Fuel control system for gas turbine engine

• US 4,378,673 A
• Filed: 06/04/1980
• Issued: 04/05/1983
• Est. Priority Date: 06/04/1979
• Status: Expired due to Term

• Current Assignee: Nissan Motor Co., Ltd.
• Original Assignee: Nissan Motor Co., Ltd.
• Inventors: Abo, Toshimi, Kanegae, Hidetoshi
• Primary Examiner(s): Garrett, Robert E.
• Assistant Examiner(s): Simenauer, Jeffrey A.
• Application Number:
  US06/156,776
• Time in Patent Office: 1,035 Days
• Field of Search: 60/39.16 R, 60/39.14 R, 60/39.28 R
• US Class Current: 60/790
• CPC Class Codes: F02C 9/26 Control of fuel supply F02C9/48 takes precedence; fuel valves F02C7/232
• CPC Class Codes: F05D 2200/15 Inverse

Abstract

A fuel control system for a dual-shaft gas turbine engine having a gasifier turbine and a power turbine comprises a device for supplying fuel to a combustor of the engine by an amount necessary for engine ignition during engine starting. Under normal operating conditions, fuel is supplied to the combustor by a closed loop controller. An accelerating device increases the fuel supply to the combustor as time progresses from a first time when engine ignition takes place to a second time when the closed loop control of fuel supply takes place, thereby shortening the time period required for the engine to reach normal operation.

Claims

1. Apparatus for controlling the speed of a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising first means for controlling the amount of fuel flowing through the fuel controller during starting of the turbine, second means for controlling the amount of fuel flowing through the fuel controller during normal operation of the turbine, and means for switching operation from the first controlling means to the second controlling means in response to a predetermined relationship between the fuel flowing through the fuel controller during starting and the smaller of first and second errors between set point and actual values of the speeds of the power and gasifier shafts.

2. The apparatus of claim 1 wherein the second means for controlling includes means for controlling the amount of fuel flowing through the fuel controller in response to a quantity proportional to the smaller of the first and second errors and the integral of the smaller of first and second errors.

3. The apparatus of claim 1 wherein the first means includes means for initially controlling the fuel controller so a predetermined amount of fuel flows through the fuel controller unit the gasifier shaft reaches a predetermined speed and for thereafter increasing the amount of fuel flowing through the fuel controller until the second means is switched to control the fuel flowing through the fuel controller.

4. The apparatus of claim 1 wherein the first means includes means for initially controlling the fuel controller so a predetermined amount of fuel flows through the fuel controller until the gasifier shaft reaches a predetermined speed and for immediately thereafter gradually increasing the amount of fuel flowing through the fuel controller until the second means is switched to control the fuel flowing through the fuel controller.

6. The apparatus of claim 3, 4, or 5 further including means for monitoring ambient air temperature, said first controlling means including means responsive to the monitoring means signalling that the ambient air temperature is less than a predetermined value for increasing the amount of fuel flowing through the fuel controller as an inverse function of monitored air temperature.

5. Apparatus for controlling the speed of a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising first means for controlling the amount of fuel flowing through the fuel controller during starting of the turbine, second means for controlling the amount of fuel flowing through the fuel controller during operation of the turbine, and means for switching operation from the first controlling means to the second controlling means, wherein the first means includes means for intially controlling the fuel controller so a predetermined amount of fuel flows through the fuel controller until the gasifier shaft reaches a predetermined speed and for immediately thereafter gradually increasing the amount of fuel flowing through the fuel controller until the second means is switched to control the fuel flowing through the fuel controller.

7. Apparatus for controlling the speed of a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising means responsive to the gasifier shaft speed for deriving a first signal indicative of the gasifier shaft speed, means responsive to the power shaft speed for deriving a second signal indicative of power shaft speed, means responsive to the first and second signals and set point values for the gasifier shaft speed and the power shaft speed for deriving a third signal having a value indicative of the smaller of the errors between the indicated shaft speeds and the set point values therefor, means responsive to the third signal for deriving a fourth signal having a value proportional to the integral of the third signal, means responsive to the first signal and a predetermined starting value for the gasifier shaft speed for deriving a start signal that increases in value after the gasifier shaft speed reaches the predetermined starting value, means responsive to the start, third and fourth signals for activating the fuel controller so the fuel controller is responsive to the start signal until the start and third signals have a predetermined amplitude relationship and for thereafter activating the fuel controller so the fuel controller is responsive to the amplitude of the third and fourth signals to the exclusion of the start signal, the amount of fuel flowing through the fuel controller being determined by the amplitudes of the signals to which the fuel controller is responsive.

8. The apparatus of claim 7 further including means for monitoring ambient air temperature, and means responsive to the monitoring means signalling that the ambient air temperature is less than a predetermined value for increasing the value of the start signal as an inverse function of monitored air temperature.

9. The apparatus of claim 7 or 8 wherein the start signal deriving means includes means for deriving the start signal so it gradually increases in value immediately after the gasifier shaft speed reaches the predetermined value.

10. Apparatus for controlling the speed of a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising first means for controlling the amount of fuel flowing through the fuel controller during starting of the turbine, second means for controlling the amount of fuel flowing through the fuel controller during normal operation of the turbine, and means for switching operation from the first controlling means to the second controlling means in response to a predetermined relationship between the speed of the gasifier shaft during starting and an error between a set point and actual value for one of the shaft speeds.

11. A method of operating a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising activating the fuel controller so a constant optimum amount of fuel flows through the controller at the time of ignition of gases driving the gasifier and until the gasifier shaft speed reaches a predetermined value, determining the magnitude of the smaller of:

an error between the gasifier shaft speed and a set point therefor and an error between the power shaft speed and a set point therefor, then gradually increasing the amount of fuel flowing through the controller until the gasifier shaft speed has a predetermined relationship with the magnitude of the smaller error, in response to the predetermined relationship being reached controlling the amount of fuel flowing through the controller as a function of the magnitude of the smaller error.

12. The method of claim 11 wherein the function is proportional to the error magnitude and the integral of the error magnitude.

14. The method of claim 11 or 13 further comprising increasing the amount of fuel flowing through the controller as the fuel is being gradually increased as an inverse function of ambient air temperature in response to the temperature being less than a predetermined value.

13. A method of operating a turbine having a power shaft mounted independently of a gasifier shaft, the gasifier shaft being driven in response to fuel flowing through a fuel controller, comprising activating the fuel controller so a constant optimum amount of fuel flows through the controller at the time of ignition of gases driving the gasifier and until the gasifier shaft speed reaches a predetermined value, determining the magnitude of the smaller of:

an error between one of the gasifier shaft speed and a set point therefor and an error between the power shaft speed and a set point therefor, in response to the predetermined relationship being reached controlling the amount of fuel flowing through the controller as a function of the magnitude of one of the errors.