Turbine blade superalloy iii

Details Turbine blade superalloy iii Turbine blade superalloy iii

C - Chemistry, Metallurgy

22

C

75/16

C22C 32/00 (2006.01) C22C 1/10 (2006.01)

Patent

CA 1254402

ABSTRACT An alloy body specifically adapted to be used as an industrial gas turbine structure having an elongated grain structure, gamma prime hardening precipitate and an oxidic yttrium dispersed phase. The alloy contains, in addition to nickel, 19 to 24% chromium, 1 to 3.4% aluminum, 1.75 to 5% titanium, and balanced amounts of cobalt, tungsten, tantalum, boron and zirconium.

503721

Affiliated with

Also associated with

Rating

Turbine blade superalloy iii does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine blade superalloy iii, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine blade superalloy iii will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1177521