US Patent 10954807 Seal for a turbine engine
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Patent abstract
An apparatus for turbine engine including a turbine section with at least one turbine stage having a stationary vane assembly and a rotating blade assembly with combustion gases flowing through the turbine stage in a fore to aft direction. An interface is formed between a portion of the outer casing and a portion of the stationary vane assembly defining a leak flow path (LFP) where a seal is placed to retard combustion gases in the leak path.
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Patent Number
109548070
Date of Patent
March 23, 2021
0Patent Application Number
159974210
Date Filed
June 4, 2018
0Official Website
Patent Citations
Patent Citations Received
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US Patent 10954807 Seal for a turbine engine
Infobox
Is a
Patent jurisdiction
Patent number
10954807
Date of patent
March 23, 2021
Patent application number
15997421
Date Filed
June 4, 2018
Patent citations
Patent primary examiner
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