System and method for cooling in a gas turbine

Details System and method for cooling in a gas turbine System and method for cooling in a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

170/67

F01D 5/08 (2006.01) F01K 23/10 (2006.01) F02C 7/14 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2008743

ABSTRACT A gas turbine is provided in which the quantity of cooling air required to cool the turbine is reduced by the evaporative cooling of air bled from the compressor discharge for cooling purposes. The evaporative cooling is accomplished by spraying pressurized water into a bleed pipe which diverts the cooling air from the compressor discharge to the turbine.

Affiliated with

Also associated with

Rating

System and method for cooling in a 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 System and method for cooling in a gas turbine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and System and method for cooling in a gas turbine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1876773