Centrifugal force enabled clutch and aircraft

Patent metadata

Field	Value
Publication number	US-12281679-B2
Application number	US-202318353664-A
Country	US
Kind code	B2
Filing date	Jul 17, 2023
Priority date	Jul 17, 2023
Publication date	Apr 22, 2025
Grant date	Apr 22, 2025

Abstract

A clutch having an inner ring, an outer ring, a plurality of sprags positioned between the inner ring and the outer ring, and a spring biasing each of the plurality of sprags towards the outer ring. Each of the plurality of sprags are movable between a disengaged position spaced from the inner ring and an engaged position contacting both the inner ring and the outer ring to rotationally unitize the inner ring and the outer ring.

First claim

What is claimed is:

1. A clutch comprising:
an inner ring;
an outer ring;
a plurality of sprags positioned between the inner ring and the outer ring; and
a spring biasing each of the plurality of sprags towards the outer ring;
wherein, according to the rotation of the outer ring and the bias of the spring, each of the plurality of sprags are movable between a disengaged position in which the sprags are spaced from the inner ring and the outer ring does not rotate with the inner ring, and an engaged position in which the sprags overcome the bias of the spring and the sprags contact both the inner ring and the outer ring such that the inner ring and the outer ring are rotationally unitized.

2. The clutch of claim 1 , wherein each of the plurality of sprags includes an outer elongated corner in contact with the outer ring and a center of gravity offset from the outer elongated corner, the offset center of gravity being configured to return each of the plurality of sprags to the disengaged position.

3. The clutch of claim 2 , wherein each of the plurality of sprags includes a contact surface having cross-sectional profile, the cross-sectional profile and an amount of offset of the center of gravity being selected such that each of the plurality of sprags are transitioned between the disengaged position and the engaged position upon a threshold difference of rotational speed between the inner ring and the outer ring.

4. The clutch of claim 3 , wherein the threshold difference of rotational speed is equal to between 15 percent and 20 percent.

5. The clutch of claim 1 , wherein the plurality of sprags are movable to the engaged position upon rotation of the outer ring in a first rotational direction.

6. The clutch of claim 1 , wherein in the disengaged position, a gap extends between the plurality of sprags and the inner ring.

7. The clutch of claim 1 , wherein in the disengaged position, the inner ring is rotatable in either a first rotational direction or an opposite second rotational direction relative to the outer ring.

8. The clutch of claim 1 , wherein the outer ring is rotated along a first rotational direction to move the plurality of sprags from the disengaged position to the engaged position.

9. The clutch of claim 1 , wherein once in the engaged position, rotation of the inner ring in the first rotational direction causes rotation of the outer ring in the first rotational direction.

10. A centrifugal force enabled clutch comprising:
an inner ring;
an outer ring;
a plurality of sprags positioned between the inner ring and the outer ring; and
a spring biasing each of the plurality of sprags towards the outer ring;
wherein each of the plurality of sprags includes an inner elongated corner adjacent the inner ring, an outer elongated corner in contact with the outer ring, and a center of gravity offset from the outer elongated corner;
wherein each of the plurality of sprags are movable between a disengaged position, with the inner elongated corner spaced from the inner ring, and an engaged position, with the inner elongated corner contacting the inner ring and the outer elongated corner contacting the outer ring such that in the engaged position, the plurality of sprags rotationally unitize the inner ring and the outer ring.

11. The centrifugal force enabled clutch of claim 10 , wherein the plurality of sprags are movable to the engaged position upon rotation of the outer ring in a first rotational direction.

12. The centrifugal force enabled clutch of claim 10 , wherein the offset center of gravity of each of the plurality of sprags is configured to return each of the plurality of sprags to the disengaged position.

13. The centrifugal force enabled clutch of claim 10 , wherein each of the plurality of sprags includes a contact surface having cross-sectional profile, the cross-sectional profile and an amount of offset of the center of gravity being selected such that each of the plurality of sprags are transitioned between the disengaged position and the engaged position upon a threshold difference of rotational speed between the inner ring and the outer ring.

14. The centrifugal force enabled clutch of claim 13 , wherein the threshold difference of rotational speed is between 15 percent and 20 percent.

Assignees

• Lockheed Corp

Inventors

• Gmirya Yuriy

Classifications

• F16D41/076

  the wedging coupling members being non-releasably joined to form a single annular piece, e.g. either the members being integral projections from the piece, or the piece being an elastic ring cast round the radial centres of the members · CPC title

• F16D45/00

  Freewheels or freewheel clutches combined with automatic clutches · CPC title

• F16D2043/145

  the centrifugal masses being pivoting · CPC title

• B64C27/06

  with single rotor · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title