发明授权
US08201664B2 Lubrication system and method, and vortex flow separator for use therewith 有权
润滑系统和方法,以及与其一起使用的涡流分离器

Lubrication system and method, and vortex flow separator for use therewith
摘要:
An aircraft engine lubrication system has a vortex separator, a first pump line having a first pump, an inlet connected to a separated lubricant area at the outlet end of the separator, and an outlet connectable to the engine. A scavenge line is provided for returning lubricant from the engine to an inlet end of the separator. A lubricant tank is connected in fluid flow communication with the separator by a connection line. A second pump line having a second pump has an inlet connected to the lubricant tank and an outlet connected to the separator for pumping lubricant from the tank to the inlet end of the separator.
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