Electrically powered downlock actuation system

Patent metadata

Field	Value
Publication number	US-10086928-B2
Application number	US-201615224096-A
Country	US
Kind code	B2
Filing date	Jul 29, 2016
Priority date	Jul 29, 2016
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

A downlock actuator may comprise an electric motor, a gearbox coupled to the electric motor, the gearbox comprising a rotary output shaft, and a connecting output shaft having a first end and a second end, the first end being coupled to the rotary output shaft of the gearbox, wherein the connecting output shaft is configured to rotate between a shaft locked position and a shaft unlocked position, wherein the gearbox is back-drivable in response to the connecting output shaft being in the shaft unlocked position.

First claim

What is claimed is:

1. A lock linkage system of a landing gear system, the lock linkage system comprising:
a lockable assembly comprising:
an upper brace defining a longitudinal axis;
a lower brace coupled to the upper brace; and
a linkage coupled to the upper brace and the lower brace, the linkage being configured to allow movement of the upper brace and the lower brace relative to one another between unlocked and locked positions; and

a downlock actuator comprising:
an electric motor coupled to the upper brace;
a gearbox coupled to the electric motor; and
a connecting output shaft having a first end and a second end, the first end coupled to a rotary output shaft of the gearbox, wherein the connecting output shaft is configured to rotate between a shaft locked position and a shaft unlocked position,
wherein the gearbox is back-drivable in response to the connecting output shaft being in the shaft unlocked position,
wherein, the downlock actuator is configured to toggle the linkage, the upper brace, and the lower brace between the unlocked and locked positions.

2. The lock linkage system of claim 1 , further comprising a link rod having a proximal end coupled to the second end of the connecting output shaft and a distal end coupled to the lockable assembly.

3. The lock linkage system of claim 2 , wherein the proximal end of the link rod is pivotally coupled to the second end of the connecting output shaft.

4. The lock linkage system of claim 2 , wherein the rotary output shaft is positioned substantially perpendicular to a longitudinal axis of the link rod.

5. The lock linkage system of claim 2 , wherein the link rod is mounted for longitudinal translation relative to the longitudinal axis of the upper brace and rotation relative to the connecting output shaft whereby the proximal end of the link rod moves away from the upper brace and the distal end of the link rod moves toward the upper brace to unlock the upper brace and the lower brace from a locked position to an unlocked position.

6. The lock linkage system of claim 1 , wherein the linkage comprises an upper lock link pivotally coupled to a lower lock link, wherein the upper lock link is coupled to the upper brace and the lower lock link is coupled to the lower brace.

7. The lock linkage system of claim 1 , further comprising an output shaft position sensor proximate the connecting output shaft, wherein output shaft position sensor is configured to detect a position of the connecting output shaft.

8. The lock linkage system of claim 1 , wherein the electric motor is controllable to produce a desired angular range of motion of the connecting output shaft between the shaft locked position and the shaft unlocked position.

9. The lock linkage system of claim 1 , wherein the gearbox is fixedly coupled to the electric motor, the rotary output shaft is fixedly coupled to the gearbox, and the connecting output shaft is fixedly coupled to the rotary output shaft.

10. A downlock actuator for a landing gear system, the downlock actuator comprising:
an electric motor;
a gearbox coupled to the electric motor, the gearbox comprising a rotary output shaft; and
a connecting output shaft having a first end and a second end, the first end being coupled to the rotary output shaft of the gearbox, wherein the connecting output shaft is configured to rotate between a shaft locked position and a shaft unlocked position,
wherein the gearbox is back-drivable in response to the connecting output shaft being in at least one of an intermediate unlocked position or the shaft unlocked position, wherein the intermediate unlocked position is between the shaft locked position and the shaft unlocked position.

11. The downlock actuator of claim 10 , further comprising a link rod having a proximal end coupled to the second end of the connecting output shaft and a distal end coupled to a lockable assembly which includes a linkage, an upper brace, and a lower brace, and wherein, the connecting output shaft and the link rod are configured to toggle the linkage, the upper brace, and the lower brace between unlocked and locked positions.

12. The downlock actuator of claim 11 , wherein a longitudinal axis of the link rod is substantially perpendicular to a rotational axis of the connecting output shaft.

13. The downlock actuator of claim 10 , further comprising an output shaft position sensor proximate to the connecting output shaft configured to detect a position of the connecting output shaft.

14. The downlock actuator of claim 10 , wherein the electric motor is controllable to produce a desired angular range of motion of the connecting output shaft between the shaft locked position and the shaft unlocked position.

15. The downlock actuator of claim 10 , wherein the gearbox is fixedly coupled to the electric motor, the rotary output shaft is fixedly coupled to the gearbox, and the connecting output shaft is fixedly coupled to the rotary output shaft.

16. A method of positioning an upper brace and a lower brace of an aircraft landing gear system in a desired relationship with one another, comprising:
rotating an electric motor in a desired rotational direction;
rotating a rotary output shaft of a back-drivable gearbox coupled to the electric motor;
rotating a connecting output shaft through a desired angular range between a shaft locked position and a shaft unlocked position, wherein the connecting output shaft comprises a first end coupled to the rotary output shaft and a second end;
translating a link rod, comprising a proximal end coupled to the second end of the connecting output shaft and a distal end, in a first longitudinal direction along a longitudinal axis defined by the link rod, wherein the distal end is coupled to a lockable assembly comprising a linkage, the upper brace, and the lower brace, and back-driving the back-drivable gearbox, while the connecting output shaft is in at least one of an intermediate unlocked position or the shaft unlocked position, in response to the link rod moving in at least one of the first longitudinal direction or a second longitudinal direction along the longitudinal axis, wherein the second longitudinal direction is opposite the first longitudinal direction,
wherein, the linkage, the upper brace, and the lower brace are configured to lock the upper brace and the lower brace in the desired relationship depending on a position of the linkage.

17. The method of claim 16 , further comprising controlling the electric motor using motor control electronics, wherein the controlling includes limiting the desired angular range of the connecting output shaft between the shaft locked position and the shaft unlocked position.

18. The method of claim 16 , further comprising detecting a shaft position of the connecting output shaft with an output shaft position sensor located proximate the connecting output shaft.

19. The method of claim 18 , wherein the translating the link rod comprises at least one of translating the link rod from the shaft locked position and stopping at the shaft unlocked position in response to the output shaft position sensor detecting the connecting output shaft arriving at the shaft unlocked position, or translating the link rod from the shaft unlocked position and stopping at the shaft locked position in response to the output shaft position sensor detecting the connecting output shaft arriving at the shaft locked position.

Assignees

• Goodrich Corp

Inventors

• Ditzler Adam J

Classifications

• B64C25/26

  Control or locking systems therefor · CPC title

• B64C25/20 Primary

  mechanical · CPC title