Control device for controlling an engine of a turbine power system having more than one engine

• US 4,644,744 A
• Filed: 04/19/1985
• Issued: 02/24/1987
• Est. Priority Date: 04/19/1985
• Status: Expired due to Fees

• Current Assignee: Allied Corp. (Honeywell International Inc.)
• Original Assignee: Allied Corp. (Honeywell International Inc.)
• Inventors: Mittendorf, Gerald C., Sollman, Francis G.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US06/725,049
• Time in Patent Office: 676 Days
• Field of Search: 60/39.15, 60/39.282
• US Class Current: 60/39.15
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F02C 9/42 specially adapted for the control of two or more plants simultaneously
• CPC Class Codes: F05D 2270/052 Torque
• CPC Class Codes: F05D 2270/053 Explicitly mentioned power
• CPC Class Codes: F05D 2270/13 to control two or more engines simultaneously

Abstract

A control device for controlling an engine of a turbine power system having more than one engine is disclosed. The control device includes a proportional-integral-differential (PID) controller based on power turbine speed and a signal representing the difference between the torque of the engine being controlled and the torque of another engine in the power system, if the controlled engine is generating a torque less than that of the other engine. Accordingly, the control loop used in the device inherently tends to bring the torque of the controlled engine up to the torque of the other engine while maintaining power turbine speed equal to its reference, thereby equalizing the torques without expensive electrical connections between the controls of the two engines. Overrides are provided so that fuel also may be controlled based on the maximum torque of the engine being controlled, the total torque exerted by all the engine of the power system, the power tubine temperature, or by positive or negative gas generator speed rate of changes.

Claims

1. Control device for controlling an engine of a turbine power system having more than one engine comprising first torque measuring means for generating a primary torque signal which varies as a function of the torque generated by the controlled engine, second torque measuring means for generating a secondary torque signal which varies as a function of the torque generated by one of the other engines of said power system, means for subtracting the secondary torque signal from the primary torque signal to form a difference signal, said controlled engine having a power turbine, means for generating a speed signal proportional to the speed of the power turbine, means for generating a summing signal as a function of the sum of said speed signal and said difference signal, means for generating a control signal as a function of the summing signal, said control signal generating means including means for integrating a difference signal which varies as a function of the difference between said summing signal and a feedback signal which varies as a function of said control signal, and means responsive to said control signal for controlling fuel flow to said controlled engine under predetermined conditions.

2. Control device for turbine power plant as claimed in claim 1, including means for generating a differential signal which varies as a function of the time differential of said speed signal, said summing signal being generated as a function of said differential signal.

3. Control device as claimed in claim 1, wherein said system includes means for summing said primary and secondary torque signals and subtracting the result from a first reference signal of predetermined value to generate a first difference signal, and selecting means for selecting between said control signal and said first difference signal to control fuel flow to said one engine.

4. Control device as claimed in claim 3, wherein said system includes means for generating a second difference signal as a function of the difference between the primary torque signal and a second reference signal of predetermined value, said selecting means selecting between said first difference signal, said second difference signal and said control signal to control fuel flow to said one engine.

5. Control device as claimed in claim 4, wherein said system includes means for generating a turbine temperature function signal as a scheduled function of the temperature in said power turbine, said selecting means selecting between said first difference signal, said second difference signal, said control signal and said turbine temperature function signal to control fuel flow to the one engine as a function of one of said first difference signal, said second difference signal, said control signal or said turbine temperature function signal.

6. Control device for controlling an engine of a turbine power system having more than one engine, comprising first torque measuring means for generating a primary torque signal which varies as a function of the torque generated by the controlled engine, secondary torque measuring means for generating a second torque signal which varies as a function of the torque generated by one of the other engines of said power system, means for generating a first difference signal which varies as a function of the difference between said primary and secondary torque signals, means for generating a second signal which varies as a function of the sum of said primary and secondary torque signals, said controlled engine having a power turbine, and means for generating a control signal as a function of said first difference signal and a signal which varies as a function of the speed of said power turbine, and means for selecting between said control signal and said second signal to control fuel flow to said one engine.

7. Control device as claimed in claim 6, wherein said system includes means for generating a third difference signal which varies as a function of the difference between said primary torque signal and a fixed reference signal, said selecting means selecting between said control signal, said second signal and said third difference signal to control fuel flow to said controlled engine.

8. Control device as claimed in claim 7, wherein said system includes means for generating a turbine temperature function signal as a scheduled function of the temperature in said power turbine, said selecting means selecting between said control signal, said second signal, said third difference signal, and said turbine temperature function signal to control fuel flow to said controlled engine.

9. Control device as claimed in claim 8, wherein said selecting means selects the smallest of said control signal, said second signal, said third difference signal and said turbine temperature function signal.

10. Control device as claimed in claim 8, wherein said one engine includes a gas generator turbine, means for generating a gas generator speed signal as a function of the speed of the gas generator turbine, and means responsive to said gas generator speed signal to maintain said control signal between predetermined levels, said predetermined levels varying as a function of the gas generator speed signal.

11. Control device as claimed in claim 6, wherein said one engine includes a gas generator turbine, means for generating a gas generator speed signal as a function of the speed of the gas generator turbine, and means responsive to said gas generator speed signal to maintain said control signal between predetermined levels, said predetermined levels varying as a function of the gas generator speed signal.