Torque tube assemblies for use with aircraft high lift devices

Patent metadata

Field	Value
Publication number	US-11053983-B2
Application number	US-201815875820-A
Country	US
Kind code	B2
Filing date	Jan 19, 2018
Priority date	Jan 19, 2018
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

Example torque tube assemblies may be used with aircraft high lift devices. An example torque tube assembly includes a torque tube having a first end and a second end opposite the first end. A first fitting is coupled to the first end and a second fitting is coupled to the second end. The first fitting is to be coupled to a first high lift device of an aircraft. The second fitting has a spline section. The torque tube assembly also includes a sliding spline shaft having a channel and a first yoke. The second fitting is slidably received within the channel. The torque tube assembly further includes a spline coupling having a second yoke, which is coupled to the first yoke of the sliding spline shaft to form a U-joint. The spline coupling is to be coupled to a second high lift device of the aircraft.

First claim

What is claimed is:

1. A torque tube assembly comprising:
a torque tube having a first end and a second end opposite the first end, a first fitting coupled to the first end and a second fitting coupled to the second end, the first fitting to be coupled to a first high lift device of an aircraft, the second fitting having a spline section;
a sliding spline shaft having a channel, the second fitting slidably received within the channel, the sliding spline shaft including a grease port to enable grease to be injected into the channel, the sliding spline shaft having a first yoke; and
a spline coupling having a second yoke, the second yoke of the spline coupling coupled to the first yoke of the sliding spline shaft to form a U-joint, the spline coupling having an annular wall with splines around a surface of the annular wall, the spline coupling to be coupled to a second high lift device of the aircraft.

2. The torque tube assembly of claim 1 , further including a retaining bolt extending into the channel, the retaining bolt to prevent the second fitting from sliding beyond a threshold distance into or out of the channel of the sliding spline shaft.

3. The torque tube assembly of claim 2 , wherein the spline section is a first spline section, the second fitting further including a second spline section spaced apart from the first spline section, the retaining bolt extending into the channel between the first and second spline sections.

4. The torque tube assembly of claim 1 , further including a grease retainer coupled to the sliding spline shaft and covering an opening of the channel to maintain the grease in the channel of the sliding spline shaft.

5. The torque tube assembly of claim 4 , wherein the grease retainer includes a first part and a second part, each of the first part and the second part including a tab and a slot that is to mate with the corresponding tab and slot of the other one of the first part or the second part.

6. The torque tube assembly of claim 4 , further including a seal between the grease retainer and the second fitting.

7. The torque tube assembly of claim 1 , wherein the sliding spline shaft includes a grease release port.

8. The torque tube assembly of claim 1 , wherein the spline coupling is a first spline coupling, the U-joint is a first U-joint, and the first fitting on the torque tube has a third yoke, and further including a second spline coupling with a fourth yoke, the fourth yoke of the second spline coupling coupled to the third yoke of the first fitting to form a second U-joint, the second spline coupling to be coupled to the first high lift device of the aircraft.

9. The torque tube assembly of claim 1 , wherein the channel in the sliding spline shaft extends between a first opening in the sliding spline shaft and a second opening in the sliding spline shaft, the second fitting extending into the channel through the first opening.

10. The torque tube assembly of claim 9 , further including a plug in the second opening to prevent the grease from escaping from the second opening.

11. A torque tube assembly comprising:
a torque tube having a first end and a second end opposite the first end, a first fitting coupled to the first end and a second fitting coupled to the second end, the first fitting to be coupled to a first high lift device of an aircraft, the second fitting having a spline section;
a sliding spline shaft having a channel, the second fitting slidably received within the channel, the sliding spline shaft having a first yoke;
a first spline coupling having a second yoke, the second yoke of the first spline coupling coupled to the first yoke of the sliding spline shaft to form a first U-joint, the first spline coupling having an annular wall with splines around a surface of the annular wall, the first spline coupling to be coupled to a second high lift device of the aircraft, wherein the first fitting on the torque tube has a third yoke; and
a second spline coupling with a fourth yoke, the fourth yoke of the second spline coupling coupled to the third yoke of the first fitting to form a second U-joint, the second spline coupling to be coupled to the first high lift device of the aircraft, wherein the first and second spline couplings include apertures to receive threaded fasteners to fixedly couple the first and second spline couplings to drive shafts of the first and second high lift devices, respectively.

12. A torque tube assembly comprising:
a torque tube having a first end and a second end opposite the first end, a first fitting coupled to the first end and a second fitting coupled to the second end, the first fitting to be coupled to a first high lift device of an aircraft, the second fitting having a spline section;
a sliding spline shaft having a channel, the second fitting slidably received within the channel, the sliding spline shaft having a first yoke;
a retaining bolt extending into the channel, the retaining bolt to prevent the second fitting from sliding beyond a threshold distance into or out of the channel of the sliding spline shaft, wherein the second fitting and the sliding spline shaft are axially slidable relative to each other while the retaining bolt is in the channel; and
a spline coupling having a second yoke, the second yoke of the spline coupling coupled to the first yoke of the sliding spline shaft to form a U-joint, the spline coupling having an annular wall with splines around a surface of the annular wall, the spline coupling to be coupled to a second high lift device of the aircraft.

13. A torque tube assembly comprising:
a torque tube having a first end and a second end opposite the first end, a first fitting coupled to the first end and a second fitting coupled to the second end, the first fitting to be coupled to a first high lift device of an aircraft, the second fitting having a first spline section and a second spline section spaced apart from the first spline section;
a sliding spline shaft having a channel, the second fitting slidably received within the channel, the sliding spline shaft having a first yoke;
a retaining bolt extending into the channel between the first and second spline sections, the first and second spline sections spaced from each other by a distance that is greater than a width of the retaining bolt, the retaining bolt to prevent the second fitting from sliding beyond a threshold distance into or out of the channel of the sliding spline shaft; and
a spline coupling having a second yoke, the second yoke of the spline coupling coupled to the first yoke of the sliding spline shaft to form a U-joint, the spline coupling having an annular wall with splines around a surface of the annular wall, the spline coupling to be coupled to a second high lift device of the aircraft.

14. A method comprising:
coupling a first fitting to a first end of a torque tube and a second fitting to a second end of the torque tube opposite the first end of the torque tube, the first fitting having a first yoke, the second fitting having a radially extending spline section;
coupling the first yoke to a second yoke of a first spline coupling to form a first U-joint;
inserting the spline section of the second fitting into a channel of a sliding spline shaft such that the second fitting is slidably received within the channel, the sliding spline shaft including a grease port to enable grease to be injected into the channel, the sliding spline shaft having a third yoke;
coupling the third yoke to a fourth yoke of a second spline coupling to form a second U-joint, the second spline coupling having an annular wall with splines around a surface of the annular wal

Assignees

• Boeing Co

Inventors

• Meyer Mark R
• Gregson Tyler S

Classifications

• F16D3/848

  allowing relative movement of joint parts due to sliding between parts of the cover · CPC title

• F16D3/387

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

• F16D2001/103

  the torque is transmitted via splined connections · CPC title

• B64C9/26

  by multiple flaps · CPC title

• B64C13/34

  using toothed gearing · CPC title