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US Patent 11008882 Blade tip clearance assembly

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
April 18, 2019
Date of Patent
May 18, 2021
Patent Application Number
16388129
Patent Citations
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US Patent 10301961 Gas turbine engine rapid response clearance control system
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US Patent 10221713 Shroud cartridge having a ceramic matrix composite seal segment
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US Patent 10662804 Profiled bellcrank vane actuation system
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US Patent 10066497 Actuator for gas turbine engine blade outer air seal
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US Patent 10087770 Shroud cartridge having a ceramic matrix composite seal segment
Patent Citations Received
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US Patent 12012859 Variable flowpath casings for blade tip clearance control
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11008882
Patent Primary Examiner
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Brian P Wolcott

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