Gas turbine motor drive

• US 5,184,456 A
• Filed: 04/09/1991
• Issued: 02/09/1993
• Est. Priority Date: 04/08/1991
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Avco Corporation (Textron Inc)
• Inventors: Hudson, George, Rumford, Kimball J.
• Primary Examiner(s): Bertsch, Richard A.
• Assistant Examiner(s): RICHMAN, HOWARD
• Application Number:
  US07/682,749
• Time in Patent Office: 672 Days
• Field of Search: 60/39.02, 60/39.08, 60/39.33, 60/39.142
• US Class Current: 60/778
• CPC Class Codes: B64D 41/00 Power installations for auxiliary purposes
• CPC Class Codes: F02C 7/268 Starting drives for the rotor , acting directly on the rotor of the gas turbine to be started
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F02N 11/04 the motors being associated with current generators
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A gas turbine engine which includes a starter/generator mechanically coupled thereto and an electric oil pump motor for driving an oil pump is started in a manner which assures a continuous and uninterrupted supply of lubricating oil to the moving components of the engine. According to one method, first and second motor controllers initiate operation of the oil pump motor. Thereupon, the second motor controller is re-directed to initiate operation of the starter/generator and the gas turbine engine itself, after which, the second motor controller again joins the first motor controller to accelerate the oil pump motor up to idle speed. The oil pump motor may then be electrically coupled to the starter/generator for continued operation. In another mode of operation, a second motor controller may not be used at all. In that event, the alternating electric power supply for the vehicle powered by the gas turbine engine may be used as an interim source for controlling the speed of the oil pump motor.

Claims

1. A method of starting a gas turbine engine powering a vehicle which has an alternating electric power supply, the gas turbine engine including a starter/generator mechanically coupled thereto and an electric oil pump motor for driving an oil pump for providing a continuous and uninterrupted supply of lubricating oil to the moving components of the engine, the method comprising the steps of:

(a) electrically coupling a motor controller to the oil pump motor to initiate operation thereof;

(b) accelerating the oil pump motor to a speed substantially synchronous with the output of the vehicle power supply;

(c) electrically uncoupling the motor controller from the oil pump motor after the oil pump motor has reached a speed substantially synchronous with the vehicle power supply;

(d) substantially simultaneously with step (c), electrically coupling the oil pump motor to the vehicle power supply for continued operation thereof at a speed substantially synchronous with the vehicle power supply;

(e) electrically coupling the motor controller to the starter/generator to initiate operation of the starter/generator for starting the gas turbine engine;

(f) accelerating the starter/generator and the gas turbine engine until at least a speed has been attained at which continued input from the motor controller is no longer required for continued operation of the gas turbine engine; and

(g) after the starter/generator and the gas turbine engine reach the speed at which continued input from the motor controller is no longer required for continued operation of the gas turbine engine, electrically uncoupling the motor controller from the starter/generator;

(h) electrically uncoupling the oil pump motor from the vehicle power supply;

(i) substantially simultaneously with steps (g) and (h), again coupling the motor controller with the oil pump motor; and

(j) accelerating the oil pump motor at a controller rate until it attains idle speed.

2. A method of starting a gas turbine engine as set forth in claim 1 wherein:

the vehicle power supply operates at a frequency of approximately 400 Hz.

3. A method of starting a gas turbine engine as set forth in claim 1 wherein:

idle speed is approximately 50% of the maximum speed of the gas turbine engine.

4. A method of starting a gas turbine engine as set forth in claim 1 wherein:

the speed attained at which continued input from the motor controller is no longer required for continued operation of the gas turbine engine is approximately 40% of the maximum speed of the gas turbine engine.

5. A method of starting a gas turbine engine which includes a starter/generator mechanically coupled thereto and an electric oil pump motor for driving an oil pump for providing a continuous and uninterrupted supply of lubricating oil to the moving components of the engine, the method comprising the steps of:

(a) electrically coupling first and second motor controllers to the oil pump motor to initiate operation thereof;

(b) accelerating the oil pump motor at a controller rate until the torque required to operate the oil pump decreases to the extent that it can be driven by the first motor controller alone;

(c) electrically uncoupling the second motor controller from the oil pump motor;

(d) continuing to operate the oil pump motor with the first motor controller alone;

(e) electrically coupling the second motor controller to the starter/generator to initiate operation of the starter/generator for starting the gas turbine engine;

(f) accelerating the starter/generator and the gas turbine engine until at least a speed has been attained at which continued input from the second motor controller is no longer required for continued operation of the gas turbine engine; and

(g) after the starter/generator and the gas turbine engine reach the speed at which continued input from the second motor controller is no longer required for continued operation of the gas turbine engine, electrically uncoupling the second motor controller from the starter/generator.

6. A method of starting a gas turbine engine as set forth in claim 5 including the steps of:

(h) again electrically coupling the second motor controller with the oil pump motor; and

(i) accelerating the oil pump motor at a controlled rate until it attains idle speed.

7. A method of starting a gas turbine engine as set forth in claim 6 including the step of:

(j) electrically coupling the oil pump motor with the starter/generator when the oil pump motor has attained idle speed.

8. A method of starting a gas turbine engine as set forth in claim 5 wherein:

the speed attained at which continued input from the second motor controller is no longer required for

continued operation of the gas turbine engine is approximately 40% of the maximum speed of the gas turbine engine.

9. A method of starting a gas turbine engine as set forth in claim 6 wherein:

idle speed is approximately 50% of the maximum speed of the gas turbine engine.