Apparatus for film cooling of turbine vane shrouds

Details Apparatus for film cooling of turbine vane shrouds Apparatus for film cooling of turbine vane shrouds

F - Mech Eng,Light,Heat,Weapons

01

D

60/185, 170/70

F01D 11/00 (2006.01) F01D 9/04 (2006.01) F02C 7/28 (2006.01)

Patent

CA 1309597

ABSTRACT OF THE INVENTION A gas turbine of the type having high pressure air supplied to the cavity formed by the inner shrouds of the turbine vanes is provided with film cooling of the shrouds. A manifold supplies high pressure cooling air to portions of the gaps between inner shrouds not otherwise supplied and intermittent reliefs in the strip seal between shrouds regulates the leakage of this air, over the outer surfaces of the shrouds.

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