Tip structure for cooled turbine rotor blade

Details Tip structure for cooled turbine rotor blade Tip structure for cooled turbine rotor blade

F - Mech Eng,Light,Heat,Weapons

01

D

170/71

F01D 5/18 (2006.01) F01D 5/20 (2006.01)

Patent

CA 1187811

ABSTRACT OF THE DISCLOSURE The invention comprises a cooled turbine rotor blade having an improved blade tip structure. A recessed tip is provided at the leading edge end of the blade tip on downstream turbine blades which are too narrow to support a blade tip cavity over the entire exterior sur- face of the blade tip without interfering with cooling airflow from apertures in the exterior surface. The recessed tip structure protects apertures therein from blockage by a blade tip smear and does not substantially reduce the performance efficiency of the blade.

415133

Affiliated with

Also associated with

Rating

Tip structure for cooled turbine rotor blade does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1238136