Lubrication system for aircraft engine

F - Mech Eng,Light,Heat,Weapons – 01 – M

Patent

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Details

F01M 1/02 (2006.01) F01D 25/20 (2006.01) F01M 1/10 (2006.01) F02C 7/06 (2006.01)

Patent

CA 2743281

A lubrication system for an aircraft engine includes a lubrication fluid tank and a fluid passage communicating with the tank to define an entry of the passage inside the tank. The entry is positioned in a location submerged in the lubrication fluid for delivery of the lubrication fluid under a pressure differential, from the tank to the lubrication system regardless of the tank or aircraft attitude.

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