US Patent 10577947 Baffle insert for a gas turbine engine component
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Patent abstract
A baffle insert for a component of a gas turbine engine is provided. The baffle insert having: a plurality of trip strips extending upwardly from an exterior surface of the baffle insert; and at least one rib extending upwardly from the exterior surface of the baffle insert.
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Patent Inventor Names
Atul Kohli0
Brandon W. Spangler0
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US Patent 10577947 Baffle insert for a gas turbine engine component
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Is a
Patent jurisdiction
Patent number
10577947
Date of patent
March 3, 2020
Patent application number
14961644
Date Filed
December 7, 2015
Patent citations
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