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基于结构健康监测的飞机结构MSG-3分析 被引量：2

Aircraft Structure MSG-3 Analysis Based on Structural Health Monitoring
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摘要 结构健康监测(SHM)技术被广泛引入到了飞机设计与维护,本文依据现阶段SHM技术的发展现状,将SHM技术与MSG-3分析思想融合,制定了一种针对采用SHM技术飞机结构的计划维修分析流程。 Structural health monitoring （SHM） technology was widely introduced to the aircraft design and ma- intenance, based on the current development of SHM technology, this paper integrates the SHM and MSG-3 analysis, and presents a formulation process of the aircraft structural scheduled maintenance task with the application of SHM technology.
作者 蔡禹舜 朱昊 卿新林
机构地区 上海飞机客户服务有限公司 中国商飞北京民用飞机技术研究中心
出处 《宇航材料工艺》 CAS CSCD 北大核心 2015年第6期71-74,共4页 Aerospace Materials & Technology
关键词 飞机结构 复合材料 结构健康监测 计划维修分析 MSG-3 Aircraft structure, Composite material, Structure health monitoring, Schedule maintenance analysis, MSG-3
分类号 V267.31 [航空宇航科学与技术—航空宇航制造工程]
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  • 1Staszewski W J,Traynor S M R. Health monitoring of aerospace composite structures-Active and passive approach [J].Composites Science and Technology, 2009,69 (11/12) : 1678--1685.
  • 2Baker A, Dutton S, Kelly D. Composite Materials for Aircraft Structures. Second Edition[M] . Virginia.. American Institute for Aeronautics and Astronautics, 2004:1--3.
  • 3Holger S, Henrik R. Structural health monitoring: a contribution to the intelligent aircraft structure[C]//19th European Conference on NDT, Berlin, Germany, 2006.
  • 4Stefani A M. Review of Air Carriers'use of Aircraft Repair Station[R]. FAA Report Number AV--2003 047, 2003.
  • 5Bethel K, Catha S C B, et al. The Development and Validation of a High Strength, Self Monitoring, Composite Tight Fit Liner for Offshore Pipelines and Risers[C]//Fourth International Conference on Composite Materials for Offshore Operations, Houston, Texas, USA, 2005.
  • 6Yan Y J, et al. Development in vibration-based structural damage detection technique[J]. Mechanical Systems and Signal Processing. 2007,21 (5) : 2198-- 2211.
  • 7Stehmeier H, Speckman H, Bolten J. Comparative vacuum monitoring of fatigue cracking in aircraft structures [C]//2^nd European Workshop on SH M, Munich Germany, July,2004.
  • 8Wheatly, et al. Comparative vacuum monitoring as an alternate means of compliance[J]. Insite-Non Destructive Testing and Condition Monitoring,2005,47(3) : 153-- 156.
  • 9Weller P P,et al. Use of heat emitted by broken optic fibers..a new approach for damage detection in composites[J].Engineering Failure Analysis, 2005,2 (6): 860 - 874.
  • 10Su Z, Ye L A. Damage identification technique for CF/EP composite laminates using distributed piezoelectric transducers[J]. Composite Structures, 2002 (57): 465 -- 471.

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宇航材料工艺
2015年 第6期

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