Flight actuated door seal

Patent metadata

Field	Value
Publication number	US-9809295-B1
Application number	US-201615175890-A
Country	US
Kind code	B1
Filing date	Jun 7, 2016
Priority date	Jun 7, 2016
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

A sealing system for an aircraft having an opening and a door movable between an open condition spaced from the opening and a closed condition covering and sealing the opening includes a cover plate connected to the aircraft adjacent the opening. A first magnetic coupling secured to the cover plate includes a first plurality of magnets. A second magnetic coupling configured for securing to the door includes a second plurality of magnets. The first magnetic coupling is repelled by the second magnetic coupling when the couplings have a first degree of alignment with one another. This causes the cove plot move away from the door. The first magnetic coupling is attracted to the second magnetic coupling when the couplings have a second degree of alignment with one another greater than the first degree, causing the magnetic couplings to engage one another and seal the opening in the aircraft.

First claim

What is claimed is:

1. A sealing system for an aircraft having an opening and a door movable between an open condition spaced from the opening and a closed condition covering the opening, the system comprising:
a cover plate connected to the aircraft adjacent the opening;
a first magnetic coupling secured to the cover plate and including a first plurality of magnets; and
a second magnetic coupling for securing to the door and including a second plurality of magnets, the first magnetic coupling being repelled by the second magnetic coupling when the couplings have a first degree of alignment with one another which causes the cover plate to move away from the door, the first magnetic coupling being attracted to the second magnetic coupling when the magnetic couplings have a second degree of alignment with one another greater than the first degree causing the magnetic couplings to engage one another and seal the opening in the aircraft.

2. The sealing system of claim 1 , wherein the first plurality of magnets includes first and second magnets having opposite polarities and being stacked atop one another, the second plurality of magnets including third and fourth magnets having opposite polarities and being stacked atop one another.

3. The sealing system of claim 2 , wherein the first and third magnets engage one another and the second and fourth magnets engage one another when the opening in the aircraft is sealed.

4. The sealing system of claim 2 , wherein the first and second plurality of magnets constitute coded magnets.

5. The sealing system of claim 1 , further comprising a shuttle secured to the cover plate and being slidable with the cover plate and the first magnetic coupling along an inner surface of the aircraft in response to magnetic interaction between the magnets.

6. The sealing system of claim 5 , wherein the shuttle, the cover plate, and the first magnetic coupling slide together away from the door when the first and second magnetic couplings have the first degree of alignment with one another and slide together towards the door when the first and second magnetic couplings have the second degree of alignment with one another.

7. The sealing system of claim 5 , wherein the shuttle is positioned within a recess of the aircraft behind the cover plate.

8. The sealing system of claim 5 , wherein the shuttle is mechanically retained by at least one of the door and the aircraft when the magnetic couplings engage one another.

9. The sealing system of claim 1 , further comprising a retaining magnet fixed to the aircraft and magnetically connected to the cover plate, the cover plate sliding over the retaining magnet and away from the door when the first and second magnetic couplings have the first degree of alignment with one another and sliding towards the door when the first and second magnetic couplings have the second degree of alignment with one another.

10. The sealing system of claim 9 , wherein the cover plate is magnetically held against the retaining magnet when the magnetic couplings engage one another and is slidable along the retaining magnet relative to the aircraft to maintain a sealed connection with the door of the aircraft during flight.

11. The sealing system of claim 1 , wherein the cover plate is sealed with the door of the aircraft when the magnetic couplings engage one another and slidable relative to the aircraft to maintain a sealed connection with the door of the aircraft during flight.

12. A sealing system for an aircraft having an opening and a door movable between an open condition spaced from the opening and a closed condition covering and sealing the opening, the system comprising:
a cover plate magnetically coupled to the aircraft adjacent the opening;
a shuttle secured to the cover plate and provided in a recess of the aircraft adjacent the opening;
a first magnetic coupling secured to the cover plate and including a first plurality of magnets; and
a second magnetic coupling for securing to the door and including a second plurality of magnets, the first magnetic coupling being repelled by the second magnetic coupling when the couplings have a first degree of alignment with one another such that the cover plate slides with the shuttle and first magnetic coupling away from the door, the first magnetic coupling being attracted to the second magnetic coupling when the magnetic couplings have a second degree of alignment with one another greater than the first degree such that the cover plate slides with the shuttle and the first magnetic coupling towards the door until the magnetic couplings engage one another and seal the opening in the aircraft.

13. The sealing system of claim 12 , wherein the first plurality of magnets includes first and second magnets having opposite polarities and being stacked atop one another, the second plurality of magnets including third and fourth magnets having opposite polarities and being stacked atop one another.

14. The sealing system of claim 13 , wherein the first and third magnets engage one another and the second and fourth magnets engage one another when the opening in the aircraft is sealed.

15. The sealing system of claim 13 , wherein the first and second plurality of magnets constitute coded magnets.

16. The sealing system of claim 12 , wherein the shuttle, the cover plate, and the first magnetic coupling slide together away from the door when the first and second magnetic couplings have the first degree of alignment with one another and slide together towards the door when the first and second magnetic couplings have the second degree of alignment with one another.

17. The sealing system of claim 12 , wherein the shuttle is positioned within a recess of the aircraft behind the cover plate.

18. The sealing system of claim 12 , further comprising a retaining magnet fixed to the aircraft and magnetically connected to the cover plate, the cover plate sliding over the retaining magnet and away from the door when the first and second magnetic couplings have the first degree of alignment with one another and sliding towards the door when the first and second magnetic couplings have the second degree of alignment with one another.

19. The sealing system of claim 12 , wherein the cover plate is magnetically held against the retaining magnet when the magnetic couplings engage one another and is slidable along the retaining magnet relative to the aircraft to maintain a sealed connection with the door of the aircraft during flight.

20. The sealing system of claim 12 , wherein the cover plate is sealed with the door of the aircraft when the magnetic couplings engage one another and slidable relative to the aircraft to maintain a sealed connection with the door of the aircraft during flight.

Assignees

• Bauer Robert E
• Rufino John C
• Northrop Grumman Systems Corp

Inventors

• Bauer Robert E
• Rufino John C

Classifications

• B64C1/1461 Primary

  Structures of doors or surrounding frames · CPC title

• E06B7/205

  with sealing strip mounted on sill · CPC title

• F16J15/061 Primary

  with positioning means (F16J15/0831 takes precedence) · CPC title

• B64C1/14 Primary

  Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens {accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers}(fairings movable in conjunction with undercarriage elements B64C25/16; bomb doors B64D1/06) · CPC title