Method of starting a gas turbine engine

• US 5,123,239 A
• Filed: 02/14/1991
• Issued: 06/23/1992
• Est. Priority Date: 02/14/1991
• Status: Expired due to Fees

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Rodgers, Colin
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US07/655,116
• Time in Patent Office: 495 Days
• Field of Search: 60/39.02, 60/39.141, 60/39.142, 74/6, 74/7 R
• US Class Current: 60/778
• CPC Class Codes: F02C 7/275 Mechanical drives
• CPC Class Codes: F05D 2220/50 for auxiliary power units (APU's)

Abstract

A method of starting a gas turbine engine eliminating the need for oversizing a starter motor or the like to attain a proper transition through the "pinch point" includes the steps of applying a torque from an external source to the gas turbine engine (10) to accelerate the same toward a self sustaining speed, igniting fuel in the engine (10) at a pre-determined speed less than the self-sustaining speed, and at or about the time of fuel ignition, momentarily increasing the torque applied to accelerate the engine (10). The acceleration torque and momentary increase can be achieved by applying torque from a gas turbine containing auxiliary power unit (20) to an engine (10) either mechanically or pneumatically and then overspeeding and/or increasing the turbine inlet temperature of the gas turbine within the APU (20) to achieve a momentary burst of torque.

Claims

1. A method of starting a gas turbine engine comprising the steps of:

a) applying a torque from an external source to a gas turbine engine to accelerate the same toward a self-sustaining speed;

b) igniting fuel in said engine at a predetermined speed less than said self-sustaining speed; and

c) at or about the time of initiation of step b), momentarily increasing the torque applied during the performance of step a).

2. The method of claim 1 wherein said external source is an operating gas turbine and step a) is performed by coupling the operating gas turbine to the gas turbine to be started.

3. The method of claim 2 wherein step c) is performed by momentarily overspeeding said operating gas turbine.

4. The method of claim 2 wherein step c) is performed by momentarily increasing the turbine inlet temperature of the gases flowing in said operating gas turbine.

5. The method of claim 2 wherein step c) is performed by momentarily increasing the turbine inlet temperature in and overspeeding said operating gas turbine.

6. A method of starting a main propulsion engine of an aircraft of the gas turbine type wherein the aircraft includes an auxiliary power unit driven by a relatively small gas turbine comprising the steps of:

a) initiating operation of said auxiliary power unit so that said relatively small gas turbine provides a source of torque;

b) applying the torque from the auxiliary power unit to the main propulsion engine to accelerate the main engine toward a self-sustaining speed;

c) igniting fuel in said main engine at a predetermined speed less than said self-sustaining speed; and

d) at or about the time of initiation of step c), momentarily increasing the torque applied during the performance of step b).

7. The method of claim 6 wherein step d) is performed by i) momentarily overspeeding the relatively small gas turbine, or ii) momentarily increasing the turbine inlet temperature of gas flowing within the relatively small gas turbine, or iii) both momentarily overspeeding the relatively small gas turbine and momentarily increasing the turbine inlet temperature of gas flowing within the relatively small gas turbine.