Gas turbine engine airfoil with wishbone baffle cooling scheme
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United States of America
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Apr 13, 2021
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app pub date -
Oct 22, 2019
filing date -
Oct 22, 2019
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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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