Systems and methods for starting aircraft engines

• US 7,513,119 B2
• Filed: 02/03/2005
• Issued: 04/07/2009
• Est. Priority Date: 02/03/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Zielinski, Edward, Bernier, Alan T., White, Jeffrey J., Knechtel, Kent W., Ralston, Mark D., Campbell, Thomas A.
• Primary Examiner(s): Kramer; Devon C
• Assistant Examiner(s): SUNG, GERALD LUTHER
• Application Number:
  US11/051,272
• Publication Number:
  US 20060168968A1
• Time in Patent Office: 1,524 Days
• Field of Search: 602/04, 602/261, 607/72, 607/78, 244/58, 324/772, 324/545
• US Class Current: 60/778
• CPC Class Codes: F02C 7/262 Restarting after flame-out
• 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 7/275 Mechanical drives
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: F05D 2220/76 an electrical generator
• CPC Class Codes: F05D 2220/764 of the alternating current (A.C.) type
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

Methods and systems for starting aircraft turbofan engines are disclosed. A system in accordance with one embodiment includes an electrically-powered starter motor coupled to a turbofan engine to provide power to the turbofan engine during an engine start procedure. The system can further include an on-board, deployable, ram air driven turbine coupled to an electrical generator, which is in turn coupled to the starter motor to provide electrical power to the starter motor. In other embodiments, the ram air driven turbine can be replaced with a fuel cell or a battery. In still further embodiments, a single controller can control operation of both the engine starter and other motors of the aircraft.

Claims

1. A method for operating a turbofan engine, comprising:

allowing an unstarted turbofan engine of an aircraft to windmill during flight;

deploying a ram air driven turbine into an airstream adjacent to the aircraft;

extracting electrical power from the ram air driven turbine via an electrical generator coupled to the ram air driven turbine;

starting the turbofan engine by directing the electrical power to a starter motor coupled to the turbofan engine; and

testing at least one of the ram air driven turbine and the electrical generator on the ground by providing electrical power to the electrical generator while the ram air driven turbine is installed on the aircraft so as to operate the electrical generator as a motor to drive the ram air driven turbine.

2. The method of claim 1 wherein the starter motor includes a starter motor/generator and wherein the method further comprises extracting electrical power from the turbofan engine via the starter motor/generator after the turbofan engine is started.

3. The method of claim 1 wherein the unstarted turbofan engine is a first unstarted turbofan engine and wherein the method further comprises:

allowing a second unstarted turbofan engine of the aircraft to windmill during flight; and

starting the second turbofan engine by directing electrical power from the first turbofan engine to a starter motor coupled to the second turbofan engine, after starting the first turbofan engine.

4. The method of claim 1 wherein starting the turbofan engine includes starting the turbofan engine in the absence of a pneumatically powered starter.

5. The method of claim 1, further comprising stowing the ram air driven turbine after the engine starts.

6. The method of claim 1, further comprising starting the turbofan engine on the ground by:

coupling the aircraft to a ground source of direct current electrical power;

converting the direct current power to variable frequency alternating current power;

directing the alternating current power to a synchronous starter motor/generator coupled to the turbofan engine to initiate rotation of engine components;

varying the frequency of the alternating current power provided to the starter motor/generator as the rotation speed of the engine components increases;

initiating combustion in the turbofan engine; and

continuing to provide the alternating current power via the ground source at least until the turbofan engine achieves a self-sustaining state.

7. The method of claim 6 wherein the starter motor includes a starter motor/generator, and wherein the method further comprises:

decoupling the aircraft from the ground source; and

extracting electrical power from the engine via the starter motor/generator.

8. The method of claim 6, further comprising continuing to provide electrical power to the engine via the ground source after the engine achieves a self-sustaining state.