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Airplane door gust lock device

A lock device and cabin door lock technology, which is applied to aircraft doors, aircraft accessories, etc., can solve problems such as difficult processing and installation, and complex structure

Active Publication Date: 2021-10-19
COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, when installing or disassembling the gust lock device or replacing the parts of the gust lock device, it is necessary to disassemble other mechanisms of the aircraft door, and the structure is complicated and difficult to process and install.

Method used

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Embodiment Construction

[0028] Hereinafter, the structure of the aircraft door gust lock device 100 of the present invention will be described with reference to the accompanying drawings.

[0029] figure 1 It is a schematic diagram showing the position of the aircraft door gust lock device 100 of the present invention when the door is opened.

[0030] Such as figure 1 As shown, there are door frames CD on both sides of the aircraft door FL 、D FR , the hatch frame CD on both sides FL 、D FR Through the hatch transom CD CB connected.

[0031] The aircraft door gust lock device 100 of the present invention locks the aircraft door at a fixed position to maintain the maximum open state of the door and prevent the door from shaking due to gusts of wind or other external forces.

[0032] In addition, when the cabin door of the aircraft needs to be closed, the gust lock device 100 for the cabin door of the aircraft needs to be released first.

[0033] figure 2 is expressed in figure 1 A schematic d...

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PUM

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Abstract

A gust lock device for an aircraft cabin door can be positioned accurately and can improve the accuracy of locking and unlocking. The aircraft door gust lock device locks the aircraft door in a fixed position to lock the door in the maximum open state, including: a locked part, which is fixedly installed on the door frame of the door, and has a locked part and a locking part, which is installed on the hinge arm of the hatch, and has a locking piece, a positioning piece and a limiting piece, wherein the locking piece has a locking part locked with the locked part, and has Three blocking parts, the positioning part is arranged adjacent to the locking part, and has two protrusions arranged opposite to the three blocking parts, and the limiting part is arranged between the locking part and the positioning part for Limit the movement range of the relative position of the locking piece and the positioning piece, and use the three blocking parts of the locking piece, the two protrusions of the positioning piece and the limit piece to define at least two different relative positions of the locking piece relative to the positioning piece. Location.

Description

technical field [0001] The invention relates to the field of aircraft door mechanism design, in particular to an aircraft door gust lock device for preventing the aircraft door from shaking due to gusts of wind or other external forces. Background technique [0002] After the aircraft door is opened, the gust lock device can keep the aircraft door in a fixed position to prevent the aircraft door from shaking due to gusts of wind or other external forces. This gust lock device is generally suitable for outward opening doors, and the gust lock device can be installed near the fixed rotating shaft of the aircraft door to ensure that the aircraft door remains in the open position. [0003] In the past, the gust lock device was realized by using a boss and a groove-type limiting structure and a strut and a support-type limiting structure. For example, non-patent literature 1 "A General Aircraft Boarding Door "Gust Lock" (Xi'an Aircraft Design Institute of Aviation Industry Corpo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14
CPCB64C1/14B64C1/1407
Inventor 袁修起岳伟柳荣刘国方
Owner COMAC
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