Fan driven emergency generator

• US 20060137355A1
• Filed: 12/27/2004
• Published: 06/29/2006
• Est. Priority Date: 12/27/2004
• Status: Abandoned Application

• Current Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Welch, Richard, Bueche, Gerard, Degroff, William, Albero, Jose, Makuszewski, Jerzy
• Application Number:
  US11/020,163
• Publication Number:
  US 20060137355A1
• Time in Patent Office: Days
• US Class Current: 60/772
• CPC Class Codes: B64D 41/007 Ram air turbines
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F05D 2220/326 to drive shrouded, low solidity propeller
• CPC Class Codes: F05D 2220/34 in ram-air turbines ("RATS")
• CPC Class Codes: F05D 2220/36 specially adapted for the fan of turbofan engines
• CPC Class Codes: F05D 2220/76 an electrical generator
• CPC Class Codes: H02K 7/1823 structurally associated with turbines or similar engines
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

An emergency electrical power generating apparatus for use with a turbofan engine comprises an electrical generator and a clutch assembly. The clutch connects the generator with a fan assembly of the engine only during a windmill action of the fan assembly.

Claims

1. An emergency electrical power generating apparatus for use with an aircraft gas turbine engine having a fan assembly, comprising:

an electrical generator; and

a clutch assembly for connecting the electrical generator with the fan assembly in order to transfer torque from the fan assembly during a windmill action of the fan assembly, and for disconnecting the generator from the fan assembly during engine operation.

2. The apparatus as claimed in claim 1 further comprising a speed increasing gearset to provide a high rotational speed to the electrical generator.

3. The apparatus as claimed in claim 2 wherein the gearset is positioned between the clutch assembly and the electrical generator.

4. The apparatus as claimed in claim 1 wherein the clutch assembly connects and disconnects the electrical generator to and from a low pressure spool shaft.

5. The apparatus as claimed in claim 4 wherein the generator is positioned in an engine tailcone compartment.

6. The apparatus as claimed in claim 4 wherein the clutch assembly connects and disconnects the electrical generator to and from a low pressure spool shaft through a tower shaft.

7. The apparatus as claimed in claim 1 wherein the electrical generator comprises a stator mounted to a bearing housing of the fan assembly and wherein the electrical generator comprises a rotor mounted to a fan shaft through the clutch assembly, for selectively controlling operation of the electrical generator.

8. An emergency electrical power generating apparatus for use with an aircraft gas turbine engine having a fan assembly, comprising:

an electrical generator stator mounted to a housing of a bearing;

an electrical generator rotor mounted to one of a fan shaft and a low pressure spool shaft, supported directly on said bearing.

9. The apparatus as claimed in claim 8 wherein said bearing is Number 1 bearing of the engine for supporting the fan shaft.

10. The apparatus as claimed in claim 9 wherein the electrical generator stator comprises at least one electrical winding and wherein the electrical generator rotor comprises at least one permanent magnet.

11. The apparatus as claimed in claim 10 wherein the electrical generator rotor further comprises an annular support member mounted on the fan shaft for supporting the at least one permanent magnet in an operative position with respect to the at least one electrical winding.

12. A method for generating emergency electrical power using a windmill action of an aircraft gas turbine engine, comprising:

disconnecting torque transmission from the engine to an emergency electrical power generator during engine operation; and

connecting torque transmission from the engine to the emergency electrical power generator during the windmill action.

13. The method as claimed in claim 12 wherein the connecting and disconnecting of torque transmission are conducted by a clutch.

14. The method as claimed in claim 13 wherein the clutch is activated by a centrifugal force being applied thereon.

15. The method as claimed in claim 13 wherein the clutch is manually activated.

16. The method as claimed in claim 13 wherein the clutch is controlled by a controller.