US Patent 10443424 Turbine engine blade outer air seal with load-transmitting carriage
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Patent abstract
A gas turbine engine includes a case disposed around a central axis, a vane structure disposed radially inwards of the case, a seal carriage mounted to the case, and a seal arc segment mounted to the seal carriage. The vane structure exerts an axial load on the seal carriage. The seal carriage defines a load path that radially transmits the axial load to the case.
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Patent Number
104434240
Date of Patent
October 15, 2019
0Patent Application Number
150712910
Date Filed
March 16, 2016
0Patent Primary Examiner
Edits on 28 Sep, 2022
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Patent Jurisdiction
Patent Number
104434240
Date of Patent
October 15, 2019
0Patent Application Number
150712910
Date Filed
March 16, 2016
0Patent Primary Examiner
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US Patent 10443424 Turbine engine blade outer air seal with load-transmitting carriage
Infobox
Is a
Patent jurisdiction
Patent number
10443424
Date of patent
October 15, 2019
Patent application number
15071291
Date Filed
March 16, 2016
Patent primary examiner
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