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
Application number
MXPA05009401A
Other languages
Spanish (es)
Inventor
Lee M Pike Jr
Original Assignee
Haynes Int Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Haynes Int Inc filed Critical Haynes Int Inc
Publication of MXPA05009401A publication Critical patent/MXPA05009401A/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys 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%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys 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.
MXPA05009401A 2004-09-03 2005-09-02 Ni-cr-co alloy for advanced gas turbine engines. MXPA05009401A (en)

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)

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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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