Device for assisting the piloting in acceleration of an aircraft in taxiing in order to control its speed, related aircraft and method

Patent metadata

Field	Value
Publication number	US-12084192-B2
Application number	US-202217872628-A
Country	US
Kind code	B2
Filing date	Jul 25, 2022
Priority date	Jul 26, 2021
Publication date	Sep 10, 2024
Grant date	Sep 10, 2024

Abstract

A device is for assisting the piloting in acceleration of an aircraft in taking in order to control its speed. The comprises a control member, adapted to be actuated by a pilot from a neutral position to define a taxiing piloting command for controlling the speed of the aircraft and a central controller, adapted to operate pilot at least one engine of the aircraft to apply the taxiing command defined by the pilot. The taxiing piloting command is an acceleration or deceleration command of the aircraft during taxiing.

First claim

What is claimed is:

1. An aircraft taxiing piloting assist device comprising:
a control member operable by a pilot from a neutral position to define a taxiing piloting command to control a speed of an aircraft;
a central controller configured to pilot at least one aircraft engine to apply the taxiing piloting command defined by the pilot, the taxiing piloting command being an acceleration or deceleration command of the aircraft during taxiing,
wherein the control member is configured to be moved to a maximum acceleration stop and/or to a minimum deceleration stop.

2. The device according to claim 1 , wherein the central controller is configured to additionally pilot at least one aircraft braking member in order to apply the acceleration or deceleration command defined by the pilot.

3. The device according to claim 1 , wherein, after application of the acceleration or deceleration command and release of the control member, the control member is automatically returned to the neutral position.

4. The device according to claim 3 , wherein the neutral position is a fixed neutral with respect to a stroke of the control member, the control member being automatically returned to the fixed neutral position.

5. The device according to claim 3 , wherein the neutral position is a movable neutral position relative to a stroke of the control member, the control member being automatically returned to the movable neutral position, or the movable neutral being movable to a current position of the control member.

6. The device according to claim 1 , wherein the maximum acceleration stop is configured to move along a stroke of the control member to limit the stroke of the control member as a function of a current aircraft speed.

7. The device according to claim 1 , wherein the minimum deceleration stop is configured to be overcome to reach a maximum deceleration detent in which the control member is locked in position.

8. The device according to claim 1 , wherein the at least one aircraft engine is a propulsion engine of the aircraft exerting a thrust force on the aircraft, and/or wherein the at least one aircraft engine is an electric motor to drive a wheel of the aircraft.

9. The device according to claim 8 , wherein the at least one aircraft engine is a jet engine or a turboprop engine.

10. The device according to claim 8 , wherein the control member comprises a movable lever configured to pilot the at least one aircraft engine to exert a thrust force and/or to pilot at least one aircraft drag modifier to reduce a mechanical energy of the aircraft, the device being configured to switch between an inactive configuration during take-off, flight and landing phases and an active configuration during taxiing.

11. The device according to claim 10 , wherein the movable lever is configured to pilot the at least one aircraft engine to exert a thrust force and to pilot the at least one aircraft drag modifier to reduce a mechanical energy of the aircraft,
wherein, in the inactive configuration, the control member is configured to be moved by the pilot to send to the central controller a command for varying the mechanical energy of the aircraft, so that the central controller pilots the at least one aircraft engine and the at least one aircraft drag modifier, without controlling a braking member of the aircraft,
and wherein, in the active configuration, the control member is configured to be moved by the pilot to set an acceleration or deceleration command for the aircraft during rolling, intended for the central controller, so that the central controller pilots the at least one aircraft engine.

12. The device according to claim 10 , comprising an activation button to switch the device in the active configuration, and/or a deactivation button to switch the device in the inactive configuration.

13. The device according to claim 12 wherein the activation button or/and the deactivation button is arranged on the movable lever.

14. The device according to claim 10 , comprising a light-up display configured to produce at least one device activation, operation and/or deactivation luminous indicator.

15. An aircraft comprising:
the device according to claim 1 ; and
at least one aircraft engine for being piloted by the central controller in order to apply the acceleration or deceleration command defined by the control member.

16. The aircraft according to claim 15 , comprising at least one braking member also configured to be piloted by the central controller to apply the acceleration or deceleration command defined by the control member.

17. A method for taxiing an aircraft, implemented with an aircraft taxiing piloting assist device, the method comprising:
determining actuation, by a pilot, of a control member of the device, from a neutral position in order to define a taxiing piloting command;
applying the taxiing piloting command defined by the pilot with a central controller of the device piloting at least one engine of the aircraft, the taxiing piloting command being an acceleration or deceleration command of the aircraft.

18. The method according to claim 17 , wherein the central controller further pilots at least one braking member of the aircraft to apply the acceleration or deceleration command defined by the pilot.

19. An aircraft taxiing piloting assist device comprising:
a control member operable by a pilot from a neutral position to define a taxiing piloting command to control a speed of an aircraft;
a central controller configured to pilot at least one aircraft engine to apply the taxiing piloting command defined by the pilot, the taxiing piloting command being an acceleration or deceleration command of the aircraft during taxiing,
wherein the central controller is configured to additionally pilot at least one aircraft braking member in order to apply the acceleration or deceleration command defined by the pilot,
wherein the neutral position is a movable neutral position relative to a stroke of the control member, the control member being automatically returned to the movable neutral position, or the movable neutral being movable to a current position of the control member.

20. An aircraft taxiing piloting assist device comprising:
a control member operable by a pilot from a neutral position to define a taxiing piloting command to control a speed of an aircraft;
a central controller configured to pilot at least one aircraft engine to apply the taxiing piloting command defined by the pilot, the taxiing piloting command being an acceleration or deceleration command of the aircraft during taxiing,
wherein the control member is configured to be moved to a maximum acceleration stop and/or to a minimum deceleration stop,
wherein the maximum acceleration stop is configured to move along a stroke of the control member to limit the stroke of the control member as a function of a current aircraft speed.

21. An aircraft taxiing piloting assist device comprising:
a control member operable by a pilot from a neutral position to define a taxiing piloting command to control a speed of an aircraft;
a central controller configured to pilot at least one aircraft engine to apply the taxiing piloting command defined by the pilot, the taxiing piloting command being an acceleration or deceleration command of the aircraft during taxiing,
wherein the at least one aircraft engine is a propulsion engine of the aircraft exerting a thrust force on the aircraft, and/or wherein the at least one aircraft engine is an electric motor to

Assignees

• Dassault Aviat

Inventors

• Beaucamp Angélique
• Fillet Laurent
• Le Corre Nicolas

Classifications

• G05D1/437

  for aircraft during their ground movement {, e.g. taxiing} · CPC title

• G05D1/0083

  to help an aircraft pilot in the rolling phase · CPC title

• Y02T50/80

  Energy efficient operational measures, e.g. ground operations or mission management · CPC title

• B64C9/323

  associated with wings · CPC title

• B64C25/426

  Braking devices providing an automatic sequence of braking · CPC title