Air supply control system

Claim 1

An air supply system including an air compressor coupled to and rotatably driven by a turbine, a combustor whose gaseous output is coupled to and drives the turbine, the compressor feeding an output line to the input of the combustor, a bleed line leading from the compressor output line, the bleed line adapted to feed compressed air to an external system requiring a pressurized air supply, a fuel line coupled to and adapted to supply a constant rate of fuel for burning to the combustor, the improvement comprising, a first valve, said first valve being a pressure relief valve in the compressor output line, said pressure relief valve being coupled to and controlled by the pressure in said compressor output line, a second valve, said second valve being in the bleed line, said second valve being of the type controlled by pressure, control means responsive to the pressure in the compressor output line, said control means controlling the second valve whereby the fuel flow to the combustor can be set to a constant, predetermined value to thereby establish a normal operating air output pressure in the compressor output line and in the bleed line, and whereby the second valve, being the valve in the bleed line operates towards its closed position to maintain pressure in the output line above a predetermined minimum pressure, and whereby the first valve opens to maintain pressure in the output line below a predetermined maximum pressure.