Method for using open-type rubber soft die for realization of thin-wall I-beam structure composite material part

A composite material and I-beam technology, applied in the field of composite material manufacturing, can solve problems such as high manufacturing and maintenance costs of metal core molds, excessive thickness of thin-walled composite parts, and reduced service life and reliability of airbags, etc., to achieve Long service life, avoid thermal hysteresis effect, avoid the effect of uneven pressure

Inactive Publication Date: 2016-05-25
航天海鹰(镇江)特种材料有限公司
View PDF4 Cites 24 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The disadvantages of using the mandrel method to form I-beams mainly include the following three aspects: 1. Because the mandrel itself has a certain rigidity, it is difficult to achieve uniform and accurate conduction of external pressure through the mandrel, and it is easy to cause the thickness of thin-walled composite parts. 2. Since the core mold has a certain thickness and the thickness is not uniform, according to the heat transfer effect, the heating rate of different regions of the part will be different, which will affect the internal molding quality of the part, resulting in Large deformation; 3. Since the mandrel is made of metal, it has a large weight and is very inconvenient to operate
At the same time, t...

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 using open-type rubber soft die for realization of thin-wall I-beam structure composite material part
  • Method for using open-type rubber soft die for realization of thin-wall I-beam structure composite material part
  • Method for using open-type rubber soft die for realization of thin-wall I-beam structure composite material part

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0024] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0025] The open rubber soft mold made of fiber-reinforced rubber is formed by the metal mold. After the rubber soft mold is formed, it will be used as a part of the forming mold to complete the molding process of the composite material part. The detailed process is as follows:

[0026] Through the method of mechanical manufacturing, process a metal dummy that is completely consistent with the outer dimensions of the composite material, and a soft rubber mold with a baffle. There is a cooperative relationship between the parts of the mold, and the clamping of the upper and lower templates The groove will play a certain role in limiting the metal dummy (such as figure 1 shown).

[0027] Use the cavity formed by the metal dummy and the upper and lower baffles to pave the rubber soft mold. The rubber soft mold uses rubber as the main material, a...

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 present invention discloses a method for using an open-type rubber soft die for realization of a thin-wall I-beam structure composite material part, by a machine manufacturing method, a metal false part with a boundary dimension which is entirely consistent with the boundary dimension of the composite material part is processed, a rubber soft die molding mold with a baffle is also processed, a rubber soft die is paved and pasted in a cavity formed by the metal false part and upper and lower templates, the external part of the rubber soft die is vacuum-sealed with a vacuum bag, and the rubber soft die is molded in a hot-pressing tank; after the rubber soft die is molded, the vacuum bag is removed, the metal false part is taken out, and filled with a composite material, then the external part of the rubber soft die is vacuum-sealed with the vacuum bag, and thee rubber soft die is molded in the hot-pressing tank to obtain the I-beam structure composite material part. The method can avoid the thickness over-deviation phenomenon of the composite material part, avoids the thermal hysteresis phenomenon, effectively guarantees the molding quality of the part, and improves the passing rate and efficiency of production.

Description

technical field [0001] The invention belongs to the technical field of composite material manufacturing, and in particular relates to a method for manufacturing high-performance carbon fiber composite structural parts in the industry of aircraft, spacecraft and automobiles. 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] Thin-walled I-beams are relatively common reinf...

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
IPC IPC(8): B29C70/34
CPCB29C70/342
Inventor 贾傲黎玉钦王国平马秀菊谢海洋黄毅
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