Aircraft, systems, and methods for trim control in fly-by-wire aircraft systems

Patent metadata

Field	Value
Publication number	US-11767102-B2
Application number	US-202217657277-A
Country	US
Kind code	B2
Filing date	Mar 30, 2022
Priority date	Oct 13, 2014
Publication date	Sep 26, 2023
Grant date	Sep 26, 2023

Abstract

Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.

First claim

The invention claimed is:

1. An aircraft comprising:
a trim control system for controlling surfaces of the aircraft; and
a fly-by-wire system communicatively coupled with the trim control system, the fly-by-wire system comprising:
an inceptor with an input device configured to receive inputs from a user; and
a controller communicatively coupled with the input device, the controller configured to:
actively control the trim control system to provide positive speed stability about a selected trim airspeed while permitting continuous manual flight;
responsive to receiving an input from the user at the input device when an autopilot is engaged, disengage the autopilot; and
responsive to receiving the input from the user at the input device when the autopilot is disengaged, reset the selected trim airspeed based on a stable flight condition at a present airspeed of the aircraft.

2. The aircraft of claim 1 , wherein the controller is configured to reset the selected trim airspeed based on the stable flight condition at the present airspeed of the aircraft based on a stabilized 1G flight condition as the stable flight condition.

3. The aircraft of claim 1 , wherein the controller is further configured to not reset the selected trim airspeed when the fly-by-wire system is currently limiting maneuvers of the aircraft based on alpha limiting, speed protecting, or both alpha limiting and speed protecting.

4. The aircraft of claim 1 , wherein the fly-by-wire system further includes a manual trim control, and wherein the controller is further configured to set a pitch trim of the aircraft based on a manual trim input from the manual trim control when the autopilot is disengaged.

5. The aircraft of claim 4 , wherein the controller is further configured to disable the manual trim control in response to receiving the input from the input device while receiving the manual trim input from the manual trim control.

6. The aircraft of claim 1 , wherein the input device is a pushbutton input device configured to receive the inputs from the user as discrete depressions of the pushbutton input device.

7. The aircraft of claim 1 , wherein the fly-by-wire system further includes a manual trim control, and wherein the controller is further configured to:
set a pitch trim of the aircraft based on a manual trim input from the manual trim control when the autopilot is disengaged;
disable the manual trim control in response to receiving the input from the input device while receiving the manual trim input from the manual trim control;
reset the selected trim airspeed based on the stable flight condition at the present airspeed of the aircraft based on a stabilized 1G flight condition as the stable flight condition; and
not reset the selected trim airspeed when the fly-by-wire system is currently limiting maneuvers of the aircraft based on alpha limiting, speed protecting, or both alpha limiting and speed protecting.

8. The aircraft of claim 1 , wherein the fly-by-wire system further includes a manual trim control input device configured to manually adjust trim airspeed.

9. A controller for use with a fly-by-wire system of an aircraft that includes an input device configured to receive inputs from a user, the controller comprising:
at least one processor; and
at least one memory unit coupled with the at least one processor, the at least one memory unit storing instructions for the at least one processor, wherein the instructions are configured to cooperate with the at least one processor to:
actively control a trim control system to provide positive speed stability about a selected trim airspeed while permitting continuous manual flight;
responsive to receiving an input from the user at the input device when an autopilot is engaged, disengage the autopilot; and
responsive to receiving the input from the user at the input device when the autopilot is disengaged, reset the selected trim airspeed based on a stable flight condition at a present airspeed of the aircraft.

10. The controller of claim 9 , wherein the controller is configured to reset the selected trim airspeed based on the stable flight condition at the present airspeed of the aircraft based on a stabilized 1G flight condition as the stable flight condition.

11. The controller of claim 9 , wherein the controller is further configured to not reset the selected trim airspeed when the fly-by-wire system is currently limiting maneuvers of the aircraft based on alpha limiting, speed protecting, or both alpha limiting and speed protecting.

12. The controller of claim 9 , wherein the fly-by-wire system further includes a manual trim control, and wherein the controller is further configured to set a pitch trim of the aircraft based on a manual trim input from the manual trim control when the autopilot is disengaged.

13. The controller of claim 12 , wherein the controller is further configured to disable the manual trim control in response to receiving the input from the input device while receiving the manual trim input from the manual trim control.

14. The controller of claim 9 , wherein the input device is a pushbutton input device on an inceptor in the aircraft, where the pushbutton input device is configured to receive the inputs from the user as discrete depressions of the pushbutton input device.

15. The controller of claim 9 , wherein the fly-by-wire system further includes a manual trim control, and wherein the controller is further configured to:
set a pitch trim of the aircraft based on a manual trim input from the manual trim control when the autopilot is disengaged;
disable the manual trim control in response to receiving the input from the input device while receiving the manual trim input from the manual trim control;
reset the selected trim airspeed based on the stable flight condition at the present airspeed of the aircraft based on a stabilized 1G flight condition as the stable flight condition; and
not reset the selected trim airspeed when the fly-by-wire system is currently limiting maneuvers of the aircraft based on alpha limiting, speed protecting, or both alpha limiting and speed protecting.

16. An aircraft comprising:
a trim control system for controlling surfaces of the aircraft; and
a fly-by-wire system communicatively coupled with the trim control system, the fly-by-wire system comprising:
an inceptor with an input device configured to receive inputs from a user; and
a controller communicatively coupled with the input device, the controller configured to:
actively control the trim control system to provide positive speed stability about a selected trim airspeed while permitting continuous manual flight, wherein the positive speed stability is a tendency of the aircraft to return to the selected trim airspeed after a disturbance of the aircraft from the selected trim airspeed;
responsive to receiving an input from the user at the input device when an autopilot is engaged
disengage the autopilot;

responsive to receiving the input from the user at the input device when the autopilot is disengaged
disengage manual trim control when the manual trim control is engaged;

responsive to receiving the input from the user at the input device when the autopilot is disengaged, and the fly-by-wire system is not currently limiting maneuvers of the aircraft based on alpha limiting or speed protecting
reset the selected trim airspeed based on a stable flight condition at a present airspeed of the aircraft.

17. The aircraft of claim 16 , wherein the controller is configured to reset the selected trim airspee

Assignees

• Gulfstream Aerospace Corp

Inventors

• Claffy Kevin
• Shin Jong-Yeob

Classifications

• B64C13/506 Primary

  overriding of personal controls; with automatic return to inoperative position · CPC title

• B64C13/0421

  control sticks for primary flight controls · CPC title

• B64C13/0427

  for actuating trim · CPC title

• B64C13/503

  Fly-by-Wire · CPC title