LUBRICATION SYSTEM

Various implementations described herein are directed to a lubrication system (305) for a gearbox (327) of an aircraft (101). A lubrication line (315) is coupled to a plurality of jets and/or orifices (525, 530, 535, 540, 545, 550, 560) to provide lubrication to one or more components of the gearbox...

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Bibliographic Details
Main Author WILCOX, Matthew Michael
Format Patent
LanguageEnglish
French
German
Published 18.03.2020
Subjects
BLASTING
ENGINEERING ELEMENTS AND UNITS
GEARING
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MECHANICAL ENGINEERING
THERMAL INSULATION IN GENERAL
WEAPONS
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Summary:Various implementations described herein are directed to a lubrication system (305) for a gearbox (327) of an aircraft (101). A lubrication line (315) is coupled to a plurality of jets and/or orifices (525, 530, 535, 540, 545, 550, 560) to provide lubrication to one or more components of the gearbox (327). A check valve (505, 510, 515) is placed within the lubrication line (315) in a location upstream from the plurality of jets and/or orifices (525, 530, 535, 540, 545, 550, 560).
Bibliography:Application Number: EP20180214745