US Patent 10316682 Composite keystoned blade track
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Patent abstract
A blade track for a gas turbine engine includes a plurality of blade track segments. The blade track segments are arranged circumferentially around a central axis to form the blade track.
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Patent Number
103166820
Date of Patent
June 11, 2019
0Patent Application Number
150888520
Date Filed
April 1, 2016
0Official Website
Patent Primary Examiner
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Patent Jurisdiction
Patent Number
103166820
Date of Patent
June 11, 2019
0Patent Application Number
150888520
Date Filed
April 1, 2016
0Official Website
Patent Primary Examiner
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US Patent 10316682 Composite keystoned blade track
Infobox
Is a
Patent jurisdiction
Patent number
10316682
Date of patent
June 11, 2019
Patent application number
15088852
Date Filed
April 1, 2016
Patent primary examiner
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