TURBOMACHINE COOLING TRENCH
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United States of America Patent
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Issued Date -
Jun 27, 2024
app pub date -
Jan 22, 2024
filing date -
Aug 6, 2018
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Abstract
A component for a turbine engine includes a body with an exterior surface abutting a combustion flowpath for a combustion gas flow through the turbine engine, a cooling passage defined within the body, and a trench on the exterior surface. The trench includes a plurality of outlets, and a plurality of cooling holes extending from the cooling passage to the corresponding plurality of outlets.
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