Indirect Drive Active Control Column

• US 20120025030A1
• Filed: 07/28/2010
• Published: 02/02/2012
• Est. Priority Date: 07/28/2010
• Status: Active Grant

• Current Assignee: Woodward MPC, Inc.
• Original Assignee: Woodward MPC, Inc.
• Inventors: Stachniak, Darryl S., Rusak, Thomas M., Dyra, Brian P.
• Granted Patent: US 9,051,045 B2
• Time in Patent Office: Days
• US Class Current: 244/223
• CPC Class Codes: B64C 13/0421 control sticks for primary flight controls
• CPC Class Codes: B64C 13/503 Fly-by-Wire
• CPC Class Codes: G05G 11/00 Manually-actuated control mechanisms provided with two or more controlling members co-operating with one single controlled member
• CPC Class Codes: G05G 5/03 Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce arrangements for indicating the position of the controlling member G05G1/015

Abstract

An indirect drive active control column for an aircraft control system is provided. The indirect drive active control column provides both active and passive feedback to the control stick. The passive feedback relates to adjustments of the control stick relative to a feedback neutral position. The active feedback actively adjusts the position of the feedback neutral position to adjust a feedback profile of the passive feedback.

Claims

1. An indirect drive active control column comprising:

a stick moveable relative to a mechanical ground;

a passive feedback arrangement movable relative to the mechanical ground, the passive feedback arrangement directly acting on the stick providing a passive feedback force profile to the stick when the stick is moved relative to the passive feedback arrangement;

an actuator coupled to the passive feedback arrangement for actively adjusting the position of the passive feedback arrangement relative to the mechanical ground.

2. The indirect drive active control column of claim 1, wherein the passive feedback assembly includes a cam including a cam surface and a resistance arrangement, the cam surface defining a feedback neutral position, the stick includes a cam follower following the cam surface, wherein the resistance arrangement increasingly biases the cam surface to resists movement of the cam follower from the feedback neutral position to provide the passive tactile feedback.

3. The indirect drive active control column of claim 2, wherein the resistance arrangement is provided by a spring and damper arrangement.

4. The indirect drive active control column of claim 3, wherein the cam surface is generally V-shaped with the cam follower positioned within the V-shape of the first cam surface, wherein the feedback neutral position is when the cam follower contacts both sides of the V-shaped surface.

5. The indirect drive active control column of claim 2, wherein the passive feedback assembly includes a gimbal arrangement that carries the cam surface and the resistance arrangement, the actuator coupled to the gimbal arrangement and configured to adjust the position of the gimbal arrangement relative to mechanical ground to adjust the position of the passive feedback assembly relative to mechanical ground.

6. The indirect drive active control column of claim 5, wherein the gimbal arrangement and the stick are pivotally affixed to the mechanical ground for pivotal movement about a common first axis.

7. The indirect drive active control column of claim 6, wherein the first actuator is a linear actuator pivotally coupled to the gimbal arrangement for relative pivotal movement therebetween about a second axis and the actuator is pivotally coupled to the mechanical ground for movement about a third axis offset from the first and second axes.

8. The indirect drive active control column of claim 1, wherein the passive feedback arrangement is operably coupled between the stick and the actuator such that any failure of the actuator does not completely prevent movement of the stick relative to the mechanical ground and the feedback assembly.

9. The indirect drive active control column of claim 1, wherein the passive feedback assembly includes at least one biasing member, the biasing member is interposed between the actuator and the stick.

10. The indirect drive active control column of claim 9, wherein, absent an external load being applied to the stick, the biasing member does not oppose actively adjusting the position of the passive feedback arrangement relative to mechanical ground by the actuator.

11. The indirect drive active control column of claim 10, wherein the biasing member is a fluidic damper.

12. The indirect drive active control column of claim 5, wherein the gimbal arrangement and cam having the cam surface are pivotally coupled to one another.

13. The indirect drive active control column of claim 12, wherein the resistance arrangement is laterally offset from the pivotal coupling between the gimbal arrangement and the cam.

14. The indirect drive active control column of claim 1, wherein the stick is movable relative to the mechanical ground in at least two dimensions, one dimension representing pitch and another dimension representing roll.

15. An aircraft control system comprising:

a stick movably coupled to a mechanical ground, and

a feedback arrangement providing a passive feedback profile for the stick relative to the mechanical ground, at least a portion of the feedback arrangement being movable relative to the mechanical ground and the stick for adjusting the feedback profile relative to the mechanical ground.

16. The air craft control system of claim 15, further comprising:

an actuator coupled to the passive feedback arrangement for adjusting the position of the passive feedback arrangement relative to the mechanical ground for adjusting the feedback profile.

17. The aircraft control system of claim 16, wherein the feedback arrangement includes a dampening member, the dampening member not working against the actuator when the actuator adjusts the position of the passive feedback arrangement relative to the mechanical ground.

18. A method of providing feedback to a control stick of an aircraft control system comprising the steps of:

passively biasing the control stick when the control stick is transitioned from a feedback neutral position; and

actively adjusting the feedback neutral position relative to a mechanical ground so as to adjust a passive feedback profile relative to the mechanical ground.

19. The method of claim 18, wherein the step of passively biasing the control stick is performed by a passive feedback arrangement and wherein the step of passively biasing the control stick includes dampening biasing of the stick as the stick is transitioned from the feedback neutral position relative to the passive feedback arrangement.

20. The method of claim 19, wherein dampening is independent of relative movement between the mechanical ground and the control stick.