民机复合材料维修试验方案设计及实施

维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提。以复合材料层压板作为模拟实际维修对象,对维修试验方案的设计及实施进行了实践探索,首先从效果评定、方法确定、模型建立、母板数量确定四个方面对维修试验方案的设计进行了说明;然后介绍了维修固化参数的确定;最后从打磨、清洁、铺层、封装、固化步骤阐述了维修过程的实施。实践证明,经过不断优化的试验方案及维修实施过程可以很好地建立实际复合材料维修中维修参数和维修效果的内在关联。...

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Published in实验室研究与探索 Vol. 34; no. 6; pp. 20 - 22
Main Author 杨文锋 张吉武 周长春 唐庆如
Format Journal Article
LanguageChinese
Published 中国民用航空飞行学院航空工程学院,四川广汉,618307 2015
Subjects
民机复合材料
维修参数
维修实施
维修方案设计
维修模型
维修方案设计
repair program designs
民机复合材料
维修实施
维修参数
repair models
civil aircraft composites
repair implementation
维修模型
repair parameters
Online AccessGet full text
ISSN1006-7167

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Abstract 维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提。以复合材料层压板作为模拟实际维修对象,对维修试验方案的设计及实施进行了实践探索,首先从效果评定、方法确定、模型建立、母板数量确定四个方面对维修试验方案的设计进行了说明;然后介绍了维修固化参数的确定;最后从打磨、清洁、铺层、封装、固化步骤阐述了维修过程的实施。实践证明,经过不断优化的试验方案及维修实施过程可以很好地建立实际复合材料维修中维修参数和维修效果的内在关联。
AbstractList TB332%V219; 维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提.以复合材料层压板作为模拟实际维修对象,对维修试验方案的设计及实施进行了实践探索,首先从效果评定、方法确定、模型建立、母板数量确定四个方面对维修试验方案的设计进行了说明;然后介绍了维修固化参数的确定;最后从打磨、清洁、铺层、封装、固化步骤阐述了维修过程的实施.实践证明,经过不断优化的试验方案及维修实施过程可以很好地建立实际复合材料维修中维修参数和维修效果的内在关联.
维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提。以复合材料层压板作为模拟实际维修对象,对维修试验方案的设计及实施进行了实践探索,首先从效果评定、方法确定、模型建立、母板数量确定四个方面对维修试验方案的设计进行了说明;然后介绍了维修固化参数的确定;最后从打磨、清洁、铺层、封装、固化步骤阐述了维修过程的实施。实践证明,经过不断优化的试验方案及维修实施过程可以很好地建立实际复合材料维修中维修参数和维修效果的内在关联。
Author 杨文锋 张吉武 周长春 唐庆如
AuthorAffiliation 中国民用航空飞行学院航空工程学院,四川广汉618307
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Author_FL YANG Wen-feng
TANG Qing-ru
ZHANG Ji-wu
ZHOU Chang-chun
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DocumentTitleAlternate Repair Test Program Designs and Implementation of Civil Aircraft Composites
DocumentTitle_FL Repair Test Program Designs and Implementation of Civil Aircraft Composites
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Issue 6
Keywords 维修方案设计
repair program designs
民机复合材料
维修实施
维修参数
repair models
civil aircraft composites
repair implementation
维修模型
repair parameters
Language Chinese
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Notes The quality of repair has a direct effect to aircrafts＇ inherent reliability and safety,and making up a scientific and reasonable test program is the precondition for the research of the internal correlation between repair parameters and the relatively repair effects of civil aircraft composites. By using composite laminates as the research object to simulate actual repairs,the designs and implementation of the repair test program were explored in practical. The study first explained the design of repair models,based on four aspects： effect assessment,method determination,model building and the number of parent plates. Then the determining of repair cure parameters was introduced. At last, the implementation of repair process was elaborated in the sequence of polishing,cleaning,laminating,packaging and curing. The results showed that,in the field of composites repair,the optimized repair test program and process implementation promised to establish better the internal correlation between repair parameters and
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PublicationTitle 实验室研究与探索
PublicationTitleAlternate Laboratory Research and Exploration
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PublicationYear 2015
Publisher 中国民用航空飞行学院航空工程学院,四川广汉,618307
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Snippet 维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提。以复合材料层压板作为模拟实际维修对...
TB332%V219; 维修效果的好坏直接影响到航空器的固有可靠性与安全性,制定科学合理的试验方案是探究民机复合材料维修参数和维修效果内在联系的前提.以复合材料层压板作为模...
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SubjectTerms 民机复合材料
维修参数
维修实施
维修方案设计
维修模型
Title 民机复合材料维修试验方案设计及实施
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