DEVICE FOR MOULDING A BLADED PART OF A TURBOMACHINE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20240059032A1
SERIAL NO

18557002

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A device for moulding at least one bladed part of a turbine engine, including a base; a mould formed from a plurality of parts nested inside one another, this mould being applied to the base. A first seal is mounted between the mould and the base; and a bell is mounted on the mould and around the mould, this bell being applied to the base. A second seal is mounted between the bell and the base, this bell being configured to be held tight against the base and having interior surfaces engaging by wedge effect with complementary exterior surfaces of the mould in order to apply a clamping force on the parts of this mould.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES2 BOULEVARD DU GÉNÉRAL MARTIAL VALIN 75015 PARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BLAISE, Maxime Marie Desire Moissy-Cramayel, FR 6 2
FABRE, Hubert Jean Marie Moissy-Cramayel, FR 28 24
POTE, Jeff Moissy-Cramayel, FR 4 2

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