Patent ID: 8950186
Filing Date: 2015-02-10
Classification: B64D,F02C,F05D

Abstract:
1. A method for supplementing fuel feed pressure and flow within an aircraft fuel system fueling an aircraft engine, the aircraft fuel system including a primary fuel tank, a first boost fuel pump delivering fuel from the primary tank to a fuel manifold, an auxiliary fuel tank, an override fuel pump delivering fuel from the auxiliary fuel tank to the fuel manifold, and a jettison fuel pump operable to draw fuel from the auxiliary fuel tank, and the method comprising the steps of: (a) sensing whether the aircraft engine is operating near maximum power; (b) upon sensing that the aircraft engine is operating near maximum power, operating the jettison fuel pump in fluid interconnection with the override fuel pump to deliver fuel to the fuel manifold; and (c) upon sensing that the aircraft engine has ceased to operate near maximum power, deactivating the jettison fuel pump; whereby operation of the jettison fuel pump in combination with the override fuel pump completely overrides fuel delivery by the first boost fuel pump from the primary fuel tank to the fuel manifold.