Torque tube assemblies for use with aircraft high lift devices

Patent metadata

Field	Value
Publication number	US-9739316-B2
Application number	US-201514817643-A
Country	US
Kind code	B2
Filing date	Aug 4, 2015
Priority date	Aug 4, 2015
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

Example torque tube assemblies for use with aircraft high lift devices are described herein. An example apparatus includes a spline coupling having a first yoke, a sliding splined shaft having a second yoke and a torque tube having a first end and a second end opposite the first end. A first fitting with a third yoke is coupled to the first end of the torque tube, and a second fitting with a fourth yoke is coupled to the second end of the torque tube. The third yoke is coupled to the first yoke to form a first U-joint, and the fourth yoke is coupled to the second yoke to form a second U-joint. The spline coupling is to be coupled to a first high lift device drive shaft and the sliding splined shaft is to be coupled to a second high lift device drive shaft.

First claim

What is claimed is:

1. An aircraft apparatus comprising:
a first drive shaft of a first rotary actuator of a first high lift device in a wing of an aircraft;
a second drive shaft of a second rotary actuator of a second high lift device in the wing of the aircraft;
a spline coupling having a first yoke, the spline coupling fixedly coupled to the first drive shaft of the first rotary actuator;
a sliding splined shaft having a second yoke, the sliding splined shaft slidably coupled to the second drive shaft of the second rotary actuator such that sliding splined shaft is movable in an axial direction along the second drive shaft; and
a torque tube having a first end and a second end opposite the first end, a first fitting with a third yoke coupled to the first end of the torque tube, and a second fitting with a fourth yoke coupled to the second end of the torque tube, the third yoke of the first fitting coupled to the first yoke of the spline coupling to form a first U-joint, and the fourth yoke of the second fitting coupled to the second yoke of the sliding splined shaft to form a second U-joint.

2. The apparatus of claim 1 , wherein the first fitting is coupled to the first end of the torque tube via an electromagnetic forming (EMF) process and the second fitting is coupled to the second end of the torque tube via the EMF process.

3. The apparatus of claim 1 , wherein the spline coupling is to receive a spline gear coupled to the first drive shaft.

4. The apparatus of claim 3 , wherein the spline coupling includes an aperture to receive a threaded fastener to fixedly couple the spline coupling to the spline gear.

5. The apparatus of claim 1 , wherein the spline coupling includes a plate and an annular wall extending from the plate in a first direction, the first yoke extending from the plate in second direction opposite the first direction.

6. The apparatus of claim 5 , wherein the annular wall and the plate form an opening to receive a spline gear, an inner surface of the annular wall having splines.

7. The apparatus of claim 5 , wherein the spline coupling is a substantially unitary structure.

8. The apparatus of claim 1 , wherein the sliding splined shaft includes a sleeve defining an opening to receive the second drive shaft, the opening including splines.

Assignees

• Boeing Co

Inventors

• Schwartz Douglas John
• Meyer Mark Robert

Classifications

• F16D3/32 Primary

  by the provision of two intermediate members each having two relatively perpendicular trunnions or bearings · CPC title

• F16D1/108

  having retaining means rotating with the coupling and acting by interengaging parts, i.e. positive coupling · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16D1/072

  involving plastic deformation (plastic welding F16D1/068) · CPC title

• F16D2001/103

  the torque is transmitted via splined connections · CPC title