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AssigneeSafran Aircraft Engines
InventorsGonzague Marie Come Jacques André Elluin, Damien Didier Clément Cordier, Bruno Alexandre Didier Jacon, Florian Benjamin Kévin Lacroix, Philippe Didier Edmond Andre Liberal Nabias, Julien Vitra
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A discharge grille of an intermediate casing of a turbomachine includes a peripheral edge and a seal mounted on the peripheral edge via an attachment system, the seal ensuring the sealing between a first turbomachine member and a second member of the turbomachine, and surrounding the discharge grille of the intermediate casing, the seal having a U-shaped cross section and includes a base plate configured to bear against the first member, a sealing lip configured to bear against the second member through deformation of the sealing lip to ensure air tightness and fire proofing through contact.
A discharge grille of an intermediate casing of a turbomachine, comprising a peripheral edge and a seal mounted on said peripheral edge via an attachment system, the seal ensuring a sealing between a first turbomachine member and a second member of the turbomachine, and surrounding the discharge grille of the intermediate casing, said seal having a U-shaped cross section and comprises:
Dependencies are inferred from the claim text.