Power management system for turbine engines

• US 5,315,819 A
• Filed: 09/17/1991
• Issued: 05/31/1994
• Est. Priority Date: 09/17/1991
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Looper, David L., Frew, James S., High, Glen T., Free, Joseph W., Prevallet, Larry C., Page, George W.
• Primary Examiner(s): Casaregola, L.
• Application Number:
  US07/762,322
• Time in Patent Office: 987 Days
• Field of Search: 60/39.281, 60/39.282, 60/243, 416/25, 416/27, 416/28, 416/30
• US Class Current: 60/39.282
• 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: F05D 2270/02 to control rotational speed (n)
• CPC Class Codes: F05D 2270/051 Thrust
• CPC Class Codes: F05D 2270/053 Explicitly mentioned power
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A power management system for turbine engines includes a plurality of switches, each allowing for engine speed and engine torque to be controlled together. The switches correspond to various modes of operation of the turbine engine. When a switch is selected, a mode signal is supplied to a FADEC which, in response, issues speed and torque commands to an associated engine. The FADEC includes function generators that issue the torque commands as a function of outside ambient conditions. The torque commands are continuously updated for changing ambient conditions. Further, takeoff torque can be corrected for heating conditions. The power management system can also provide torque commands as a linear function of power lever angle.

Claims

1. A power management system for at least one turbine engine, comprising:

indicating means for providing a mode signal indicating a selected one of a plurality of modes of operation; and

at least one engine control means for providing torque and speed commands to a corresponding turbine engine, each said engine control means including;

torque command means, responsive to said mode signal, for generating said torque commands; and

speed command means, responsive to said mode signal, for selecting said speed commands from a plurality of apriori values of engine speeds, each said value corresponding to a mode of operation.

2. A power management system according to claim 1, wherein each engine is a turboprop engine, and wherein said modes of operation are flight modes.

3. A power management system according to claim 1, wherein said speed command means includes:

a plurality of storage means for storing said apriori values; and

selecting means, responsive to said mode signal, for selecting a value from said plurality of storage means according to the mode selected, an output of said selecting means providing said speed commands.

4. A power management system according to claim 1, wherein said indicating means includes:

at least one switch for each mode of operation; and

means, responsive to the selection of said switches, for providing said mode signal.

5. A power management system according to claim 1, wherein said torque command means includes:

at least one function generator corresponding to each mode of operation, each function generator providing target torque requests; and

selection means, responsive to said mode signal, for selecting target torque requests from said function generators, an output of said selection means providing said torque commands.

6. A power management system according to claim 5, further including input means for generating input signals indicative of ambient conditions, wherein said function generators provide said target torque requests in response to said input signals.

7. A power management system according to claim 1, further including power lever means for each said engine,each said power lever means including a power lever and means for providing a pla signal indicating power lever angle;

and wherein said torque command means includes;

target torque means for providing first and second target torque requests; and

torque scheduling means, responsive to said pla signals and said first and second target torque requests, for generating said torque commands as a function of power lever angle.

8. A power management system according to claim 7, wherein each said torque scheduling means outputs said first target torque requests as said torque commands when its corresponding pla signal indicates a power lever angle at a first position;

wherein said torque scheduling means outputs said second target torque requests as said torque commands when said corresponding pla signal indicates a power lever angle at a second position; and

wherein said torque scheduling means interpolates said torque commands between said first and second target torque requests when said pla signal indicates a power lever angle between said first and second positions.

9. A power management system according to claim 8, wherein said torque scheduling means interpolates said torque commands as a linear function of power lever angle.

10. A power management system according to claim 9, wherein said target torque means includes means for generating maximum target torque requests as a function of said first target torque requests;

and

wherein said torque scheduling means provides said maximum target torque request when said pla signal indicates a power lever angle at a third position, which is above said first and second positions.

11. A power management system according to claim 10, wherein said torque scheduling means linearly interpolates said torque commands between said first and maximum target torque requests when said pla signal indicates a power lever angle between said first and third positions.

12. A power management system according to claim 11, wherein said torque scheduling means linearly extrapolates said torque commands when said pla signal indicates a power lever angle below said second position.

13. A power management system according to claim 7, wherein each said power lever means further includes filtering means, operative on said pla signal, for removing high frequency components from said pla signal.

14. A power management system according to claim 11, wherein said torque scheduling means includes flats at said first, second and third positions.

15. A power management system according to claim 7, wherein said target torque means provides apriori values as said second target torque requests.

16. A power management system according to claim 7, wherein said target torque means includes a first flight idle function generator for providing flight idle torque orders for a corresponding propeller speed.

17. A power management system according to claim 16, wherein said target torque means further includes:

at least one additional flight idle function generator for providing flight idle torque orders for corresponding propeller speeds; and

flight idle selecting means for selecting an output of said flight idle function generators, an output of said selecting means providing said second target torque requests.

18. A power management system according to claim 17, further including means for providing input signals indicative of temperature, altitude and mach number, wherein said flight idle function generators generate said flight idle torque orders in response to said input signals.

19. A power management system according to claim 6, wherein said input means provides input signals indicative of temperature, altitude and mach number.

20. A power management system according to claim 19, wherein said torque commands are generated also as a function of engine speed.

21. A power management system according to claim 3, wherein said speed command means further includes rate limiting means, operative on said speed command, for limiting the rate at which said speed commands change values.

28. A power management system according to claim 8, further including at least one set of sensor means associated with each turbine engine for generating input signals indicating ambient conditions;

and providing means for providing the same set of input signals to each said engine control means; and

wherein said target torque means includes at least one function generator for providing said first target torque requests in response to said input signals provided by said providing means, whereby matching power lever angles produce matching torque commands for said engines.

22. Apparatus for generating torque and engine speed commands for a turboprop engine in response to a mode signal indicating a selected one of a plurality of operating modes, said apparatus comprising:

at least one function generator corresponding to each mode of flight, each function generator providing target torque requests in response to input signals indicating temperature, altitude and mach number;

first selecting means, responsive to said mode signal, for selecting target torque requests from said function generators;

supplying means, responsive to said first selecting means, for supplying said selected target torque requests as said torque commands;

storing means for storing apriori values of engine speeds corresponding to said modes of operation; and

second selecting means, responsive to said mode signal, for selecting said values from said storing means according to the mode selected, an output of said second selecting means providing said engine speed commands.

23. Apparatus according to claim 22, wherein said at least one function generator includes a first function generator for providing target torque requests for takeoff, and wherein each said engine control means further includes:

overriding means, responsive to a cockpit signal, for overriding said input signal indicating temperature with a second signal indicating a corrected temperature; and

saving means, responsive to said cockpit signal, for saving a first target torque request generated by said first function generator, wherein said first selecting means selects an output of said saving means when takeoff is indicated by said mode signal and when an altitude signal indicating a predetermined altitude is not issued, and wherein said first selecting means selects said output of said first function generator when said altitude signal is issued and said mode signal indicates takeoff.

24. Apparatus according to claim 22, further comprising:

power lever means for providing a pla signal indicating power lever angle;

idle command means for providing flight idle torque requests; and

wherein said supplying means includes torque scheduling means, responsive to said pla signal, for outputting said target torque requests from said first selecting means when said pla signal indicates a power lever angle at a first position and for outputting said flight idle torque requests when said pla signal indicates a power lever angle at a second position, an output of said torque scheduling means providing said torque commands.

25. Apparatus according to claim 24, wherein said torque scheduling means linearly interpolates said torque commands when said pla signal indicates a power lever angle between said first and second positions.

26. Apparatus according to claim 25, wherein said idle command means includes:

at least two function generators for generating flight idle torque orders for corresponding propeller speeds; and

third selecting means for selecting an output of said at least two function generators, an output of said third selecting means providing said flight idle torque requests.

27. Apparatus according to claim 25, wherein said idle command means provides an apriori value as said flight idle torque request.