Patent · US5554837A · A · US
Interactive laser welding at elevated temperatures of superalloy articles
- (11) Publication number
- US5554837A
- (21) Application number
- US-11667093-A
- (22) Filing date
- 1993-09-03
- (30) Priority date
- 1993-09-03
- (43) Publication date
- 1996-09-10
- (45) Date of grant
- 1996-09-10
- (52) CPC
- 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: 26/034, 2101/001, 2103/26, 26/123, 26/32, 26/60
- F01D Non-positive displacement machines or engines, e.g. steam turbines: 5/005
- F05B Indexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses F03B, F03D and F03G: 2220/302
- (73) Assignee
- CHROMALLOY GAS TURBINE CORP
- (54) Title
- Interactive laser welding at elevated temperatures of superalloy articles
- (57) Abstract
A process and apparatus is provided for laser welding a nickel and/or cobalt based superalloy article comprising: preheating the entire weld area and adjacent region to a ductile temperature with an induction heat coil and maintaining such temperature during welding and solidification of the weld; and welding the preheated article utilizing a laser with a powder alloy feed with a control means controlling the laser, power feed and motion system on which the article is fixtured, wherein the control means includes a vision system which digitizes the weld area providing a path for the laser welding to follow.
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Claims (25)
- A process for laser welding a nickel and/or cobalt based superalloy article chosen from the group consisting of a gama-prime precipitation strengthened superalloy containing titanium and aluminum in a combined amount of at least 5% and an MCrAlY alloy wherein M is nickel and/or cobalt comprising: preheating an entire weld area and region adjacent to the weld area of the article to a ductile temperature which is above an aging temperature and below an incipient melting temperature for said superalloy and within the range of 1400° F. to 2100° F. with an induction heat coil and maintaining such temperature during welding and solidification of a weld; and welding the preheated article utilizing a laser with a powder alloy feed, with a control means preprogrammed with values for control of the laser, the powder feed and a general path for a motion system on which the article is fixtured, said values based on the configuration and composition of the article wherein the control means further includes a vision system which digitizes the weld area of the article providing a precise path for the laser welding to follow individualized for the weld area of the specific article being welded.
- Process of claim 1 wherein the control means includes a computer numerical control.
- Process of claim 2 wherein the motion system has at least 3-axis of motion.
- Process of claim 3 further comprising providing an optical pyrometer to measure and control the temperature of the weld area of the article.
- Process of claim 4 further comprising controlling temperature heat-up and cool down rates of the article to reduce strain and cracking.
- Process of claim 5 further comprising providing an inert gas shroud during welding to shield the weld area of the article.
- Process of claim 6 wherein the powder alloy is a gamma-prime precipitation-strengthened nickel base superalloy containing titanium and aluminum in a combined amount of at least 5% or an MCrAlY alloy wherein M is Ni and/or Co.
- Process of claim 7 wherein the superalloy article and the powder alloy comprise substantially the same alloy.
- Process of claim 8 wherein the article is a turbine blade, turbine vane or turbine rotor.
- Process of claim 9 wherein the article is maintained in the same fixture for laser welding and machining and wherein the machining is controlled utilizing the same digitized information as provided by the vision system for laser welding.
- Process of claim 7 wherein the superalloy article is a component for a gas turbine engine.
- Process of claim 7 wherein the ductile temperature is in the range of 1725° F. to 1975° F.
- Process of claim 7 wherein the superalloy article is directionally solidified.
- Process of claim 2 wherein the motion system has 4-axis of motion.
- Process of claim 2 wherein the motion system has 5-axis of motion.
- Process of claim 2 further comprising machining the welded article.
- Process of claim 1 wherein the vision system digitizes the precise path for the laser welding to follow for the specific article prior to preheating the article.
- A laser welding apparatus for welding superalloy articles comprising: an induction heating coil for heating a weld area and adjacent region of the article to 1400° F. to 2100° F. and maintaining such temperature during welding and solidification of a weld; a laser with a powder feed system for welding the article; a motion system having at least 3-axis of motion on which the article is fixtured; and a control means preprogrammed with values for control the laser, the powder feed and a general path for a motion system, said values based on the configuration and composition of the article to provide a weld on a predetermined surface area of the article, wherein the control means further includes a vision system which digitizes the weld area of the article providing a precise path for the laser welding to follow individualized for the weld area of the specific article being welded.
- Apparatus of claim 18 wherein the control means includes a computer numerical control.
- Apparatus of claim 19 further comprising a means to control temperature and heat-up and cool down rates of the weld area of the article.
- Apparatus of claim 20 wherein the motion system has 4-axis of motion.
- Apparatus of claim 20 wherein the motion system has 5-axis of motion.
- Apparatus of claim 18 further comprising an optical pyrometer to measure the temperature of the article.
- Apparatus of claim 23 further comprising a gas shroud to shield the weld area of the article with inert gas during welding.
- Apparatus of claim 18 wherein the vision system digitizes the precise path for the laser welding to follow for the specific article prior to heating the article.
Citations (23)
- US3246392A
- US3535768A
- US3619547A
- US3660882A
- US4402447A
- US4498617A
- US4576874A
- US4611744A
- US4613744A
- US4675204A
- US4675502A
- US4733049A
- US4737613A
- US4804815A
- US4918805A
- US4998005A
- US5106010A
- US5160822A
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- US5208431A
- US5224997A
- US5225247A
- US5229571A
Record as JSON
{
"publication_number": "US5554837A",
"country": "US",
"kind": "A",
"title": "Interactive laser welding at elevated temperatures of superalloy articles",
"abstract": "A process and apparatus is provided for laser welding a nickel and/or cobalt based superalloy article comprising: preheating the entire weld area and adjacent region to a ductile temperature with an induction heat coil and maintaining such temperature during welding and solidification of the weld; and welding the preheated article utilizing a laser with a powder alloy feed with a control means controlling the laser, power feed and motion system on which the article is fixtured, wherein the control means includes a vision system which digitizes the weld area providing a path for the laser welding to follow.",
"claims": [
"1. A process for laser welding a nickel and/or cobalt based superalloy article chosen from the group consisting of a gama-prime precipitation strengthened superalloy containing titanium and aluminum in a combined amount of at least 5% and an MCrAlY alloy wherein M is nickel and/or cobalt comprising: preheating an entire weld area and region adjacent to the weld area of the article to a ductile temperature which is above an aging temperature and below an incipient melting temperature for said superalloy and within the range of 1400° F. to 2100° F. with an induction heat coil and maintaining such temperature during welding and solidification of a weld; and welding the preheated article utilizing a laser with a powder alloy feed, with a control means preprogrammed with values for control of the laser, the powder feed and a general path for a motion system on which the article is fixtured, said values based on the configuration and composition of the article wherein the control means further includes a vision system which digitizes the weld area of the article providing a precise path for the laser welding to follow individualized for the weld area of the specific article being welded.",
"2. Process of claim 1 wherein the control means includes a computer numerical control.",
"3. Process of claim 2 wherein the motion system has at least 3-axis of motion.",
"4. Process of claim 3 further comprising providing an optical pyrometer to measure and control the temperature of the weld area of the article.",
"5. Process of claim 4 further comprising controlling temperature heat-up and cool down rates of the article to reduce strain and cracking.",
"6. Process of claim 5 further comprising providing an inert gas shroud during welding to shield the weld area of the article.",
"7. Process of claim 6 wherein the powder alloy is a gamma-prime precipitation-strengthened nickel base superalloy containing titanium and aluminum in a combined amount of at least 5% or an MCrAlY alloy wherein M is Ni and/or Co.",
"8. Process of claim 7 wherein the superalloy article and the powder alloy comprise substantially the same alloy.",
"9. Process of claim 8 wherein the article is a turbine blade, turbine vane or turbine rotor.",
"10. Process of claim 9 wherein the article is maintained in the same fixture for laser welding and machining and wherein the machining is controlled utilizing the same digitized information as provided by the vision system for laser welding.",
"11. Process of claim 7 wherein the superalloy article is a component for a gas turbine engine.",
"12. Process of claim 7 wherein the ductile temperature is in the range of 1725° F. to 1975° F.",
"13. Process of claim 7 wherein the superalloy article is directionally solidified.",
"14. Process of claim 2 wherein the motion system has 4-axis of motion.",
"15. Process of claim 2 wherein the motion system has 5-axis of motion.",
"16. Process of claim 2 further comprising machining the welded article.",
"17. Process of claim 1 wherein the vision system digitizes the precise path for the laser welding to follow for the specific article prior to preheating the article.",
"18. A laser welding apparatus for welding superalloy articles comprising: an induction heating coil for heating a weld area and adjacent region of the article to 1400° F. to 2100° F. and maintaining such temperature during welding and solidification of a weld; a laser with a powder feed system for welding the article; a motion system having at least 3-axis of motion on which the article is fixtured; and a control means preprogrammed with values for control the laser, the powder feed and a general path for a motion system, said values based on the configuration and composition of the article to provide a weld on a predetermined surface area of the article, wherein the control means further includes a vision system which digitizes the weld area of the article providing a precise path for the laser welding to follow individualized for the weld area of the specific article being welded.",
"19. Apparatus of claim 18 wherein the control means includes a computer numerical control.",
"20. Apparatus of claim 19 further comprising a means to control temperature and heat-up and cool down rates of the weld area of the article.",
"21. Apparatus of claim 20 wherein the motion system has 4-axis of motion.",
"22. Apparatus of claim 20 wherein the motion system has 5-axis of motion.",
"23. Apparatus of claim 18 further comprising an optical pyrometer to measure the temperature of the article.",
"24. Apparatus of claim 23 further comprising a gas shroud to shield the weld area of the article with inert gas during welding.",
"25. Apparatus of claim 18 wherein the vision system digitizes the precise path for the laser welding to follow for the specific article prior to heating the article."
],
"cpc": [
"B23K 26/034",
"B23K 2101/001",
"B23K 2103/26",
"B23K 26/123",
"B23K 26/32",
"B23K 26/60",
"F01D 5/005",
"F05B 2220/302"
],
"assignees": [
"CHROMALLOY GAS TURBINE CORP"
],
"filing_date": "1993-09-03",
"publication_date": "1996-09-10",
"grant_date": "1996-09-10",
"priority_date": "1993-09-03",
"application_number": "US-11667093-A",
"family_id": "22368541",
"citations": [
"US3246392A",
"US3535768A",
"US3619547A",
"US3660882A",
"US4402447A",
"US4498617A",
"US4576874A",
"US4611744A",
"US4613744A",
"US4675204A",
"US4675502A",
"US4733049A",
"US4737613A",
"US4804815A",
"US4918805A",
"US4998005A",
"US5106010A",
"US5160822A",
"US5168141A",
"US5208431A",
"US5224997A",
"US5225247A",
"US5229571A"
]
}
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