Invention Application
US20160208621A1 GAS TURBINE ENGINE AIRFOIL WITH WISHBONE BAFFLE COOLING SCHEME 审中-公开
燃气涡轮发动机空气与WISHBONE BAFFLE冷却方案

GAS TURBINE ENGINE AIRFOIL WITH WISHBONE BAFFLE COOLING SCHEME
Abstract:
A gas turbine engine component includes a structure including spaced apart first and second exterior walls that extend in a first direction to an endwall. The first and second exterior walls are joined at the endwall to provide a cooling cavity. A wishbone baffle is arranged in the cooling cavity and includes first and second interior walls respectively adjacent to the first and second exterior walls. The first and second interior walls extend in the first direction to and are joined by an apex to provide a first cavity. The wishbone baffle separates the first cavity from a second cavity provided between the apex and the endwall.
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