US Patent 10208622 Spacer for power turbine inlet heat shield
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Patent abstract
A gas turbine engine comprises an exhaust section member, a turbine section member, a heat shield and a spacer. The turbine section member is coupled to the exhaust section member. The heat shield is retained between the exhaust section member and the turbine section member. The spacer is positioned between the exhaust section member and the turbine section member to produce a gap for the heat shield. In one embodiment, the exhaust section member comprises a duct and the turbine section member comprises a bearing support.
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Patent Inventor Names
Fabian D. Betancourt0
Fernando K. Grant0
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Patent Applicant
Patent Jurisdiction
Patent Number
102086220
Date of Patent
February 19, 2019
0Patent Application Number
150270270
Date Filed
October 6, 2014
0Patent Citations Received
Patent Primary Examiner
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US Patent 10208622 Spacer for power turbine inlet heat shield
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10208622
Date of patent
February 19, 2019
Patent application number
15027027
Date Filed
October 6, 2014
Patent primary examiner
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