US2640792A - Inert monatomic-gas shielded refractory metal remelting surface-defect removal process - Google Patents
Inert monatomic-gas shielded refractory metal remelting surface-defect removal process Download PDFInfo
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- US2640792A US2640792A US208395A US20839551A US2640792A US 2640792 A US2640792 A US 2640792A US 208395 A US208395 A US 208395A US 20839551 A US20839551 A US 20839551A US 2640792 A US2640792 A US 2640792A
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- metal
- gas shielded
- refractory metal
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- 238000000034 method Methods 0.000 title description 7
- 239000003870 refractory metal Substances 0.000 title description 4
- 229910052751 metal Inorganic materials 0.000 description 33
- 239000002184 metal Substances 0.000 description 33
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 16
- 239000007789 gas Substances 0.000 description 14
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 12
- 230000007547 defect Effects 0.000 description 11
- 238000005260 corrosion Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 8
- 229910052757 nitrogen Inorganic materials 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 230000008018 melting Effects 0.000 description 7
- 238000002844 melting Methods 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 229910052786 argon Inorganic materials 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 239000001307 helium Substances 0.000 description 6
- 229910052734 helium Inorganic materials 0.000 description 6
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 239000002893 slag Substances 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- 229910000599 Cr alloy Inorganic materials 0.000 description 3
- 239000010953 base metal Substances 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 239000000788 chromium alloy Substances 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 229910002065 alloy metal Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- -1 chromium carbides Chemical class 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- DSMZRNNAYQIMOM-UHFFFAOYSA-N iron molybdenum Chemical compound [Fe].[Fe].[Mo] DSMZRNNAYQIMOM-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000005555 metalworking Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- SNICXCGAKADSCV-UHFFFAOYSA-N nicotine Chemical compound CN1CCCC1C1=CC=CN=C1 SNICXCGAKADSCV-UHFFFAOYSA-N 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 229910000753 refractory alloy Inorganic materials 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D3/00—Diffusion processes for extraction of non-metals; Furnaces therefor
- C21D3/02—Extraction of non-metals
Definitions
- This invention relates to metal working, and more particularly to the removal of surface defacts in refractory metal ingots by remelting the adjacent metal.
- High-chromium alloys require careful'surface conditioning prior to hot-rolling inorder to ensure satisfactory surface quality. Because of their inherent resistance to oxidation, these alloys do not scale readily, hence they retain surface defects which normally are eliminated in the reheating furnaces in the case of more freely scaling metals. Most oithe ingot'defects causing surface rejections are laps and seams due to metal splashing Since they are located near the surface, the standard commercial prac- Y tice is to remove these defects mechanically by hand grinding with abrasive wheels. More recen-tly, -powder scarfing techniques have been developed. However, both processes result in considerable loss .of metal, and the hand-grinding process is slow, relatively costly, and presents labor problems due to the disagreeable nature of the work.
- the corrosion resistance of stainless steels and related high-chromium .alloys' is a function of chromium content; higher chromium contents imparting greater resistance. Any impoverishment of the surface by oxidation of chromium would reduce the general corrosion resistance of the metal. In borderline cases, oxidation could reduce the concentration to a dangerous minimum. Loss of easily oxidizable metals such as columbium, titanium, and tantalum must also be avoided as their loss would have a dangerous effect on the corrosion resistance of the :i'.
- High-chromium alloys always carry a certain percentage of carbon and nitrogen. These elements normally are kept in solid solution and do not seriously affect the corrosion resistance of the metal. On heating in certain temperature ranges, these elements combine with chromium precipitate along the grain boundaries of The formation of carbides and niboundaries of chromium. When exposed to certain media, these areas tend to dissolve leading to inter-granular corrosion of the metal. Commonly accepted means for preventing precipitation of chromium carbides and nitrides is to keep the percentages of carbon and nitrogen in the metal low. In some cases, columbium, tantalum, or titanium are added to combine with carbon and nitrogen as these elements form relatively 1 Claim. (01. ne -i0) cast.
- High-chromium alloys are susceptible to cracking during hot-working if improperly melted and Oxygen, carbon, and nitrogen have adirect influence, and the pickup of these elements should he kept to a minimum.
- Protective. slags tend to oxidize the metal unless they are kept on the'reducing side, and they do not prevent nitrogen pickup, particularly when the slag and metal are exposed to electric arc temperatures.
- the main object of this invention to .provide an economical and eflicient method of removing all which yield the same composition in the melted as in the unmelted portions.
- surface melting according to the invention in an inert monatomic gas atmosphere has the following distinct advantages: there is no loss of easily oxidizable metals, hence the metal retains its corrosion resistance; there is no porosity due to pickup of hydrogen or nitrogen; there is no pickup of carbon or nitrogen to cause inter-granular corrosion suscepti bility; there is no loss of hot-workabilitydue to oxidation of the metal; and since no slag is used, there is no problem due to entrapmentrof slag'during solidification -or-to pickup of delerequired to remove the surface defects.
- a metal body Ill such as billet is moved horizontally under a tungsten electrode [2 provided with a gas nozzle or cup 14.
- the body l and electrode l2 are connected by leads l6 and I8 to an electric power source 20 of sufficient current-supplying capacity to energize an electric metal meltingarc 22 between the surface of the body and the tip of the electrode during such movement of the work l0.
- an electric power source 20 of sufficient current-supplying capacity to energize an electric metal meltingarc 22 between the surface of the body and the tip of the electrode during such movement of the work l0.
- an annular stream 24 of inert monatomic-gas which is delivered to the nozzle H from a suitable source via an inlet 26.
- the are 22 melts the adjacent metal containing defects, forming a. molten puddle 30 which pro nickel rich iron-molybdenum, and related alloys can be satisfactorily surface-conditioned prior to rolling by remelting the surface of the ingot with a shielded arc, according to the invention
- amperage value of the current during remelting depends on the depth of penetration An arc current of 450 amperes using argon, and a 1 in. diameter tungsten electrode will remove defects about in. deep. Somewhat lower amperage may be used with helium for substantially the same depth of penetration.
- the speed of melting depends on the surface condition of the ingot and the amperage of the arc current. A work-speed of in./minute at 450 amperes has been found satisfactory for small ingots though somewhat faster speed can be -ing inch. Surfaces of satisfactory quality were obtained, according to the invention, with a gas flow of cu. ft./hour with argon, and
- Precautions should be taken to minimize arc interruptions as the craters form areas of shallow surface cracking in the rolled surface.
- the starting craters are relatively shallow and can be removed by grinding without too much difliculty prior to rolling, and in most instances, the craters formed at the end of each pass can be confined to the piped section which is eventually discarded.
- Another scheme is to tack-weld suitable metal pieces on the ends of the ingot for starting and stopping purposes.
- an electrode composed of metal of the same composition as that of the base metal can be used, without departing from the invention, to supply the additional metal required to fill such deep cracks.
- the electrode preferably is compossed of tungsten containing significant amounts of oxidic materials, such as thoria', which improve arc stability and/or other additions which improve the operation of the electrode.
- Process of removing surface and subsurface defects including laps and scams due to metal splashing, from ingots composed of relatively high-alloy refractory metals prior to hot rolling in order to insure satisfactory surface quality of the resulting product without the loss of any of the refractory alloy metal thereof and without any change in the composition of the base metal which comprises positioning the ingot so that the surface to be conditioned is uppermost and substantially level, striking a relatively heavy duty are between such surface of the ingot and a refractory metal electrode composed of tungsten; continuously shielding such are and the adjacent portions of the electrodeand ingot with an annular stream of monatomic gas of the class consisting of argon and helium and mixtures of argon and helium discharged from a nozzle surrounding such electrode in spaced concentric relation therewith at a gas flow rate of twenty-five to forty cubic feet 'per hour, positioning the end of such nozzle as closely as possible to the surface of said ingot at a distance of not more than three-eighths of an inch, continuously moving
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
June 2, 1953 w, o, BINDER 2,640,792
INERT'MONATOMIC-GAS SHIELDED REFRACTORY. METAL REMELTING SURFACE-DEF REMOVAL PROCESS Filed Jan 1951' ECT 29 Elecfrode Lead Gas Nozzle Tungsfen Elecirode Electric Power Source Inert Gas Surface defects such as seams, laps and entrapped oxldes.
Ground Le ad INVENTOR WILLIAM O. BINDER the metal. trides depletes the areas adjacent to the grain Patented June 2, 1953 um'rao starss "eraser OFFICE 1 INERT MEONATOMIC-GAS SHIELDED as resources! METAL REMELTING SUR. sacs-career REMOVAL raocuss William 0. Binder, Niagara Falls, N. Y., assignor. to. Union Carbide and Carbon Corporation, a corporation of New York Application January 29, 1951, Serial No. 208 ,395
1 Y This invention relates to metal working, and more particularly to the removal of surface defacts in refractory metal ingots by remelting the adjacent metal. I
High-chromium alloys require careful'surface conditioning prior to hot-rolling inorder to ensure satisfactory surface quality. Because of their inherent resistance to oxidation, these alloys do not scale readily, hence they retain surface defects which normally are eliminated in the reheating furnaces in the case of more freely scaling metals. Most oithe ingot'defects causing surface rejections are laps and seams due to metal splashing Since they are located near the surface, the standard commercial prac- Y tice is to remove these defects mechanically by hand grinding with abrasive wheels. More recen-tly, -powder scarfing techniques have been developed. However, both processes result in considerable loss .of metal, and the hand-grinding process is slow, relatively costly, and presents labor problems due to the disagreeable nature of the work.
The corrosion resistance of stainless steels and related high-chromium .alloys'is a function of chromium content; higher chromium contents imparting greater resistance. Any impoverishment of the surface by oxidation of chromium would reduce the general corrosion resistance of the metal. In borderline cases, oxidation could reduce the concentration to a dangerous minimum. Loss of easily oxidizable metals such as columbium, titanium, and tantalum must also be avoided as their loss would have a dangerous effect on the corrosion resistance of the :i'.
alloys.
High-chromium alloys always carry a certain percentage of carbon and nitrogen. These elements normally are kept in solid solution and do not seriously affect the corrosion resistance of the metal. On heating in certain temperature ranges, these elements combine with chromium precipitate along the grain boundaries of The formation of carbides and niboundaries of chromium. When exposed to certain media, these areas tend to dissolve leading to inter-granular corrosion of the metal. Commonly accepted means for preventing precipitation of chromium carbides and nitrides is to keep the percentages of carbon and nitrogen in the metal low. In some cases, columbium, tantalum, or titanium are added to combine with carbon and nitrogen as these elements form relatively 1 Claim. (01. ne -i0) cast.
2 fects from steel billets by melting the adjacent metal with an are protected from the air by, a
' stream of hydrogen; However, the latter is not suitable for high-alloy metals, due to contamination of the metal by such gas. Hydrogen, aswell as nitrogen, pickup during melting is detrimental because they dissolve readily in molten highchromium alloys and may produce porosity when the metal solidifies.
Excessive silicon pickup during melting must also be avoided, as it not only decreases general corrosion resistance in some media, but also it causes brittleness, decreases weldabi'lity and hotworkability. Silicon is apt to be picked up when slags are employed'to protect the metal during melting.
High-chromium alloys are susceptible to cracking during hot-working if improperly melted and Oxygen, carbon, and nitrogen have adirect influence, and the pickup of these elements should he kept to a minimum. Protective. slags tend to oxidize the metal unless they are kept on the'reducing side, and they do not prevent nitrogen pickup, particularly when the slag and metal are exposed to electric arc temperatures.
The main object of this invention to .provide an economical and eflicient method of removing all which yield the same composition in the melted as in the unmelted portions.
ity to melt the metal in the area of the surface defect to be removed. Such are and the molten 4 metal are continuously shielded from the air by a stream of inert monatomic gas during such are remelting operation. As a result, the defect. is removed, leaving the metal that has been melted of the same composition as that of the base metal.
Summarizing, surface melting according to the invention in an inert monatomic gas atmosphere has the following distinct advantages: there is no loss of easily oxidizable metals, hence the metal retains its corrosion resistance; there is no porosity due to pickup of hydrogen or nitrogen; there is no pickup of carbon or nitrogen to cause inter-granular corrosion suscepti bility; there is no loss of hot-workabilitydue to oxidation of the metal; and since no slag is used, there is no problem due to entrapmentrof slag'during solidification -or-to pickup of delerequired to remove the surface defects.
terious impurities present in the slag-making materials.
In the drawing, the single figure is diagrammatic view illustrating the invention.
As shown in the drawing, a metal body Ill, such as billet is moved horizontally under a tungsten electrode [2 provided with a gas nozzle or cup 14. The body l and electrode l2 are connected by leads l6 and I8 to an electric power source 20 of sufficient current-supplying capacity to energize an electric metal meltingarc 22 between the surface of the body and the tip of the electrode during such movement of the work l0. Simultaneously therewith the arc and heated surface portions of the electrode andwork are shielded from the air by an annular stream 24 of inert monatomic-gas which is delivered to the nozzle H from a suitable source via an inlet 26.
As the work l0 moves under the inert monatomi'c-gas shielded arc welding torch 28, the are 22 melts the adjacent metal containing defects, forming a. molten puddle 30 which pro nickel rich iron-molybdenum, and related alloys can be satisfactorily surface-conditioned prior to rolling by remelting the surface of the ingot with a shielded arc, according to the invention,
"by using either argon or helium gas as the protective atmosphere. The surface can be premelted manually, but mechanized premelting is more satisfactory as it is subject to better control.
The amperage value of the current during remelting depends on the depth of penetration An arc current of 450 amperes using argon, and a 1 in. diameter tungsten electrode will remove defects about in. deep. Somewhat lower amperage may be used with helium for substantially the same depth of penetration.
The speed of melting depends on the surface condition of the ingot and the amperage of the arc current. A work-speed of in./minute at 450 amperes has been found satisfactory for small ingots though somewhat faster speed can be -ing inch. Surfaces of satisfactory quality were obtained, according to the invention, with a gas flow of cu. ft./hour with argon, and
' 40 cu. ft./hour with helium. No significant difference in the quality of the surface was noted between the ingots premelted in argon and in v helium.
Precautions should be taken to minimize arc interruptions as the craters form areas of shallow surface cracking in the rolled surface.
However, the starting craters are relatively shallow and can be removed by grinding without too much difliculty prior to rolling, and in most instances, the craters formed at the end of each pass can be confined to the piped section which is eventually discarded. Another scheme is to tack-weld suitable metal pieces on the ends of the ingot for starting and stopping purposes.
In cases where the defects are relatively deep cracks, an electrode composed of metal of the same composition as that of the base metal can be used, without departing from the invention, to supply the additional metal required to fill such deep cracks. However, the electrode preferably is compossed of tungsten containing significant amounts of oxidic materials, such as thoria', which improve arc stability and/or other additions which improve the operation of the electrode.
I claim:
Process of removing surface and subsurface defects including laps and scams due to metal splashing, from ingots composed of relatively high-alloy refractory metals prior to hot rolling in order to insure satisfactory surface quality of the resulting product without the loss of any of the refractory alloy metal thereof and without any change in the composition of the base metal, which comprises positioning the ingot so that the surface to be conditioned is uppermost and substantially level, striking a relatively heavy duty are between such surface of the ingot and a refractory metal electrode composed of tungsten; continuously shielding such are and the adjacent portions of the electrodeand ingot with an annular stream of monatomic gas of the class consisting of argon and helium and mixtures of argon and helium discharged from a nozzle surrounding such electrode in spaced concentric relation therewith at a gas flow rate of twenty-five to forty cubic feet 'per hour, positioning the end of such nozzle as closely as possible to the surface of said ingot at a distance of not more than three-eighths of an inch, continuously moving said gas shielded arc with respect to the ingot surface at a speed of the order of about ten inches per minute while maintaining such critical spacing between said nozzle and the ingot surface, continuously supplying such are with a current of the order of 400-450 amperes, deeply melting the ingot metal under such are to a depth of the order of about one References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,512,787 Morton Oct. 21, 1924 2,125,172 Kinzel July 26, 1938 2,185,496 Brown Jan. 2, 1940 2,405,542 Wassell Aug. 6, 1946 2,474,023 Wyer June 21, 1949 2,475,357 Miller July 5, 1949 2,515,559 Lancaster et al. July 18, 1950 2,532,410 Kennedy Dec. 5, 1950
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US208395A US2640792A (en) | 1951-01-29 | 1951-01-29 | Inert monatomic-gas shielded refractory metal remelting surface-defect removal process |
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Application Number | Priority Date | Filing Date | Title |
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US208395A US2640792A (en) | 1951-01-29 | 1951-01-29 | Inert monatomic-gas shielded refractory metal remelting surface-defect removal process |
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US2640792A true US2640792A (en) | 1953-06-02 |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2853408A (en) * | 1954-12-21 | 1958-09-23 | Westinghouse Electric Corp | Process and apparatus for treating ingots |
US2858586A (en) * | 1954-01-28 | 1958-11-04 | Joseph B Brennan | Smelting apparatus and method |
US2884510A (en) * | 1955-10-17 | 1959-04-28 | Union Carbide Corp | Constricted arc apparatus and process |
US2933594A (en) * | 1957-07-26 | 1960-04-19 | Westinghouse Electric Corp | Metals joining apparatus |
US3074602A (en) * | 1958-11-26 | 1963-01-22 | Shillady Marion Charlton | Pressure relief devices for pressure vessels and methods of making the same |
US4050958A (en) * | 1975-02-28 | 1977-09-27 | Mitsubishi Denki Kabushiki Kaisha | Method of removing surface defects of a steel product |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1512787A (en) * | 1924-02-05 | 1924-10-21 | Harry D Morton | Means and method for effecting continuous electric-arc welds |
US2125172A (en) * | 1932-07-29 | 1938-07-26 | Union Carbide & Carbon Corp | Process of treating the defective surface metal of billets or the like |
US2185496A (en) * | 1938-04-15 | 1940-01-02 | Int Nickel Co | Process of deseaming blooms, billets, sheet bars, and the like |
US2405542A (en) * | 1943-09-13 | 1946-08-06 | Gen Electric | Fusion welding |
US2474023A (en) * | 1944-02-17 | 1949-06-21 | British Thomson Houston Co Ltd | Method of gas-shielded alternating current arc welding |
US2475357A (en) * | 1944-12-23 | 1949-07-05 | Linde Air Prod Co | Argon-gas-blanketed alternating electric current arc welding aluminum and the alloysthereof with a tungsten electrode and superimposed high-frequency high-voltage electric current |
US2515559A (en) * | 1947-09-22 | 1950-07-18 | Apv Co Ltd | Arc welding in inert atmospheres |
US2532410A (en) * | 1949-10-29 | 1950-12-05 | Linde Air Prod Co | Inert monatomic gas shielded metalarc welding process |
-
1951
- 1951-01-29 US US208395A patent/US2640792A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1512787A (en) * | 1924-02-05 | 1924-10-21 | Harry D Morton | Means and method for effecting continuous electric-arc welds |
US2125172A (en) * | 1932-07-29 | 1938-07-26 | Union Carbide & Carbon Corp | Process of treating the defective surface metal of billets or the like |
US2185496A (en) * | 1938-04-15 | 1940-01-02 | Int Nickel Co | Process of deseaming blooms, billets, sheet bars, and the like |
US2405542A (en) * | 1943-09-13 | 1946-08-06 | Gen Electric | Fusion welding |
US2474023A (en) * | 1944-02-17 | 1949-06-21 | British Thomson Houston Co Ltd | Method of gas-shielded alternating current arc welding |
US2475357A (en) * | 1944-12-23 | 1949-07-05 | Linde Air Prod Co | Argon-gas-blanketed alternating electric current arc welding aluminum and the alloysthereof with a tungsten electrode and superimposed high-frequency high-voltage electric current |
US2515559A (en) * | 1947-09-22 | 1950-07-18 | Apv Co Ltd | Arc welding in inert atmospheres |
US2532410A (en) * | 1949-10-29 | 1950-12-05 | Linde Air Prod Co | Inert monatomic gas shielded metalarc welding process |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2858586A (en) * | 1954-01-28 | 1958-11-04 | Joseph B Brennan | Smelting apparatus and method |
US2853408A (en) * | 1954-12-21 | 1958-09-23 | Westinghouse Electric Corp | Process and apparatus for treating ingots |
US2884510A (en) * | 1955-10-17 | 1959-04-28 | Union Carbide Corp | Constricted arc apparatus and process |
US2933594A (en) * | 1957-07-26 | 1960-04-19 | Westinghouse Electric Corp | Metals joining apparatus |
US3074602A (en) * | 1958-11-26 | 1963-01-22 | Shillady Marion Charlton | Pressure relief devices for pressure vessels and methods of making the same |
US4050958A (en) * | 1975-02-28 | 1977-09-27 | Mitsubishi Denki Kabushiki Kaisha | Method of removing surface defects of a steel product |
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