producing laminated structures of porous. alloy and non-porous stronger metal laminae which comprises inlow cylinder of peripherally laminated structure, one of the laminations of which timately mixing finely divided alloy con-' stituents; compressing said constituents in a die of which the said metal lamina suitably prepared constitutes a portion; removing the so formed laminated article-from the die and heating under non-oxidizing conditions to cause alloying of the said constituents and bonding of the laminae.
9. A process of producing laminated structures of porous alloy and non-porous stronger metal laminae which comprises intimately mixing finely divided alloy constituents; compressing said constituents in a die of which the said metal laminasuitably prepared constitutes a portion; adjusting the pressure'to such an amount that, in the subsequent heating, the alloy in formation will exert pressure against the said metal lamina. Y
10. The process which comprises intimately mixing finelydivided alloy constituents and finely divided supporting filling material; compressing the mixture into a tinned metal sleeve under such a pressure that the alloy material will expand in a subsequent heating step; and heating the thus formed article to cause alloying and bondin of the alloy to the sleeve.
11. he process of producing reenforced bearing bushings which comprises simulta-- neously forming a porous alloy bearing element and bonding said bearing element to a reenforcing sleeve by a metallic bond which alloys with the porous bearing element.
12. A process of making reinforced members adapted to be used with one surface in rubbing contact with another member, which consists in mixing finely divided particles of metal, compressing and thereby molding a quantity of the metallic particles in contact with a reinforceing body of solid metal, and highly heating the so combined molded metallic particles and solid metal until coherence is effected between the molded particles and between said molded particles and the said solid metal.
13. The method of making a bearing member which consists in roviding a bearing back, tinning the back applying powdered metal to the back, subjecting the metal to very heavy pressure to cause it to adhere to the back, and highly heating the resulting article to cause the metal to unite with the tinned back in good heat conducting relation.
14. In the method as defined in claim 13, said pressure being of such degree as to cause the metals to exert pressure a ainst the back during the heating operation or facilitating the union.
15. The method of making a bearing .member which consists in providing a bearing back placing a quantity of finely powdered metal in the back and applying heavy pressure to the powdered metal to cause it to adhere to the back.
attached to a relatively therefor by an alloy bond.
20. A bearing element comprising a bearing lining of porous metallic structure capable of absorbing lubricant, a relatively strong metal back therefor, and an interposed metal stratum alloyed with both said lining and backing.
21. A bearing element comprising a bearing lining of porous metallic structure capable of absorbing a considerable amount of lubricant, a ferrous metal back for said lining having a metal coating on its surface adjacent said lining, said coating being alloyed with the metal of said lining to give an alloy bond.
In testimony whereof we hereto aflix our signatures.
HARRY M. WILLIAMS. ALFRED L. BOEGEHOLD.
strong metal back 16. The method of making a" bearing I member which consists in providing a bearing back, tinning the back, placing a quantity of finely powdered metal in the back and applying heavy pressure to the powdered metal to cause it to adhere to the back.
17. The method of making a bearing member which consists in providing a bearing back, placing a quantity of finely pow dered metallic alloy constituents in the back and applying heavy pressure to the said constituents to cause them to adhere to the back.
18. The method of making a. bearing member which consists in providing a hearing back, tinning the back, placing a quantity of finely powdered metallic alloy constituents in the back and applying heavy pressure to the alloy constituents to cause them to adhere to the back.
19. A bearing element comprising a bearing lining of porous metallic structure
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2585818A (en) * 1946-09-23 1952-02-12 Moravec Josef Device for generation of high pressure
US2663069A (en) * 1951-07-20 1953-12-22 Philips Lab Inc Method of making incandescent cathodes
US2717300A (en) * 1953-12-15 1955-09-06 Tyne George Henry Thermal-expansion extreme-pressure apparatus
US2769611A (en) * 1951-08-15 1956-11-06 Schwarzkopf Dev Co Gas turbine rotors and their production
US2818339A (en) * 1955-02-28 1957-12-31 Harry W Dodds Method for producing malleable and ductile beryllium bodies
US2885287A (en) * 1954-07-14 1959-05-05 Harold F Larson Method of forming elongated compacts
US2913819A (en) * 1957-08-26 1959-11-24 American Hardware Corp Powdered metal armature
US2996791A (en) * 1956-11-23 1961-08-22 Hughes Aircraft Co Method of manufacturing a composite rotor
US3123471A (en) * 1964-03-03 Nickel bonding method
US3370947A (en) * 1964-02-03 1968-02-27 Talmage Charles Robert Method of securing a sintered metal brake track in a brake drum shell by expanding a green compact during sintering
WO2021026750A1 (en) * 2019-08-13 2021-02-18 潍柴动力股份有限公司 Porous valve guide and processing process thereof

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123471A (en) * 1964-03-03 Nickel bonding method
US2585818A (en) * 1946-09-23 1952-02-12 Moravec Josef Device for generation of high pressure
US2663069A (en) * 1951-07-20 1953-12-22 Philips Lab Inc Method of making incandescent cathodes
US2769611A (en) * 1951-08-15 1956-11-06 Schwarzkopf Dev Co Gas turbine rotors and their production
US2717300A (en) * 1953-12-15 1955-09-06 Tyne George Henry Thermal-expansion extreme-pressure apparatus
US2885287A (en) * 1954-07-14 1959-05-05 Harold F Larson Method of forming elongated compacts
US2818339A (en) * 1955-02-28 1957-12-31 Harry W Dodds Method for producing malleable and ductile beryllium bodies
US2996791A (en) * 1956-11-23 1961-08-22 Hughes Aircraft Co Method of manufacturing a composite rotor
US2913819A (en) * 1957-08-26 1959-11-24 American Hardware Corp Powdered metal armature
US3370947A (en) * 1964-02-03 1968-02-27 Talmage Charles Robert Method of securing a sintered metal brake track in a brake drum shell by expanding a green compact during sintering
WO2021026750A1 (en) * 2019-08-13 2021-02-18 潍柴动力股份有限公司 Porous valve guide and processing process thereof

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