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Anti-misoperation device for aircraft passenger cabin door

A technology for an anti-misoperation device and a cabin door, which is applied to aircraft doors, aircraft accessories, etc., can solve the problems of large driving force, large volume of the anti-misoperation device, and a large number of parts, and achieves the effect of a simple structure.

Active Publication Date: 2021-08-13
COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the anti-misoperation device has a large volume, a large number of parts, a high complexity, and a large weight. The device contains finished parts or small equipment parts, and the cost is high. The driving force required by the device is relatively large. The opening load has a great influence

Method used

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  • Anti-misoperation device for aircraft passenger cabin door
  • Anti-misoperation device for aircraft passenger cabin door
  • Anti-misoperation device for aircraft passenger cabin door

Examples

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Embodiment Construction

[0049] Specific implementations of the present invention will be described below. It should be noted that in the process of specific descriptions of these implementations, for the sake of concise description, it is impossible for this specification to describe all the features of the actual implementations in detail. It should be understood that, in the actual implementation process of any embodiment, just like in the process of any engineering project or design project, in order to achieve the developer's specific goals and to meet system-related or business-related constraints, Often a variety of specific decisions are made, and this can vary from one implementation to another. In addition, it will be appreciated that while such development efforts may be complex and lengthy, the technology disclosed in this disclosure will be Some design, manufacturing or production changes based on the content are just conventional technical means, and should not be understood as insuffici...

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PUM

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Abstract

The invention relates to an anti-misoperation device for aircraft passenger cabin doors. The anti-misoperation device for the aircraft passenger cabin door includes a guide groove, a rocker, a torsion spring, a hook, a spline shaft, a rocker bushing and a roller; wherein the roller is rigidly connected to one end of the rocker, And can move in the guide groove close to the inner wall of the guide groove; one end of the torsion spring acts on the frame of the first cabin door, and the other end of the torsion spring acts on the hook; the spline shaft is rigidly connected to the other end of the rocker, The hook is rigidly connected to the spline shaft so that the rocker, the spline shaft and the hook can rotate coaxially; the rocker bushing is installed on the latch shaft of the aircraft passenger door lift system and is rigidly connected The latch shaft rotates coaxially. The anti-misoperation device for the aircraft passenger cabin door of the present invention can have the following beneficial technical effects: the structure is relatively simple, and it can effectively prevent the cabin door from being closed by wrong operation of the aircraft personnel in the open state.

Description

technical field [0001] The invention relates to an anti-misoperation device for aircraft passenger cabin doors. Background technique [0002] The anti-misoperation device that prevents the personnel on the aircraft from closing the passenger compartment door by mistake is applied to the passenger compartment door of the aircraft. EASA 783d(8) states that a door that would be dangerous if left open must have means to prevent the latch from moving to the latched position, unless it can be shown that the open door would be apparent prior to flight. [0003] In order to comply with the provisions of this article, a certain model has designed an anti-misoperation device for the passenger cabin door of the aircraft. The anti-misoperation device directly acts on the handle mechanism and locks the handle when the door is fully opened, which meets the EASA 783d(8) article. Require. However, the anti-misoperation device has a large volume, a large number of parts, a high complexity,...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14
CPCB64C1/1423B64C1/143
Inventor 刘若斯张仲桢吴斌黄振庭沙钊武戎戎
Owner COMAC
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