| 某战术导弹发动机扩散段绝热层缠绕成型工艺改进 |
| |
| 引用本文： | 王建华.某战术导弹发动机扩散段绝热层缠绕成型工艺改进[J].上海航天,2006,23(4):58-60. |
| |
| 作者姓名： | 王建华 |
| |
| 作者单位： | 国防科学技术大学,航天与材料工程学院,湖南,长沙,410073 |
| |
| 基金项目： | 致谢：作者对上海新力动力设备研究所范世达研究员在试验前期的工艺指导,以及上海复合材料科技有限公司苑玲总经理和陈孝银副总工程师的支持表示衷心感谢. |
| |
| 摘 要： | 为消除某战术导弹发动机扩散段绝热层内表面出现沟槽等缺陷,对缠绕热压罐成型工艺进行了研究。通过分析和试验确定了高硅氧/酚醛预浸布带性能、缠绕张力、缠绕温度和加压时间等工艺参数,以及热压罐固化曲线,并从理论上讨论了成型的缠绕张力、缠绕温度和加压时间等的影响。性能测试结果表明,工艺改进后扩散段绝热层沟槽基本消除,制品性能提高。
|
| 关 键 词： | 战术导弹发动机 扩散段绝热层 缠绕 热压罐成型 沟槽 工艺参数 固化曲线 |
| 文章编号： | 1006-1630（2006）04-0058-03 |
| 收稿时间： | 2005-08-30 |
| 修稿时间： | 2005-11-14 |
Forming Technology Improvement of Winding Extendible Nozzle Exit for Some Tactical Missile Engine |
| |
| WANG Jian-hua.Forming Technology Improvement of Winding Extendible Nozzle Exit for Some Tactical Missile Engine[J].Aerospace Shanghai,2006,23(4):58-60. |
| |
| Authors: | WANG Jian-hua |
| |
| Institution: | College of Aerospace and Material Engineering, NUDT, Changsha Hunan 410073, China |
| |
| Abstract: | The technology of autoclave moulding was studied to eliminate the ditches on the inner surface of extendible nozzle exit cone for some tactical missile engine in this paper.The technological parameters such as the performance of high silicone/phenolic resin prepreg tape,winding tension,winding tempreture and pressure opportunity were determined by analysis and experiment,and so was the curing curve of autoclave moulding.The effect of winding tension,winding tempreture and pressure opportunity was discussed in theory.The performance test result showed that the ditches were disappeared after the technology improved,and performance of the product was improved. |
| |
| Keywords: | Tactical missile engine Extendible nozzle exit Winding Autoclave moulding Technological performance Curing curve |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
