Patent · US Expired

Stress rupture properties of nickel-chromium-cobalt alloys by adjustment of the levels of phosphorus and boron

US6106767A · kind A · utility

16Cited by
6References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 18, 1998
Grant dateAug 22, 2000
Priority date
Expiry dateJun 18, 2018

Classification

  • Technology area (CPC C)Chemistry; Metallurgy
  • CPC primaryC22C19/055
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

Nickel-base alloys with improved elevated temperature creep and stress rupture lives are disclosed which are particularly useful for components in gas turbine engines exposed to high temperatures and stresses for long periods of time. The alloys are nickel-based consisting essentially of 0.005 to 0.15% C, 0.10 to 11% Mo, 0.10 to 4.25% W, from 12 to 31% Cr, 0.25 to 21% Co, up to 5% Fe, 0.10 to 3.75% Nb, 0.10 to 1.25% Ta, 0.01 to 0.10% Zr, 0.10 to 0.50% Mn, 0.10 to 1% V, l.8-4.75% Ti, 0.5 to 5.25% Al, less than 0.003% P, and 0.004 to 0.025% B. Key to the improvement of creep and stress rupture lives is the extremely low P content in conjunction with high B contents.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.