Aircraft flight control column device with force-feedback having an emergency group

Patent metadata

Field	Value
Publication number	US-10279897-B2
Application number	US-201515509739-A
Country	US
Kind code	B2
Filing date	Sep 9, 2015
Priority date	Sep 9, 2014
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

The invention relates to an aircraft flight control column device (1) comprising: a casing (2) for attaching to an aircraft structure; an output shaft (3) for connecting to a flight control column (56), the output shaft (3) being mounted such that it rotates in relation to the casing (2); a primary group (4) comprising a first torque-generating body (7, 8) for applying a first torque to the output shaft (3); a secondary group (5) comprising a second torque-generating body (7, 8) for applying a second torque to the output shaft (3); and a clutch for selectively connecting the primary group (4) and the secondary group (5) to the output shaft (3).

First claim

The invention claimed is:

1. An aircraft flight control stick device, comprising:
a casing intended to be attached to a structure of the aircraft,
an output shaft intended to be connected to a flight control stick, the output shaft being mounted movable in rotation with respect to the casing,
a primary path comprising a first torque-generating member capable of exerting a first torque on the output shaft,
a secondary path comprising a second torque-generating member capable of exerting a second torque on the output shaft, and
a clutch capable of selectively connecting the primary path and the secondary path to the output shaft.

2. The device according to claim 1 , wherein the clutch comprises a clutch part movable with respect to the casing between a first position in which the clutch part is engaged with the primary path and a second position in which the clutch part is engaged with the secondary path.

3. The device according to claim 2 , wherein the clutch comprises an electromagnet which, when it is energized, biases the clutch part toward the first position.

4. The device according to claim 2 , wherein the clutch comprises an elastic return member capable of biasing the clutch part toward the second position.

5. The device according to claim 2 , wherein the clutch part is movable in translation with respect to the casing.

6. The device according to claim 5 , wherein the output shaft is movable in rotation with respect to the casing along an axis of rotation, and the clutch part is movable in translation with respect to the casing parallel to the axis of rotation of the output shaft.

7. The device according to claim 2 , wherein the clutch part is mounted secured in rotation to the output shaft while being movable in translation with respect to the output shaft.

8. The device according to claim 2 , comprising a flexible membrane by means of which the output shaft is connected to the clutch part.

9. The device according to claim 1 , wherein the first torque-generating member comprises at least one electric motor.

10. The device according to claim 9 , wherein the primary path comprises a reduction gear through which the electric motor exerts the first torque on the output shaft.

11. The device according to claim 1 , wherein the second torque-generating member is a friction system.

12. The device according to claim 11 , wherein the friction system comprises a drum and a cable in contact with the drum, the second torque being generated by friction between the cable and the drum when the drum is driven in rotation with respect to the cable.

13. The device according to claim 12 , wherein the cable is attached to the casing and the drum is rotationally mounted with respect to the casing.

14. The device according to claim 12 , wherein the second torque-generating member comprises an elastic element connecting the cable to the casing.

15. The device according to claim 1 , comprising at least one position sensor capable of measuring an angular position of the output shaft and an electronic control unit capable of controlling the first torque-generating member depending on the measured angular position.

16. The device according to claim 1 , wherein the flight control stick is a helicopter collective stick.

Assignees

• Safran Electronics & Defense

Inventors

• Cremiere Benoit

Classifications

• F16D21/02

  for interconnecting three or more shafts or other transmission members in different ways (in endless-track vehicles B62D) · CPC title

• B64C13/46

  with artificial feel · CPC title

• B64C27/56 Primary

  characterised by the control initiating means, e.g. manually actuated · CPC title

• B64C13/10

  comprising warning devices · CPC title

• F16D27/108

  with axially movable clutching members · CPC title