Tiltrotor aircraft having journal bearing mounted pylon assemblies

Patent metadata

Field	Value
Publication number	US-10040562-B2
Application number	US-201715844451-A
Country	US
Kind code	B2
Filing date	Dec 15, 2017
Priority date	Aug 14, 2013
Publication date	Aug 7, 2018
Grant date	Aug 7, 2018

Abstract

A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and outboard pedestals are supported by the airframe and positioned above the wing. A pylon assembly is rotatably coupled between the inboard and outboard pedestals. The pylon assembly includes a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast. The spindle gearbox is rotatable about a conversion axis to selectively operate the tiltrotor aircraft between helicopter and airplane modes. A common shaft, rotatable about the conversion axis, is configured to transfer torque from an output gear of the fixed gearbox to the input gear of the spindle gearbox. Each of the inboard and outboard pedestals includes a journal bearing that provides a stiff coupling with the pylon assembly.

First claim

What is claimed is:

1. A pedestal assembly for receiving a pylon assembly of a tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft having an airframe including a fuselage and a wing, the pedestal assembly comprising:
an inboard pedestal supported by the airframe and positioned above the wing, the inboard pedestal including an inboard journal bearing; and
an outboard pedestal supported by the airframe and positioned above the wing, the outboard pedestal including an outboard journal bearing;
wherein, the inboard and outboard journal bearings are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard pedestals to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode;
wherein, the inboard journal bearing provides a stiff coupling between the pylon assembly and the inboard pedestal;
wherein, the outboard journal bearing provides a stiff coupling between the pylon assembly and the outboard pedestal; and
wherein, the stiff couplings control dynamic modes between the pylon assembly and the airframe.

2. The pedestal assembly as recited in claim 1 wherein the coupling between the pylon assembly and the outboard pedestal further comprises a fixed bearing coupling to substantially prevent lateral movement of the pylon assembly relative to the outboard pedestal.

3. The pedestal assembly as recited in claim 2 wherein the fixed bearing coupling further comprises a lock washer and spanner nut coupling the pylon assembly to an inboard side of the outboard pedestal and a washer and clamp ring coupling the pylon assembly to an outboard side of the outboard pedestal.

4. The pedestal assembly as recited in claim 1 wherein the coupling between the pylon assembly and the inboard pedestal further comprises a floating bearing coupling to allow lateral movement of the pylon assembly relative to the inboard pedestal.

5. The pedestal assembly as recited in claim 1 wherein the pylon assembly further comprises an inboard sleeve positioned within the inboard journal bearing and an outboard sleeve positioned within the outboard journal bearing.

6. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard pedestals further comprises a full pillow block housing.

7. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard pedestals further comprises a split pillow block housing.

8. The pedestal assembly as recited in claim 1 wherein the inboard pedestal further comprises a full pillow block housing and wherein the outboard pedestal further comprises a split pillow block housing.

9. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard pedestals further comprises a tip rib extending above the wing and defining a slot and wherein each of the inboard and outboard journal bearings further comprises a bearing cartridge received within the respective slot.

10. The pedestal assembly as recited in claim 1 wherein the inboard and outboard pedestals support fore/aft loads when the tiltrotor aircraft is in the airplane mode.

11. The pedestal assembly as recited in claim 1 wherein the inboard and outboard pedestals support vertical loads when the tiltrotor aircraft is in the helicopter mode.

12. A tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft comprising:
an airframe including a fuselage and a wing;
an inboard pedestal supported by the airframe and positioned above the wing, the inboard pedestal including an inboard journal bearing;
an outboard pedestal supported by the airframe and positioned above the wing, the outboard pedestal including an outboard journal bearing; and
a pylon assembly coupled to the inboard and outboard journal bearings such that the pylon assembly is rotatably mounted between the inboard and outboard pedestals to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode;
wherein, the inboard journal bearing provides a stiff coupling between the pylon assembly and the inboard pedestal;
wherein, the outboard journal bearing provides a stiff coupling between the pylon assembly and the outboard pedestal; and
wherein, the stiff couplings control dynamic modes between the pylon assembly and the airframe.

13. The tiltrotor aircraft as recited in claim 12 wherein the coupling between the pylon assembly and the outboard pedestal further comprises a fixed bearing coupling to substantially prevent lateral movement of the pylon assembly relative to the outboard pedestal.

14. The tiltrotor aircraft as recited in claim 13 wherein the fixed bearing coupling further comprises a lock washer and spanner nut coupling the pylon assembly to an inboard side of the outboard pedestal and a washer and clamp ring coupling the pylon assembly to an outboard side of the outboard pedestal.

15. The tiltrotor aircraft as recited in claim 12 wherein the coupling between the pylon assembly and the inboard pedestal further comprises a floating bearing coupling to allow lateral movement of the pylon assembly relative to the inboard pedestal.

16. The tiltrotor aircraft as recited in claim 12 wherein the pylon assembly further comprises an inboard sleeve positioned within the inboard journal bearing and an outboard sleeve positioned within the outboard journal bearing.

17. The tiltrotor aircraft as recited in claim 12 wherein each of the inboard and outboard pedestals further comprises a full pillow block housing.

18. The tiltrotor aircraft as recited in claim 12 wherein each of the inboard and outboard pedestals further comprises a split pillow block housing.

19. The tiltrotor aircraft as recited in claim 12 wherein the inboard pedestal further comprises a full pillow block housing and wherein the outboard pedestal further comprise a split pillow block housing.

20. The tiltrotor aircraft as recited in claim 12 wherein each of the inboard and outboard pedestals further comprises a tip rib extending above the wing and defining a slot and wherein each of the inboard and outboard journal bearings further comprises a bearing cartridge received within the respective slot.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Kooiman James Everett
• Decker George Ryan
• Vanbuskirk Matthew Carl
• Baines Andrew G
• Stanney Keith Alan

Classifications

• B64D35/00

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title

• Y10T29/49318

  Repairing or disassembling · CPC title

• F16H2057/02043

  for vehicle transmissions · CPC title

• F16C17/26

  Systems consisting of a plurality of sliding-contact bearings · CPC title

• F16C17/02

  for radial load only · CPC title