U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Single crystal nickel-based superalloy

Patent 5366695 Issued on November 22, 1994. Estimated Expiration Date: Icon_subject June 29, 2012. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Re29920

3765879

Directionally solidified eutectic γ+ଲ nickel-base superalloys
Patent #: 4045255
Issued on: 08/30/1977
Inventor: Jackson

Directionally solidified eutectic γ-γ' nickel-base superalloys
Patent #: 4055447
Issued on: 10/25/1977
Inventor: Jackson

Heat treated superalloy single crystal article and process
Patent #: 4116723
Issued on: 09/26/1978
Inventor: Gell ,   et al.

Cast nickel-base alloy article
Patent #: 4169742
Issued on: 10/02/1979
Inventor: Wukusick ,   et al.

Heat treated superalloy single crystal article and process
Patent #: 4209348
Issued on: 06/24/1980
Inventor: Duhl ,   et al.

Single crystal nickel superalloy
Patent #: 4222794
Issued on: 09/16/1980
Inventor: Schweizer ,   et al.

Transverse ductile fiber reinforced eutectic nickel-base superalloys
Patent #: 4292076
Issued on: 09/29/1981
Inventor: Gigliotti ,   et al.

Single crystal nickel superalloy
Patent #: 4371404
Issued on: 02/01/1983
Inventor: Duhl ,   et al.

More ...

Inventor

Application

No. 905462 filed on 06/29/1992

US Classes:

420/448, Molybdenum or tungsten containing148/404, Directionally solidified148/410, Chromium containing415/200, Specific casing or vane material416/241R, Coating, specific composition or characteristic420/443Rare earth, magnesium or alkaline earth metal containing

Examiners

Primary: Andrews, Melvyn
Assistant: Phipps, Margery S.

Attorney, Agent or Firm

Foreign Patent References

  • 2029539 CA. 11/10/1990
  • 240451 EP 10/10/1987
  • 2234521 GB. 02/10/1991
  • 2235697 GB. 03/10/1991

International Class

C22C 019/05

Abstract

This invention relates to a nickel-based superalloy comprising the following elements in percent by weight: from about 5.0 to about 7.0 percent rhenium, from about 1.8 to about 4.0 percent chromium, from about 1.5 to about 9.0 percent cobalt, from about 7.0 to about 10.0 percent tantalum, from about 3.5 to about 7.5 percent tungsten, from about 5.0 to about 7.0 percent aluminum, from about 0.1 to about 1.2 percent titanium, from about 0 to about 0.5 percent columbium, from about 0.25 to about 2.0 percent molybdenum, from about 0 to about 0.15 percent hafnium, and the balance nickel+incidental impurities, the superalloy having a phasial stability number Nv3B less than about 2.10.

Other References

  • H. J. Murphy; C. T. Sims and A. M. Beltran, "Phacomp Revisited" International Symposium on Structural Stability in Superalloys Sep. 196
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