A connecting rod throwing device

A technology of connecting rod and double-ear joint, which is applied in the direction of aircraft doors and aircraft accessories, can solve the problems of the risk of not being able to provide exit, stuck, and large throwing operation force.

Active Publication Date: 2022-05-06
CHINA HELICOPTER RES & DEV INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the design process of the hatch of some models, due to the limitation of the outer surface of the hatch or the space of the hatch, the rotation plane of the throwing handle cannot be on the same plane as the motion trajectory of the hinge cleaner. At this time, the straight line of the cleaner There is a problem of uncoordinated movement between the movement and the rotation of the throwing handle, which will cause excessive throwing operation force and throwing stagnation
[0004] Most of the mechanical throwing mechanisms are not linked with the door locking mechanism. Operating the throwing handle only removes the hinge shaft, and the door is still connected to the door frame through the locking mechanism. After the hinge shaft is taken off, the door itself Still stuck on the frame of the door frame, the risk of not being able to provide an exit in an emergency

Method used

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Embodiment Construction

[0044] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0045] A connecting rod throwing device linked with a locking mechanism, such as figure 1 with figure 2 As shown, comprising: upper hinge assembly 1, lower hinge assembly 2, throwing device 3;

[0046] Such as image 3 As shown, the upper hinge assembly is divided into an upper lug joint 11, an upper joint bearing 12, a cylindrical pin shaft 13, and a bending rod 14;

[0047] The upper binaural joint 11 is fixed on the fuselage structure, a...

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Abstract

The invention belongs to the technical field of helicopter structure design, and discloses a connecting rod release device, which is used to solve the problem that when the rotation plane of the handle shaft of the release handle is not on the same plane as the motion track of the hinge rod, the operation force of the release mechanism is large and the cabin The door is thrown and stuck. Solve the linkage problem between the throwing mechanism and the hatch locking mechanism, operate the throwing mechanism to drive the locking mechanism to unlock, completely separate the hatch from the hatch frame, and provide emergency exits.

Description

technical field [0001] The invention belongs to the technical field of helicopter structure design, and in particular relates to a connecting rod throwing device. Background technique [0002] Existing helicopter door release mechanism can be divided into two types: explosive type and mechanical type. Because the explosive type release mechanism needs to do a lot of tests to verify the explosion equivalent, direction, explosion effect, etc., and operate the release handle in an emergency During this time, personnel are close to the explosion point, and there are certain potential safety hazards. Therefore, except for a few military aircraft that use explosive release mechanisms, the release mechanisms of most helicopter hatches are mechanical release mechanisms. [0003] The principle of most mechanical throwing mechanisms is that by turning the throwing handle, the hinge strip connected between the door and the door frame moves downward until the door hinge is disengaged, a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14
CPCB64C1/1407
Inventor 郑国朋谷长河邹蒙王春辉
Owner CHINA HELICOPTER RES & DEV INST
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