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US 4,307,451 AGranted
Backup control
AssigneeChandler Evans Inc.
InventorsRaymond D. Zagranski, Albert H. White
Life of this patent
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Abstract
A method of controlling fuel flow to a gas turbine engine includes computing the compressor discharge pressure from signals indicative of engine inlet temperature, engine speed and the computed scheduled fuel flow. The method permits accurate scheduling of fuel flow without employing a compressor discharge pressure sensor or continued engine operation in the event of sensor failure.
Claims2
In a method of controlling fuel flow to a gas turbine engine of the type including the steps of:
- sensing compressor inlet temperature and providing a first signal indicative of the sensed temperature;
- sensing engine speed and providing a second signal indicative of the sensed speed;
- providing a third signal indicative of compressor discharge pressure;
- the improvement comprising generating the third signal by the method which includes the steps of:
- calculating a fuel flow to compressor discharge pressure ratio by utilizing the first and second signals together with known engine steady state running characteristics;
- calculating a lagged value of fuel flow by utilizing the second signal, known engine time constant characteristics, and a scheduled fuel signal;
- dividing the calculated lagged value of fuel flow by the calculated fuel flow to compressor discharge pressure ratio to obtain the third signal;
- calculating a forth signal indicative of scheduled fuel flow by utilizing the first, second and third signal;
- and utilizing the fourth signal to control a fuel metering device adapted to deliver fuel to the engine.
6 more elements
Dependencies are inferred from the claim text.