首页> 美国政府科技报告 >Integrity Control of Carbon Fiber Reinforced Plastics (CFRP) Structural Elements. Conclusion with Respect to the Control Methodology of CFRP Primary Structures in Manned Space Flight and the Implications to the Design, Analysis an
【24h】

Integrity Control of Carbon Fiber Reinforced Plastics (CFRP) Structural Elements. Conclusion with Respect to the Control Methodology of CFRP Primary Structures in Manned Space Flight and the Implications to the Design, Analysis an

机译:碳纤维增强塑料(CFRp)结构元素的完整性控制。关于载人航天飞行中CFRp主要结构控制方法的结论及其对设计的启示,分析

获取原文

摘要

A three fold control logic related to development, manufacturing, and operation of safety relevant structures is established in order to exclude catastrophic failures of CFRP-elements due to the existence of global degradation or local defects. Verification of integrity control requirements during development; design concepts for critical structural items; global deviations and local defects; stress evaluation; material properties; the impact of macroscopic defects on the static capability; the degradation of capabilities with increasing operational life; nondestructive inspection of CFRP elements; and a simplified design procedure are discussed.

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