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一种多参数小型化飞机结构腐蚀环境监测技术
引用本文:常鸣,袁慎芳,王长春.一种多参数小型化飞机结构腐蚀环境监测技术[J].装备环境工程,2014,11(6):15-21.
作者姓名:常鸣  袁慎芳  王长春
作者单位:1. 南京航空航天大学 机械结构力学及控制国家重点实验室,南京210016; 扬州大学 水利与能源动力工程学院,江苏 扬州225000
2. 南京航空航天大学 机械结构力学及控制国家重点实验室,南京,210016
基金项目:国家杰出青年基金,江苏省优势学科建设项目资助@@@@Fund:Supported by National Science Fund for Distinguished Young Scholars,Advanced Discipline Construction Foundation of Jiangsu Province of China
摘    要:目的研究腐蚀与环境条件之间的关系,提出一种用于飞机腐蚀环境监测的小型化监测节点的实现方法。方法针对影响腐蚀的4个关键环境参数(温度、相对湿度、湿润时间和氯离子浓度),研究其传感方法并研发选型相应传感器。在此基础上设计基于MSP430处理器的多参数飞机腐蚀环境监测节点。结果通过实验验证了节点中的温湿度传感器、湿润时间传感器和电化学传感器的适用性,能够完成对环境参数的的测量。结论设计的节点满足机载装置小型化、轻量化的要求,可以实现在线的腐蚀环境监测,从而保障飞行安全。

关 键 词:飞机结构  腐蚀环境监测  多参数  监测节点
收稿时间:2014/8/12 0:00:00
修稿时间:2014/12/15 0:00:00

A Multi-parameter Miniaturization Monitoring Node for Aircraft Corrosive Environments
CHANG Ming,YUAN Shen-fang and WANG Chang-chun.A Multi-parameter Miniaturization Monitoring Node for Aircraft Corrosive Environments[J].Equipment Environmental Engineering,2014,11(6):15-21.
Authors:CHANG Ming  YUAN Shen-fang and WANG Chang-chun
Institution:1. The State Key Lab of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2. School of Hydraulic, Energy and Power Engineering, Yangzhou University, Yangzhou 225000, China;The State Key Lab of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;;The State Key Lab of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Abstract:Objective To study the relationship between corrosion and environment, a realizing method of the multi-pa- rameter miniaturization monitoring node for aircraft corrosive environments was proposed in this paper. Methods Four key environmental parameters which are the major factors affecting the corrosion were selected: temperature, humidity, time of wetness (TOW) and chloride ion concentration. And the corresponding sensors were chosen or designed for monitoring. Besides, this paper introduced a miniaturization monitoring node which could realize the measurements of multiple corrosive environmental parameters. The monitoring node was based on the Texas Instruments MSP430 micro-controller and includ- ed the aforementioned sensors. Results In the end, the verifications showed that the humidity and temperature sensor, the TOW sensor, and the electrochemical sensor were available; the measurements of four parameters could be performed cor- rectly by the node. Conclusion Featuring a small volume and low weight, the node was applicable for on-aircraft corrosion monitoring. And this approach will provide actionable knowledge for aircraft maintainers, such that the aircraft safety could be driven to increased levels.
Keywords:aircraft structure  monitoring of corrosive environments  multi-parameter  monitoring node
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