Method for realization of co-curing of reinforcing rib web composite produced part by high strength soft tooling

A high-strength, stiffening rib technology, applied in the field of high-performance carbon fiber composite structural parts manufacturing, can solve the problems of high manufacturing and maintenance costs of metal core molds, affecting the internal molding quality of the parts, and excessive thickness of the T-shaped ribs of the parts. , to improve the qualification rate and efficiency, avoid the thermal hysteresis effect, and reduce the manufacturing cycle.

Inactive Publication Date: 2015-01-21
航天海鹰(镇江)特种材料有限公司
View PDF3 Cites 14 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantages of using the mandrel mainly include the following three aspects: (1) Since the mandrel itself has a certain rigidity, it is difficult to achieve uniformity and accuracy in transmitting external pressure through the mandrel, and it is easy to cause the thickness of the T-shaped rib part of the part to be out of tolerance; ( 2) Since the core mold has a certain thickness, according to the heat conduction effect, the temperature rise rate of the T-shaped rib part of the part will lag behind that of other parts, thus affecting the internal molding quality of the part; (3) Since the core mold is made of metal, its own weight is relatively large , very inconvenient to operate
At the same time, the manufacturing and maintenance costs of the metal mandrel are relatively high, and the manufacturing cycle for repair or reprocessing is relatively long

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
  • Method for realization of co-curing of reinforcing rib web composite produced part by high strength soft tooling
  • Method for realization of co-curing of reinforcing rib web composite produced part by high strength soft tooling
  • Method for realization of co-curing of reinforcing rib web composite produced part by high strength soft tooling

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0027] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0028] The invention uses a metal mold to form a fiber-reinforced rubber soft tooling. After the soft tooling is formed, it has a certain structural rigidity through reinforcement means. Finally, the soft tooling is used to complete the vertical and horizontal T-shaped ribs to strengthen the web structure. molding process. The detailed process is as follows:

[0029] Firstly, by means of mechanical manufacturing, a metal dummy that is exactly the same in size as the composite material part, and the bottom plate of the soft tooling molding mold with surrounding baffles are processed. There is a cooperative relationship between the two, such as figure 1 shown.

[0030] Use the cavity formed by the metal dummy and the surrounding baffles to lay soft tooling. The soft tooling uses silicone rubber as the main material, and the rubber is laid laye...

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 discloses a method for realization of co-curing of a reinforcing rib web composite produced part by high strength soft tooling, rubber produced soft tooling is formed by use of a metal false piece, and the composite produced part is formed by use of the soft tooling. The soft tooling self is provided with a carbon fiber reinforced layer, the size of the product formed by use of the soft tooling can be guaranteed, outside pressure and temperature can be better transferred to the composite produced part, uneven partial pressure, heating rate hysteresis and other phenomena of the produced part can be avoided, the soft tooling is provided with a support structure, paving and preloading and other operation of the produced part can be completed on the soft tooling, the relative position precision and shape size of each part of the formed produced part can be ensured, the soft tooling can be used repeatedly, the reproduction is also more convenient, and the production cost and the manufacturing cycle are effectively reduced.

Description

technical field [0001] The invention relates to the technical field of advanced composite material manufacturing, in particular to the manufacturing of high-performance carbon fiber composite structural parts in the aircraft, spacecraft and automobile industries. Background technique [0002] Resin-based carbon fiber composite materials have superior properties such as specific strength and specific stiffness, strong designability, good fatigue fracture resistance, corrosion resistance, and good dimensional stability. They are currently widely used in aviation, aerospace, transportation and other fields. High-performance structural materials. Among various carbon fiber composite molding processes, the autoclave process has uniform molding temperature and pressure, and has good adaptability to parts of different materials, shapes, sizes and structures. One of the main process methods of material components. [0003] With the increasing requirements for the strength and stif...

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): B29C70/44B29C70/34B29C70/54
CPCB29C70/44B29C70/54
Inventor 贾傲黎玉钦王国平高志强左扬盛毅郭渊缪伟民
Owner 航天海鹰(镇江)特种材料有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products