航空学报 > 1996, Vol. 17 Issue (4): 473-476

强度型损伤自诊断智能结构中四点法布置的研究

袁慎芳, 陶宝祺, 熊克, 梁大开   

  1. 南京航空航天大学智能结构研究所,南京,210016
  • 收稿日期:1995-04-04 修回日期:1995-08-10 出版日期:1996-08-25 发布日期:1996-08-25

RESEARCH ON STRENGTH DAMAGE SELF-DIAGNOSTIC SMART STRUCTURE USING FOUR SENSORS ARRANGEMENT

Yuan Shenfang,Tao Baoqi,Xiong Ke,Liang Dakai   

  1. Smart Structure Institute of Nanjing University of Aeronautics and Astronautics,Nanjing,210016
  • Received:1995-04-04 Revised:1995-08-10 Online:1996-08-25 Published:1996-08-25

摘要: 介绍了一种能够实时大面积地进行复合材料损伤或大应变位置自诊断的智能结构系统 ,从理论及实验两方面对复合材料平板进行了应力分析 ,讨论了作为传感元件的电阻应变丝阵列在结构中的布置方案 ,提出了四点布置法的方案 ,还介绍了按此方案实际实现的实时损伤自诊断智能结构系统 ,该系统具有较高的自诊断成功率

Abstract: This article introduces a kind of smart structure system which can in real time and in a large area self\|diagnose the damage or large strain position in the composite material. From theory and experiment,the strain distribution in the composite material plate is analysed in this article and the arrangement of the strain resistant wires as sensors in the structure is discussed. A four sensors arrangement method is put forward. This article also introduces an actually realised real\|time damage self\|diagnosis smart structure system.This structure can work well.

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