US Patent 10563517 Gas turbine engine v-shaped film cooling hole
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Patent abstract
A component for a gas turbine engine includes a wall that adjoins an interior cooling passage and provides an exterior surface. A film cooling hole fluidly connects the interior cooling passage and the exterior surface. The film cooling passage includes inlet and outlet passages that fluidly interconnect and adjoin one another in a misaligned non-line of sight relationship.
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Patent Inventor Names
JinQuan Xu0
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Patent Number
105635170
Date of Patent
February 18, 2020
0Patent Application Number
147699830
Date Filed
March 13, 2014
0Patent Citations Received
Patent Primary Examiner
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US Patent 10563517 Gas turbine engine v-shaped film cooling hole
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10563517
Date of patent
February 18, 2020
Patent application number
14769983
Date Filed
March 13, 2014
Patent primary examiner
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