Modular counter rotating propeller system

• US 8,740,565 B2
• Filed: 08/12/2011
• Issued: 06/03/2014
• Est. Priority Date: 08/12/2011
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Perkinson, Robert H.
• Primary Examiner(s): Landrum, Ned
• Assistant Examiner(s): MCDOWELL, LIAM J
• Application Number:
  US13/208,648
• Publication Number:
  US 20130039764A1
• Time in Patent Office: 1,026 Days
• Field of Search: 416/66, 416/128, 416/129, 416/160, 60/391.62, 602/68
• US Class Current: 416/129
• CPC Class Codes: B64C 11/306 specially adapted for contrarotating propellers
• CPC Class Codes: B64C 11/48 Units of two or more coaxial propellers
• CPC Class Codes: B64D 2027/005 Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A self-contained counter rotating turbo prop system is driven by a gas turbine engine through a reduction gearbox. A gear train housed separate from the reduction gearbox provides the counter-rotation of a first and second pluralities of propeller blades. The entire counter-rotating propeller system is disposed within cowlings and is separate from the gas turbine engine and reduction gearbox. The example counter rotating propeller system includes a collective blade angle actuation system that provides for adjustment of blade angle of both the first and second plurality of propeller blades with a single actuator.

Claims

1. A counter rotating propeller system comprising:

a first input shaft rotatable about an axis and driven by a main engine;

a first hub supporting a first plurality of propeller blades, the first hub supported for rotation directly by the first input shaft such that the first hub is rotatable relative to the first input shaft;

a second input shaft supported by the first hub for rotation relative to the first hub and the first input shaft;

a second hub supporting a second plurality of propeller blades, the second hub supported by the second input shaft; and

a planetary gear train driven by the first input shaft, the planetary gear train including a sun gear attached for rotation with the first input shaft, at least one planet gear supported on a planet gear carrier attached to the second input shaft, and a ring gear defined by the first hub, wherein the planetary gear train drives the first hub in a first direction and the second hub in a second direction opposite the first direction.

2. The counter rotating propeller system as recited in claim 1, wherein the first hub includes an inner surface defining the ring gear.

3. The counter rotating propeller system as recited in claim 1, including an actuator disposed within the second hub for adjusting a pitch of the first and second pluralities of propeller blades.

4. The counter rotating propeller system as recited in claim 3, wherein the first input shaft and the second input shaft comprise hollow shafts and a transfer tube extends through each of the first and second input shafts to the actuator within the second hub.

5. The counter rotating propeller system as recited in claim 4, including a yoke plate moveable axially responsive to the actuator and a plurality of cam plates attached to corresponding ones of the second plurality of propeller blades for rotation of the second plurality of propeller blades responsive to axial movement of the yoke plate.

6. The counter rotating propeller system as recited in claim 5, wherein the actuator comprises a hydraulic actuator and the transfer tube communicates hydraulic pressure to the actuator for moving the yoke plate axially.

7. The counter rotating propeller system as recited in claim 5, including a transfer mechanism translating rotation of the second plurality of propellers blades to the first plurality of propeller blades.

8. The counter rotating propeller system as recited in claim 7, wherein the transfer mechanism includes a first cam arm extending from the first plurality of propeller blades to a bearing and a second cam arm extending from the second plurality of propeller blades to the bearing.

9. The counter rotating propeller system as recited in claim 8, wherein the bearing includes a plurality of thrust bearings disposed between a first ring and a second ring movable relative to each other with the bearing movable axially.

10. The counter rotating propeller system as recited in claim 9, wherein the transfer mechanism rotates the first plurality of propeller blades in a first direction and the second plurality of blades in a second direction opposite the first direction to adjust a corresponding pitch angle for each of the first and second pluralities of propeller blades.

11. A counter rotating propeller system comprising:

a first input shaft rotatable about an axis and driven by a main engine;

a first hub supporting a first plurality of propeller blades, the first hub supported for rotation directly by the first input shaft such that the first hub is rotatable relative to the first input shaft;

a second input shaft supported by the first hub for rotation relative to the first hub and the first input shaft;

a second hub supporting a second plurality of propeller blades, the second hub supported by the second input shaft;

a planetary gear train driven by the first input shaft for driving the first hub in a first direction and the second hub in a second direction opposite the first direction;

an actuator for adjusting an angle of the first and second pluralities of propeller blades disposed within the second hub, the actuator driving a yoke plate axially that in turn rotates each of the second plurality of blades; and

a transfer mechanism translating rotation of the second plurality of blades to the first plurality of blades.

12. The counter rotating propeller system as recited in claim 11, wherein the first input shaft and the second input shaft comprise hollow shafts and a transfer tube extends through each of the first and second input shafts to the actuator within the second hub.

13. The counter rotating propeller system as recited in claim 11, including a plurality of cam plates attached to corresponding ones of the second plurality of propeller blades for rotation of the second plurality of propeller blades responsive to axial movement of the yoke plate.

14. The counter rotating propeller system as recited in claim 12, wherein the actuator comprises a hydraulic actuator and the transfer tube communicates hydraulic pressure to the actuator for moving the yoke plate axially.

15. The counter rotating propeller system as recited in claim 11, wherein the transfer mechanism includes a first cam arm extending from the first plurality of propeller blades to a bearing and a second cam arm extending from the second plurality of propeller blades to the bearing, the bearing movable along the axis.

16. The counter rotating propeller system as recited in claim 15, wherein the bearing includes a plurality of thrust bearings disposed between a first ring and a second ring rotatable relative to each other about the axis.

17. The counter rotating propeller system as recited in claim 11, wherein the transfer mechanism rotates the first plurality of propeller blades in a first direction and the second plurality of blades in a second direction opposite the first direction to adjust a corresponding pitch angle for each of the first and second pluralities of propeller blades.