Controller

Patent metadata

Field	Value
Publication number	US-9791886-B2
Application number	US-201114116383-A
Country	US
Kind code	B2
Filing date	May 12, 2011
Priority date	May 12, 2011
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

A controller includes a first body portion, adapted to be grasped by a person's middle finger, ring finger, and pinky finger, a second body portion adapted to be grasped by a person's index finger, and a third body portion that defines a first surface adapted to receive a person's thumb. A finger switch is positioned on a front surface of the second body portion. The finger switch is positioned such that it may be actuated by the person's index finger. The second body portion is disposed between the first body portion and the third body portion. The second body portion defines an offset with respect to the first body portion. The third body portion defines a second surface above the finger switch, which may receive the person's index finger.

First claim

What is claimed is:

1. An aircraft controller, comprising:
a first body portion, adapted to be grasped by a person's middle finger, ring finger, and pinky finger;
a second body portion adapted to be grasped by a person's index finger; and
a third body portion defining a first surface adapted to receive a person's thumb; and
a finger switch positioned on a front surface of the second body portion, wherein the finger switch is positioned so as to be actuated by the person's index finger;
wherein the second body portion is disposed between the first body portion and the third body portion,
wherein the second body portion defines an offset with respect to the first body portion, wherein the third body portion defines a second surface above the finger switch, which is adapted to receive at least the person's index finger,
wherein the finger switch is configured to be actuated by movement in lateral directions with respect to a central axis of the controller,
wherein actuation of the finger switch in a first lateral direction actuates a radio transmit function, and
wherein actuation of the finger switch in a second lateral direction actuates an intercom function.

2. The aircraft controller of claim 1 , wherein the finger switch is at least one selected from a group comprising a toggle switch and a slide switch.

3. The aircraft controller of claim 1 , wherein the offset is selected from a group comprising at least axial, at least radial, and both axial and radial.

4. The aircraft controller of claim 1 , further comprising a base to which the first body portion connects, wherein the base comprises an essentially annular structure that flares outwardly from the first body portion.

5. The aircraft controller of claim 1 , further comprising at least one thumb switch disposed on the third body portion.

6. The aircraft controller of claim 5 , wherein the at least one thumb switch comprises a trim switch.

7. The aircraft controller of claim 6 , wherein the trim switch comprises two toggle switches, disposed side-by-side, that permit control of a trim of an aircraft.

8. The aircraft controller of claim 5 , wherein the at least one thumb switch comprises a push button autopilot release switch that actuates an autopilot priority function.

9. The aircraft controller of claim 1 , wherein the controller is adapted for use on an aircraft that is controlled by a fly-by-wire system that provides resistive feedback to the controller.

10. The aircraft controller of claim 9 , wherein the resistive feedback increases proportionately with a magnitude of an angular displacement of the controller from a rest position.

11. The aircraft controller of claim 9 , wherein the resistive feedback provided to the controller, when the controller is displaced from a rest position, exceeds about 20 pounds (89 Newtons) of force at a maximum.

12. The aircraft controller of claim 11 , wherein the resistive feedback is about 40 pounds (178 Newtons) of force at a maximum.

13. The aircraft controller of claim 1 , wherein the finger switch, being a lateral switch, discourages actuation when the controller is pulled by the person in a rearward direction from a rest position.

14. The aircraft controller of claim 1 , wherein the second surface on the third body portion permits the person to apply pressure thereto in a rearward direction by positioning at least the person's index finger there against.

Assignees

• Ouellette Benoit
• Bombardier Inc

Inventors

• Ouellette Benoit

Classifications

• G06F3/0338

  with detection of limited linear or angular displacement of an operating part of the device from a neutral position, e.g. isotonic or isometric joysticks · CPC title

• G05G13/00 Primary

  Manually-actuated control mechanisms provided with two or more controlling members and also two or more controlled members (interlocking G05G5/08) · CPC title

• G05G9/047 Primary

  the controlling member being movable by hand about orthogonal axes, e.g. joysticks {(for switches H01H25/04)} · CPC title

• B64C13/08

  Trimming zero positions · CPC title

• B64C13/0427

  for actuating trim · CPC title