Patent ID: 8925322
Filing Date: 2015-01-06
Classification: F02C,F05D,F23K

Abstract:
1. A turbine fuel supply system including a first sub-system having: a first nozzle for injecting fuel into a combustor of a turbine engine; a first valve controllable to communicate fuel to the first nozzle; a first fuel manifold for communicating fuel to the first valve from a fuel source; and a first recirculating conduit in fluid communication with the first fuel manifold and the fuel source, the first recirculating conduit allowing fuel not communicated by the first valve to be returned to the fuel source, wherein the first recirculating conduit is located downstream from the first valve, the system further including a controller assembly for raising the pressure of fuel in the first fuel manifold; and the system being characterized in that the first valve is adapted to open in direct response to a crack pressure predetermined by a pressure difference between a varying pressure in the first fuel manifold and the pressure in the combustor, thereby allowing fuel to be communicated from the first fuel manifold to the first nozzle.