...
首页> 外文期刊>SAMPE Journal >Technical Developments in Thermoplastic Composite Fuselages
【24h】

Technical Developments in Thermoplastic Composite Fuselages

机译:热塑性复合材料机身的技术发展

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Tomorrow's aircraft fuselage will have to meet increasingly optimized performance requirements and cost reduction objectives. The use of composite materials, associated with the development of new industrial scenarios should enable both these objectives to be achieved. For the last three years, a thermoplastic composite fuselage has been under study [1] and development within the framework of a research project associating Aerospatiale Aircraft, Eurocopter and Dassault-Aviation. Two technological processes studied in this research project, a thermoplastic "sheet forming" process and a process called "in-situ consolidation" are presented and several examples of aeronautical applications are given.
机译:明天的飞机机身将必须满足日益优化的性能要求和降低成本的目标。与新工业情景的发展相关的复合材料的使用应使这两个目标得以实现。在过去的三年中,一直在研究热塑性复合材料机身[1],并在航空航天飞机,欧洲直升机公司和达索航空的研究项目框架内进行了开发。在此研究项目中研究了两个技术过程,即热塑性“片材成型”过程和称为“原位固结”的过程,并给出了航空应用的几个示例。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号