US Patent 10100646 Gas turbine engine component cooling circuit
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Patent abstract
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion, a cooling circuit disposed within the body portion and including at least a first cavity and a microcircuit in fluid communication with the first cavity. A plunged hole intersects at least a portion of the microcircuit.
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Patent Inventor Names
San Quach0
Steven Bruce Gautschi0
Tracy A. Propheter-Hinckley0
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US Patent 10100646 Gas turbine engine component cooling circuit
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Is a
Patent jurisdiction
Patent number
10100646
Date of patent
October 16, 2018
Patent application number
13565877
Date Filed
August 3, 2012
Patent primary examiner
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