Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Multi-freedom-degree constraint auxiliary supporting device for reverse guided missile launching

An auxiliary support and degree of freedom technology, which is applied in the direction of launching devices, devices for preventing multi-way movement of goods, load handling devices, etc., can solve the problems of insufficient constraints on degrees of freedom, low firmness, and poor reliability, so as to improve the safety of product transportation Sexuality, reliable constraints, and the effect of realizing multi-degree-of-freedom full constraints

Active Publication Date: 2020-08-11
SHANGHAI INST OF ELECTROMECHANICAL ENG
View PDF7 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This patent document discloses a support mechanism with a guide that can be adjusted steplessly. It does not solve the problems of insufficient freedom constraints and low firmness during missile transportation, and the reliability of missile transportation is poor.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Multi-freedom-degree constraint auxiliary supporting device for reverse guided missile launching
  • Multi-freedom-degree constraint auxiliary supporting device for reverse guided missile launching
  • Multi-freedom-degree constraint auxiliary supporting device for reverse guided missile launching

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0040] like Figure 1~6 Shown is a multi-degree-of-freedom restraint auxiliary support device for reverse launching missiles provided by the present invention. The parallelogram mechanism also includes a connecting piece 19, and the connecting piece 19 is fastened on the bottom plate 8. On the connecting piece 19, A pressing block 15 is provided for fastening.

Embodiment 2

[0042] like Figure 1~6 Shown is a multi-degree-of-freedom restraint auxiliary support device for reverse launching missiles provided by the present invention. The parallelogram mechanism also includes an explosive bolt 10, and one end of the explosive bolt 10 is installed on the connecting piece 19 and the pressure block 15. , and the other end is sleeved on the third rotating shaft 17 . There are semicircular grooves on the connecting piece 19 and the briquetting block 15, and two semicircular grooves form a cylindrical hole. In the semicircular groove, the explosive bolt 10 is fixed.

Embodiment 3

[0044] like Figure 1~6Shown is a reverse launch missile multi-degree-of-freedom restraint auxiliary support device provided by the present invention, which also includes a pair of tension springs 6, and the pair of tension springs 6 are correspondingly arranged at both ends of the second rotating shaft 16; One end of the tension spring 6 is connected to the second connecting rod 5 , and the other end is connected to the bottom plate 8 .

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a multi-freedom-degree constraint auxiliary supporting device for reverse guided missile launching. The multi-freedom-degree constraint auxiliary supporting device comprises a guide rail, the guide rail is mounted in launching equipment in a fastened manner, a groove is formed in the guide rail, and an axial limiting block is arranged on the guide rail in a fastened manner.A push plate is located between the axial limiting block and the groove, the axial limiting block is in close contact with the push plate, and the push plate is in close contact with the groove. A parallelogram mechanism comprises a bottom plate, a first rotating shaft, a second rotating shaft, a third rotating shaft, a fourth rotating shaft, a first connecting rod, a second connecting rod and anarc baffle device. The bottom plate is mounted on the launching equipment in a fastened manner, and the first connecting rod and the second connecting rod are connected with the bottom plate through the first rotating shaft and the second rotating shaft. The first connecting rod and the second connecting rod are connected with the arc baffle device through the third rotating shaft and the fourth rotating shaft. The first connecting rod and the second connecting rod are in linkage through the first rotating shaft, the second rotating shaft, the third rotating shaft and the fourth rotating shaft. Multi-freedom-degree full constraining of the guided missile is achieved, and the product transporting safety is improved.

Description

technical field [0001] The invention relates to the technical field of missile auxiliary support, in particular to a multi-degree-of-freedom restraint auxiliary support device for reverse launch missiles. Background technique [0002] Missile transportation, also known as "missile handling" or "missile transfer". The process of using vehicles, trains, planes, ships and other means of transportation to transfer missiles from one point to another. [0003] At present, the missiles are mostly fixed by the ammunition-fixing mechanism during transportation, but the function of the ammunition-fixing mechanism is single, and most of them can only restrain a single degree of freedom of the missile, while the remaining five degrees of freedom still have a certain range of motion, and it is impossible to realize the full freedom of the missile. The degree of reliability is constrained, resulting in a decrease in the firmness and an increase in the danger of the missile during transpo...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): F41F1/00B60P7/135B61D45/00B63B25/00B63B25/24B64D9/00
CPCF41F1/00B60P7/135B61D45/00B64D9/00B63B25/24B63B25/002
Inventor 李微微张保刚俞刘建夏津刘广许斌蒋君庭陶勇鹏胡珊王波兰
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com