System for remote interaction with a pointing means of an aircraft cockpit display system
A system for remote interaction with a pointing means of an aircraft cockpit display system, equipped with HMIs, includes three layers: a lower layer configured so as to receive wired electric power supply and data exchange connections; an upper layer comprising a hand-rest knob, at least one physical interaction means configured so as to interact on the pointing means for pointing at the HMIs of the cockpit, and a module with a touch-sensitive flat surface configured so as to interact on the pointing device for pointing at the HMIs of the cockpit and arranged in the extension of the hand-rest knob; and an intermediate layer configured so as to make it possible to modify the position of the upper layer.
1. A system for remote interaction with a pointing means of an aircraft cockpit display system equipped with HMIs, comprising three layers:
a lower layer configured so as to receive wired electric power supply and data exchange connections;
an upper layer comprising a hand-rest knob, at least one physical interaction means configured so as to interact on the pointing means for pointing at the HMIs of the cockpit, and a module with a touch-sensitive flat surface configured so as to interact on the pointing device for pointing at the HMIs of the cockpit and arranged in the extension of the hand-rest knob; and
an intermediate layer configured so as to make it possible to modify the position of the upper layer;
wherein the upper layer has a V-shaped structure and the hand-rest knob has an inverted-V-shaped structure, and
wherein the V has an angular aperture of between 65° and 250°.
2. The system according to claim 1 , wherein the module with a touch-sensitive flat surface configured so as to interact on the pointing device for pointing at the HMIs of the cockpit comprises a multi-contact capacitive touch pad, or a touch screen configured so as to implement an alphanumeric keypad, or a touch surface associated with an infrared sensor.
3. The system according to claim 1 , wherein the inverted V has an angular aperture of between 110° and 160°.
4. The system according to claim 3 , wherein the inverted V has an angular aperture of 145°.
5. The system according to claim 1 , wherein the front part of the inverted-V-shaped hand-rest knob is parallel to the rear part of the V-shaped structure.
6. The system according to claim 1 , wherein the gap between the upper surface of the rear part of the V-shaped structure and the lower surface of the front part of the inverted-V-shaped hand-rest knob is greater than or equal to 20 mm.
7. The system according to claim 1 , wherein the intermediate layer comprises a baseplate configured so as to be adapted to its installation position in the cockpit and to the fastening required by the aircraft.
8. The system according to claim 1 , wherein the intermediate layer comprises a rotary adaptor, configured so as to rotate the upper layer about a horizontal axis, for example configured so as to tilt up to 45° with respect to the horizontal.
9. The system according to claim 1 , wherein the intermediate layer comprises a translatory adaptor, configured so as to move the upper layer in translation with respect to the intermediate layer.
10. The system according to claim 7 , wherein the intermediate layer comprises a rotary adaptor, configured so as to rotate the elements arranged above the baseplate jointly about a vertical axis.
11. The system according to claim 1 , wherein the upper layer comprises a device configured so as to modify the angular aperture of the V-shaped structure.
12. The system according to claim 1 , wherein the upper layer comprises a device configured so as to make it possible to retract the module with a touch-sensitive flat surface.
13. The system according to claim 1 , wherein the upper layer comprises an ambient light device.
14. The system according to claim 7 , wherein the baseplate comprises fastening screw cover devices.