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A dual manifold fuel supply system for the combustor of gas generator in a turbofan engine wherein alternating circumferentially aligned fuel injectors are alternately supplied with fuel by a first or second fuel manifold. Fuel flow to both manifolds are controlled by a fuel control, preferably a fu

A dual manifold fuel supply system for the combustor of gas generator in a turbofan engine wherein alternating circumferentially aligned fuel injectors are alternately supplied with fuel by a first or second fuel manifold. Fuel flow to both manifolds are controlled by a fuel control, preferably a full authority digital electronic control, and the second manifold has an off valve interposed between it and the fuel control.

대표청구항 ▼

1. A fuel injection system for use in the combustor section of a gas turbine engine said fuel injection system comprising: a plurality of generally downstream facing fuel nozzles wherein a portion of said fuel nozzles are connected to a shutoff valve means which is interruptible, a means for inte

1. A fuel injection system for use in the combustor section of a gas turbine engine said fuel injection system comprising: a plurality of generally downstream facing fuel nozzles wherein a portion of said fuel nozzles are connected to a shutoff valve means which is interruptible, a means for interrupting said valve means in response to a control signal, and a means for generating said control signal based on the gas turbine engine fuel to air ratio and an overriding weight on wheels signal. 2. A fuel injection system for use in the combustor section of a gas turbine engine said fuel injection system comprising: first and second fuel lines, first and second pluralities of generally downstream facing fuel nozzles in fluid supply communication with said first and second fuel lines respectively, a shutoff valve interposed in said first fuel line, a means for shutting on and off said valve in response to a control signal; and a means for generating said control signal based upon the gas turbine engine fuel to air ratio and an overriding weight on wheels signal. 3. A fuel injection system as set forth in claim 2 comprising: first and second fuel manifolds disposed between said first and second fuel lines and said first and second pluralities of fuel nozzles respectively. 4. A fuel injection system as set forth in claim 3 wherein: said first and second pluralities of fuel nozzles are arranged in a generally circular and alternating pattern. 5. A fuel injection system as set forth in claim 4 including: a fuel control in supply communication with said first and second fuel lines. 6. A fuel injection system as set forth in claim 5 wherein said means for generating said control signal is an electronic engine control which controls said shutoff valve and said fuel control. 7. A fuel injection system as set forth in claim 6 wherein: said electronic engine control is a digital electronic engine control.