Invention Grant
US08486261B2 Fuel scavenge water removal system 有权
燃油清除除水系统

Fuel scavenge water removal system
Abstract:
An aircraft fuel scavenge system incorporates a scavenge pump receiving fuel from a center tank and depositing the fuel in a wing tank. A water separator receives fuel through an inlet tube providing a plurality of momentum changes to incoming fuel, the water separator having a fuel outlet connected to the scavenge pump and a water outlet. A water manifold is connected from the water outlet to an input to a fuel supply line to an engine.
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