AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING A HOLDER FOR FITTINGS

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20240052788A1
SERIAL NO

18257830

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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Assembly for an aircraft turbine engine, comprising an intermediate casing hub, an accessory gearbox, and a transfer case including a power transmission shaft configured to transmit mechanical power, taken off an engine shaft of the turbine engine, to at least one accessory mounted on the accessory gearbox, in which the transfer case comprises a structural element surrounding the power transmission shaft and rigidly attaching the accessory gearbox to the intermediate casing hub.

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Patent Owner(s)

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

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BEUTIN, Bruno Albert Moissy-Cramayel, FR 23 291
DELAFORGE, Anthony Pierre Guy Moissy-Cramayel, FR 1 0
ZSIGA, Zoltan Moissy-Cramayel, FR 7 70

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