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Cabin door system for aircraft and aircraft having at least one such cabin door system

A door system, aircraft technology, applied in the field of cabin door system, can solve problems such as damage

Pending Publication Date: 2020-10-09
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This may result in damage to the peripheral equipment of the aircraft

Method used

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  • Cabin door system for aircraft and aircraft having at least one such cabin door system
  • Cabin door system for aircraft and aircraft having at least one such cabin door system
  • Cabin door system for aircraft and aircraft having at least one such cabin door system

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Embodiment Construction

[0033] figure 1 Shown is a cabin door system 2 having a cabin door 4 with an outer side 6 and an inner side 8. Furthermore, a drive device 10 is provided, which remains highly schematic in this illustration. It can be proposed that, depending on the configuration of the cabin door 4, completely different driving devices are used, which can move the cabin door 4 to the open position. figure 1 Accordingly, the illustrations in should not be construed as limitations on size, installation location or other details.

[0034] On the inner side 8, a first actuation device 12 is schematically shown, which has an operating lever pivotable about a pivot axis 14 with a handle 18 spaced apart from the pivot axis 14 16. This illustration should also be understood as an example, and should not be understood as limiting the subject matter to such a first actuation device 12. In order to open the door 4, the user can grasp the handle 18 and pivot the operating lever 16 upwards about the pivot ...

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Abstract

A cabin door system for an aircraft and an aircraft having the cabin door system are disclosed. The aircraft cabin door system has a cabin door having an outer side and an inner side, a drive device coupled to the cabin door for moving the cabin door into an open position, a first actuation device arranged on the inner side surface of the cabin door, a second actuation device, and an emergency chute unit coupled to the cabin door and having an emergency chute and an actuation mechanism. The emergency chute unit can be moved into an active state, in which opening the cabin door leads to activation of the emergency chute, and an inactive state, in which opening the cabin door does not lead to activation of the emergency chute. The emergency chute unit is in the inactive state when the cabindoor is opened after actuation of the first actuation device. The second actuation device is coupled to the drive device and configured such that the cabin door is opened by the drive device during actuation of the second actuation device. The emergency chute unit is in the active state when the cabin door is opened after actuation of the second actuation device.

Description

Technical field [0001] The invention relates to a cabin door system for an aircraft and an aircraft having at least one such cabin door system. Background technique [0002] Due to safety regulations, traffic aircraft have inflatable emergency slides that are inflated when the cabin door is opened in an emergency and then extend from the corresponding door to the ground. For this purpose, a cabin can be provided on the bottom side of the cabin door or below the door area, in which the compacted emergency slide is stored. The emergency slide is usually fixed by a belt rod, which can be coupled to the door through a mechanism. [0003] The emergency slide system can be activated and deactivated. In the activated state, the emergency slide is automatically inflated when the corresponding door is opened; while in the deactivated state, the emergency slide remains in the storage compartment. The transformation from the deactivated state to the activated state can be performed by flip...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/14B64D25/14
CPCB64C1/1423B64D25/14B64C1/1407E05B1/0038E05B1/003E05B1/00
Inventor 卡伊·布雷德迈尔迈克·科克
Owner AIRBUS OPERATIONS GMBH
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