Methods and apparatus for gas turbine engines

Details Methods and apparatus for gas turbine engines Methods and apparatus for gas turbine engines

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/02 (2006.01) F01D 5/18 (2006.01) F02C 7/047 (2006.01)

Patent

CA 2571652

A gas turbine engine component 50 that includes a first side (64), an opposite second side (66), at least one capillary (84) positioned adjacent to an external surface (88) of at least one of said first and second sides, and a composite layer (90) securing the at least one said capillary to said component.

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