STATOR VANE WITH A COOLED PLATFORM FOR A GAS TURBINE ENGINE

A stator vane (60) for a gas turbine engine includes an airfoil (78) that extends radially from a first side of a platform (76). A pocket (90) is provided in the platform (76) on a second side opposite the airfoil (78). Forward and aft rails (100,102) extend from the second side of the platform (76)...

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Bibliographische Detailangaben
1. Verfasser: BANGERTER, James P
Format: Patent
Sprache:eng ; fre ; ger
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