Fuel scavenge water removal system

摘要

An aircraft fuel scavenge system incorporates a scavenge pump (30) receiving fuel from a center tank (10) and depositing the fuel in a wing tank (14). A water separator (40) receives fuel through an inlet tube (38) providing a plurality of momentum changes to incoming fuel, the water separator having a fuel outlet (32) connected to the scavenge pump and a water outlet. A water manifold (80) is connected from the water outlet to an input to a fuel supply line to an engine.