MXPA05009401A - Ni-cr-co alloy for advanced gas turbine engines. - Google Patents
Ni-cr-co alloy for advanced gas turbine engines.Info
- Publication number
- MXPA05009401A MXPA05009401A MXPA05009401A MXPA05009401A MXPA05009401A MX PA05009401 A MXPA05009401 A MX PA05009401A MX PA05009401 A MXPA05009401 A MX PA05009401A MX PA05009401 A MXPA05009401 A MX PA05009401A MX PA05009401 A MXPA05009401 A MX PA05009401A
- Authority
- MX
- Mexico
- Prior art keywords
- gas turbine
- chromium
- alloy
- nickel
- turbine engines
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Abstract
A wrought age-hardenable nickel-chromium-cobalt based alloy suitable for use in high temperature gas turbine transition ducts possessing a combination of three specific key properties, namely resistance to strain age cracking, good thermal stability, and good creep-rupture strength contains in weight percent 17 to 22 chromium, 8 to 15 cobalt, 4.0 to 9.5 molybdenum, up to 7 tungsten, 1.28 to 1.65 aluminum, 1.50 to 2.30 titanium, up to 0.80 niobium, 0.01 to 0.2 carbon, up to 0.01 boron, and up to 3 iron, with a balance of nickel and impurities. Certain alloying elements must be present in amounts according to two equations here disclosed.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/934,920 US20060051234A1 (en) | 2004-09-03 | 2004-09-03 | Ni-Cr-Co alloy for advanced gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
MXPA05009401A true MXPA05009401A (en) | 2006-03-07 |
Family
ID=35198601
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MXPA05009401A MXPA05009401A (en) | 2004-09-03 | 2005-09-02 | Ni-cr-co alloy for advanced gas turbine engines. |
Country Status (16)
Country | Link |
---|---|
US (1) | US20060051234A1 (en) |
EP (1) | EP1640465B1 (en) |
JP (1) | JP4861651B2 (en) |
KR (1) | KR100788527B1 (en) |
CN (2) | CN102586652B (en) |
AT (1) | ATE447048T1 (en) |
AU (1) | AU2005205736B2 (en) |
CA (1) | CA2517056A1 (en) |
DE (1) | DE602005017338D1 (en) |
DK (1) | DK1640465T3 (en) |
ES (1) | ES2335503T3 (en) |
GB (1) | GB2417729B (en) |
MX (1) | MXPA05009401A (en) |
PL (1) | PL1640465T3 (en) |
RU (1) | RU2377336C2 (en) |
TW (1) | TWI359870B (en) |
Families Citing this family (63)
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EP1835040A1 (en) * | 2006-03-17 | 2007-09-19 | Siemens Aktiengesellschaft | Welding material, use of the welding material and method of welding a structural component |
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US8506883B2 (en) * | 2007-12-12 | 2013-08-13 | Haynes International, Inc. | Weldable oxidation resistant nickel-iron-chromium-aluminum alloy |
JP5232492B2 (en) * | 2008-02-13 | 2013-07-10 | 株式会社日本製鋼所 | Ni-base superalloy with excellent segregation |
EP2103700A1 (en) * | 2008-03-14 | 2009-09-23 | Siemens Aktiengesellschaft | Nickel base alloy and use of it, turbine blade or vane and gas turbine |
JP5254693B2 (en) * | 2008-07-30 | 2013-08-07 | 三菱重工業株式会社 | Welding material for Ni-base alloy |
EP2330225B1 (en) * | 2008-10-02 | 2015-03-25 | Nippon Steel & Sumitomo Metal Corporation | Nickel based heat-resistant alloy |
JP2010150585A (en) * | 2008-12-24 | 2010-07-08 | Toshiba Corp | Ni-based alloy for casting part of steam turbine excellent in high-temperature strength, castability and weldability, turbine casing of steam turbine, valve casing of steam turbine, nozzle box of steam turbine, and pipe of steam turbine |
JP5127749B2 (en) * | 2009-03-18 | 2013-01-23 | 株式会社東芝 | Ni-base alloy for turbine rotor of steam turbine and turbine rotor of steam turbine using the same |
JP2010249050A (en) * | 2009-04-16 | 2010-11-04 | Toshiba Corp | Steam turbine and steam turbine installation |
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ITMI20110830A1 (en) * | 2011-05-12 | 2012-11-13 | Alstom Technology Ltd | VALVE FOR ONE STEAM TURBINE 700 C |
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US2712498A (en) * | 1948-06-01 | 1955-07-05 | Rolls Royce | Nickel chromium alloys having high creep strength at high temperatures |
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JP2000502405A (en) * | 1995-12-21 | 2000-02-29 | テレダイン インダストリーズ インコーポレイテッド | Stress fracture characteristics of nickel-chromium-cobalt alloys by adjusting the levels of phosphorus and boron |
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CN1101479C (en) * | 1999-01-28 | 2003-02-12 | 住友电气工业株式会社 | Heat-resistant alloy wire |
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-
2004
- 2004-09-03 US US10/934,920 patent/US20060051234A1/en not_active Abandoned
-
2005
- 2005-05-26 TW TW094117291A patent/TWI359870B/en active
- 2005-06-08 RU RU2005117714/02A patent/RU2377336C2/en active
- 2005-06-17 CN CN201210057737.8A patent/CN102586652B/en active Active
- 2005-06-17 CN CNA2005100781613A patent/CN1743483A/en active Pending
- 2005-07-15 JP JP2005206381A patent/JP4861651B2/en active Active
- 2005-08-24 CA CA002517056A patent/CA2517056A1/en not_active Abandoned
- 2005-08-30 AT AT05018830T patent/ATE447048T1/en active
- 2005-08-30 EP EP05018830A patent/EP1640465B1/en active Active
- 2005-08-30 DE DE602005017338T patent/DE602005017338D1/en active Active
- 2005-08-30 PL PL05018830T patent/PL1640465T3/en unknown
- 2005-08-30 ES ES05018830T patent/ES2335503T3/en active Active
- 2005-08-30 DK DK05018830.9T patent/DK1640465T3/en active
- 2005-08-31 AU AU2005205736A patent/AU2005205736B2/en active Active
- 2005-08-31 GB GB0517657A patent/GB2417729B/en active Active
- 2005-09-02 MX MXPA05009401A patent/MXPA05009401A/en active IP Right Grant
- 2005-09-02 KR KR1020050081625A patent/KR100788527B1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
DK1640465T3 (en) | 2010-03-01 |
AU2005205736A1 (en) | 2006-03-23 |
JP2006070360A (en) | 2006-03-16 |
CN1743483A (en) | 2006-03-08 |
TWI359870B (en) | 2012-03-11 |
RU2005117714A (en) | 2006-12-20 |
CA2517056A1 (en) | 2006-03-03 |
ES2335503T3 (en) | 2010-03-29 |
CN102586652B (en) | 2016-05-11 |
ATE447048T1 (en) | 2009-11-15 |
KR20060050963A (en) | 2006-05-19 |
GB0517657D0 (en) | 2005-10-05 |
EP1640465A2 (en) | 2006-03-29 |
KR100788527B1 (en) | 2007-12-24 |
RU2377336C2 (en) | 2009-12-27 |
EP1640465B1 (en) | 2009-10-28 |
GB2417729A (en) | 2006-03-08 |
JP4861651B2 (en) | 2012-01-25 |
CN102586652A (en) | 2012-07-18 |
DE602005017338D1 (en) | 2009-12-10 |
US20060051234A1 (en) | 2006-03-09 |
TW200609359A (en) | 2006-03-16 |
AU2005205736B2 (en) | 2012-02-23 |
EP1640465A3 (en) | 2006-04-05 |
PL1640465T3 (en) | 2010-06-30 |
GB2417729B (en) | 2008-01-16 |
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