Strain wave gearing system

Patent metadata

Field	Value
Publication number	US-12241536-B2
Application number	US-202318541177-A
Country	US
Kind code	B2
Filing date	Dec 15, 2023
Priority date	Dec 16, 2022
Publication date	Mar 4, 2025
Grant date	Mar 4, 2025

Abstract

A strain wave gearing system is includes: wave generator; a rigid spline; a flex spline disposed between the wave generator and the rigid spline; and a coupling element. The flex spline comprises a first mating element. The coupling element comprises a second mating element. The coupling element and the flex spline are mated by cooperation of the first mating element and the second mating element so as to prevent rotational motion of the flex spline relative to the coupling element. The first mating element is movable relative to the second mating element to thereby permit deformation of the flex spline relative to the coupling element.

First claim

The invention claimed is:

1. A strain wave gearing system comprising:
a wave generator;
a rigid spline;
a flex spline disposed between the wave generator and the rigid spline, the flex spline comprising a first mating element; and
a coupling element comprising a second mating element;
wherein the coupling element and the flex spline are mated by cooperation of the first mating element and the second mating element so as to prevent rotational motion of the flex spline relative to the coupling element; and
wherein the first mating element is movable relative to the second mating element to thereby permit deformation of the flex spline relative to the coupling element.

2. The strain wave gearing system of claim 1 , wherein the first mating element is adjacent the second mating element.

3. The strain wave gearing system of claim 1 , comprising a plurality of coupling elements mated with the flex spline in series.

4. The strain wave gearing system of claim 1 , wherein:
the flex spline comprises the first mating element at a first axial end of the flex spline;
the flex spline comprises a third mating element at an opposing second axial end of the flex spline; and
the strain wave gearing system comprises a second coupling element comprising a fourth mating element;
wherein the second coupling element and the flex spline are mated by cooperation of the third mating element and the fourth mating element of the second coupling element, so as to prevent rotational motion of the flex spline relative to the second coupling element.

5. The strain wave gearing system of claim 4 , wherein the flex spline is a first flex spline, and wherein the second coupling element is mated to a second flex spline.

6. The strain wave gearing system of claim 1 , wherein at least one of the first mating element and the second mating element comprises a friction reducing surface feature.

7. The strain wave gearing system of claim 1 , wherein:
the flex spline comprises a first plurality of mating elements, wherein each of the first plurality of mating elements comprises a tab; and
the coupling element comprises a second plurality of mating elements, wherein each of the second plurality of mating elements comprises a tab;
wherein the first plurality of tabs engages with the second plurality of tabs to thereby prevent rotational motion of the flex spline relative to the coupling element.

8. The strain wave gearing system of claim 1 , wherein:
one of the flex spline or the coupling element comprises a plurality of mating elements, wherein each of the plurality of mating elements comprises a tab; and
the other of the flex spline and the coupling element comprises a plurality of pins;
wherein the plurality of tabs engages with the plurality of pins to thereby prevent rotational motion of the flex spline relative to the coupling element.

9. The strain wave gearing system of claim 1 , wherein the average position of the first mating element over time relative to the second mating element is fixed.

10. The strain wave gearing system of claim 1 , comprising lubrication between the first mating element and the second mating element.

11. An aircraft comprising:
a strain wave gearing system of claim 1 , wherein the strain wave gearing system is operable to actuate a flight control surface.

12. The aircraft of claim 11 , wherein the flight control surface is a leading-edge flap.

13. The aircraft of claim 11 , wherein the coupling element is fixedly attached to the aircraft so as not to rotate relative thereto, and the rigid spline is engaged with an actuator for the flight control surface.

14. The aircraft of claim 11 , wherein the coupling element is engaged with an actuator for the flight control surface, and the rigid spline is fixedly attached to the aircraft so as not to rotate relative thereto.

15. A method of assembling a strain wave gearing system as claimed in claim 1 , the method comprising:
mating the first mating element and the second mating element to thereby mate the flex spline and the coupling element.

Assignees

• Goodrich Actuation Systems Ltd

Inventors

• Whitfield Neil Stuart Russell
• Timms Jack William

Classifications

• F16H2049/003

  Features of the flexsplines therefor · CPC title

• B64C13/34

  using toothed gearing · CPC title

• F16H57/04

  Features relating to lubrication or cooling {or heating} (control of lubrication or cooling in hydrostatic gearing F16H61/4165) · CPC title

• F16H49/001 Primary

  Wave gearings, e.g. harmonic drive transmissions · CPC title