Invention Grant
US08713909B2 Elimination of unfavorable outflow margin 有权
消除不利流出边际

Elimination of unfavorable outflow margin
Abstract:
A panel for use in a gas turbine engine exhaust case is disclosed. The panel has an airfoil section and a flow diverting structure adjacent a leading edge, wherein the flow diverting structure directs fluid flow into an area of the airfoil that lacks sufficient internal pressure for cooling fluid flow.
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