Dual cut-back trailing edge for airfoils

Details Dual cut-back trailing edge for airfoils Dual cut-back trailing edge for airfoils

2007-01-24

2010-12-07

Edgar, Richard (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

Reexamination Certificate

active

07845906

ABSTRACT:
A cooling system for an airfoil portion of a turbine engine component is provided. The cooling system includes a first cavity dedicated to cooling a trailing edge portion of an airfoil portion and a second cavity dedicated to cooling an aft portion of a pressure side wall.

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patent: 2009/0324385 (2009-12-01), Liang

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