USRE22282E - Method of bonding powdered - Google Patents
Method of bonding powdered Download PDFInfo
- Publication number
- USRE22282E USRE22282E US22282DE USRE22282E US RE22282 E USRE22282 E US RE22282E US 22282D E US22282D E US 22282DE US RE22282 E USRE22282 E US RE22282E
- Authority
- US
- United States
- Prior art keywords
- steel
- powdered
- bonding
- coating
- protective coating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000000034 method Methods 0.000 title description 23
- 229910000831 Steel Inorganic materials 0.000 description 27
- 239000010959 steel Substances 0.000 description 27
- 239000012254 powdered material Substances 0.000 description 17
- 239000011253 protective coating Substances 0.000 description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 12
- 229910052802 copper Inorganic materials 0.000 description 12
- 239000010949 copper Substances 0.000 description 12
- 229910052751 metal Inorganic materials 0.000 description 10
- 239000011248 coating agent Substances 0.000 description 9
- 238000000576 coating method Methods 0.000 description 9
- 239000007769 metal material Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 6
- 238000004140 cleaning Methods 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 239000001301 oxygen Substances 0.000 description 6
- 229910052760 oxygen Inorganic materials 0.000 description 6
- 238000005245 sintering Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 239000010953 base metal Substances 0.000 description 4
- 239000002131 composite material Substances 0.000 description 4
- 238000007747 plating Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture 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
- B22F7/02—Manufacture 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
- B22F7/04—Manufacture 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
- the present invention relates to a novel method for bonding a powdered metallic material or mixture to a solid supporting body such as steel.
- the general object and nature of the invention is to provide such a bonding process which will produce an eflicient and satisfactory union of the powdered material, in sintered form, to the solid material or steel.
- a further object of the invention is to eliminate the formation of various oxides, metallic alloys, and other chemical compounds which heretofore have weakened and contaminated the bond or juncture between the sintered metallic material and the solid body so that a practical and commercially adaptable product was not obtainable.
- the method embodying the principle of my invention comprises the initial step of properly cleaning, both mechanically and chemically, the surface of the supporting steel body, and then maintaining such cleaned surface in uncontaminated and protected condition while the powdered metallic material, placed in contact therewith, is heated to a sintering temperature.
- cleaning as here used means the removal of all particles and films of foreign material from the surface of the steel and the maintaining of the cleaned surface in such a condition during the cleaning operation and immediately thereafter that it will not again immediately collect such foreign particles or films by oxidation.
- the herein described and claimed method is particularly adaptable for the manufacture of composite metallic elements intended for use wherein the elements are subjected to rubbing or frictional surface contact.
- Articles of manufacture fabricated from the composite metallic elements produced by my process may take the form of brake linings, clutch facings, bearings, and the like.
- the particular article here described by way of exemplary illustration in the practice of my method is a clutch facing element in the form of a flat ring and consisting of the reinforcing supporting body I of solid metal such as steel with the layer 6 of sintered metallic powdered material boned thereto.
- the first step consists of mechanically and chemically cleaning the surface of the steel supporting body I.
- cleaning is effected by any of the customary methods such as grinding, abrading, polishing, machining, sand blasting, pickling, or a combination thereof.
- the surface is covered with a protective coating capable of remaining stable at all elevated temperatures.
- elevated temperature is meant that temperature at which the bonding is begun between the powdered composition and the steel and also the temperature at which all of the oxygen entrapped in the powdered material or carried on the surface of the steel or coming from any compound which would give off oxygen has been dissipated or combined so that it will not be able to prevent bonding of the material to the steel.
- protective coating is used herein to refer to a coating which will remain protective up to the temperature referred to as an elevated temperature, which is the temperature at which the bonding between the steel and the compound begins, that is, the temperature at which all of the oxygen, which might otherwise prevent bonding, has been dissipated or combined.
- a flash coat of copper plating is particularly suitable for the purpose of supplying such protective coating. In order to produce such a flash coating of copper on the surface of the steel ring I, the latter is placed in an electrolytic deposition bath and allowed to remain at least until there is produced a copper color on the steel surface.
- the protective coating 2 applied to the steel ring I may also consist of a non-reactive material, such as a high flash point oil, which will remain protective and will not become completely decomposed or gaseous until subjected to a. temperature above that herein referred to as an elevated temperature.
- a non-reactive material such as a high flash point oil
- the steel ring I with its protective coating 2 is next placed in a forming die, consisting of the femaledie member 4 and the male die member or plunger 5, with the layer of powdered metallic material 3 superimposed on the steel ring I.
- the assembled elements in the apparatus shown in Fig. 3, consisting of the steel ring I, the protective coating 2 and the layer of powdered metallic material 3 are then subjected to pressure and a temperature sufiicient to sinter the powdered material 3 and to thereby bond the layer to the steel ring I.
- One method of compressing and sintering the powdered material and the steel supporting layer is more particularly described and claimed in my co-pending application Method of making composite metallic elements," filed July 22, 1936, Serial No. 91,- 869 (United States Patent 2,156,611)
- the resultant product of the above described process is shown in Fig. 4, and consists of the layer of sintered, powdered metallic material 8 strongly bonded to the steel layer I along the bonding line 1.
- the metallic powdered material 3 may consist of a mixture of a base metal such as aluminum or copper with smaller proportions of other materials such as tin and lead and also relatively inert material such as powdered silica, magnesia, talc, graphite or silicon carbide.
- the use of a protective coating 2, consisting of a flash coat of copper is particularly desirable in the performance of my process where a copper base metallic powder is used, and almost mandatory in case a high carbon steel is used.
- graphite is especially desirable to be used when a protective coating of copper is employed for the steel.
- the fine particles of the powdered material contain a substantial amount of oxygen and nitrogen in the form of air, some entrained in the mixture and some contained by surface adhesion on the particles, which if allowed to come in contact with the cleaned surface of the steel layer I during the heating step, will prevent the formation of an eflicient and satisfactory bond due to chemical reaction of the faces to be bonded with these gases.
- the protective coating of copper plating 2 prevents any 0! the constituents of the powdered material 3, uch as tin, from contacting the surface of the steel layer l and in turn alloying with the iron in the steel, which alloy would also be of a brittle and nonductile nature susceptible of fracture upon flexing 1 of the finished composite element.
- the layer 2 of copper plating disappears after the heating and sintering of the powdered material 3, since it is absorbed by the copper already present in the powdered mixture, leaving the direct bonding line 1 between the steel layer 1 and the sintered layer 6.
- the protective coating 2 in the performance of the above described method, whether it be in the nature of the copper plating, the high flash point oil, or a similar material capable of remaining stable at an elevated temperature, prevents the entrapped oxygen in the powdered material 3 from coming in contact with the cleaned steel surface during heating and sintering, so that the bonding line is not contaminated and the efiiciency of the bond is not destroyed.
- a method of bonding powdered metallic material to a ferrous metal support comprising the.
- a method as claimed in claim 1 comprising the step of covering the clean surface of the terrou's 1metal support with a protective coating of me a 3.
- a method as claimed in claim 1 comprising the steps of covering the clean surface of the ferrous metal support with a protective coating of copper, and effecting substantially complete diffusion of said coating into the base metal o"fthe powdered material in the heating of the assembled support, coating and powdered material.
- a method as claimed in claim 1 comprising the step of covering the clean surface of the ferrous metal support with a protective coating of high flash-point oil.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
Description
March 2, 1943. c. E. SWARTZ 22,232
METHOD OF BONDING POWDERED METALLIC MATERIAL Original Filed July 22, 1936 ficQZ' ATTORNE- 6" Reissued Mar. 2, 1943 22,282 METHOD or nonnmc. POWDERED METALLIC MATERIAL Carl E. Swartz, Shaker Heights, Ohio, assignor,
by mesne assignments, to S. K. Wellman Company, Cleveland, Ohio, a corporation of Ohio Original No. 2,161,597, dated June 6, 1939, Serial No. 91,870, July 22, 1936. Application for reissue June 5, 1941, Serial No. 396,786
4 Claims.
The present invention relates to a novel method for bonding a powdered metallic material or mixture to a solid supporting body such as steel.
The general object and nature of the invention is to provide such a bonding process which will produce an eflicient and satisfactory union of the powdered material, in sintered form, to the solid material or steel.
A further object of the invention is to eliminate the formation of various oxides, metallic alloys, and other chemical compounds which heretofore have weakened and contaminated the bond or juncture between the sintered metallic material and the solid body so that a practical and commercially adaptable product was not obtainable.
Brieflly outlined, the method embodying the principle of my invention comprises the initial step of properly cleaning, both mechanically and chemically, the surface of the supporting steel body, and then maintaining such cleaned surface in uncontaminated and protected condition while the powdered metallic material, placed in contact therewith, is heated to a sintering temperature. The term cleaning as here used means the removal of all particles and films of foreign material from the surface of the steel and the maintaining of the cleaned surface in such a condition during the cleaning operation and immediately thereafter that it will not again immediately collect such foreign particles or films by oxidation.
To the accomplishment of the foregoing and related ends, said invention, then, consists of the steps hereinafter fully described and particularly pointed out in the claims, the annexed drawing and the following description setting forth in detail one approved method of carrying out the invention, such disclosed method however, constituting but one of the various'ways in which the principle of the invention may be used.
In said annexed drawing:
Fig. l is a. perspective view of a ringof the solid supporting metal body such as steel; Fig. is a sectional view of the ring of Fig. 1, showing a layer of the protective material applied to the surface of the ring; Fig. 3 is a cross-sectional view of an apparatus illustrating the performance of the sintering and bonding step of my process; and Fig. 4 is a sectional view of the finished product.
The herein described and claimed method is particularly adaptable for the manufacture of composite metallic elements intended for use wherein the elements are subjected to rubbing or frictional surface contact. Articles of manufacture fabricated from the composite metallic elements produced by my process may take the form of brake linings, clutch facings, bearings, and the like. The particular article here described by way of exemplary illustration in the practice of my method is a clutch facing element in the form of a flat ring and consisting of the reinforcing supporting body I of solid metal such as steel with the layer 6 of sintered metallic powdered material boned thereto.
In the practice of my process, the first step consists of mechanically and chemically cleaning the surface of the steel supporting body I. Such cleaning is effected by any of the customary methods such as grinding, abrading, polishing, machining, sand blasting, pickling, or a combination thereof. After such cleaning of the surface of the steel ring I has been accomplished, the surface is covered with a protective coating capable of remaining stable at all elevated temperatures. By the term elevated temperature is meant that temperature at which the bonding is begun between the powdered composition and the steel and also the temperature at which all of the oxygen entrapped in the powdered material or carried on the surface of the steel or coming from any compound which would give off oxygen has been dissipated or combined so that it will not be able to prevent bonding of the material to the steel. The term protective coating is used herein to refer to a coating which will remain protective up to the temperature referred to as an elevated temperature, which is the temperature at which the bonding between the steel and the compound begins, that is, the temperature at which all of the oxygen, which might otherwise prevent bonding, has been dissipated or combined. Particularly suitable for the purpose of supplying such protective coating is a flash coat of copper plating. In order to produce such a flash coating of copper on the surface of the steel ring I, the latter is placed in an electrolytic deposition bath and allowed to remain at least until there is produced a copper color on the steel surface.
The protective coating 2 applied to the steel ring I may also consist of a non-reactive material, such as a high flash point oil, which will remain protective and will not become completely decomposed or gaseous until subjected to a. temperature above that herein referred to as an elevated temperature.
The steel ring I with its protective coating 2 is next placed in a forming die, consisting of the femaledie member 4 and the male die member or plunger 5, with the layer of powdered metallic material 3 superimposed on the steel ring I. The assembled elements in the apparatus shown in Fig. 3, consisting of the steel ring I, the protective coating 2 and the layer of powdered metallic material 3 are then subjected to pressure and a temperature sufiicient to sinter the powdered material 3 and to thereby bond the layer to the steel ring I. One method of compressing and sintering the powdered material and the steel supporting layer is more particularly described and claimed in my co-pending application Method of making composite metallic elements," filed July 22, 1936, Serial No. 91,- 869 (United States Patent 2,156,611)
The resultant product of the above described process is shown in Fig. 4, and consists of the layer of sintered, powdered metallic material 8 strongly bonded to the steel layer I along the bonding line 1. The metallic powdered material 3 may consist of a mixture of a base metal such as aluminum or copper with smaller proportions of other materials such as tin and lead and also relatively inert material such as powdered silica, magnesia, talc, graphite or silicon carbide. The use of a protective coating 2, consisting of a flash coat of copper, is particularly desirable in the performance of my process where a copper base metallic powder is used, and almost mandatory in case a high carbon steel is used. f the relatively inert materials above specified as suitable constituents of the powdered material, graphite is especially desirable to be used when a protective coating of copper is employed for the steel.
The fine particles of the powdered material contain a substantial amount of oxygen and nitrogen in the form of air, some entrained in the mixture and some contained by surface adhesion on the particles, which if allowed to come in contact with the cleaned surface of the steel layer I during the heating step, will prevent the formation of an eflicient and satisfactory bond due to chemical reaction of the faces to be bonded with these gases. Furthermore, the protective coating of copper plating 2 prevents any 0! the constituents of the powdered material 3, uch as tin, from contacting the surface of the steel layer l and in turn alloying with the iron in the steel, which alloy would also be of a brittle and nonductile nature susceptible of fracture upon flexing 1 of the finished composite element. As will be noted from the illustration of Fig. 4, the layer 2 of copper plating disappears after the heating and sintering of the powdered material 3, since it is absorbed by the copper already present in the powdered mixture, leaving the direct bonding line 1 between the steel layer 1 and the sintered layer 6.
The provision of the protective coating 2 in the performance of the above described method, whether it be in the nature of the copper plating, the high flash point oil, or a similar material capable of remaining stable at an elevated temperature, prevents the entrapped oxygen in the powdered material 3 from coming in contact with the cleaned steel surface during heating and sintering, so that the bonding line is not contaminated and the efiiciency of the bond is not destroyed.
Other modes of applying the principle of my invention may be employed instead of the one explained, change being made as regards the process herein disclosed, provided the step or steps stated by the following claims or the equivalent of such stated step or steps be employed.
I therefore particularly point out and distinctly claim as my invention:
1. A method of bonding powdered metallic material to a ferrous metal support comprising the.
steps of providing a mechanically and chemically clean surface on the support, covering such surface with a thin protective coating capable of protecting the ferrous metal of the support from oxidation up to an elevated temperature, holding a body of the powdered material having a metal base with a melting point not lower than that of aluminum in contact with the said coating, and effecting substantially complete diffusion of the coating and sintering of base metal of the powdered material directly to the ferrous support by suitably heating the assembled support, coating and powdered material, the said coating serving during the heating to protect the clean surface of the ferrous support from the action of oxygen in the body of powdered material and the diffusion of said coating permitting a strong bond resistant to high temperatures to be formed directly between the ferrous support and the high melting point base metal of said body.
A method as claimed in claim 1 comprising the step of covering the clean surface of the terrou's 1metal support with a protective coating of me a 3. A method as claimed in claim 1 comprising the steps of covering the clean surface of the ferrous metal support with a protective coating of copper, and effecting substantially complete diffusion of said coating into the base metal o"fthe powdered material in the heating of the assembled support, coating and powdered material.
4. A method as claimed in claim 1 comprising the step of covering the clean surface of the ferrous metal support with a protective coating of high flash-point oil.
CARL E. SWAR'I'Z.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USRE22282E true USRE22282E (en) | 1943-03-02 |
Family
ID=2088711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US22282D Expired USRE22282E (en) | Method of bonding powdered |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | USRE22282E (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2462821A (en) * | 1945-01-22 | 1949-02-22 | Sk Wellman Co | Method of making composite articles |
| US2483996A (en) * | 1944-06-02 | 1949-10-04 | Sk Wellman Co | Method of reconditioning backing members having powdered material facings |
-
0
- US US22282D patent/USRE22282E/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2483996A (en) * | 1944-06-02 | 1949-10-04 | Sk Wellman Co | Method of reconditioning backing members having powdered material facings |
| US2462821A (en) * | 1945-01-22 | 1949-02-22 | Sk Wellman Co | Method of making composite articles |
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