一种海上火箭发射的缓冲防回弹机构及其使用方法

By combining shock-absorbing components and one-way braking components in the marine rocket launch device, and using hydraulic dampers and roller units to achieve buffering and anti-rebound, the structural damage and rebound problems during the tilting process of marine rocket launch are solved, and the stability and safety of the device are improved.

CN122192094BActive Publication Date: 2026-07-17LUDONG UNIVERSITY +1

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
LUDONG UNIVERSITY
Filing Date
2026-05-15
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing marine rocket launchers cannot effectively buffer and prevent rebound during the tilting process, resulting in a high risk of structural damage and launch failure.

Method used

The system employs a combination of shock-absorbing components and one-way braking components, using hydraulic dampers and roller units to achieve buffering and anti-rebound, ensuring that the contact surface is always in close contact with the anti-overturning arm, and absorbing impact force by utilizing self-amplifying braking and nonlinear damping characteristics.

Benefits of technology

It improves the stability and safety of rocket launch, extends the service life of the device, reduces friction damage, and ensures the reliability and safety of launch.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明公开了一种海上火箭发射的缓冲防回弹机构及其使用方法,属于火箭发射的技术领域,包括防倾覆装置底座和防倾覆臂,防倾覆臂置于防倾覆装置底座上且与防倾覆装置底座铰接,所述防倾覆装置底座上设有单向制动组件和缓震组件,单向制动组件置于两个缓震组件中间位置,单向制动组件和缓震组件置于防倾覆臂的同一侧,防倾覆臂朝向靠近单向制动组件和缓震组件的方向倾斜转动;单向制动组件包括制动弧、制动蹄、摩擦衬片、压紧弹簧和制动连杆单元;缓震组件包括液压阻尼器单元、滚轮单元和缓震连杆单元。本发明通过缓震组件与单向制动组件,对防倾覆臂进行缓震,并在倾倒过程中以及倾倒结束后起到防回弹的作用。
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