Device for limiting the deflection on a door arranged in a fuselage cell of an aircraft

US9409641B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9409641-B2
Application numberUS-201414289690-A
CountryUS
Kind codeB2
Filing dateMay 29, 2014
Priority dateDec 13, 2007
Publication dateAug 9, 2016
Grant dateAug 9, 2016

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  1. Title

    What the patent document calls the invention.

  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to a device for limiting the deflection of a door ( 1 ), particularly a hatch or a freight door, arranged in a fuselage cell ( 3 ) of an aircraft, having at least one holding element ( 5 ) arranged preferably in the region of a door jamb ( 4 ) or in the region of a door leaf edge ( 7 ). In order to ensure deflection limitation for doors, hatches and freight doors in aircraft which can be triggered manually independently of an actuation of the normal locking system, it is proposed according to the invention that the at least one holding element ( 5 ) can, if there is a sufficient pressure difference Δp between the internal pressure p i prevailing in the fuselage cell ( 3 ) and the outside air pressure p a prevailing outside of the fuselage cell ( 3 ), be brought into engagement with at least one abutment ( 6 ) arranged in the region of the door leaf edge ( 7 ) or the door jamb ( 4 ). In addition it is proposed that if there is a sufficiently large pressure difference Δp the at least one holding element ( 30, 55 ) is automatically pivoted or can be manually pivoted and can hereby be brought into engagement with the at least one abutment ( 31, 52 ).

First claim

Opening claim text (preview).

The invention claimed is: 1. A device for limiting deflection of a door having a pivoting door leaf edge and the door being arranged in a fuselage cell of an aircraft, the device comprising: at least one abutment; and at least one holding element; wherein the at least one holding element is pivotable automatically in case of a sufficiently large pressure difference between internal pressure in the fuselage cell and outside air pressure, whereby the at least one holding element is brought into engagement with the at least one abutment while the door is in a closed position; and wherein the at least one holding element comprises a lever coupled to an elastic membrane which has a hook and the at least one abutment comprises a barbed hook, and wherein the elastic membrane is subjected to a pressure difference between the internal pressure and the outside air pressure such that if there is the sufficiently large pressure difference the hook is brought into engagement with the barbed hook. 2. The device according to claim 1 , wherein the elastic membrane is arranged in a region of a door jamb or in a region of the pivoting door leaf edge and completely covers a recess arranged therein. 3. The device according to claim 1 , wherein the hook is connected so as to be pivotable by a joint disposed in a region of a door jamb or in a region of the pivoting door leaf edge, and the hook is arranged at an end of the lever pointing in a direction away from the end of the lever. 4. The device according to claim 1 , wherein the lever is provided with a pin and the elastic membrane lies against the pin or is connected to the pin in a jointed way. 5. The device according to claim 1 , wherein the barbed hook comprises a thickened area for holding the barbed hook. 6. The device according to claim 1 , wherein the elastic membrane is coupled to a spring in such a way that the hook is configured to lift away from the barbed hook if the sufficiently large pressure difference is around 0 hPa. 7. The device according to claim 1 , wherein the hook is connected so as to be pivotable by a joint in a region of a door jamb or in a region of the pivoting door leaf edge, and wherein the lever is pivotable automatically in such a way that the hook is brought into engagement with the barbed hook arranged in the region of the door jamb or in the region of the door leaf edge.

Assignees

Inventors

Classifications

  • B64C1/14Primary

    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

  • B64C1/1461Primary

    Structures of doors or surrounding frames · CPC title

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Frequently asked questions

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What does patent US9409641B2 cover?
The invention relates to a device for limiting the deflection of a door ( 1 ), particularly a hatch or a freight door, arranged in a fuselage cell ( 3 ) of an aircraft, having at least one holding element ( 5 ) arranged preferably in the region of a door jamb ( 4 ) or in the region of a door leaf edge ( 7 ). In order to ensure deflection limitation for doors, hatches and freight doors in …
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B64C1/14. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Aug 09 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).