Door system for aircraft fuselage

Patent metadata

Field	Value
Publication number	US-11548611-B2
Application number	US-201916559919-A
Country	US
Kind code	B2
Filing date	Sep 4, 2019
Priority date	Sep 6, 2018
Publication date	Jan 10, 2023
Grant date	Jan 10, 2023

Abstract

In order to simplify the kinematics involved in opening an aircraft door, a plurality of mobile stop members is provided at the periphery of the door, these being intended to press against complementary stop arrangement provided on the door frame. A door control device is configured to bring the door from its closed position into a set-back intermediate position by moving it towards the interior of the compartment, and a stop arrangement control device is configured to allow the mobile stop members to be moved, when the door is occupying its set-back intermediate position, from a deployed locking position to a retracted unlocking position, allowing the door to be moved outward through the opening in the fuselage.

First claim

The invention claimed is:

1. A door system for aircraft fuselage, the system comprising:
a door frame delimiting an opening in the fuselage, the opening giving access to a compartment of the aircraft;
a door provided to block the opening when the door occupies a closed position, this closed position of the door being intended to be maintained by pressure difference between the outside of the fuselage and the compartment;
stop means arranged at a periphery of the door, and intended to press on complementary stop means provided on the door frame,
wherein the system also comprises a door control device configured to bring the door from the closed position into a set-back intermediate position by moving the door towards the interior of the compartment and, vice versa, by moving the door outward,
wherein the stop means comprise a plurality of mobile stop members following each other along the periphery of the door,
wherein the system also comprises a stop means control device configured such that, when the door occupies the set-back intermediate position, a movement is provoked of the mobile stop members from a deployed locking position to a retracted unlocking position allowing the door to be moved outward through the opening in the fuselage,
wherein the system is configured so that, in the closed position of the door, the pressing of the mobile stop members, against the complementary stop means of the door frame, prevents these mobile members from being moved to their retracted unlocking position, and
wherein the stop means control device comprises:
an actuation membrane arranged at the periphery of the door and cooperating with the mobile stop members, the membrane delimiting a control chamber, the actuation membrane secured to the mobile stop members; and
pressure control means for the control chamber, the pressure inside the chamber conditioning the position of the membrane and that of the mobile stop members cooperating with this membrane.

2. The door system as claimed in claim 1 , wherein each mobile stop member has a first end articulated on the periphery of the door, and a second end opposite the first and forming an end for contact with the door frame.

3. The door system as claimed in claim 2 , wherein the second end delimits a rounded contact surface.

4. The door system as claimed in claim 1 , wherein the stop means control device also comprises elastic return means, returning the mobile stop members to the retracted unlocking position, by generating a force opposing the pressure forces that are exerted on the actuation membrane inside the control chamber, the elastic return means being arranged inside the control chamber.

5. The door system as claimed in claim 1 , wherein the actuation membrane forms a seal between the door and the door frame, the seal being continuous all along the periphery of the door.

6. The door system as claimed in claim 1 , wherein the door control device comprises:
at least one control handle;
at least one control member driven by the control handle and mounted articulated on the door along an articulation axis, each control member defining a guiding track receiving a following member secured to the door frame.

7. The door system as claimed in claim 6 , wherein the door control device is configured such that each control member can be rotated between a holding position and a release position, this rotation of the control member about the articulation axis, between the holding position and the release position, provoking a movement of the following member along the guiding track, conducting the door from the closed position to the set-back intermediate position.

8. The door system as claimed in claim 7 , wherein, in the holding position, the control member is prevented by the following member from moving relative to the door frame, toward the interior of the compartment, and wherein, in the release position, the control member can be moved outward relative to the door frame.

9. An aircraft comprising a fuselage equipped with at least one door system as claimed in claim 1 .

10. A door system for aircraft fuselage, the system comprising:
a door frame delimiting an opening in the fuselage, the opening giving access to a compartment of the aircraft;
a door provided to block the opening when the door occupies a closed position, this closed position of the door being intended to be maintained by pressure difference between the outside of the fuselage and the compartment;
stop means arranged at a periphery of the door, and intended to press on complementary stop means provided on the door frame,
wherein the system also comprises a door control device configured to bring the door from the closed position into a set-back intermediate position by moving the door towards the interior of the compartment and, vice versa, by moving the door outward,
wherein the stop means comprise a plurality of mobile stop members following each other along the periphery of the door,
wherein the system also comprises a stop means control device configured such that, when the door occupies the set-back intermediate position, a movement is provoked of the mobile stop members from a deployed locking position to a retracted unlocking position allowing the door to be moved outward through the opening in the fuselage,
wherein the system is configured so that, in the closed position of the door, the pressing of the mobile stop members, against the complementary stop means of the door frame, prevents these mobile members from being moved to their retracted unlocking position,
wherein the stop means control device comprises:
an actuation membrane arranged at the periphery of the door and cooperating with the mobile stop members, the membrane delimiting a control chamber; and
pressure control means for the control chamber, the pressure inside the chamber conditioning the position of the membrane and that of the mobile stop members cooperating with this membrane, and,

wherein the door control device comprises:
at least one control handle, and
at least one control member driven by the control handle and mounted articulated on the door along an articulation axis, each control member defining a guiding track receiving a following member secured to the door frame.

11. The door system as claimed in claim 10 , wherein the door control device is configured such that each control member can be rotated between a holding position and a release position, this rotation of the control member about the articulation axis, between the holding position and the release position, provoking a movement of the following member along the guiding track, conducting the door from the closed position to the set-back intermediate position.

12. The door system as claimed in claim 10 , wherein, in the holding position, the control member is prevented by the following member from moving relative to the door frame, toward the interior of the compartment, and wherein, in the release position, the control member can be moved outward relative to the door frame.

13. An aircraft comprising a fuselage equipped with at least one door system as claimed in claim 10 .

14. The door system as claimed in claim 10 , wherein each mobile stop member has a first end articulated on the periphery of the door, and a second end opposite the first and forming an end for contact with the door frame.

15. The door system as claimed in claim 14 , wherein the second end delimits a rounded contact surface.

Assignees

• Airbus Operations Sas

Inventors

• Lieven Patrick
• Lache Laurent
• Dourel Pierre

Classifications

• E05B15/00

  Other details of locks; Parts for engagement by bolts of fastening devices · CPC title

• B64C1/1415

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

• E05B17/0025

  Devices for forcing the wing firmly against its seat or to initiate the opening of the wing (E05B15/022, E05B65/0817, E05B81/20, E05C19/14 take precedence) · CPC title

• B64C1/143 Primary

  of the plug type · CPC title

• E05Y2900/502

  for aircraft or spacecraft · CPC title