Tip rib mounted pylon assemblies

Patent metadata

Field	Value
Publication number	US-10065743-B2
Application number	US-201715719807-A
Country	US
Kind code	B2
Filing date	Sep 29, 2017
Priority date	Aug 14, 2013
Publication date	Sep 4, 2018
Grant date	Sep 4, 2018

Abstract

A pedestal assembly receives a pylon assembly of a tiltrotor aircraft having an airframe including a fuselage and a wing. The pedestal assembly includes inboard and outboard tip ribs that extend above the wing and respectively define inboard and outboard slots. The pedestal assembly also includes inboard and outboard bearing cartridges. The inboard bearing cartridge is received within the inboard slot, is coupled to the inboard tip rib and includes an inboard bearing assembly. The outboard bearing cartridge is received within the outboard slot, is coupled to the outboard tip rib and includes an outboard bearing assembly. The inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard tip ribs to selectively operate the tiltrotor aircraft between a helicopter mode and an airplane mode.

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 tip rib extending above the wing and defining an inboard slot;
an outboard tip rib extending above the wing and defining an outboard slot;
an inboard bearing cartridge received within the inboard slot and coupled to the inboard tip rib, the inboard bearing cartridge including an inboard bearing assembly; and
an outboard bearing cartridge received within the outboard slot and coupled to the outboard tip rib, the outboard bearing cartridge including an outboard bearing assembly;
wherein, the inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard tip ribs to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode.

2. The pedestal assembly as recited in claim 1 wherein the inboard bearing cartridge has a close fitting relationship with the inboard slot and wherein the outboard bearing cartridge has a close fitting relationship with the outboard slot.

3. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard tip ribs provides a stiff coupling with the pylon assembly.

4. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard tip ribs provides a stiff coupling with the pylon assembly to control dynamic modes between the pylon assembly and the airframe.

5. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard bearing cartridges further comprises a full diameter bearing housing.

6. The pedestal assembly as recited in claim 1 wherein the inboard bearing cartridge is coupled to the inboard tip rib and the outboard bearing cartridge is coupled to the outboard tip rib with a plurality of bolts.

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

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

9. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard bearing assemblies further comprises a journal bearing.

10. The pedestal assembly as recited in claim 1 wherein each of the inboard and outboard bearing assemblies further comprises a spherical bearing.

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

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

13. The pedestal assembly as recited in claim 1 wherein the inboard and outboard tip ribs are integral with the airframe.

14. A tiltrotor aircraft having a pylon assembly, a helicopter mode and an airplane mode, the tiltrotor aircraft comprising:
an airframe including a fuselage and a wing; and
a pedestal assembly disposed above the wing distal from the fuselage, the pedestal assembly including:
an inboard tip rib extending above the wing and defining an inboard slot;
an outboard tip rib extending above the wing and defining an outboard slot;
an inboard bearing cartridge received within the inboard slot and coupled to the inboard tip rib, the inboard bearing cartridge including an inboard bearing assembly; and
an outboard bearing cartridge received within the outboard slot and coupled to the outboard tip rib, the outboard bearing cartridge including an outboard bearing assembly;
wherein, the inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard tip ribs to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode.

15. The tiltrotor aircraft as recited in claim 14 wherein the inboard bearing cartridge has a close fitting relationship with the inboard slot and wherein the outboard bearing cartridge has a close fitting relationship with the outboard slot.

16. The tiltrotor aircraft as recited in claim 14 wherein each of the inboard and outboard tip ribs provides a stiff coupling with the pylon assembly to control dynamic modes between the pylon assembly and the airframe.

17. The tiltrotor aircraft as recited in claim 14 wherein each of the inboard and outboard bearing assemblies further comprises a journal bearing.

18. The tiltrotor aircraft as recited in claim 14 wherein each of the inboard and outboard bearing assemblies further comprises a spherical bearing.

19. The tiltrotor aircraft as recited in claim 14 wherein the inboard and outboard tip ribs support fore/aft loads when the tiltrotor aircraft is in the airplane mode and wherein the inboard and outboard tip ribs support vertical loads when the tiltrotor aircraft is in the helicopter mode.

20. The tiltrotor aircraft as recited in claim 14 wherein the inboard and outboard tip ribs are integral with the airframe.

Assignees

• Bell Helicopter Textron Inc

Inventors

• King James Elbert
• Williams Jeffrey Matthew
• Jackson Christopher R
• Baines Andrew G
• Kooiman James Everett

Classifications

• B64D27/12

  within, or attached to, wings · CPC title

• B64C3/32

  specially adapted for mounting power plant · CPC title

• F16C29/002

  Elastic or yielding linear bearings or bearing supports · CPC title

• F16H2057/02043

  for vehicle transmissions · CPC title

• F16H57/021

  Shaft support structures, e.g. partition walls, bearing eyes, casing walls or covers with bearings · CPC title