Aviation actuator assembly with mechanical fuse

Patent metadata

Field	Value
Publication number	US-10717518-B2
Application number	US-201815901773-A
Country	US
Kind code	B2
Filing date	Feb 21, 2018
Priority date	Feb 21, 2018
Publication date	Jul 21, 2020
Grant date	Jul 21, 2020

Abstract

An aviation actuator assembly for various aviation servo and/or autopilot applications can include an actuator having an output shaft and a mechanical fuse for joining to the output shaft and another rotating body. The mechanical fuse can include a fuse body having a first connection point for joining to the output shaft, a second connection point for joining to the rotating body, and at least one channel defined in the fuse body. The first connection point and the second connection point are configured to be disposed in a line generally parallel to a common axis of rotation of the output shaft and the rotating body. The fuse body has a generally flat cross-sectional profile along its length between the first connection point and the second connection point, and the channel extends generally perpendicular to the length of the fuse body and narrows the cross-sectional profile.

First claim

What is claimed is:

1. An aviation actuator assembly comprising:
an actuator having an output shaft;
a mechanical fuse joining the output shaft of the actuator and a rotating body to connect the output shaft and the rotating body together and impart a rotational force from the output shaft to the rotating body, the output shaft and the rotating body sharing a common axis of rotation, the mechanical fuse comprising:
a fuse body having a first connection point for joining to the output shaft and a second connection point for joining to the rotating body, the first connection point and the second connection point disposed in a line parallel to the common axis of rotation, and the first connection point and the second connection point each disposed at a radial distance from the common axis of rotation when joined to the output shaft and the second rotating body;
at least one channel defined in the fuse body, the fuse body having a rectangular cross-sectional profile along a length of the fuse body between the first connection point and the second connection point, the at least one channel extending perpendicular to the length of the fuse body and narrowing the cross-sectional profile at the channel, the fuse body circumferentially oriented with respect to rotation of the fuse body with the output shaft and the second rotating body to expose the fuse body to substantially constant shear stress along the cross-sectional profile; and
at least one notch oriented perpendicularly to the at least one channel.

2. The aviation actuator assembly as recited in claim 1 , wherein a first radial distance of the first connection point from the common axis of rotation and a second radial distance of the second connection point from the common axis of rotation are at least substantially the same.

3. The aviation actuator assembly as recited in claim 1 , wherein the mechanical fuse defines a second channel in the fuse body opposite the at least one channel.

4. The aviation actuator assembly as recited in claim 1 , wherein the at least one channel comprises a base defining a radius.

5. The aviation actuator assembly as recited in claim 1 , wherein the fuse body defines a second notch oriented perpendicularly to the at least one channel, the second notch opposite the at least one notch.

6. A mechanical fuse joining a first rotating body and a second rotating body to connect the first rotating body and the second rotating body together and impart a rotational force from one of the first rotating body and the second rotating body to the other of the first rotating body and the second rotating body, the first rotating body and the second rotating body sharing a common axis of rotation, the mechanical fuse comprising:
a fuse body having a first connection point for joining to the first rotating body and a second connection point for joining to the second rotating body, the first connection point and the second connection point disposed in a line parallel to the common axis of rotation, and the first connection point and the second connection point each disposed at a radial distance from the common axis of rotation when joined to the first rotating body and the second rotating body;
at least one channel defined in the fuse body, the fuse body having a rectangular cross-sectional profile along a length of the fuse body between the first connection point and the second connection point, the at least one channel extending perpendicular to the length of the fuse body and narrowing the cross-sectional profile at the channel, the fuse body circumferentially oriented with respect to rotation of the fuse body with the first rotating body and the second rotating body to expose the fuse body to substantially constant shear stress along the cross-sectional profile, wherein a first radial distance of the first connection point from the common axis of rotation and a second radial distance of the second connection point from the common axis of rotation are substantially the same; and
at least one notch oriented perpendicularly to the at least one channel.

7. The mechanical fuse as recited in claim 6 , further comprising a second channel in the fuse body opposite the at least one channel.

8. The mechanical fuse as recited in claim 6 , wherein the at least one channel comprises a base defining a radius.

9. The mechanical fuse as recited in claim 6 , wherein the fuse body defines a second notch oriented perpendicularly to the at least one channel, the second notch opposite the at least one notch.

10. A mechanical fuse joining a first rotating body and a second rotating body to connect the first rotating body and the second rotating body together and impart a rotational force from one of the first rotating body and the second rotating body to the other of the first rotating body and the second rotating body, the first rotating body and the second rotating body sharing a common axis of rotation, the mechanical fuse comprising:
a fuse body having a first connection point for joining to the first rotating body and a second connection point for joining to the second rotating body, the first connection point and the second connection point disposed in a line parallel to the common axis of rotation, and the first connection point and the second connection point each disposed at a radial distance from the common axis of rotation when joined to the first rotating body and the second rotating body;
at least one channel defined in the fuse body, the fuse body having a rectangular cross-sectional profile along a length of the fuse body between the first connection point and the second connection point, the at least one channel generally perpendicular to the length of the fuse body and narrowing the cross-sectional profile at the channel, the fuse body circumferentially oriented with respect to rotation of the fuse body with the first rotating body and the second rotating body to expose the fuse body to substantially constant shear stress along the cross-sectional profile; and
at least one notch oriented perpendicularly to the at least one channel.

11. The mechanical fuse as recited in claim 10 , wherein a first radial distance of the first connection point from the common axis of rotation and a second radial distance of the second connection point from the common axis of rotation are at least substantially the same.

12. The mechanical fuse as recited in claim 10 , further comprising a second channel in the fuse body opposite the at least one channel.

13. The mechanical fuse as recited in claim 10 , wherein the at least one channel comprises a base defining a radius.

14. The mechanical fuse as recited in claim 10 , wherein the fuse body defines a second notch oriented perpendicularly to the at least one channel, the second notch opposite the at least one notch.

Assignees

• Garmin Int Inc

Inventors

• Dinger Perry L

Classifications

• F16D9/06

  by breaking due to shear stress · CPC title

• B64C13/22

  readily revertible to personal control · CPC title

• B64C13/28 Primary

  mechanical · CPC title