Turbine blade impingement baffle

Details Turbine blade impingement baffle Turbine blade impingement baffle

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F01D 5/14 (2006.01)

Patent

CA 2072386

13DV-101370 ABSTRACT An impingement-cooled gas turbine blade includes an impingement baffle which, during engine operation, is subject only to shear loading. A tubular baffle body is provided with a pair of mounting flanges which are bonded between a forward portion of the turbine blade and an aft portion of the turbine blade. The bond extends from the blade dovetail to the blade tip.

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