Exhaust cone with flexible fitting

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United States of America Patent

PATENT NO 11519361
SERIAL NO

17267361

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Abstract

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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 Owner(s)

Patent OwnerAddress
SAFRAN CERAMICSRUE DE TOUBAN LES CINQ CHEMINS 33185 LE HAILLAN 33185

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Carrere, Benoit Moissy-Cramayel, FR 11 119
Conete, Eric Moissy-Cramayel, FR 37 637

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