Aircraft door control

Patent metadata

Field	Value
Publication number	US-11420720-B2
Application number	US-201815980004-A
Country	US
Kind code	B2
Filing date	May 15, 2018
Priority date	May 15, 2017
Publication date	Aug 23, 2022
Grant date	Aug 23, 2022

Abstract

An aircraft door controller 100 including a receiver 110 configured to receive a command 14 to move an aircraft door between an open position and a closed position relative to a door frame. The aircraft door controller 100 is configured to not store the command 14 when power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable.

First claim

The invention claimed is:

1. An aircraft door control system comprising:
an aircraft door controller including:
a receiver configured to receive a command to move an aircraft door between an open position and a closed position relative to a door frame; and
a memory,
wherein the aircraft door controller is configured to determine whether power to move the aircraft door between the open position and the closed position relative to the door frame is available;
wherein the aircraft door controller is configured to not store the command or information representative of the command in the memory when the power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable, and
wherein the aircraft door controller is configured to store the command or the information representative of the command in the memory when the power to move the aircraft door between the open position and the closed position relative to the door frame is available; and

a user control configured to cause generation of the command when operated by a user regardless of whether the power to move the aircraft door is available.

2. The aircraft door control system according to claim 1 , wherein the controller is configured to not store the command by the controller by not latching the command in memory.

3. The aircraft door control system according to claim 1 , wherein the user control is configured to cause generation of the command by movement of the user control to a first position, and wherein the user control is biased away from the first position.

4. The aircraft door control system according to claim 1 , further comprising a detector configured to detect a position of the aircraft door relative to the door frame, wherein the aircraft door controller is configured to cause movement of the aircraft door between the open position and the closed position relative to the door frame on the basis of an output of the detector.

5. The aircraft door control system according to claim 1 , wherein the user control is a first user control and the control system comprises a second user control, and
wherein the aircraft door control system is configured such that operation of the first user control causes generation of the command in dependence on a status of the second user control.

6. The aircraft door control system according to claim 1 , wherein the aircraft door control system is an aircraft landing gear bay door control system.

7. The aircraft door control system of claim 1 wherein the aircraft the aircraft door controller is configured to execute the stored command and thereby issue a further command to move the aircraft door.

8. A method of controlling an aircraft door, the method comprising:
receiving a command to move the aircraft door between an open position and a closed position relative to a door frame, regardless of whether power is available to move the aircraft door;
determining whether power to move the aircraft door between the open and closed positions is available;
not storing the command or information representative of the command in a memory, when the power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable, and
storing the command or information representative of the command in the memory, when the power to move the aircraft door between the open position and the closed position relative to the door frame is available.

9. The method according to claim 8 , comprising causing generation of the command by operation of a user control, and
wherein the user control is operable to cause generation of the command when the power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable.

10. The method according to claim 8 , wherein the command comprises a command to move the aircraft door from the open position to the closed position relative to the door frame.

11. The method according to claim 8 , wherein the power comprises hydraulic power and/or electrical power.

12. The method according to claim 8 , wherein the aircraft door is a landing gear bay door or a cargo bay door.

13. The method according to claim 8 further comprising:
if the determination is that the power is available, a controller retrieves the stored command or information representative of the command in the memory and executes the stored command to issue a further command which causes the aircraft door to move.

14. A non-transitory computer-readable storage medium storing instructions that, if executed by a processor of an aircraft door controller, cause the processor to carry out the method of claim 8 .

15. An aircraft door controller comprising:
a receiver configured to receive a command to move an aircraft door between an open position and a closed position relative to a door frame, the receiver configured to receive the command regardless of whether power is available to move the door; and
a memory;
wherein the aircraft door controller is configured to determine whether power to move the aircraft door between the open position and the closed position relative to the door frame is available;
wherein the aircraft door controller is configured to not store the command or information representative of the command in the memory when the power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable; and
wherein the aircraft door controller is configured to store the command or the information representative of the command in the memory when the power to move the aircraft door between the open position and the closed position relative to the door frame is available.

Assignees

• Airbus Operations Ltd

Inventors

• Grufferty Mark
• Elliott Nicholas
• Rowlands Martin Griffith
• Perkins Christopher James

Classifications

• B64C25/16

  Fairings movable in conjunction with undercarriage elements · CPC title

• B64C25/001

  Devices not provided for in the groups B64C25/02 - B64C25/68 · CPC title

• B64C1/1415 Primary

  Cargo doors, e.g. incorporating ramps · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• B64C1/1407 Primary

  Doors; surrounding frames · CPC title