Patent ID: 8793971

Claim:
A fuel supply system for a gas turbine engine comprising: a first pump for delivering fuel to a first line extending to a first use on a gas turbine engine; a second pump for delivering fuel to a second line extending to a second use on the gas turbine engine; a valve allowing flow from said first pump to be delivered to the first line, but also routing some fuel flow from said first pump to supplement fuel flow from said second pump until a pressure downstream of said second pump increases, and said valve then allowing fuel flow from said second pump to flow to the first line to supplement the fuel flow from said first pump; said first pump supplementing fuel flow from said second pump to said second line; wherein said first use will be a combustion chamber for the gas turbine engine, and said second use will be as a hydraulic fuel for at least one accessory actuator; said valve includes a valve housing, said valve housing being provided with a first port to communicate said first pump to said first line, and to said second line, and said valve housing being provided with a second port to communicate said second pump to the first line; and said valve includes a bias force which biases a valve spool in opposition to the pressure downstream of said second pump, said valve spool being positioned to allow fuel flow from said first pump to supplement fuel flow from said second pump to the second line, and also allow fuel flow from said first pump to be delivered to the first line, and block fuel flow from said second pump from passing to the first line until the pressure downstream of said second pump increases enough to overcome the bias force on said valve spool.