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材料工程  2017, Vol. 45 Issue (11): 139-142    DOI: 10.11868/j.issn.1001-4381.2017.001084
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民用航空材料适航审定
沈小明1, 陈挺2, 张迎春2
1. 中国民用航空 适航审定中心, 北京 100102;
2. 中国民用 航空 上海航空器适航审定中心, 上海 200335
Airworthiness Certification of Civil Aviation Materials
SHEN Xiao-ming1, CHEN Ting2, ZHANG Ying-chun2
1. Airworthiness Certification Center of CAAC, Beijing 100102, China;
2. Shanghai Aircraft Airworthiness Certification Center of CAAC, Shanghai 200335, China
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摘要 以适航规章研究为基础,结合民用航空器适航审定的经验,分析适航规章对材料的适航条款,总结出对材料的核心适航要求是:材料应符合某种材料规范,材料规范保证材料具有设计资料所采用的强度性能和其他性能。分析国内民用航空材料适航管理方法,提出改进建议:(1)依据CCAR21.351至371条和CCAR 37的有关规定,对民用航空材料开展单独适航管理;(2)研究并推广基于统计的材料规范制定方法,用于建立能够保证材料具有设计资料所采用的强度性能和其他性能的材料规范;(3)建立民用航空材料协作机制,基于统计建立民用航空材料设计值手册,降低适航取证成本。最后给出材料规范建立过程中可采用的统计方法,为材料规范的建立提供了技术方法。
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沈小明
陈挺
张迎春
关键词 民用航空适航审定材料规范统计    
Abstract:Based on years of airworthiness regulations research, combined with the experience of airworthiness certification of civil aviation products, the airworthiness requirement to materials for civil aviation products was analyzed. The key airworthiness requirement for materials is that materials should conform to some material specification to ensure their having the strength and other properties adopted in the design data. The shortcomings of domestic airworthiness management methods for civil aviation materials was discussed and three recommendations for improvement were proposed:(1) conduct individual airworthiness management for civil aviation materials according to CCAR 21.351 through 371 and CCAR 37; (2) develop and promote statistical-based material specification developing methods, to establish material specifications which could ensure material having the strength and other properties adopted in the design data; (3) establish a cooperation mechanism for developing material design value data base for civil aviation materials to reduce the cost of airworthiness certification activities. At the end of this paper, statistical methods used for establishing material specifications were discussed.
Key wordscivil aviation    airworthiness certification    material specification    statistics
收稿日期: 2017-08-26      出版日期: 2017-11-18
中图分类号:  V250  
通讯作者: 沈小明(1963-),男,高级工程师,长期从事民用飞机适航审定管理和适航审定技术研究,联系地址:北京市朝阳区花家地东路3号中国适航审定中心(100102),E-mail:shenxm_acc@caac.gov.cn     E-mail: shenxm_acc@caac.gov.cn
引用本文:   
沈小明, 陈挺, 张迎春. 民用航空材料适航审定[J]. 材料工程, 2017, 45(11): 139-142.
SHEN Xiao-ming, CHEN Ting, ZHANG Ying-chun. Airworthiness Certification of Civil Aviation Materials. Journal of Materials Engineering, 2017, 45(11): 139-142.
链接本文:  
http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2017.001084      或      http://jme.biam.ac.cn/CN/Y2017/V45/I11/139
[1] 中国民用航空局. 正常类、实用类、特技类和通勤类飞机适航标准(CCAR23-R3)[S].2005.
[2] 中国民用航空局. 运输类飞机适航标准(CCAR25-R4)[S].2011.
[3] 中国民用航空局. 正常类旋翼航空器适航规定(CCAR27-R1)[S].2002.
[4] 中国民用航空局. 运输类旋翼航空器适航规定(CCAR29-R1)[S].2001.
[5] 中国民用航空局. 航空发动机适航规定(CCAR33-R2)[S].2011.
[6] 中国民用航空局. 螺旋桨适航标准(CCAR-35)[S].1987.
[7] SAE International. Editorial style manual for the preparation of aerospace material specifications metallic and process and nonmetallic materials[S].2002.
[8] Federal Aviation Administration. Metallic materials properties development and standardization (MMPDS)[Z].2012.
[9] Federal Aviation Administration. Material strength properties and material design values (AC 25.613-1)[Z].2003.
[10] Federal Aviation Administration. Acceptance of composite specifications and design values developed using the NCAMP process (Memorandum AIR100-2010-120-003)[Z].2010.
[11] WARD S, McCARVILL W, TOMBLIN J. Guidelines and recommended criteria for the development of a material specification for carbon fiber/epoxy fabric prepregs(DOT/FAA/AR-06/10)[R]. Federal Aviation Administration, 2007.
[12] McCARVILL W, WARD W, BOGUCKI G. Guidelines and recommended criteria for the development of a material specification for carbon fiber/epoxy unidirectional prepregs update (DOT/FAA/AR-07/3)[R]. Federal Aviation Administration, 2007.
[13] TOMBLIN J S, NG Y C, RAJU K S. Material qualification and equivalency for polymer matrix composite material systems:updated procedure (DOT/FAA/AR-03/19)[R]. Federal Aviation Administration, 2003.
[14] SAE International. Composite materials handbook-17 composite materials handbook-17(CMH-17) volume 1[M].PA:SAE International, 2012.
[15] AIR4779 C. User's guide to AMS specifications[S].
[16] AS9103A. Aerospace series-quality management systems-variation management of key characteristics[S].2012.
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