GB0517657D0 - Ni-cr-co alloy for advanced gas turbine engines - Google Patents

Ni-cr-co alloy for advanced gas turbine engines

Info

Publication number
GB0517657D0
GB0517657D0 GBGB0517657.3A GB0517657A GB0517657D0 GB 0517657 D0 GB0517657 D0 GB 0517657D0 GB 0517657 A GB0517657 A GB 0517657A GB 0517657 D0 GB0517657 D0 GB 0517657D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
alloy
turbine engines
advanced gas
age
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
GBGB0517657.3A
Other versions
GB2417729A (en
GB2417729B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Haynes International Inc
Original Assignee
Haynes International 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 International Inc filed Critical Haynes International Inc
Publication of GB0517657D0 publication Critical patent/GB0517657D0/en
Publication of GB2417729A publication Critical patent/GB2417729A/en
Application granted granted Critical
Publication of GB2417729B publication Critical patent/GB2417729B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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%

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Hydrogen, Water And Hydrids (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Catalysts (AREA)

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
GB0517657A 2004-09-03 2005-08-31 Ni-Cr-Co alloy for advanced gas turbine engines Active GB2417729B (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 (3)

Publication Number Publication Date
GB0517657D0 true GB0517657D0 (en) 2005-10-05
GB2417729A GB2417729A (en) 2006-03-08
GB2417729B GB2417729B (en) 2008-01-16

Family

ID=35198601

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0517657A Active GB2417729B (en) 2004-09-03 2005-08-31 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) CN1743483A (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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JP5919980B2 (en) * 2012-04-06 2016-05-18 新日鐵住金株式会社 Ni-base heat-resistant alloy
JP2014005528A (en) * 2012-05-29 2014-01-16 Toshiba Corp Ni-BASED HEAT-RESISTANT ALLOY AND TURBINE COMPONENT
JP5981251B2 (en) * 2012-07-20 2016-08-31 株式会社東芝 Ni-based alloy and forged parts for forging
JP5743161B2 (en) * 2012-09-24 2015-07-01 株式会社日本製鋼所 Covering structure material with excellent Mg corrosion resistance
KR101476145B1 (en) * 2012-12-21 2014-12-24 한국기계연구원 Ni-Cr-Co base alloys showing an excellent combination of bonding to porcelain and mechanical properties used as a porcelain-fused-to-metal
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DE102014200121A1 (en) 2014-01-08 2015-07-09 Siemens Aktiengesellschaft Manganese-containing high-temperature soldering alloy based on cobalt, powder, component and soldering process
RU2542195C1 (en) * 2014-02-19 2015-02-20 Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" Refractory alloy on nickel base for casting of nozzle vanes with equiaxial structure of gas turbine plants
RU2542194C1 (en) * 2014-02-19 2015-02-20 Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" Refractory nickel-based alloy for casting gas turbine working blades
RU2538054C1 (en) * 2014-02-19 2015-01-10 Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" Heat-resistant alloy based on nickel for manufacture of blades of gas-turbine units
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Also Published As

Publication number Publication date
TWI359870B (en) 2012-03-11
PL1640465T3 (en) 2010-06-30
AU2005205736A1 (en) 2006-03-23
CN102586652A (en) 2012-07-18
GB2417729A (en) 2006-03-08
MXPA05009401A (en) 2006-03-07
TW200609359A (en) 2006-03-16
GB2417729B (en) 2008-01-16
CN1743483A (en) 2006-03-08
EP1640465B1 (en) 2009-10-28
US20060051234A1 (en) 2006-03-09
RU2005117714A (en) 2006-12-20
KR100788527B1 (en) 2007-12-24
CN102586652B (en) 2016-05-11
CA2517056A1 (en) 2006-03-03
AU2005205736B2 (en) 2012-02-23
JP4861651B2 (en) 2012-01-25
DE602005017338D1 (en) 2009-12-10
RU2377336C2 (en) 2009-12-27
DK1640465T3 (en) 2010-03-01
EP1640465A3 (en) 2006-04-05
KR20060050963A (en) 2006-05-19
EP1640465A2 (en) 2006-03-29
ES2335503T3 (en) 2010-03-29
JP2006070360A (en) 2006-03-16
ATE447048T1 (en) 2009-11-15

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