Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets

LUO Peng; GAO Lanning; WANG Bin; XIAO Jun

doi:10.16080/j.issn1671-833x.2017.1/2.112

您当前的位置：

首页 >

文章列表页 >

Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets

更新时间：2025-10-30

- Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets
- Aeronautical Manufacturing Technology Vol. 60, Issue 1/2, (2017)
- 作者机构：
  
  1. 南京航空航天大学材料学院,南京,210016
  2. 中航通飞华南飞机工业有限公司,珠海,519040
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2017.1/2.112
  CLC：
- Published：2017
- 稿件说明：
移动端阅览
罗　鹏1，2，高兰宁2，王　彬2，肖　军1. 轻型公务机碳纤维复合材料增压舱共固化成型工艺的试验研究*[J]. 航空制造技术, 2017, 60(1/2): 112-116. LUO Peng1,2,GAO Lanning2, WANG Bin2, XIAO Jun1. Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets. Aeronautical Manufacturing Technology, 2017, 60(1/2): 112-116.

LUO Peng, GAO Lanning, WANG Bin, et al. Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets[J]. Aeronautical Manufacturing Technology, 2017, 60(1/2).
罗　鹏1，2，高兰宁2，王　彬2，肖　军1. 轻型公务机碳纤维复合材料增压舱共固化成型工艺的试验研究*[J]. 航空制造技术, 2017, 60(1/2): 112-116. LUO Peng1,2,GAO Lanning2, WANG Bin2, XIAO Jun1. Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets. Aeronautical Manufacturing Technology, 2017, 60(1/2): 112-116. DOI： 10.16080/j.issn1671-833x.2017.1/2.112.

LUO Peng, GAO Lanning, WANG Bin, et al. Experimental Study on the Pressurized Cabin Co-Curing Process of Carbon Fiber/Epoxy Prepreg of Light Business Jets[J]. Aeronautical Manufacturing Technology, 2017, 60(1/2). DOI： 10.16080/j.issn1671-833x.2017.1/2.112.

摘要

以轻型高端公务机领世300 增压舱共固化成型技术为研究背景，针对增压舱为固化炉整体成型的特点，借助DSC 对T700G-12K 碳纤维/ 环氧预浸料的固化温度和固化度进行了研究与分析

优化固化工艺参数。通过无损检测C 扫描和力学测试进行验证。试验结果表明：增压舱固化工艺采用凝胶点温度80℃下处理240min

105℃下保温保压120min 以及130℃下保温保压120min 为本组试验的最优方案，产品缺陷少。

Abstract

The pressurized cabin Co-curing technique of carbon fiber/epoxy prepreg for light high-end business jet AG300 was introduced and studied in this work common background.According to the characteristics of overall molding pressure cabin for curing furnace

with the aid of DSC to T700G-12K carbon fiber/epoxy presoak curing temperature and curing degree has carried on the research and analysis

optimization of curing process parameters validated through the nondestructive testing(NDT) C scan and mechanical testing.The results of the test indicate

The prepreg curing progress of the pressurized cabin using the gel point temperature of 80℃ for 240min under pressure

then cured at 105℃ for 120min

finally at 130℃ for 120min. It was the optimal scheme of the experimental group

fewer product defects.

关键词

Keywords

references

Views

610

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

A Novel Approach of Liquid Composite Molding Co-Curing Process of T-Stiffened Composite Structure

Development of Reinforced Composites Skin

Manufacture Process and Quality Control of Composites Cover Panel of Wing Fuel Tank

Modulation of Pore Structure and Properties in Phenolic Aerogels by Cationic Polyelectrolytes

Research Progress on Matrix Composition Regulation of SiC/SiC Composites

Related Author

LIU Yanan

YUAN Chongxin

ZHAO Xinfu

LI Yonghang

程勇

彭建

罗辑

李建川

Related Institution

Beijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science & Technology Research Institute of COMAC

成都飞机工业集团复合材料加工厂

北京航空材料研究院

空军某部军事代表室

The platform construction and operation are provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：34726 Visits Today：204

⁰