System and method for providing gas turbine engine output torque sensor validation and sensor backup using a speed sensor
First Claim
1. A gas turbine engine control system, comprising:
- a gas turbine engine including an output shaft, the gas turbine engine adapted to receive fuel flow and, upon receipt thereof, to generate an output torque and supply the output torque via the output shaft;
a reference torque sensor operable to sense the output torque and supply a torque sensor signal representative thereof;
a speed sensor operable to sense a rotational speed of the gas turbine engine and supply a speed sensor signal representative thereof; and
an engine control operable to implement one or more control laws, based in part on the output torque and rotational speed of the gas turbine engine, the engine control coupled to receive the torque sensor signal and the speed sensor signal and further operable to;
(i) calculate the output torque from the sensed rotational speed of the gas turbine engine,(ii) compare the sensed output torque to the calculated output torque to determine if the reference torque sensor is operating properly,(iii) use the sensed output torque in the one or more control laws if the reference torque sensor is determined to be operating properly, and(iv) use the calculated output torque in the one or more control laws if the reference torque sensor is determined to be not operating properly.
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Accused Products
Abstract
Methods and apparatus are provided for verifying proper operation of a gas turbine engine output torque sensor using a speed sensor, and using the speed sensor as a backup torque sensor. Gas turbine engine output torque is sensed using a reference torque sensor, and gas turbine engine output shaft rotational speed is sensed. Gas turbine engine output torque is calculated from the sensed gas turbine engine output shaft rotational speed. The sensed gas turbine engine output torque is compared to the calculated gas turbine engine output torque to determine if the reference torque sensor is operating properly. The gas turbine engine is controlled at least partially based on the sensed gas turbine engine output torque if the reference torque sensor is determined to be operating properly, and is controlled at least partially based on the calculated output torque if the reference torque sensor is determined to be not operating properly.
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Citations
20 Claims
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1. A gas turbine engine control system, comprising:
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a gas turbine engine including an output shaft, the gas turbine engine adapted to receive fuel flow and, upon receipt thereof, to generate an output torque and supply the output torque via the output shaft; a reference torque sensor operable to sense the output torque and supply a torque sensor signal representative thereof; a speed sensor operable to sense a rotational speed of the gas turbine engine and supply a speed sensor signal representative thereof; and an engine control operable to implement one or more control laws, based in part on the output torque and rotational speed of the gas turbine engine, the engine control coupled to receive the torque sensor signal and the speed sensor signal and further operable to; (i) calculate the output torque from the sensed rotational speed of the gas turbine engine, (ii) compare the sensed output torque to the calculated output torque to determine if the reference torque sensor is operating properly, (iii) use the sensed output torque in the one or more control laws if the reference torque sensor is determined to be operating properly, and (iv) use the calculated output torque in the one or more control laws if the reference torque sensor is determined to be not operating properly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. An engine controller, comprising:
a processor adapted to receive a torque sensor signal from a reference torque sensor and a speed sensor signal from a speed sensor, the torque sensor signal representative of a sensed engine output torque, the speed sensor signal representative of a sensed engine rotational speed, the processor configured to implement one or more engine control laws, based in part on engine output torque and engine rotational speed, the engine control operable to; (i) calculate engine output torque from the sensed engine output shaft rotational speed, (ii) compare the sensed engine output torque to the calculated engine output torque to determine if the reference torque sensor is operating properly, (iii) use the sensed output torque in the one or more control laws if the reference torque sensor is determined to be operating properly, and (iv) use the calculated engine output torque in the one or more control laws if the reference torque sensor is determined to be not operating properly. - View Dependent Claims (13, 14, 15, 16)
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17. A method for a gas turbine engine, comprising the steps of:
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sensing gas turbine engine output torque using a reference torque sensor; sensing gas turbine engine rotational speed; calculating gas turbine engine output torque from the sensed gas turbine engine rotational speed; comparing the sensed gas turbine engine output torque to the calculated gas turbine engine output torque to determine if the reference torque sensor is operating properly; controlling the gas turbine engine at least partially based on the sensed gas turbine engine output torque if the reference torque sensor is determined to be operating properly; and controlling the gas turbine engine at least partially based on the calculated output torque if the reference torque sensor is determined to be not operating properly. - View Dependent Claims (18, 19, 20)
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Specification