Vane platform tangential injection

Details Vane platform tangential injection Vane platform tangential injection

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2568692

An improved vane platform flow arrangement comprising a plurality of holes defined in at least one vane platform downstream edge at an angle substantially parallel to the airfoil trailing edge angle, the holes adapted to eject a cooling flow into the annular gas path generally in the direction of the gas path flow.

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