Gas turbine engine fuel control system and regulating valves therefor
View Patent ↗A fuel control system for reheat burners of a gas turbine engine has a plurality of metering valves for respective burners, and throttle valves in series with the respective metering valves. A pressure regulating valve is provided for introducing pressurized fuel into fuel manifolds downstream of the respective throttle valves when the metering and throttle valves are shut. The pressure regulating valve also acts to relieve pressure in low pressure parts of the system when the latter is closed down and to prevent excessive temperature rise at the inlet of a fuel supply pump. The metering valves include pressure return ports which communicate with the metering valve outlets when those valves are shut.
1. A fuel control system for the reheat burners of a gas turbine engine, comprising:
a source of pressurized fuel,
a plurality of metering valve means for regulating fuel flow from said source to respective ones of a plurality of burner manifolds, and
means, operable when one of said metering valve means is shut, for introducing fuel at regulated reference pressure into the manifold associated with said one valve means.
2. A system as claimed in claim 1 which includes a plurality of throttle valves between respective ones of said metering valve means and their respective manifolds, one of said throttle valves including ports which, when said throttle valve is shut, connect said reference pressure to the manifold associated with said one throttle valve.
3. A system as claimed in claim 2 in which said one throttle valve is operable when closed to connect said reference pressure to a further manifold of the engine.
4. A system as claimed in claim 1 which includes relief valves in the respective burner manifolds, said relief valves being arranged to lift at pressures greater than said reference pressure.
5. A system as claimed in claim 1 , including a valve for regulating a pressure of a fluid, comprising a housing having a first port for connection to a fluid pressure source by way of a flow restrictor and a second port for connection to a low pressure, an outlet port communicating with said first port, a control element for regulating flow between said first and second ports, and a device for urging said control element to increase said flow in response to an increase in pressure at said first outlet port.
6. A system as claimed in claim 5 in which said device is a pressure-responsive bellows and there is provided means for adjusting the pressure at said outlet port at which said control element interconnects said first and second ports.
7. A fuel control system for the reheat burners of a gas turbine engine, comprising:
a source of pressurized fuel;
a plurality of metering valve means for regulating fuel flow from said source to respective ones of a plurality of burner manifolds;
means, operable when one of said metering valves is shut, for introducing fuel at predetermined reference pressure into the manifold associated with said one valve means; and
a plurality of throttle valves between respective ones of said metering valve means and their respective manifolds, one of said throttle valves including ports which, when said throttle valve is shut, connect said reference pressure to the manifold associated with said one throttle valve.
8. A system as claimed in claim 7 which includes relief valves in the respective burner manifolds, said relief valves being arranged to lift at pressures greater than said reference pressure.