Axial load capable torque tube assembly and manufacturing methods thereof

Patent metadata

Field	Value
Publication number	US-11912396-B2
Application number	US-202017075933-A
Country	US
Kind code	B2
Filing date	Oct 21, 2020
Priority date	Nov 15, 2019
Publication date	Feb 27, 2024
Grant date	Feb 27, 2024

Abstract

An assembly and a method for manufacturing an assembly for transmitting torque to an aircraft actuator. The assembly and method include a torque tube having a longitudinal axis and an end fitting. The ending fitting includes a connector portion and an engagement portion that is inserted into the torque tube. The engagement portion includes a first end adjacent the connector portion, a second end opposite the first end, and a coupling region between the first and second end that includes an outer coupling surface having an outer diameter and a continuous groove formed thereon. The continuous groove includes two axial grooves that extend along the outer coupling surface along the longitudinal axis and a first parallel groove that extends circumferentially about the longitudinal axis along the outer coupling surface that joins the two axial grooves.

First claim

What is claimed is:

1. An assembly for transmitting torque to an aircraft actuator comprising:
a torque tube having a longitudinal axis;
an end fitting comprising:
a connector portion; and
an engagement portion inserted into the torque tube,
wherein the engagement portion includes:
a first end adjacent the connector portion;
a second end opposite the first end; and
a coupling region between the first and second end that includes an outer coupling surface having an outer diameter and having a continuous groove formed thereon;
wherein the continuous groove includes two axial grooves that extend along outer coupling surface along the longitudinal axis and a first parallel groove that extends circumferentially about the longitudinal axis along the outer coupling surface and that joins the two axial grooves;
wherein the continuous groove further includes a third axial groove and a second parallel groove, the second parallel groove connecting one of the two axial grooves to the third axial groove;
wherein the first parallel groove is at the first end and the second parallel groove is at the second end.

2. The assembly of claim 1 , wherein the connector portion is connected to a power drive unit.

3. The assembly of claim 1 , wherein the parallel groove is at least one half the length of at least one of the two axial grooves.

4. The assembly of claim 1 , wherein a depth of the continuous groove is in a range of 0.05 mm to ½ the outer diameter of the coupling surface.

5. The assembly of claim 4 , wherein the continuous groove has a concave shape relative to the outer coupling surface.

6. The assembly of claim 5 , wherein the end fitting is formed of stainless steel.

7. The assembly of claim 6 , wherein the end fitting has the outer coupling surface is machined to form the continuous groove.

8. The assembly of claim 7 , wherein the end fitting includes an anti-corrosion surface treatment deposited thereon.

9. The assembly of claim 8 , wherein the torque tube includes aluminum.

10. The assembly of claim 1 , wherein the torque tube includes titanium.

11. The assembly of claim 10 , wherein the torque tube includes an anti-corrosion surface treatment deposited thereon.

12. A method for manufacturing an assembly for transmitting torque to an aircraft actuator, the method comprising:
forming an end fitting such that the fitting includes: a connector portion; an engagement portion; a first end adjacent the connector portion: a second end opposite the first end; and an outer coupling surface between the first and second end;
creating a continuous groove on the engagement portion such that it includes two axial grooves that extend along a longitudinal axis of the end fitting and a first parallel groove that extends circumferentially about the longitudinal axis and joins the two axial grooves, wherein the continuous groove further includes a third axial groove and a second parallel groove, the second parallel groove connecting one of the two axial grooves to the third axial groove and the first parallel groove is at the first end and the second parallel groove is at the second end;
inserting the second end of the end fitting into a torque tube; and
electromagnetically forming the torque tube to the outer coupling surface of the engagement portion.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Barger Victor
• Bielefeldt Joseph M
• Lai Jude C
• Karlen Eric W

Classifications

• B64C13/28 Primary

  mechanical · CPC title

• B21D39/04

  of tubes with tubes; of tubes with rods {(crimped pipe joints as such F16L13/14)} · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16D1/10

  Quick-acting couplings in which the parts are connected by simply bringing them together axially · CPC title

• F16D2001/103

  the torque is transmitted via splined connections · CPC title