Methods and apparatus for gas turbine engines

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

2005-12-20

2008-09-30

Nguyen, Ninh H (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Laminated, embedded member or encased material

C416S22900R, C416S095000, C415S191000, C415S211200

Reexamination Certificate

active

07429166

ABSTRACT:
A method for manufacturing a turbine engine component includes forming a component to include a first side and an opposite second side, positioning at least one capillary adjacent to an external surface of at least one of the first and second sides, and securing the at least one capillary to the component with at least one composite layer.

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