Gas turbine

Details Gas turbine Gas turbine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/00 (2006.01) F01D 5/14 (2006.01) F01D 5/16 (2006.01) F01D 25/30 (2006.01)

Patent

CA 2365090

The pressure ratio .DELTA.P4S of a final stage moving blade is reduced. As a result, the Mach number in the final stage moving blade can be suppressed, and in the gas turbine operating at a pressure ratio of 20 or more, therefore, decline of turbine efficiency due to shock wave loss can be prevented securely.

Affiliated with

Also associated with

Rating

Gas turbine does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2045312