研究和验证基于CF/PEEK的杆压和压工艺,用于轨道上的异形成型
Jiayong Yan1,2, Peng Li1,3, Chao Geng1,3
1Mechanical Engineering College, Yanshan University, Qinhuangdao 066004, China.
Materials (Basel, Switzerland)
|May 25, 2024
概括
开发了一种新工艺,用于制造用于太空制造的连续碳纤维 (CF) /聚-- (PEEK) 杆. 这种高效的成型技术优化了高性能,具有成本效益的空间结构的参数.
科学领域:
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
- 制造过程 制造过程 制造过程
背景情况:
- 在轨道上不断制造太空架构带来了重大挑战.
- 现有的方法可能不适合在太空中制造高性能结构部件.
研究的目的:
- 建议和验证碳纤维 (CF) /聚乙基 (PEEK) 前带的新型压和压成型工艺,以实现在轨道上的连续螺杆制造.
- 调查关键过程参数对杆形成的影响,并优化成型技术.
主要方法:
- 利用数值模拟和实验验证来分析压缩和压缩过程.
- 开发了一种高效的杆卷,内轨,均等材料成型方法,并确定了模具配置.
- 对于单向CF/PEEK prepreg条的相当宏观机械性能,用于杆形成研究.
主要成果:
- 建立了形成负载,温度和形成速度之间的关系.
- 证明温度和速度显著影响杆表面质量,材料填充密度和机械性能.
- 通过模拟和实验验证,确定了最佳的成型过程参数.
结论:
- 开发的成型技术提供了高效率,低能耗和高集成,用于制造高性能杆.
- 这一过程为降低制造成本和提高航空航天应用效率提供了新的有效解决方案.
- 该技术适用于在轨道环境中连续制造结构.
相关概念视频
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