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

Composite material made box body structure for storage and conveying launch box

A composite material and box structure technology, used in projectiles, self-propelled bombs, offensive equipment, etc., can solve problems such as cracks in joints, difficult air tightness of box structure, etc., to achieve good balance and ensure fast speed Combat responsiveness, light weight effect

Inactive Publication Date: 2003-05-21
SHANGHAI JIAO TONG UNIV
View PDF0 Cites 12 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the thermal expansion coefficient of the metal flange does not match the thermal expansion coefficient of the composite material. No matter how the metal flange and the composite material structure are connected under the environment of temperature changes, cracks will appear at the connection between the metal flange and the composite material structure, which is difficult. Ensure that the box structure has good airtightness

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
  • Composite material made box body structure for storage and conveying launch box
  • Composite material made box body structure for storage and conveying launch box
  • Composite material made box body structure for storage and conveying launch box

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0036] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0037] Composite box body structure of the present invention such asfigure 1 As shown, the box is surrounded by the four-sided base plate 1 of the box body, and transverse reinforcing ribs 2 are arranged at equal intervals along the length direction of the four-sided base plate 1 of the box body. The layers 11 form a whole full-composite flanging flange 3, and there is a reinforcing transition layer 4 between the full-composite flanging flange 3 and the thickened layer 11 at the end of the box substrate.

[0038] The box base plate 1 of the present invention is taken as R=R by taking the shallow arched shell plate 5 and the four corners of the box body that the four sides arch height of the box body is f O The cylindrical shell plate consists of 6 smooth connections, such as figure 2 As shown, one side of the four-sided subs...

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 composite material box body structure for storage and transportion box of missile is characterized by that said box body structure possesses the shallow arched single shell plate structure with longitudinal reinforcement member and transverse reinforcing rib and correspondent symmetrical layer-spread form, its four-side base plate of said box body structure is made up by using four-side small arch degree and shallow arched shell plate and four-corner cylindrical shell plate which are smoothly connected togher, along the length direction of base plate of box body the transverse reinforcing ribs are uniformly-spaced and placed, two ends of said box body adpots the all-composite material flange flanges which are connected with box body base plates together and formed into one body, so that said box body structure possesses high specific strength.

Description

Technical field: [0001] The invention relates to a composite material box structure of a storage and transportation launch box, which is the main load-bearing structure of the storage and transportation launch box, and is used for supporting and fixing, transporting, airtight and dry storage and vertical heat-launching missiles. Background technique: [0002] The high performance, high reliability and low cost of advanced launch vehicles and missiles largely depend on the application of new materials and the corresponding structural optimization design, which can effectively reduce the structural mass of launch vehicles and missiles, increase the payload and range , Reduce launch costs. The function of the general missile launching box is only used to launch missiles and does not possess the functions of storing and transporting missiles simultaneously. Such a box body structure is cylindrical. In the MX missile finalized by the United States in the late 1980s, the cylindri...

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): F42B15/00
Inventor 王熙李思简
Owner SHANGHAI JIAO TONG UNIV
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