DK1127948T3 - High-temperature corrosion-resistant monocrystalline nickel-based superalloys - Google Patents

High-temperature corrosion-resistant monocrystalline nickel-based superalloys

Info

Publication number
DK1127948T3
DK1127948T3 DK95116194T DK95116194T DK1127948T3 DK 1127948 T3 DK1127948 T3 DK 1127948T3 DK 95116194 T DK95116194 T DK 95116194T DK 95116194 T DK95116194 T DK 95116194T DK 1127948 T3 DK1127948 T3 DK 1127948T3
Authority
DK
Denmark
Prior art keywords
percent
gas turbine
superalloy
component
temperature corrosion
Prior art date
Application number
DK95116194T
Other languages
Danish (da)
Inventor
Gary L Erickson
Original Assignee
Cannon Muskegon Corp
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 Cannon Muskegon Corp filed Critical Cannon Muskegon Corp
Application granted granted Critical
Publication of DK1127948T3 publication Critical patent/DK1127948T3/en

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
    • 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)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Powder Metallurgy (AREA)
  • Laminated Bodies (AREA)

Abstract

This invention relates to a hot corrosion resistant nickel-based superalloy comprising the following elements in percent by weight: from about 14.2 to about 15.5 percent chromium, from about 2.0 to about 4.0 percent cobalt, from about 0.30 to about 0.45 percent molybdenum, from about 4.0 to about 5.0 percent tungsten, from about 4.5 to about 5.8 percent tantalum, from about 0.05 to about 0.25 percent columbium, from about 3.2 to about 3.6 percent aluminum, from about 4.0 to about 4.4 percent titanium, from about 0.01 to about 0.06 percent hafnium, ard the balance nickel plus incidental impurities, the superalloy having a phasial stability number NV3B less than about 2.45. Single crystal articles can be suitably made from the superalloy of this invention. The article can be a component for a gas turbine engine and, more particularly, the component can be a gas turbine blade or gas turbine vane. <IMAGE>
DK95116194T 1995-10-13 1995-10-13 High-temperature corrosion-resistant monocrystalline nickel-based superalloys DK1127948T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP95116194A EP1127948B1 (en) 1995-10-13 1995-10-13 Hot corrosion resistant single crystal nickel-based superalloys

Publications (1)

Publication Number Publication Date
DK1127948T3 true DK1127948T3 (en) 2002-11-11

Family

ID=8219715

Family Applications (1)

Application Number Title Priority Date Filing Date
DK95116194T DK1127948T3 (en) 1995-10-13 1995-10-13 High-temperature corrosion-resistant monocrystalline nickel-based superalloys

Country Status (5)

Country Link
EP (1) EP1127948B1 (en)
AT (1) ATE221138T1 (en)
DE (1) DE69527557T2 (en)
DK (1) DK1127948T3 (en)
ES (1) ES2184779T3 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115044805B (en) * 2022-05-30 2023-04-11 北京科技大学 Nickel-based single crystal superalloy with balanced multiple properties and preparation method thereof

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2153848B (en) * 1984-02-10 1987-09-16 United Technologies Corp High strength hot corrosion resistant single crystals
US4677035A (en) * 1984-12-06 1987-06-30 Avco Corp. High strength nickel base single crystal alloys
EP0207874B1 (en) * 1985-05-09 1991-12-27 United Technologies Corporation Substrate tailored coatings for superalloys
CA1291350C (en) * 1986-04-03 1991-10-29 United Technologies Corporation Single crystal articles having reduced anisotropy
US5366695A (en) * 1992-06-29 1994-11-22 Cannon-Muskegon Corporation Single crystal nickel-based superalloy

Also Published As

Publication number Publication date
DE69527557D1 (en) 2002-08-29
EP1127948B1 (en) 2002-07-24
EP1127948A2 (en) 2001-08-29
ES2184779T3 (en) 2003-04-16
EP1127948A3 (en) 2001-09-05
ATE221138T1 (en) 2002-08-15
DE69527557T2 (en) 2002-11-07

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