US Patent 11519361 Exhaust cone with flexible fitting
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Patent Inventor Names
Benoit Carrere0
Eric Conete0
Edits on 7 Dec, 2022
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US Patent 11519361 Exhaust cone with flexible fitting
Article
An assembly for an aircraft turbojet engine is described. The assembly includes a central gas-exhaust element and a connecting flange interposed between, upstream, a metallic outlet of a turbojet engine and, downstream, the central element. The connecting flange consists of an annular part and flexible lugs having axially: a first end where the lug is connected to the annular part, and a second free end, projecting radially outwards from the first end and towards which the lug is fixed with the central element.
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Patent Jurisdiction
Patent Number
115193610
Date of Patent
December 6, 2022
0Patent Application Number
172673610
Date Filed
August 9, 2019
0Patent Citations
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