High reliability generator with dual drive path

• US 8,456,051 B2
• Filed: 11/30/2010
• Issued: 06/04/2013
• Est. Priority Date: 05/05/2010
• Status: Active Grant

• Current Assignee: OECO, LLC (Meggitt PLC)
• Original Assignee: OECO, LLC (Meggitt PLC)
• Inventors: Raad, Bernard Anthony
• Primary Examiner(s): Nguyen, Tran N.
• Assistant Examiner(s): GONZALEZ QUINONES, JOSE A
• Application Number:
  US12/956,345
• Publication Number:
  US 20110273043A1
• Time in Patent Office: 917 Days
• Field of Search: 310/83, 310/84, 310112-120, 310/121, 744/70, 745/67, 192/90, 192/94, 322/40, 417/199.1, 417/205
• US Class Current: 310/83
• CPC Class Codes: H02K 16/00 Machines with more than one rotor or stator machines for transmitting mechanical power from a driving shaft to a driven shaft and comprising structurally interrelated motor and generator parts H02K51/00; permanent magnet machines with multiple rotors or stators relatively rotated for vectorially combining the excitation fields or the armature voltages H02K21/029
• CPC Class Codes: H02K 2213/06 Machines characterised by the presence of fail safe, back up, redundant or other similar emergency arrangements
• CPC Class Codes: H02K 7/003 Couplings; Details of shafts means for mounting rotors on shafts H02K1/28
• CPC Class Codes: H02K 7/116 with gears

Abstract

A generator arrangement is provided in which the functionality of two typically separate electrical power generators are combined together into a single generator that forms part of a three-in-one combined multi-generator which has a dual drive path with a shear section that immunizes one of the generators (e.g., the permanent magnet generator) within the single combined multi-generator from a failure of another generator (e.g., the main generator) within the single combined multi-generator.

Claims

1. An electrical generator, comprising:

a first generator having a stator and a rotor;

a second generator having a stator and a rotor;

a drive gear that is connected to the rotor of the first generator to rotationally drive the rotor of the first generator; and

a drive shaft that is connected to the drive gear to rotationally drive the rotor of the second generator, wherein a portion of the drive shaft has a shear section formed therein to break apart the drive shaft at the shear section when a predetermined load condition within the second generator occurs, wherein when the predetermined load condition causes the shear section to break apart the rotational driving of the rotor of the first generator by the drive gear continues.

2. The electrical generator of claim 1, further comprising a rotor shaft connected to the rotor of the second generator and to the drive shaft, wherein the drive shaft rotationally drives the rotor of the second generator through the rotor shaft.

3. The electrical generator of claim 2, wherein the rotor shaft is connected to the rotor of the second generator by a spline.

4. The electrical generator of claim 1, wherein the drive gear is connected to the rotor of the first generator by a spline.

5. The electrical generator of claim 1, wherein the drive gear is part of a gearbox that connects to the electrical generator.

6. The electrical generator of claim 1, wherein the shear section comprises a reduced diameter portion of the drive shaft.

7. The electrical generator of claim 1, wherein the first generator comprises a permanent magnet generator, and the second generator comprises a main generator.

8. The electrical generator of claim 7, further comprising a third generator having a stator and a rotor, wherein the third generator comprises an exciter generator, and wherein the drive shaft rotationally drives the rotor of the third generator.

9. The electrical generator of claim 8, further comprising a housing that encloses the first, second and third generators.

10. The electrical generator of claim 1, wherein the shear section is located axially along a length of the drive shaft at a predetermined location after the rotor of the first generator.

11. An electrical generator that connects to a gearbox and provides electrical power to various components on an aircraft, comprising:

a housing;

a first generator having a stator and a rotor;

a second generator having a stator and a rotor;

a third generator having a stator and a rotor;

a drive gear that is connected to the rotor of the first generator to rotationally drive the rotor of the first generator; and

a drive shaft that is connected to the drive gear to rotationally drive the rotor of the second generator and to rotationally drive the rotor of the third generator, wherein a portion of the drive shaft has a shear section formed therein to break apart the drive shaft at the shear section when a predetermined load condition within the second generator occurs, wherein when the predetermined load condition causes the shear section to break apart the rotational driving of the rotor of the first generator by the drive gear continues.

12. The electrical generator of claim 11, wherein the first, second and third generators are located within the housing.

13. The electrical generator of claim 11, further comprising a rotor shaft connected to the rotor of the second generator and to the rotor of the third generator and to the drive shaft, wherein the drive shaft rotationally drives the rotor of the second generator and the rotor of the third generator through the rotor shaft.

14. The electrical generator of claim 13, wherein the rotor shaft is connected to the rotor of the second generator by a spline.

15. The electrical generator of claim 11, wherein the drive gear is connected to the rotor of the first generator by a spline.

16. The electrical generator of claim 11, wherein the shear section comprises a reduced diameter portion of the drive shaft.

17. The electrical generator of claim 11, wherein the shear section is located axially along a length of the drive shaft at a predetermined location after the rotor of the first generator.

18. The electrical generator of claim 11, wherein the first generator comprises a permanent magnet generator, the second generator comprises a main generator, and the third generator comprises an exciter generator.

19. The electrical generator of claim 13, further comprising one or more bearings that support the rotor shaft, wherein the rotor shaft includes a hollow portion, and wherein a lubricating fluid passes through passages in the housing and into the hollow portion of the rotor shaft where the lubricating fluid is pressurized and passes through one or more orifices formed in the rotor shaft and then impinges upon the one or more bearings to thereby lubricate the one or more bearings.

20. The electrical generator of claim 11, further comprising one or more drain passages formed in the housing, wherein the lubricating fluid passes through the one or more drains in the housing and to the gearbox after the lubricating fluid impinges upon the one or more bearings.