IP Library › Granted Patent US 12,208,900
Granted Patent B2
US 12,208,900 · App. 18/076,650 · Granted Jan 28, 2025

Aircraft interior unit with detachable panel

Inventors: Joseph Vuagniaux (Wales, GB); Mark Douglas (Wales, GB); Daniel Parish (Wales, GB)
Assignee: Safran Seats GB Limited
B64D11/0606B64D2011/0046
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Quick Facts
Patent No.
US 12,208,900
App. No.
18/076,650
Granted
Jan 28, 2025
Kind
B2
Abstract

An aircraft interior unit with a detachable panel. The aircraft interior unit comprises a wall comprising a hollow panel, and a door mounted to the wall. The door is slidable between a closed position in which it covers an entrance to the aircraft interior unit, and an open position in which the entrance to the aircraft interior unit is uncovered. In the open position, the door is at least partially disposed within the hollow panel of the wall. The hollow panel can be detached from the rest of the aircraft interior unit, and the door, when moved from the open position, can be detached from the wall.

Claims (17)

1. An aircraft interior unit comprising:

a wall,

a hollow panel detachably mounted to the wall, and

a door detachably mounted to the wall, the door being slidable between a closed position in which it covers an entrance to the aircraft interior unit, and an open position in which the entrance to the aircraft interior unit is uncovered;

wherein the door, when in the open position, is at least partially disposed within the hollow panel;

wherein the hollow panel can be detached from the wall while the door is still attached to the wall; and

wherein the door, when moved from the open position, can be detached from the wall while the hollow panel is still attached to the wall.

2. The aircraft interior unit as claimed in claim 1 , wherein a portion of the wall extends above the hollow panel.

3. The aircraft interior unit as claimed in claim 1 , wherein the portion of the wall to which the hollow panel is detachably mounted is on the opposite side of the hollow panel to the door when in the open position.

4. The aircraft interior unit as claimed in claim 1 , wherein the hollow panel is located adjacently to the entrance to the aircraft interior unit.

5. The aircraft interior unit as claimed in claim 1 , wherein the door is mounted on a rail within the panel.

6. The aircraft interior unit as claimed in claim 1 , wherein the door, when in the open position, is disposed entirely within the wall.

7. The aircraft interior unit as claimed in claim 6 , wherein the door, when in the open position, is disposed entirely within the hollow panel.

8. The aircraft interior unit as claimed in claim 1 , wherein the hollow panel comprises one or more pins on an edge that, when the hollow panel is attached to the rest of the aircraft interior unit, extend into corresponding holes in the rest of the aircraft interior unit.

9. The aircraft interior unit as claimed in claim 1 , wherein the hollow panel is secured to the rest of the aircraft interior unit by a latch.

10. The aircraft interior unit as claimed in claim 1 , wherein the door is secured to the wall by a latch.

11. The aircraft interior unit as claimed in claim 1 , wherein the aircraft interior unit is an aircraft seating unit.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 8, 2024
From: VUAGNIAUX, JOSEPH; PARISH, DANIEL
To: SAFRAN SEATS GB LIMITED
Reel/Frame 069517/0972 →
Priority Claims (1)
GB 2117901 · Dec 10, 2021 · national
Continuity (1)
Related Publication 20230182902A1 · Jun 15, 2023
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Cited By (1)
US 12,741,741