航空学报 > 1992, Vol. 13 Issue (12): 641-650

智能复合材料结构在未来飞机上的应用

陶宝祺, 梁大开, 王征, 袁慎芳   

  1. 南京航空学院传感器与测试技术研究所 南京 210016
  • 收稿日期:1992-10-15 修回日期:1900-01-01 出版日期:1992-12-25 发布日期:1992-12-25

APPLICATIONS OF SMART COMPOSITE STRUCTURE IN FUTURE AIRCRAFT

Tao Bao-qi, Liang Da-kai, Wang Zheng, Yuan Shen-fang   

  1. Sensoring and Testing Research Institute, Nanjing Aeronautical Institute, Nanjing, 210016
  • Received:1992-10-15 Revised:1900-01-01 Online:1992-12-25 Published:1992-12-25

摘要: 智能复合材料结构是将传感器阵列、接收器件、发射器件埋嵌在复合材料中,将结构与电子系统功能溶合的一种新结构。美国计划在21世纪初研制出全智能结构飞机。本文仅说明智能复合材料结构在飞机上的应用前景,并从损伤评估、应变测量、改变应力、抑制振动以及天线元件等方面介绍当前的研究成果。

关键词: 智能结构, 飞机, 复合材料

Abstract: Smart composite structure is a novel structure in which sensor arrays, receivers and transmitters are embedded. It combines the functions of electronic systems with those of structure. The United States intends to design an aircraft of intergrated smart structure at the beginning of the 21st century. The prospects of smart composite structure for future aircraft applications are discussed in this paper. And the research results of damage assessment, strain measurement, stress changing, vibration suppression and antenna components will also be introduced.

Key words: smart structure, aircraft, composite