Access systems and methods for a vehicle

Patent metadata

Field	Value
Publication number	US-12037832-B2
Application number	US-202217832751-A
Country	US
Kind code	B2
Filing date	Jun 6, 2022
Priority date	Jun 6, 2022
Publication date	Jul 16, 2024
Grant date	Jul 16, 2024

Abstract

An access system for a vehicle includes a door moveably coupled to a portion of a fuselage. The door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed. One or more actuators are secured to the door. The one or more actuators are configured to move the door between the open position and the closed position.

First claim

What is claimed is:

1. An access system for a vehicle, the access system comprising:
a plug door moveably coupled to a portion of a fuselage, wherein the plug door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed, wherein the plug door is configured to mate with a socket frame surrounding the opening when the plug door is in the closed position; and
one or more actuators mounted to the plug door, wherein the one or more actuators are configured to move the plug door between the open position and the closed position.

2. The access system of claim 1 , wherein the one or more actuators are separated from a floor within the fuselage.

3. The access system of claim 1 , wherein the internal chamber comprises a cargo hold of the vehicle.

4. The access system of claim 1 , wherein the vehicle is an aircraft.

5. The access system of claim 1 , wherein the one or more actuators comprise one or more rotary motors.

6. The access system of claim 1 , wherein the one or more actuators comprise one or more linear motors.

7. The access system of claim 1 , further comprising a control unit configured to control operation of the one or more actuators.

8. The access system of claim 1 , wherein the one or more actuators are secured to a mounting plate that is mounted on an internal surface of the plug door.

9. The access system of claim 1 , wherein the one or more actuators comprise one or more rotary motors coupled to a rod, wherein the rod is coupled to a first linkage and a second linkage opposite from the first linkage, wherein each of the first linkage and the second linkage comprises a plurality of arms, wherein the one or more rotary motors are configured to operate the drive rod, which in turn drives motion of the first linkage and the second linkage to linearly and outwardly move the plug door away from the socket frame into an initial position, and then pivotally move the plug door from the initial position into the open position.

10. The access system of claim 1 , further comprising one or more linkages coupled to the one or more actuators, wherein the one or more actuators are configured to move the one or more linkages to move the plug door between the open position and the closed position.

11. The access system of claim 10 , wherein the one or more linkages connect to a portion of a floor within the fuselage.

12. The access system of claim 11 , wherein the one or more linkages connect to an underside of the portion of the floor.

13. A method of manufacturing an access system for a vehicle, the method comprising:
coupling a plug door to a portion of a fuselage, wherein the plug door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed, wherein the plug door is configured to mate with a socket frame surrounding the opening when the plug door is in the closed position; and
mounting one or more actuators to the plug door, wherein the one or more actuators are configured to move the door between the open position and the closed position.

14. The method of claim 13 , further comprising coupling one or more linkages to the one or more actuators, wherein the one or more actuators are configured to move the one or more linkages to move the plug door between the open position and the closed position.

15. The method of claim 13 , further comprising connecting the one or more linkages to a portion of a floor within the fuselage, wherein the one or more actuators are separated from the floor.

16. An aircraft comprising:
a fuselage including a floor over a cargo hold having an opening formed in the fuselage; and
an access system comprising:
a plug door moveably coupled to a socket frame surrounding the opening, wherein the plug door is configured to be moved between an open position in which the opening is opened, and a closed position in which the opening is closed;
one or more actuators mounted to the door, wherein the one or more actuators are configured to move the door between the open position and the closed position; and
one or more linkages coupled to the one or more actuators, wherein the one or more actuators are configured to move the one or more linkages to move the door between the open position and the closed position, wherein the one or more linkages connect to an underside of the floor, and wherein the one or more actuators are separated from the floor.

17. The aircraft of claim 16 , wherein the one or more actuators comprise one or more rotary motors.

18. The aircraft of claim 16 , wherein the one or more actuators comprise one or more linear motors.

19. The aircraft of claim 16 , wherein the one or more actuators are secured to a mounting plate that is mounted on an internal surface of the door.

20. The aircraft of claim 16 , wherein the one or more actuators comprise one or more rotary motors coupled to a rod, wherein the one or more linkages comprise a first linkage and a second linkage opposite from the first linkage, wherein the rod is coupled to the first linkage and the second linkage, wherein each of the first linkage and the second linkage comprises a plurality of arms, wherein the one or more rotary motors are configured to operate the drive rod, which in turn drives motion of the first linkage and the second linkage to linearly and outwardly move the plug door away from the socket frame into an initial position, and then pivotally move the plug door from the initial position into the open position.

Assignees

• Boeing Co

Inventors

• Skilton Richard A
• Fleming Michael A

Classifications

• E05Y2900/502

  for aircraft or spacecraft · CPC title

• E05Y2400/40

  Control units therefor · CPC title

• E05Y2201/686

  Rods, links · CPC title

• E05Y2201/624

  Arms · CPC title

• E05Y2201/434

  Electromotors; Details thereof · CPC title