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US2060959A - Process of copper brazing - Google Patents

Process of copper brazing Download PDF

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Publication number
US2060959A
US2060959A US750517A US75051734A US2060959A US 2060959 A US2060959 A US 2060959A US 750517 A US750517 A US 750517A US 75051734 A US75051734 A US 75051734A US 2060959 A US2060959 A US 2060959A
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United States
Prior art keywords
copper
paste
copper brazing
particles
space
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Expired - Lifetime
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US750517A
Inventor
Terry Robert
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Motors Liquidation Co
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Motors Liquidation Co
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Publication date
Application filed by Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to US750517A priority Critical patent/US2060959A/en
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Publication of US2060959A publication Critical patent/US2060959A/en
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Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/19Soldering, e.g. brazing, or unsoldering taking account of the properties of the materials to be soldered
    • 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
    • Y10T428/12069Plural nonparticulate metal components

Definitions

  • This invention relates to copper brazing.
  • the use of copper brazing to secure close fitting metal parts together is quite generally used throughout manufacturing methods. 5 method of accomplishing this is to place the cleaned parts in juxtaposition and then to melt a portion of copper and allow it to flow into the opening between the two parts and fill the same, adhering to the sides of the parts. In order to accomplish this satisfactorily, the spacing between the two parts is very small. If the distance between them is large or is irregular, it has been found that this method will not give a satisfactory bond.
  • Figure 1 is a perspective view showing two parts so that it is desired to braze.
  • FIG. 1' a In Figure 1' is shown a part to to. which it is desired to secure a tip [2 similar to'the application of a cutting point on a turning cutter for a lathe.
  • the two surfaces do not fit'closely, the space ll be- 40 tween the two being, of course, exaggerated.
  • Figure 3 is shown a microscopic view of the joint, the particles of iron 10 are shown which have not changed their form, and the spaces between them are filled now with copper 22 in- 10 stead of lacquer.
  • lacquer as a binder has proven very satisfactory, since it decomposes, leaving very little residue before the copper flows in.
  • the action of the 15 paste is two-fold in that it absorbs the copper into the opening by a sponge action and supports the copper therein until it is hard.
  • a method of copper brazing two metals tom gether comprising packing the space between the two with a paste of a vehicle and particles, placing a piece of copper adjacent the space, applying heat to decompose the vehicle first and later cause the molten copper to be soaked into the voids left a by the vehicle, the mass being held by the particles until solidification.
  • a method of copper brazing two metals together comprising packing the space between the two with a paste, applying heat which causes an voids therein while the remainder still retains sufilcient structure to support the whole mixture, then sucking intothe voids a binding material to provide a tight joint upon solidification.
  • a method of copper brazing two metals toas gether comprising filling the space between the two with a paste having a vehicle and particles therein in which upon an application of heat the vehicle decomposes and leaves voids, applying a sealing material adjacent the space, heating the 40 whole which draws the material into the voids, the particles maintaining the structure in the space between the metals until the sealing material has solidified.
  • a method of copper brazing two metals together comprising packing the space between the two parts with a paste composed of iron particles and lacquer, placing adjacent the space a piece of copper and applying heat whereby the lacquer first decomposes leaving voids that'suck in the so copper upon its melting and the iron particles hold it in place until it solidifies.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Description

I NOV. 17, 1936. R TERRY 2,060,959
PROCESS OF COPPER BRAZING Filed Oct. 29, 1954 gwumrm 1 2305M? 72h? Patented Nov. 11, 1936 PATENT OFFICE PROCESS OF COPPER BRAZING Robert Terry, Detroit, Mich, assignor to General Motors Corporation, Detroit, Mich., a corporation of Delaware Application October 29, 1934, Serial No. 750,517
4 Claims. (01. 113-112) This invention relates to copper brazing. The use of copper brazing to secure close fitting metal parts together is quite generally used throughout manufacturing methods. 5 method of accomplishing this is to place the cleaned parts in juxtaposition and then to melt a portion of copper and allow it to flow into the opening between the two parts and fill the same, adhering to the sides of the parts. In order to accomplish this satisfactorily, the spacing between the two parts is very small. If the distance between them is large or is irregular, it has been found that this method will not give a satisfactory bond.
- It is the object of this invention to provide a method of satisfactorily copper brazing two metals together where the fitvbetween the two is irregular or too wide to support the molten copper alone therein until it hardens. It is a further object of this invention to provide a method of copper brazing in which the molten copper is drawn into and held in the joint until solidification occurs. v
,For a better understanding of the nature and objects of this invention, reference is made to the following specification, wherein there are described the embodiments of my invention which are illustrated in the accompanying drawing.
Figure 1 is a perspective view showing two parts so that it is desired to braze.
a In Figure 1' is shown a part to to. which it is desired to secure a tip [2 similar to'the application of a cutting point on a turning cutter for a lathe. As is clearly shown in the drawing, the two surfaces do not fit'closely, the space ll be- 40 tween the two being, of course, exaggerated.
' A paste it as shown in Figure 2 is pressed into this opening with a spatula or similar device until the opening is filled. 'lhis paste is composed of reduced iron powder and clear lacquer I or any other suitable vehicle which are mixed together to form a, suitable plastic mass which will not flow but is similar to ordinary paste in constitution.
when the opening has been filled with this 50 paste, a piece of copper, indicated at I8, is placed adjacent the-edge ofthe crack and the whole is heated. During heating, the lacquer between the particles of iron decomposes and gas is driven oil,
The usual creating voids between the particles of iron so that the paste is transformed to the character of a sponge. As the copper melts, the molten copper is sucked in by the sponge action completely filling the crack and being held there by the iron 5 particles until solidification takes place.
In Figure 3 is shown a microscopic view of the joint, the particles of iron 10 are shown which have not changed their form, and the spaces between them are filled now with copper 22 in- 10 stead of lacquer. The use of lacquer as a binder has proven very satisfactory, since it decomposes, leaving very little residue before the copper flows in.
It will therefore be seen that the action of the 15 paste is two-fold in that it absorbs the copper into the opening by a sponge action and supports the copper therein until it is hard.
I claim:
1. A method of copper brazing two metals tom gether comprising packing the space between the two with a paste of a vehicle and particles, placing a piece of copper adjacent the space, applying heat to decompose the vehicle first and later cause the molten copper to be soaked into the voids left a by the vehicle, the mass being held by the particles until solidification.
2. A method of copper brazing two metals together comprising packing the space between the two with a paste, applying heat which causes an voids therein while the remainder still retains sufilcient structure to support the whole mixture, then sucking intothe voids a binding material to provide a tight joint upon solidification.
3. A method of copper brazing two metals toas gether comprising filling the space between the two with a paste having a vehicle and particles therein in which upon an application of heat the vehicle decomposes and leaves voids, applying a sealing material adjacent the space, heating the 40 whole which draws the material into the voids, the particles maintaining the structure in the space between the metals until the sealing material has solidified.
4. A method of copper brazing two metals together comprising packing the space between the two parts with a paste composed of iron particles and lacquer, placing adjacent the space a piece of copper and applying heat whereby the lacquer first decomposes leaving voids that'suck in the so copper upon its melting and the iron particles hold it in place until it solidifies.
. ROBERT TERRY.
US750517A 1934-10-29 1934-10-29 Process of copper brazing Expired - Lifetime US2060959A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE750457C (en) * 1939-11-15 1945-01-17 Intermediate hard-soldering layer for tension-free soldering of workpieces with very different coefficients of thermal expansion, especially of hard metal cutters with steel cutter carriers
US2456418A (en) * 1944-08-28 1948-12-14 Imerman Stanley Bushing and method of manufacturing same
US2464591A (en) * 1944-04-04 1949-03-15 Mallory & Co Inc P R Method of bonding a tungsten member to a backing member
US2577187A (en) * 1946-08-12 1951-12-04 North American Aviation Inc Method of forming bearings
US2606132A (en) * 1950-04-15 1952-08-05 Glidden Co Copper brazing compositions
DE946322C (en) * 1950-10-05 1956-07-26 Wallram Hartmetall Tension-equalizing intermediate layer for tools to be fitted with hard metal
US2782489A (en) * 1952-02-04 1957-02-26 Boeing Co Rotary metal cutter
US2816355A (en) * 1954-05-24 1957-12-17 Rohr Aircraft Corp Method of forming a sandwich structure with a cellular core
US2909643A (en) * 1956-11-01 1959-10-20 Gibson Electric Company Solder joint containing metallic particles
US3131779A (en) * 1962-02-01 1964-05-05 Jersey Prod Res Co Erosion resistant nozzle assembly and method for forming
US3673676A (en) * 1970-05-13 1972-07-04 Exxon Production Research Co Method for forming tool assembly

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE750457C (en) * 1939-11-15 1945-01-17 Intermediate hard-soldering layer for tension-free soldering of workpieces with very different coefficients of thermal expansion, especially of hard metal cutters with steel cutter carriers
US2464591A (en) * 1944-04-04 1949-03-15 Mallory & Co Inc P R Method of bonding a tungsten member to a backing member
US2456418A (en) * 1944-08-28 1948-12-14 Imerman Stanley Bushing and method of manufacturing same
US2577187A (en) * 1946-08-12 1951-12-04 North American Aviation Inc Method of forming bearings
US2606132A (en) * 1950-04-15 1952-08-05 Glidden Co Copper brazing compositions
DE946322C (en) * 1950-10-05 1956-07-26 Wallram Hartmetall Tension-equalizing intermediate layer for tools to be fitted with hard metal
US2782489A (en) * 1952-02-04 1957-02-26 Boeing Co Rotary metal cutter
US2816355A (en) * 1954-05-24 1957-12-17 Rohr Aircraft Corp Method of forming a sandwich structure with a cellular core
US2909643A (en) * 1956-11-01 1959-10-20 Gibson Electric Company Solder joint containing metallic particles
US3131779A (en) * 1962-02-01 1964-05-05 Jersey Prod Res Co Erosion resistant nozzle assembly and method for forming
US3673676A (en) * 1970-05-13 1972-07-04 Exxon Production Research Co Method for forming tool assembly

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