Skirted turbine blade

Details Skirted turbine blade Skirted turbine blade

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01)

Patent

CA 2511155

A turbine blade (16) includes an airfoil (18), platform (20), shank (22), and dovetail (24). The shank (22) includes opposite forward and aft faces (46,48) corresponding with leading and trailing edges (36,38) of the airfoil, and opposite first and second sides (50,52) corresponding with pressure and suction sides (32,34) of the airfoil. The shank (22) further includes lugs (56) extending outwardly from the two sides, with a first lug having an inverted skirt (66) extending outwardly toward the platform (20) to join the shank aft face (48). The skirt (66) cooperates with a seal body (58) when mounted in the engine for reducing inter-blade leakage.

Affiliated with

Also associated with

Rating

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1771742