Aircraft handle locking device

A locking device and handle technology, applied in the aviation field, can solve the problems of broken engine blades, poor rigidity, large deformation, etc., and achieve the effects of less weight and cost, less space occupation, and simple structure

Active Publication Date: 2020-05-12
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The doors and hatches on the aircraft that are opened by the handle are often opened due to false triggers and accidental operations during the field use, resulting in the inability to complete follow-up tasks
In addition, due to the poor design of the hatch and the cover, the rigidity difference is large and the deformation is large, and the reliability of the handle lock is low, the lock is accidentally opened in the air and flies off, thereby damaging other structures, and in severe cases, it enters the air inlet and damages the engine blades.

Method used

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Embodiment Construction

[0021] In order to make the purpose, technical solution and advantages of the present invention more clear, the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined arbitrarily with each other.

[0022] In view of the existing requirements: rationally arrange the hatch in a limited space and a position with a large curvature, open it conveniently and quickly by operating the handle lock, and ensure the reliability of the handle lock.

[0023] Embodiments of the present invention provide a handle locking device that occupies less space, has a simple structure, and is light in weight. When the door is closed, it is automatically locked by a smooth slope, and the spring keeps the locked state. The operating force of the handle under load is not more than 222 N (N). The l...

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PUM

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Abstract

The embodiment of the invention discloses an airplane handle locking device. The device comprises a locking assembly arranged on an airplane door frame plate and a lock shaft arranged on an airplane handle; the lock shaft comprises a shaft body arranged inside the handle and a locking connector located outside the handle, and the axial movement of the handle drives the lock shaft to axially move;the locking assembly comprises a lock hook and a fixing sleeve used for fixedly connecting the first end of the lock hook to the airplane door frame plate, a hook-shaped lock groove matched with the locking connector for locking is formed in the second end of the lock hook, and the locking connector is clamped into the hook-shaped lock groove in the lock hook when the lock shaft is driven by the handle; and the lock hook assembly further comprises a spring mechanism connected with the lock hook, and the spring mechanism is configured to release the lock shaft by pressing the second end of thelock hook. According to the embodiment, a handle locking device which is simple in structure and light in weight on the premise of meeting the use functions is provided.

Description

technical field [0001] This application relates to but is not limited to the field of aviation technology, especially an aircraft handle locking device. Background technique [0002] The doors and flaps on the aircraft that are opened by the handle are often opened due to false triggers and accidental operations during the field use, resulting in the inability to complete follow-up tasks. In addition, due to poor design of hatches and flaps, large deformation due to poor rigidity, and low reliability of handle locks, the locks may accidentally be unlocked and fly off in the air, thereby damaging other structures. In severe cases, they may enter the air intake and damage engine blades. [0003] Therefore, it is required to reasonably arrange the hatch in a limited space and a position with a large curvature, to open it conveniently and quickly by operating the handle lock, and to ensure the reliability of the handle lock. [0004] A handle locking device with small space occ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E05B13/00B64C1/14
CPCB64C1/14E05B13/004
Inventor 王哲郭祥孙兆兵
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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