Control for start-up of a gas turbine engine

• US 4,274,255 A
• Filed: 05/07/1979
• Issued: 06/23/1981
• Est. Priority Date: 05/07/1979
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Pollak, Robert R.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US06/036,721
• Time in Patent Office: 778 Days
• Field of Search: 60/39.14 R, 60/39.28
• US Class Current: 60/790
• CPC Class Codes: F02C 7/26 Starting; Ignition

Abstract

A closed loop control for starting a gas turbine engine is disclosed. Upon engine ignition, fuel flow is adjusted as a function of the difference between a desired torque and actual torque so as to provide an optimum schedule to accelerate the engine to the idle speed condition.

Claims

1. A system for controlling fuel flow to a turbine type power plant for starting the engine from ignition to idle speed mode of operation including means responsive to certain engine operating parameters to schedule a reference torque signal, means responsive to the actual torque produced by said engine upon engine start-up for being compared to said referenced torque signal and means, including a fuel control for regulating fuel flow in accordance with the difference of said referenced torque signal and said actual torque signal for regulating the amount of fuel being fed to the engine during said mode of power plant operation.

2. A system as claimed in claim 1 wherein said power plant is utilized in addition to powering aircraft for driving aircraft accessories, means responsive to an engine operating parameter for converting said parameter into a torque signal and means responsive to the aircraft accessory torque and the actual torque for producing a signal that reflects the power plant propulsive torque which signal is utilized as the actual torque signal for controlling fuel flow during said mode of power plant operation.

3. A system as in claim 1 wherein said power plant includes a compressor, said scheduled torque signal being manifested as a function of compressor speed and compressor inlet pressure and said actual torque being manifested by compressor acceleration and a predetermined constant.

4. A system as in claim 1 wherein said fuel flow commences to said engine upon a predetermined actuated signal for initiating ignition and time delay means rendering said system inoperative until said ignition has been achieved.

5. A system as in claim 4 wherein said fuel fed to said power plant for ignition purposes is controlled as a function of the temperature at the inlet or outlet of said turbine.

6. A system as in claim 3 wherein a signal indicative of Mach No. biases said scheduled torque signal.

7. A system for controlling fuel flow to a turbine type power plant having a compressor and turbine for starting the power plant from ignition to idle speed mode of operation, a starter for imparting rotary motion to said compressor and turbine until a predetermined speed is achieved for ignition, an initial start-up portion responding to compressor inlet pressure and turbine inlet temperature for initiation ignition upon actuation of said starter, a closed loop start-up portion having means responsive to certain power plant operating parameters to schedule a referenced torque signal, means responsive to the actual torque produced by said power plant upon power plant start-up for being compared to said referenced torque signal and means including a fuel control for regulating fuel flow in accordance with the difference of said referenced torque signal and said actual torque signal for regulating the amount of fuel being fed to the power plant during said mode of power plant operation.

8. A system according to claim 7 wherein said certain power plant operating parameters includes compressor speed and compressor inlet or outlet pressure.

9. A system as claimed in claim 7 wherein said actual torque is measured by sensing compressor acceleration and multiplying it by a given constant.

10. A system as claimed in claim 7 including means responsive to turbine inlet or outlet temperatures for detecting a hot start of said power plant for biasing said actual torque signal to limit the heat generated in said power plant.

11. A system as claimed in claim 7 including means responsive to the torque generated by said starter and the torque from said power plant for aircraft accessories for biasing said referenced torque signal.