US Patent 11834953 Seal assembly in a gas turbine engine
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US Patent 11834953 Seal assembly in a gas turbine engine
Article
Patent abstract
A seal assembly in a gas turbine engine is presented. The seal assembly is arranged at a forward side of an inner compressor exit diffusor. The seal assembly is arranged between an outlet guide vane assembly and the forward side of the inner compressor exit diffusor to reduce cooling air leakage therebetween or is arranged between adjacent outlet guide vane assemblies to reduce cooling air leakage therebetween. The seal assembly includes a plurality of seal segments. The seal assembly includes at least one seal, such as a brush seal.
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Patent Jurisdiction
Patent Number
Patent Inventor Names
Amit K. Paspulati0
Anil L. Salunkhe0
Dimitri Zelmer0
Krishna Chaitanya Veluru0
Date of Patent
December 5, 2023
0Patent Application Number
175971270
Date Filed
April 24, 2020
0Patent Citations
Patent Primary Examiner
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