Apparatus and methods for rigging a torque tube assembly in an aircraft

Patent metadata

Field	Value
Publication number	US-11060566-B2
Application number	US-201815941859-A
Country	US
Kind code	B2
Filing date	Mar 30, 2018
Priority date	Jan 19, 2018
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A torque tube assembly includes a torque tube and a spline coupling coupled to an end of the torque tube. The spline coupling has an opening to receive a spline gear on a drive shaft of an aircraft high lift device. The torque tube assembly also includes a retainer coupled to the spline coupling. The retainer blocks at least a portion of the opening in the spline coupling to prevent the spline coupling from being moved off of the spline gear on the drive shaft.

First claim

What is claimed is:

1. A torque tube assembly, comprising:
a torque tube;
a spline coupling, coupled to an end of the torque tube, wherein the spline coupling comprises an opening to receive a spline gear on a drive shaft of an aircraft high lift device, and wherein the opening is formed in an end of the spline coupling;
a retainer, coupled to the spline coupling, wherein the retainer comprises a ring portion, coupled to an outer surface of the spline coupling at or near the end of the spline coupling, and wherein the retainer blocks at least a portion of the opening in the spline coupling so that the spline coupling is prevented from moving off the spline gear on the drive shaft; and
threaded fasteners, extending through the ring portion of the retainer and into the outer surface of the spline coupling, so that the retainer is coupled to the spline coupling.

2. The torque tube assembly of claim 1 , wherein the retainer comprises a shoulder portion, extending radially inward from the ring portion and covering at least a portion of the opening in the spline coupling.

3. The torque tube assembly of claim 2 , wherein:
the shoulder portion comprises an opening, and
a diameter of the opening in the shoulder portion is smaller than a diameter of the opening in the spline coupling.

4. The torque tube assembly of claim 1 , wherein the threaded fasteners do not extend into the opening in the spline coupling.

5. The torque tube assembly of claim 1 , further comprising a first torque tube fitting, coupled to the end of the torque tube,
wherein:
the first torque tube fitting comprises a first yoke,
the spline coupling further comprises a second yoke, and
the first yoke of the first torque tube fitting is coupled to the second yoke of the spline coupling, such that the first yoke and the second yoke form a U-joint.

6. A method of rigging the torque tube assembly of claim 1 in an aircraft, the method comprising steps of:
coupling the spline gear to the drive shaft of the aircraft high lift device; and
sliding the spline coupling onto the spline gear on the drive shaft such that the spline gear is disposed within the opening in the spline coupling.

7. The method of claim 6 , further comprising, prior to the step of coupling the spline gear to the drive shaft, placing the retainer onto the drive shaft.

8. The method of claim 6 , wherein the step of coupling the spline gear to the drive shaft comprises sliding the spline gear onto a spline section on the drive shaft and coupling a retaining nut to the drive shaft.

9. The method of claim 6 , further including inserting the threaded fasteners into corresponding holes, extending through the retainer and into the spline coupling.

10. An aircraft, comprising:
the torque tube assembly of claim 1 ;
a geared rotary actuator (GRA), coupled to a wing of the aircraft,
the GRA comprising the drive shaft; and
the spline gear, coupled to the drive shaft, wherein the spline gear is located in the opening of the spline coupling.

11. The aircraft of claim 10 , wherein the spline gear does not have threaded holes to receive the threaded fasteners.

12. The aircraft of claim 10 , wherein the spline gear comprises an inner splined opening, configured to mate with a spline section on the drive shaft.

13. The aircraft of claim 10 , further comprising a retaining nut, coupled to the drive shaft, wherein the spline gear is captured between the retaining nut and a step in the drive shaft.

14. The aircraft of claim 10 , wherein:
the retainer comprises a shoulder portion, comprising an opening, and
a diameter of the opening in the shoulder portion is smaller than an outer diameter of the spline gear.

15. The aircraft of claim 10 , wherein:
the spline gear comprises a groove, formed circumferentially around the spline gear, and
the groove provides space for the threaded fasteners, extending into the opening in the spline coupling.

16. A torque tube assembly, comprising:
a torque tube;
a first torque tube fitting, coupled to a first end of the torque tube, wherein the first torque tube fitting comprises a first yoke;
a first spline coupling, comprising a second yoke, wherein the first yoke of the first torque tube fitting is coupled to the second yoke of the first spline coupling, such that the first yoke and the second yoke form a first U-joint, and wherein the first spline coupling comprises an opening to receive a first spline gear, located on a first drive shaft of a first aircraft high lift device and having an outer diameter;
a retainer, coupled to the first spline coupling, wherein the retainer blocks at least a portion of the opening in the first spline coupling so that the first spline coupling is prevented from moving off the first spline gear, located on the first drive shaft;
a second torque tube fitting, coupled to a second end of the torque tube, wherein the second torque tube fitting comprises a spline section;
a sliding spline shaft, comprising a channel, wherein the second torque tube fitting is slidably received within the channel, and wherein the sliding spline shaft comprises a third yoke; and
a second spline coupling, comprising a fourth yoke,
wherein:
the fourth yoke of the second spline coupling is coupled to the third yoke of the sliding spline shaft, such that the third yoke and the fourth yoke form a second U-joint, and
the second spline coupling is configured to be coupled to a second spline gear on a second drive shaft of a second aircraft high lift device.

17. The torque tube assembly of claim 16 , wherein:
the retainer is a first retainer,
the torque tube assembly further comprises a second retainer, coupled to the second spline coupling, and
the second retainer blocks at least a portion of an opening in the second spline coupling so that the second spline coupling is prevented from moving off the second spline gear on the second drive shaft.

18. The torque tube assembly of claim 16 , further comprising a retaining bolt, extending into the channel, wherein the retaining bolt is configured to prevent the second torque tube fitting from sliding beyond a threshold distance into or out of the channel of the sliding spline shaft.

19. The torque tube assembly of claim 16 , wherein the retainer comprises:
a ring portion, coupled to an outer surface of the first spline coupling at or near an end of the first spline coupling, wherein the opening in the first spline coupling is formed in the end of the first spline coupling; and
a shoulder portion, extending radially inward from the ring portion and covering at least a portion of the opening in the first spline coupling, wherein the shoulder portion comprises an opening, and wherein a diameter of the opening in the shoulder portion is smaller than the outer diameter of the first spline gear.

20. The torque tube assembly of claim 19 , further comprising threaded fasteners, extending through the ring portion of the retainer and into the outer surface of the first spline coupling, so that the retainer is coupled to the first spline coupling.

Assignees

• Boeing Co

Inventors

• Meyer Mark
• Popov Maxim

Classifications

• F16D2300/06

  Lubrication details not provided for in group F16D13/74 · CPC title

• B64C13/28

  mechanical · CPC title

• B64C9/16

  at the rear of the wing · CPC title

• F16D1/06

  for attachment of a member on a shaft or on a shaft-end (attachment of marine propellers on shafts B63H23/34) · CPC title

• F16D3/387 Primary

  Fork construction; Mounting of fork on shaft; Adapting shaft for mounting of fork · CPC title