Door opening system with a deceleration mechanism

Patent metadata

Field	Value
Publication number	US-10940933-B2
Application number	US-201916597179-A
Country	US
Kind code	B2
Filing date	Oct 9, 2019
Priority date	Oct 10, 2018
Publication date	Mar 9, 2021
Grant date	Mar 9, 2021

Abstract

A door opening system with a deceleration mechanism may be adapted to control an opening of a door module that includes a door panel and a door frame. Deceleration mechanism may include strap that connects door panel with door frame, spool, and spool. Spool may receive one end of strap, is biased to roll up a first portion of strap, and adapted to perform a first unwinding of the first portion of strap. Spool may receive a second end of strap, is biased to roll up a second portion of strap, and adapted to perform a second unwinding of the second portion of strap from spool. Spool may include a braking apparatus that is adapted to decelerate the second unwinding when a velocity of the second unwinding is above a predetermined threshold.

First claim

What is claimed is:

1. A door opening system adapted to control an opening of a door module that separates compartments of an aircraft and comprises a door panel and a door frame, comprising:
a deceleration mechanism that comprises:
a strap that connects the door panel with the door frame,

a first spool that receives a first end of the strap, is biased to roll up a first portion of the strap, and adapted to perform a first unwinding of the first portion of the strap from the first spool with a first resistive force, and
a second spool that receives a second end of the strap, is biased to roll up a second portion of the strap, and adapted to perform a second unwinding of the second portion of the strap from the second spool with a second resistive force that is greater than the first resistive force, and wherein the second spool comprises a braking apparatus that is adapted to decelerate the second unwinding when a velocity of the second unwinding is above a predetermined threshold.

2. The door opening system of claim 1 , wherein the door module further comprises:
a door damper that biases the door panel into a closed position; and
a door locking system that is at least partially arranged on the door panel and maintains the door panel in the closed position.

3. The door opening system of claim 1 , wherein the door damper further comprises:
a first pivot arm that is coupled to the door panel; and
a second pivot arm that is coupled between the first pivot arm and the door frame.

4. The door opening system of claim 1 , wherein the door panel is biased towards a closed position and the door locking system is adapted to release the door panel from the closed position when a predetermined air pressure difference threshold between the compartments of the aircraft is exceeded.

5. The door opening system of claim 1 , wherein the predetermined threshold is selected based on a predetermined air pressure difference threshold between the compartments of the aircraft.

6. The door opening system of claim 5 , wherein the first spool performs the first unwinding of the first portion of the strap during a first move of the door panel from a closed position to a first predetermined position of the door panel, and wherein the second spool performs the second unwinding of the second portion of the strap during a second move of the door panel from the first predetermined position to a second predetermined position of the door panel.

7. The door opening system of claim 6 , wherein the first spool absorbs a first kinetic energy during the first move of the door panel.

8. The door opening system of claim 7 , wherein the second spool absorbs a second kinetic energy that is greater than the first kinetic energy during the second move of the door panel.

9. The door opening system of claim 8 , wherein the deceleration mechanism further comprises:
a mechanical end stop that stops the door panel at a third predetermined position of the door panel.

10. The door opening system of claim 9 , wherein the mechanical end stop absorbs a third kinetic energy during a third move of the door panel from the second predetermined position to the third predetermined position of the door panel.

11. The door opening system of claim 9 , wherein the mechanical end stop is attached to the door frame.

12. The door opening system of claim 1 , wherein the first spool is fixedly attached to the door panel, and wherein the second spool is fixedly attached to the door frame.

13. The door opening system of claim 1 , wherein the first and second spools are fixedly attached to the door frame, and wherein the deceleration mechanism further comprises:
a pulley that is fixedly attached to the door panel and adapted to guide the strap between the first and second spools.

14. The door opening system of claim 1 , wherein the strap is selected from the group including a belt, a rope, a cable, a string, and a chain.

15. A method for controlling an opening of a door module that separates compartments of an aircraft and comprises a door panel and a door frame, when a predetermined air pressure difference threshold between the compartments of the aircraft is exceeded using a door opening system, the method comprising:
determining whether a difference between a first air pressure of a first compartment and a second air pressure of a second compartment exceeds the predetermined air pressure difference threshold;
in response to determining that the difference between the first air pressure of the first compartment and the second air pressure of the second compartment exceeds the predetermined air pressure difference threshold, disabling a door locking system that keeps the door panel in a closed position;
unwinding a first portion of a strap from a first spool that guides a first move of the door panel from the closed position to a first predetermined position;
activating a braking apparatus in a second spool;
unwinding a second portion of the strap with the second spool that guides a second move of the door panel from the first predetermined position to a second predetermined position; and
stopping the door panel using at least one mechanical end stop that guides a third move of the door panel from the second predetermined position to a third predetermined position.

16. A door opening system adapted to control an opening of a door module that separates compartments of an aircraft and comprises a door panel and a door frame, comprising:
a strap connecting the door panel with the door frame,
a first spool that receives a first end of the strap, is biased to roll up a first portion of the strap, and adapted to perform a first unwinding of the first portion of the strap from the first spool with a first resistive force, and
a second spool that receives a second end of the strap, is biased to roll up a second portion of the strap, and adapted to perform a second unwinding of the second portion of the strap from the second spool with a second resistive force that is greater than the first resistive force.

17. The door opening system of claim 16 , wherein the second spool comprises a brake adapted to decelerate the second unwinding when a velocity of the second unwinding is above a predetermined threshold.

18. The door opening system of claim 17 , wherein the first spool is fixedly attached to the door panel, and wherein the second spool is fixedly attached to the door frame.

19. The door opening system of claim 17 , wherein the first and second spools are fixedly attached to the door frame, and wherein the door opening system further comprises a pulley that is fixedly attached to the door panel and adapted to guide the strap between the first and second spools.

20. The door opening system of claim 17 , wherein the door panel is biased into a closed position, and the door module further comprises a door locking system that is at least partially arranged on the door panel and maintains the door panel in the closed position, wherein the first spool performs the first unwinding of the first portion of the strap during a first move of the door panel from a closed position to a first predetermined position of the door panel, and wherein the second spool performs the second unwinding of the second portion of the strap during a second move of the door panel from the first predetermined position to a second predetermined position of the door panel, and wherein the first spool absorbs a first kinetic energy during the first move of the door panel, and wherein the second spool absorbs a se

Assignees

• Airbus Helicopters Deutschland GmbH

Inventors

• Tendyra Thomas
• Ward Stephen
• Borchers Guido
• Renner Uwe
• Pascoe Xaver
• Buehlmeyer Markus

Classifications

• E05B51/023

  actuated in response to external pressure, blast or explosion (E05B65/102 takes precedence) · CPC title

• B64C1/1469 Primary

  Doors between cockpit and cabin · CPC title

• B64C2001/009

  comprising decompression panels or valves for pressure equalisation in fuselages or floors · CPC title

• E05B17/0041

  Damping means (for vehicles E05B77/42; time locks with retarders E05B43/00) · CPC title