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Locking mechanism capable of being tensioned and pushed

A locking mechanism and locking force technology, which is applied in electric locks, building locks, vehicle locks, etc., can solve the problems that the locking mechanism lacks the push-open function and affects the reliability of the door opening, and achieves a large locking force , High reliability effect

Active Publication Date: 2019-07-02
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, after the hatch has been closed for a long time, it is affected by factors such as cold welding of the contact surface and increased structural deformation resistance. When the hatch is unlocked and opened again, it needs to overcome a large resistance. The current locking mechanism lacks the push-open function. Affects the reliability of hatch opening

Method used

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  • Locking mechanism capable of being tensioned and pushed
  • Locking mechanism capable of being tensioned and pushed
  • Locking mechanism capable of being tensioned and pushed

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Embodiment Construction

[0016] To facilitate the understanding of the embodiments of the present invention, as Figure 1~3 As shown, the components in the above drawings are named as follows: 1—passive end housing; 2—passive lock cylinder; 3—active end housing; 4—drive motor; 5—three-stage planetary reduction 6—transmission gear; 7—crank shaft; 8—active lock hook; 9—connecting rod; 10—crank; d—push open gap;

[0017] According to the present invention, the passive end shell 1 and the active end shell 3 that can tighten and push the locking mechanism are respectively fixedly installed on the aircraft cabin door. The driving assembly is composed of a driving motor 4 , a three-stage planetary reducer 5 and a transmission gear 6 .

[0018] The transmission process of motion and power is that the output shaft of the driving motor 4 rotates, and the motion and power are transmitted to the three-stage planetary reducer 5. After deceleration, the power increases, and is transmitted to the transmission gear ...

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Abstract

The invention discloses a locking mechanism capable of being tensioned and pushed. The locking mechanism comprises a driving assembly, a active end and a passive end; the active end and the passive end are fixedly connected to the cabin door on two sides, and when the locking mechanism is tensioned and pushed, the cabin door can be driven to move; and the driving assembly outputs motion and force,so that the requirement of cabin door locking force can be met. A driving motor outputs motion and force to a three-stage planetary reducer, and rotation speed reduces and torque increases through larger reduction ratio, so that the requirement of cabin door locking force can be met. Motion and force are output to the active end through a transmission gear. An active end shell body and a passiveend shell body are fixedly connected to the cabin door on the two sides respectively, and when the locking mechanism is tensioned and pushed, the cabin door can be driven to move. The locking mechanism has the advantages of being high in reliability, large in locking force, tensioning and pushing functions and the like.

Description

technical field [0001] The invention relates to a locking mechanism that can be tightened and pushed open, in particular to a locking mechanism with the function of overcoming initial resistance, which is suitable for tightening and pushing open a cabin door. [0002] technical background [0003] At present, most space vehicles such as space shuttles, spaceships, and space stations have door mechanisms, which can realize the sealing of the cabin when the door is locked; when the door is opened, the functional load can be released. The cabin door needs to be locked by a locking mechanism, and most of the current locking mechanisms can realize the locking function. [0004] However, after the hatch has been closed for a long time, it is affected by factors such as cold welding of the contact surface and increased structural deformation resistance. When the hatch is unlocked and opened again, it needs to overcome a large resistance. The current locking mechanism lacks the push-...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E05B81/06E05B85/20E05C19/10E05B79/12
CPCE05B79/12E05B81/06E05B85/20E05C19/10E05Y2900/502E05Y2900/531
Inventor 韩大为张晓伟杨晓青罗小桃屠国俊牛中轲徐荣杨永常孙西龙赵蔚
Owner SHANGHAI AEROSPACE SYST ENG INST