IP Library Granted Patent US 11,927,290
Granted Patent B2
US 11,927,290 · App. 16/824,058 · Granted Mar 12, 2024

Multipurpose connector for an aircraft monument and aircraft monument, aircraft area and aircraft having a multipurpose connector

Inventors: Christian Le Polotec (Hamburg, DE); Tammo Bahns (Hamburg, DE)
Assignee: AIRBUS OPERATIONS GMBH
F16L39/00B64D11/00B64D11/02B64D11/04
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Quick Facts
Patent No.
US 11,927,290
App. No.
16/824,058
Granted
Mar 12, 2024
Kind
B2
Abstract

A multipurpose connector for connecting a multiplicity of lines of an aircraft monument. The multipurpose connector comprises a base bracket, a system connector plate configured to receive a multiplicity of first line adapters, a monument connector plate configured to receive at least one second line adapter, and a movement device configured to move the system connector plate relative to the base bracket and the monument connector plate between an open position and a closed position. The system connector plate is, in the closed position, arranged relative to the monument connector plate such that the at least one second line adapter of the monument connector plate is operatively connected to an associated first line adapter of the system connector plate, and, in the open position of the system connector plate, the multiplicity of first line adapters and the at least one second line adapter are detached from one another.

Claims (57)

1. A multipurpose connector for connecting a multiplicity of lines of an aircraft monument, wherein the multipurpose connector comprises:

a base bracket configured to be fastened to a structural component of an aircraft;

a system connector plate which is configured to receive a multiplicity of first line adapters;

a monument connector plate which is configured to receive at least one second line adapter, wherein the monument connector plate together with the base bracket defines a space therebetween, in which the system connector plate is movably arranged; and

a movement device which is configured to move the system connector plate relative to the base bracket and also relative to the monument connector plate between an open position and a closed position,

wherein the system connector plate is, in the closed position, arranged relative to the monument connector plate such that the at least one second line adapter of the monument connector plate is operatively connected to an associated first line adapter of the system connector plate, and, in the open position of the system connector plate, the multiplicity of first line adapters and the at least one second line adapter are detached from one another,

wherein the movement device comprises a threaded spindle and a nut which is screwed onto the threaded spindle and which is connected to the system connector plate, wherein a rotation of the threaded spindle effects a movement of the system connector plate between the open position and closed position, or

wherein the movement device comprises a rotatably mounted lever which is operatively connected to the system connector plate, wherein a rotation of the lever effects a movement of the system connector plate between the open position and closed position.

2. The multipurpose connector as claimed in claim 1 , furthermore comprising:

at least one guide pin which is fastened to one of the system connector plate and the base bracket and which is mounted in sliding fashion on the other of the system connector plate and the base bracket.

3. The multipurpose connector as claimed in claim 1 , wherein each line adapter comprises at least one of the following:

a guide surface;

a seal; or

an electrical contact.

4. The multipurpose connector as claimed in claim 1 , furthermore comprising:

a signal transmitter which is configured to generate a contact signal when the system connector plate is in at least one of the open position or closed position.

5. An aircraft having at least one multipurpose connector as claimed in claim 1 .

6. An aircraft monument, comprising:

at least one multipurpose connector for connecting a multiplicity of lines of an aircraft monument comprising:

a base bracket;

a system connector plate which is configured to receive a multiplicity of first line adapters;

a monument connector plate which is configured to receive at least one second line adapter, wherein the monument connector plate together with the base bracket defines a space, in which the system connector plate is movably arranged; and

a movement device which is configured to move the system connector plate relative to the base bracket and also relative to the monument connector plate between an open position and a closed position,

wherein the system connector plate is, in the closed position, arranged relative to the monument connector plate such that the at least one second line adapter of the monument connector plate is operatively connected to an associated first line adapter of the system connector plate, and, in the open position of the system connector plate, the multiplicity of first line adapters and the at least one second line adapter are detached from one another; and

at least one line, wherein in each case, one line is connected to the at least one second line adapter of the monument connector plate and connects the associated second line adapter to a device arranged in the aircraft monument.

7. The aircraft monument as claimed in claim 6 , furthermore comprising:

at least one holding device which is configured to fasten the monument connector plate of the multipurpose connector at variable positions.

8. The aircraft monument as claimed in claim 7 , furthermore comprising:

an aligning device which is configured to be fastened at variable positions to the holding device and which is furthermore configured to fasten the monument connector plate to the aligning device at variable positions relative to the aligning device.

9. The aircraft monument as claimed in claim 6 , wherein the monument connector plate of the at least one multipurpose connector is arranged parallel to a rear wall of the monument.

10. An aircraft area, comprising:

at least one aircraft monument as claimed in claim 6 ,

wherein the base bracket of the multipurpose connector is attached to at least one primary structural component of the aircraft area in a position which is fixed relative to the primary structural component.

11. The aircraft area as claimed in claim 10 , furthermore comprising:

at least one floor element,

wherein at least one of the base bracket or the system connector plate of the multipurpose connector is arranged independently of the floor element in the aircraft area.

12. The aircraft area as claimed in claim 10 , furthermore comprising:

at least one floor element,

wherein at least one of the base bracket or the system connector plate of the multipurpose connector is integrated into the floor element.

13. An aircraft area, comprising:

at least one multipurpose connector for connecting a multiplicity of lines of an aircraft monument comprising:

a base bracket;

a system connector plate which is configured to receive a multiplicity of first line adapters;

a monument connector plate which is configured to receive at least one second line adapter, wherein the monument connector plate together with the base bracket defines a space, in which the system connector plate is movably arranged; and

a movement device which is configured to move the system connector plate relative to the base bracket and also relative to the monument connector plate between an open position and a closed position,

wherein the system connector plate is, in the closed position, arranged relative to the monument connector plate such that the at least one second line adapter of the monument connector plate is operatively connected to an associated first line adapter of the system connector plate, and, in the open position of the system connector plate, the multiplicity of first line adapters and the at least one second line adapter are detached from one another,

wherein the base bracket of the multipurpose connector is attached to at least one primary structural component of the aircraft area in a position which is fixed relative to the primary structural component.

14. The aircraft area as claimed in claim 13 , furthermore comprising:

at least one floor element,

wherein at least one of the base bracket or the system connector plate of the multipurpose connector is arranged independently of the floor element in the aircraft area.

15. The aircraft area as claimed in claim 13 , furthermore comprising:

at least one floor element,

wherein at least one of the base bracket or the system connector plate of the multipurpose connector is integrated into the floor element.

16. The aircraft area as claimed in claim 13 , having an aircraft monument, with at least one line,

wherein in each case, one line is connected to the at least one second line adapter of the monument connector plate and connects the associated second line adapter to a device arranged in the aircraft monument,

wherein the monument connector plate of the at least one multipurpose connector is arranged parallel to a rear wall of the monument, and

wherein the monument connector plate is arranged on the aircraft monument such that the at least one line adapter of the monument connector plate and the multiplicity of line adapters of the system connector plate of the multipurpose connector correspond in terms of their position and assume the open position of the system connector plate when the aircraft monument is arranged and fastened in the aircraft area.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 19, 2020
From: LE POLOTEC, CHRISTIAN; BAHNS, TAMMO ERNST
To: AIRBUS OPERATIONS GMBH
Reel/Frame 052169/0514 →
Priority Claims (1)
DE 10 2019 107 359.6 · Mar 22, 2019 · national
Continuity (1)
Related Publication 20200300398A1 · Sep 24, 2020
Cited By (1)
US 12,674,532