TURBOMACHINE LUBRICATION SYSTEM COMPRISING A BYPASS FOR PREFERENTIALLY SUPPLYING LUBRICANT TO A LOW-SPEED REDUCTION GEAR

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United States of America Patent

APP PUB NO 20230407764A1
SERIAL NO

18249148

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Abstract

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A lubrication system for a turbomachine which includes a reduction gear. The lubrication system includes a main branch and a bypass branch which is arranged in parallel with the main branch. The main branch includes a heat exchanger. The bypass branch includes a hydraulic resistance that is lower than the hydraulic resistance of the main branch. The reduction gear is located downstream of the main branch and the bypass branch. The lubrication system includes at least one bypass device that is configured to supply the bypass branch with lubricant when a pressure value of the lubricant is below a threshold value.

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Patent Owner(s)

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

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
AURIOL, Jacques Moissy-Cramayel, FR 6 2
FERT, Jérémy Edmond Moissy-Cramayel, FR 11 28

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