US2465978A - Thermochemical powder-scarfing method - Google Patents
Thermochemical powder-scarfing method Download PDFInfo
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- US2465978A US2465978A US644550A US64455046A US2465978A US 2465978 A US2465978 A US 2465978A US 644550 A US644550 A US 644550A US 64455046 A US64455046 A US 64455046A US 2465978 A US2465978 A US 2465978A
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- powder
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- scarfing
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- 238000000034 method Methods 0.000 title description 18
- 229910052751 metal Inorganic materials 0.000 description 39
- 239000002184 metal Substances 0.000 description 39
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 37
- 229910052760 oxygen Inorganic materials 0.000 description 37
- 239000001301 oxygen Substances 0.000 description 37
- 239000000843 powder Substances 0.000 description 33
- 238000006243 chemical reaction Methods 0.000 description 21
- 238000010438 heat treatment Methods 0.000 description 8
- 239000002671 adjuvant Substances 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 239000007789 gas Substances 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 230000000750 progressive effect Effects 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- QFXZANXYUCUTQH-UHFFFAOYSA-N ethynol Chemical group OC#C QFXZANXYUCUTQH-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- -1 ferrous metals Chemical class 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 229910000616 Ferromanganese Inorganic materials 0.000 description 1
- 229910001296 Malleable iron Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- DALUDRGQOYMVLD-UHFFFAOYSA-N iron manganese Chemical compound [Mn].[Fe] DALUDRGQOYMVLD-UHFFFAOYSA-N 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 230000037390 scarring Effects 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K7/00—Cutting, scarfing, or desurfacing by applying flames
- B23K7/08—Cutting, scarfing, or desurfacing by applying flames by applying additional compounds or means favouring the cutting, scarfing, or desurfacing procedure
Definitions
- This invention relates to a method for thermochemically scarfing metals and alloys which resist progressive oxidation by the sole action of a jet of oxygen impinging on heated portions thereof.
- thermochemically removing metal from such resistant metals and alloys as alloy steels containing over 5% of chromium (e. g. 18% Cr-8% Ni stainless steel), cast iron, and non ferrous metals and alloys, such as those comprising copper, aluminum, and nickel.
- chromium e. g. 18% Cr-8% Ni stainless steel
- non ferrous metals and alloys such as those comprising copper, aluminum, and nickel.
- the powder comprises highly combustible material such as an exothermically oxidizable metal, for example, iron or ferromanganese powder.
- scarfing such a metal body to remove a surface layer of metal
- an oxygen jet flowing at a velocity between 550 and 750 ft./sec. is directed at an acute angle to the heated surface in the direction of the path of metal removal, and the thermochemical reaction is advanced by effecting movement of the oxygen jet, preheating medium, and powder stream lengthwise of the path.
- the term scarfing as used herein to denote removal of a surface layer to a shallow depth embraces such diverse operations as desurfacing by a plurality of adjacent oxygen jets, deseaming, and flame machining.
- the objects of the present invention are to improve the efiiciency of the foregoing method for thermochemically scarfing resistant metals; and to improve the character of surface obtained on a resistant metal body scarfed by the foregoing method.
- Fig. l is a fragmentary longitudinal sectional view, parts being in elevation, of a scarfing blowpipe and supporting device therefor in position for scarring a resistant metal body;
- Fig. 2 is a side elevational view showing in detail the supporting device of Fig. 1;
- Fig. 3 is an elevational view of the supporting device as seen from the right in Fig. 2.
- thermochemically scarfing a resistant metal body such as a billet of stainless steel
- a preheating me- 2 dium such as an oxy-acetylene heating flame
- a stream of finely-divided powder comprising particles of exothermically oxidizable metal through between 2.5 and 6 inches of free space before they enter the reaction zone on the metal body.
- a jet of commercially pure oxygen is directed into the reaction zone through the same distance as the powder and flame, but effective results can be obtained even if the oxygen flows through a greater or smaller distance.
- the powder is fully preheated to combustion temperature by the flame when it enters the reaction zone, thus providing a high rate of. powder combustion in the reaction zone, and increasing the efficiency of the process.
- Less than 2.5 inches of travel retards the rate of powder combustion in the reaction zone, decreases efficiency, and causes the scarfed groove or furrow to have undesirably rough and stringy edges which are likely to reduce the quality of the products obtained upon further processing the scarfed body. If there is a greater travel than 6 inches it may not be possible to maintain the scarfing reaction at all, but even if the scaring reaction can be maintained, there is a substantial reduction in efficiency.
- the distance traveled in free space is meant the distance traveled without restraint by a physical object, although during such travel in free space the powder, oxygen, and preheating flame gases may interfere with one another to some extent.
- increasing efficiency is meant increasing the quantity of metal removed per cubic foot of oxygen, the quantity of metal removed per pound of powder, and the cubic feet of oxygen consumed per pound of powder.
- the distance through which the powder travels for the best combination of high efficiency and good surface character also depends on powder size. If a relatively coarse powder is used, e. g. pr
- the powder travel should be near the 6 inch upper limit; and if a relatively fine powder is used, e. g. 100% fin-er than 100 mesh and 58% finer than 325 mesh, the powder travel should be near the lower limit.
- the heating flame, the jet of scarfing oxygen, and the powder stream are advantageously all inclined at an acute angle to the surface and are directed along the surface lengthwise of the selected path toward the successive reaction zones from which metal is to be removed.
- the axis of the scarfing oxygen jet advantageously is inclined at an angle between 20 and 35 to the surface, and ordinarily the preheating flames and the stream of powder have the same inclination.
- the heating flames may be inclined more or less than the scarfing oxygen jet, and, if the powder stream is separate from the oxygen jet, the powder stream may be directed at a different angle than the jet.
- an oxygen jet of low velocity is used, generally being maintained below 980 ft./sec. (the acoustic velocity in oxygen).
- Suitable apparatus for carrying out the method described above comprises a scarfing nozzle N secured in a blowpipe head H.
- Nozzle N has a large diameter central longitudinal oxygen passage ll coaxially within which is a relatively small diameter tubular oxygen injector l2 spaced from the cylindrical wall of the passage H by radial fins ll, and supplied with scarfing oxygen from a conduit l3.
- Adjuvant powder suspended in a gas, such as compressed air, is supplied by a conduit l9 to the annular space 2! surrounding the injector l2 from which it is aspirated between th fins ll into oxygen passage i! and mixes intimately with the scarfing oxygen before leaving the nozzle.
- a combustible gas such as an oxy-acetylene gas mixture
- a conduit 23 For heating the powder and the workpiece a combustible gas, such as an oxy-acetylene gas mixture, is supplied by a conduit 23 to a plurality of annularly arranged longitudinal passages 25 surrounding passage H, and ignition of the resulting gas jets forms a preheating fiame composed of a plurality of intensely hot flame jets surrounding the central powder-laden oxygen jet.
- the nozzle N When scarfing a metal body B by the method of the invention, the nozzle N is held by the operator in such a position that the preheating flame jets, and the central oxygen jet carrying a stream of adjuvant powder are all directed toward th surface of the body at an angle between 20 and 35 to its surface, and the end of the nozzle N is held at least 2.5 but not more than 6 inches from the original surface of the body so that the required distance of travel is obtained before the powder enters the reaction zone Z and impinges against the body.
- a fluid slag containing both molten metal and oxides forms in the I reaction zone Z and is blown ahead by the oxygen jet to preheat the surface of the metal in ad- Vance of the nozzle, as shown at M in Fig. 1.
- the nozzle is provided with a projecting support or skid S which rides in the groove G on the hot newlyexposed surface of the work behind the reaction zone Z.
- the support S is so constructed and so arranged with respect to the nozzle that when the operator holds the nozzle at an angle between 20 and 35 to the surface with the support in contact with the surface, the proper spacing of the discharge orifices of the nozzle from the reaction zone Z is obtained automatically.
- the preferred form of supporting device or skid S comprises a split ring clamp 21 which fits over the nozzle N at an appropriate short distance behind its discharge orifices, and a leg 29 which is integral with an extends radially from the clamp and has a foot end 3
- the foot end 3! of the skid S is subject to severe abrasion by the hot newly-exposed surface of the groove G as the nozzle N traverses the metal body B.
- the nd 3! is provided with a rounded surface to reduce friction; and the relatively soft metal of the rounded surface is provided with a welded-on layer 35 of a suitable relatively hard and abrasion resistant material, such as a cobalt-chromiumtungsten alloy.
- the nozzle skid S can be loosened from and tightened on the nozzle N simply by manipulating a bolt 31, the head of which bears against a lug 38 integral with the clamp 21 and the threaded end of which fits in a threaded recess 39 in the upper end of the leg 29 to connect together the adjacent ends of the split ring clamp 72?.
- Turning in the bolt 3'! draws the ends of the ring together and decreases the effective opening of the clamp to firmly secure the skid to the nozzle.
- Backing out the bolt 37 causes the ends of the ring to separate due to the resilience of the metal, and increases the effective opening of the clamp so that the skid can be removed from the nozzle.
- thermochemically removing a layer of metal on a path extending along the surface of a body of metal or alloy which resists the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, and concurrently directing into said successive reaction zones a jet of oxygen flowing obliquely toward and along the surface of said body lengthwise of said path in the direction of such successive reaction zones at a velocity between 550 and 750 ft./sec.
- thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 556 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, while concurrently directing such flame, oxygen jet and powder obliquely toward and along the surface of said body lengthwise of said path toward such successive reaction zones.
- thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 550 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, while concurrently directing such flame, oxygen jet, and powder obliquely toward and along the surface of said body lengthwise of said path toward such successive zones, at least said oxygen jet being inclined at an angle between 20 and 35 to said surface.
- thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 550 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body,
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Description
March 29, 1949. E. MEINCKE THERMOCHEMICAL POWDER-SCARFING METHOD Filed Jan. 51, 1946 INVENTOR EDWARD MEINCKE ATTORNEY Patented Mar. 29, 1949 THERMOCHEMICAL POWDEB-SCARFING METHDD Edward Meincke, Summit, N. J., assignor to The Linde Air Products Company, a corporation of Ohio Application January 31, 1946, Serial No. 644,550
4 Claims.
This invention relates to a method for thermochemically scarfing metals and alloys which resist progressive oxidation by the sole action of a jet of oxygen impinging on heated portions thereof.
There has recently been developed a process for thermochemically removing metal from such resistant metals and alloys as alloy steels containing over 5% of chromium (e. g. 18% Cr-8% Ni stainless steel), cast iron, and non ferrous metals and alloys, such as those comprising copper, aluminum, and nickel. In the new process a flowing stream of powdered adjuvant material which promotes the metal removing reaction is applied against the resistant metal body concurrently with the usual oxygen jet and preheating medium, such as an oxyacetylene flame. Generally the powder comprises highly combustible material such as an exothermically oxidizable metal, for example, iron or ferromanganese powder.
When scarfing such a metal body to remove a surface layer of metal, an oxygen jet flowing at a velocity between 550 and 750 ft./sec. is directed at an acute angle to the heated surface in the direction of the path of metal removal, and the thermochemical reaction is advanced by effecting movement of the oxygen jet, preheating medium, and powder stream lengthwise of the path. The term scarfing as used herein to denote removal of a surface layer to a shallow depth embraces such diverse operations as desurfacing by a plurality of adjacent oxygen jets, deseaming, and flame machining.
Among the objects of the present invention are to improve the efiiciency of the foregoing method for thermochemically scarfing resistant metals; and to improve the character of surface obtained on a resistant metal body scarfed by the foregoing method.
The above and other objects, and the novel features of the invention, will become apparent from the following description, having reference to the annexed drawing wherein:
Fig. l is a fragmentary longitudinal sectional view, parts being in elevation, of a scarfing blowpipe and supporting device therefor in position for scarring a resistant metal body;
Fig. 2 is a side elevational view showing in detail the supporting device of Fig. 1; and
Fig. 3 is an elevational view of the supporting device as seen from the right in Fig. 2.
I have found that the efficiency and the character of the surface obtained when thermochemically scarfing a resistant metal body, such as a billet of stainless steel, are improved considerably by concurrently directing a preheating me- 2 dium, such as an oxy-acetylene heating flame, and a stream of finely-divided powder comprising particles of exothermically oxidizable metal through between 2.5 and 6 inches of free space before they enter the reaction zone on the metal body. Usually a jet of commercially pure oxygen is directed into the reaction zone through the same distance as the powder and flame, but effective results can be obtained even if the oxygen flows through a greater or smaller distance. If these limits are observed, the powder is fully preheated to combustion temperature by the flame when it enters the reaction zone, thus providing a high rate of. powder combustion in the reaction zone, and increasing the efficiency of the process. Less than 2.5 inches of travel retards the rate of powder combustion in the reaction zone, decreases efficiency, and causes the scarfed groove or furrow to have undesirably rough and stringy edges which are likely to reduce the quality of the products obtained upon further processing the scarfed body. If there is a greater travel than 6 inches it may not be possible to maintain the scarfing reaction at all, but even if the scaring reaction can be maintained, there is a substantial reduction in efficiency.
By the distance traveled in free space is meant the distance traveled without restraint by a physical object, although during such travel in free space the powder, oxygen, and preheating flame gases may interfere with one another to some extent. By increasing efficiency is meant increasing the quantity of metal removed per cubic foot of oxygen, the quantity of metal removed per pound of powder, and the cubic feet of oxygen consumed per pound of powder.
The distance through which the powder travels for the best combination of high efficiency and good surface character also depends on powder size. If a relatively coarse powder is used, e. g. pr
lominantly coarser than mesh, the powder travel should be near the 6 inch upper limit; and if a relatively fine powder is used, e. g. 100% fin-er than 100 mesh and 58% finer than 325 mesh, the powder travel should be near the lower limit.
When scarfing, the heating flame, the jet of scarfing oxygen, and the powder stream (either separately or entrained by and mixed with the scarfing oxygen) are advantageously all inclined at an acute angle to the surface and are directed along the surface lengthwise of the selected path toward the successive reaction zones from which metal is to be removed. The axis of the scarfing oxygen jet advantageously is inclined at an angle between 20 and 35 to the surface, and ordinarily the preheating flames and the stream of powder have the same inclination. However, for some operations the heating flames may be inclined more or less than the scarfing oxygen jet, and, if the powder stream is separate from the oxygen jet, the powder stream may be directed at a different angle than the jet. As in the scarfing of carbon steels, an oxygen jet of low velocity is used, generally being maintained below 980 ft./sec. (the acoustic velocity in oxygen).
Suitable apparatus for carrying out the method described above, as shown in Fig. 1, comprises a scarfing nozzle N secured in a blowpipe head H. Nozzle N has a large diameter central longitudinal oxygen passage ll coaxially within which is a relatively small diameter tubular oxygen injector l2 spaced from the cylindrical wall of the passage H by radial fins ll, and supplied with scarfing oxygen from a conduit l3. Adjuvant powder suspended in a gas, such as compressed air, is supplied by a conduit l9 to the annular space 2! surrounding the injector l2 from which it is aspirated between th fins ll into oxygen passage i! and mixes intimately with the scarfing oxygen before leaving the nozzle. For heating the powder and the workpiece a combustible gas, such as an oxy-acetylene gas mixture, is supplied by a conduit 23 to a plurality of annularly arranged longitudinal passages 25 surrounding passage H, and ignition of the resulting gas jets forms a preheating fiame composed of a plurality of intensely hot flame jets surrounding the central powder-laden oxygen jet.
When scarfing a metal body B by the method of the invention, the nozzle N is held by the operator in such a position that the preheating flame jets, and the central oxygen jet carrying a stream of adjuvant powder are all directed toward th surface of the body at an angle between 20 and 35 to its surface, and the end of the nozzle N is held at least 2.5 but not more than 6 inches from the original surface of the body so that the required distance of travel is obtained before the powder enters the reaction zone Z and impinges against the body. A fluid slag containing both molten metal and oxides forms in the I reaction zone Z and is blown ahead by the oxygen jet to preheat the surface of the metal in ad- Vance of the nozzle, as shown at M in Fig. 1. By moving nozzle N over the body B, metal is progressively removed from successive surface zones, leaving a shallow groove or furrow G.
To insure that the angle of impingement of the oxygen jet against the work and the spacing of the end of the nozzle N from the work are maintained substantially constant during traverse of the nozzle over the work, the nozzle is provided with a projecting support or skid S which rides in the groove G on the hot newlyexposed surface of the work behind the reaction zone Z. The support S is so constructed and so arranged with respect to the nozzle that when the operator holds the nozzle at an angle between 20 and 35 to the surface with the support in contact with the surface, the proper spacing of the discharge orifices of the nozzle from the reaction zone Z is obtained automatically.
The preferred form of supporting device or skid S comprises a split ring clamp 21 which fits over the nozzle N at an appropriate short distance behind its discharge orifices, and a leg 29 which is integral with an extends radially from the clamp and has a foot end 3| adapted to slide along or ride on the newly-exposed hot surface of the body B. It is essential that such a nozzle skid be light in weight, so that the operator of the blowtorch will not become unduly fatigued, yet it must be suificiently strong and rigid to insure that the correct operating conditions are obtained. Both of these requirements are met by making the skid of metal such as malleable iron and by providing the skid with a T-shaped cross-section between the clamp 2? and the foot end of the leg 29 so that there is a narrow central reinforcing rib 33 extending lengthwise of the leg of the skid.
The foot end 3! of the skid S is subject to severe abrasion by the hot newly-exposed surface of the groove G as the nozzle N traverses the metal body B. To reduce wear to a minimum the nd 3! is provided with a rounded surface to reduce friction; and the relatively soft metal of the rounded surface is provided with a welded-on layer 35 of a suitable relatively hard and abrasion resistant material, such as a cobalt-chromiumtungsten alloy.
The nozzle skid S can be loosened from and tightened on the nozzle N simply by manipulating a bolt 31, the head of which bears against a lug 38 integral with the clamp 21 and the threaded end of which fits in a threaded recess 39 in the upper end of the leg 29 to connect together the adjacent ends of the split ring clamp 72?. Turning in the bolt 3'! draws the ends of the ring together and decreases the effective opening of the clamp to firmly secure the skid to the nozzle. Backing out the bolt 37 causes the ends of the ring to separate due to the resilience of the metal, and increases the effective opening of the clamp so that the skid can be removed from the nozzle.
Specific embodiments of my novel method have been described in detail solely to illustrate the principles of the invention. It is to be understood that changes in procedure can be made within the scope of the invention as defined in the appended claims.
I claim:
1. A method of thermochemically removing a layer of metal on a path extending along the surface of a body of metal or alloy which resists the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, and concurrently directing into said successive reaction zones a jet of oxygen flowing obliquely toward and along the surface of said body lengthwise of said path in the direction of such successive reaction zones at a velocity between 550 and 750 ft./sec.
2. A method of thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 556 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, while concurrently directing such flame, oxygen jet and powder obliquely toward and along the surface of said body lengthwise of said path toward such successive reaction zones.
3. A method of thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 550 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body, while concurrently directing such flame, oxygen jet, and powder obliquely toward and along the surface of said body lengthwise of said path toward such successive zones, at least said oxygen jet being inclined at an angle between 20 and 35 to said surface.
4. A method of thermochemically scarfing metal and alloy bodies which resist the progressive removal of metal by the sole action of a jet of oxygen upon heated portions thereof, such method comprising concurrently directing together through between 2.5 and 6 inches of free space a heating flame, a jet of oxygen flowing at a velocity between 550 and 750 ft./sec., and finely divided adjuvant powder comprising particles of exothermically oxidizable metal into successive reaction zones along a selected path on said body,
while concurrently directing such flame, oxygen jet, and powder obliquely toward and along the surface of said body lengthwise of said path toward such successive zones, said powder being intimately mixed with and carried by said oxygen jet.
EDWARD MEINCKE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 936,438 Fitzgerald Oct. 12, 1909 1,097,746 Benton May 26, 1914 1,704,473 Greene Mar. 5, 1929 1,714,329 Stevens May 21, 1929 1,823,194 Gray Sept. 15, 1931 1,944,125 Halbing Jan. 16, 1934 1,957,351 Oldham May 1, 1934 2,125,180 Serner July 26, 1938 2,205,890 Nicholson et a1. June 25, 1940 2,280,151 Hughey Apr. 21, 1942 2,286,191 Aitchison et al. June 16, 1942 2,415,815 Deming Feb. 18, 1947 2,444,900 Meincke et a1. July 6, 1948
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US644550A US2465978A (en) | 1946-01-31 | 1946-01-31 | Thermochemical powder-scarfing method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US644550A US2465978A (en) | 1946-01-31 | 1946-01-31 | Thermochemical powder-scarfing method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2465978A true US2465978A (en) | 1949-03-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US644550A Expired - Lifetime US2465978A (en) | 1946-01-31 | 1946-01-31 | Thermochemical powder-scarfing method |
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| US (1) | US2465978A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2536201A (en) * | 1946-04-19 | 1951-01-02 | Linde Air Prod Co | Thermochemical metal removal method and apparatus |
| US2622048A (en) * | 1950-04-18 | 1952-12-16 | Union Carbide & Carbon Corp | External powder scarfing process and apparatus |
| US2674210A (en) * | 1950-09-29 | 1954-04-06 | Union Carbide & Carbon Corp | External powder feed-hand scarfing apparatus |
| US3169851A (en) * | 1960-02-04 | 1965-02-16 | Union Carbide Corp | Process for the oxidation of powders |
| US3734477A (en) * | 1971-07-19 | 1973-05-22 | N Enfantino | Guide for cutting torch |
| US3982883A (en) * | 1973-11-23 | 1976-09-28 | Etter Berwyn E | Method of flame cutting |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US936438A (en) * | 1908-07-31 | 1909-10-12 | James W Fitz Gerald | Hose-support. |
| US1097746A (en) * | 1912-05-18 | 1914-05-26 | Fred H Benton | Hose-nozzle holder. |
| US1704473A (en) * | 1927-10-20 | 1929-03-05 | Irl D Greene | Torch support |
| US1714329A (en) * | 1927-10-05 | 1929-05-21 | Charles D Stevens | Nozzle holder |
| US1823194A (en) * | 1930-09-02 | 1931-09-15 | Jesse L Gray | Motion controlling attachment for cutting torches |
| US1944125A (en) * | 1932-07-23 | 1934-01-16 | Linde Air Prod Co | Welding and cutting apparatus |
| US1957351A (en) * | 1931-07-10 | 1934-05-01 | Linde Air Prod Co | Method of removing metal from metal articles |
| US2125180A (en) * | 1935-05-07 | 1938-07-26 | Union Carbide & Carbon Corp | Method of flame machining |
| US2205890A (en) * | 1937-06-11 | 1940-06-25 | Linde Air Prod Co | Method of cutting or flamemachining metal |
| US2280151A (en) * | 1940-05-03 | 1942-04-21 | Air Reduction | Flame machining |
| US2286191A (en) * | 1939-04-18 | 1942-06-16 | Linde Air Prod Co | Mineral piercing and cutting |
| US2415815A (en) * | 1945-08-17 | 1947-02-18 | Air Reduction | Method of thermochemically cutting metal |
| US2444900A (en) * | 1943-04-21 | 1948-07-06 | Linde Air Prod Co | Blowpipe apparatus |
-
1946
- 1946-01-31 US US644550A patent/US2465978A/en not_active Expired - Lifetime
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US936438A (en) * | 1908-07-31 | 1909-10-12 | James W Fitz Gerald | Hose-support. |
| US1097746A (en) * | 1912-05-18 | 1914-05-26 | Fred H Benton | Hose-nozzle holder. |
| US1714329A (en) * | 1927-10-05 | 1929-05-21 | Charles D Stevens | Nozzle holder |
| US1704473A (en) * | 1927-10-20 | 1929-03-05 | Irl D Greene | Torch support |
| US1823194A (en) * | 1930-09-02 | 1931-09-15 | Jesse L Gray | Motion controlling attachment for cutting torches |
| US1957351A (en) * | 1931-07-10 | 1934-05-01 | Linde Air Prod Co | Method of removing metal from metal articles |
| US1944125A (en) * | 1932-07-23 | 1934-01-16 | Linde Air Prod Co | Welding and cutting apparatus |
| US2125180A (en) * | 1935-05-07 | 1938-07-26 | Union Carbide & Carbon Corp | Method of flame machining |
| US2205890A (en) * | 1937-06-11 | 1940-06-25 | Linde Air Prod Co | Method of cutting or flamemachining metal |
| US2286191A (en) * | 1939-04-18 | 1942-06-16 | Linde Air Prod Co | Mineral piercing and cutting |
| US2280151A (en) * | 1940-05-03 | 1942-04-21 | Air Reduction | Flame machining |
| US2444900A (en) * | 1943-04-21 | 1948-07-06 | Linde Air Prod Co | Blowpipe apparatus |
| US2415815A (en) * | 1945-08-17 | 1947-02-18 | Air Reduction | Method of thermochemically cutting metal |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2536201A (en) * | 1946-04-19 | 1951-01-02 | Linde Air Prod Co | Thermochemical metal removal method and apparatus |
| US2622048A (en) * | 1950-04-18 | 1952-12-16 | Union Carbide & Carbon Corp | External powder scarfing process and apparatus |
| US2674210A (en) * | 1950-09-29 | 1954-04-06 | Union Carbide & Carbon Corp | External powder feed-hand scarfing apparatus |
| US3169851A (en) * | 1960-02-04 | 1965-02-16 | Union Carbide Corp | Process for the oxidation of powders |
| US3734477A (en) * | 1971-07-19 | 1973-05-22 | N Enfantino | Guide for cutting torch |
| US3982883A (en) * | 1973-11-23 | 1976-09-28 | Etter Berwyn E | Method of flame cutting |
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