Method and apparatus for controlling an engine start system

• US 7,227,271 B2
• Filed: 09/02/2005
• Issued: 06/05/2007
• Est. Priority Date: 09/21/2004
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Anghel, Cristian E., McGinley, Ray M.
• Primary Examiner(s): Ponomarenko; Nicholas
• Application Number:
  US11/217,357
• Publication Number:
  US 20060061336A1
• Time in Patent Office: 641 Days
• Field of Search: 322/10, 322/11, 322/59, 322/89, 322/99, 290/31, 290/36.R, 290/37.A
• US Class Current: 290/31
• CPC Class Codes: F02N 11/04 the motors being associated with current generators
• CPC Class Codes: F02N 11/0859 specially adapted to the type of the starter motor or integrated into it
• CPC Class Codes: F02N 2300/102 Control of the starter motor speed; Control of the engine speed during cranking
• CPC Class Codes: F02N 2300/104 Control of the starter motor torque
• CPC Class Codes: H02P 2101/30 for aircraft
• CPC Class Codes: H02P 25/06 Linear motors
• CPC Class Codes: H02P 9/30 using semiconductor devices

Abstract

An apparatus (80) controls a synchronous machine (20) used to start an engine (300) during an engine start operation. The apparatus comprises: an exciter current control unit (84) for controlling exciter current output to the synchronous machine (20) during the engine start operation; and a main current control unit (82) for controlling main current output to the synchronous machine (20) during the engine start operation as a function of machine speed. In one implementation, the main current control unit (82) controls main current output to the synchronous machine (20) so that the synchronous machine (20) exhibits a reduced output torque during an initial torque application stage. The reduced viscous drag effects and reduced impact torque are beneficial to the engine system (100).

Claims

1. An apparatus for controlling a synchronous machine used to start an engine during an engine start operation, said apparatus comprising:

an exciter current control unit for controlling exciter current output to the synchronous machine during the engine start operation; and

a main current control unit for controlling main current output to the synchronous machine during the engine start operation as a function of machine speed, wherein said main current control unit controls main current output to the synchronous machine so that the synchronous machine exhibits a produced torque during an initial torque application stage that is lower than a produced torque exhibited during a subsequent torque application stage.

2. The apparatus according to claim 1, wherein said main current control unit controls main current output to the synchronous machine such that:

main current is increased from an initial value to a maximum value during the initial torque application stage; and

main current is maintained at its maximum value during the subsequent torque application stage.

3. The apparatus according to claim 2, wherein main current is increased linearly from the initial value during the initial torque application stage.

4. The apparatus according to claim 2, wherein the initial value of main current is non-zero.

5. The apparatus according to claim 4, wherein the initial value of main current is greater than approximately 50% of the maximum value.

6. The apparatus according to claim 2, wherein the subsequent torque application stage is a second torque application stage, and said main current control unit controls main current output to the synchronous machine such that:

main current is decreased from the maximum value during a third torque application stage.

7. The apparatus according to claim 1, wherein said apparatus controls multiple synchronous machines used to start the same engine during the engine start operation, said multiple synchronous machines being mechanically coupled to the same gearbox.

8. The apparatus according to claim 1, wherein said main current control unit controls a main inverter, which converts DC electrical power to multi-phase AC electrical power, which the main inverter outputs to a main stator winding of the synchronous machine.

9. The apparatus according to claim 1, wherein the engine is a gas turbine engine of an aircraft.

10. An apparatus for controlling a synchronous machine used to start an engine during an engine start operation, said apparatus comprising:

a main current control unit for controlling main current output to the synchronous machine during the engine start operation; and

an exciter current control unit for controlling exciter current output to the synchronous machine during the engine start operation as a function of machine speed, wherein said exciter current control unit controls exciter current output to the synchronous machine so that the synchronous machine exhibits a produced torque during an initial torque application stage that is lower than a produced torque exhibited during a subsequent torque application stage.

11. The apparatus according to claim 10, wherein said exciter current control unit controls exciter current output to the synchronous machine such that:

exciter current is increased from an initial value to a maximum value during the initial torque application stage; and

exciter current is maintained at its maximum value during the subsequent torque application stage.

12. The apparatus according to claim 11, wherein exciter current is increased linearly from the initial value during the initial torque application stage, wherein the initial value is non-zero.

13. The apparatus according to claim 11, wherein the subsequent torque application stage is a second torque application stage, and said exciter current control unit controls exciter current output to the synchronous machine such that:

exciter current is decreased from the maximum value during a third torque application stage.

14. The apparatus according to 10, wherein said apparatus controls multiple synchronous machines used to start the same engine during the engine start operation, said multiple synchronous machines being mechanically coupled to the same gearbox.

15. A method for controlling a synchronous machine used to start an engine during an engine start operation, said method comprising:

controlling exciter current output to the synchronous machine during the engine start operation; and

controlling main current output to the synchronous machine during the engine start operation,

wherein said method controls at least one of main current and exciter current output to the synchronous machine during the engine start operation as a function of machine speed so that the synchronous machine exhibits produced torque during an initial torque application stage that is lower than a produced torque exhibited during a subsequent torque application stage.

16. The method according to claim 15, wherein main current output to the synchronous machine is controlled such that:

main current is increased from an initial, non-zero, value to a maximum value during the initial torque application stage;

main current is maintained at its maximum value during the subsequent torque application stage, which is a second torque application stage; and

main current is decreased from the maximum value during a third torque application stage.

17. The method according to claim 15, wherein exciter current output to the synchronous machine is controlled such that:

exciter current is increased from an initial, non-zero, value to a maximum value during the initial torque application stage;

exciter current is maintained at its maximum value during the subsequent torque application stage, which is a second torque application stage; and

exciter current is decreased from the maximum value during a third torque application stage.

18. The method according to claim 15, wherein said method controls multiple synchronous machines used to start the same engine during an engine start operation, said multiple synchronous machines being mechanically coupled to the same gearbox.

19. The method according to claim 15, wherein

said step of controlling main current output to the synchronous machine controls a main inverter, which converts DC electrical power to multi-phase AC electrical power, which the main inverter outputs to a main stator winding of the synchronous machine;

and

said step of controlling exciter current output to the synchronous machine controls an exciter inverter, which converts DC electrical power to AC electrical power, which the exciter inverter outputs to a stator excitation winding of the synchronous machine.

20. The method according to claim 15, wherein the engine is a gas turbine engine of an aircraft.