航空科学技术
航空科學技術
항공과학기술
AERONAUTICAL SCIENCE AND TECHNOLOGY
2015年
3期
54-58
,共5页
飞机%复合材料结构%适航符合性%验证思路
飛機%複閤材料結構%適航符閤性%驗證思路
비궤%복합재료결구%괄항부합성%험증사로
aircraft%composite structure%airworthiness%veriifcation
总结了复合材料结构的特点，分析了CCAR-25部中适用于复合材料结构的适航条款，明晰了复合材料结构在材料、设计、制造、验证等方面需遵循的适航要求。在此基础上结合咨询通告AC20-107B和相关工业标准，给出复合材料结构适航符合性验证思路。
總結瞭複閤材料結構的特點，分析瞭CCAR-25部中適用于複閤材料結構的適航條款，明晰瞭複閤材料結構在材料、設計、製造、驗證等方麵需遵循的適航要求。在此基礎上結閤咨詢通告AC20-107B和相關工業標準，給齣複閤材料結構適航符閤性驗證思路。
총결료복합재료결구적특점，분석료CCAR-25부중괄용우복합재료결구적괄항조관，명석료복합재료결구재재료、설계、제조、험증등방면수준순적괄항요구。재차기출상결합자순통고AC20-107B화상관공업표준，급출복합재료결구괄항부합성험증사로。
Compared with metal structure, the characteristics of composites structures were presented. Then, based on the research of airworthiness requirement applicable to composite aircraft structures in CCAR-25, clariifed the airworthiness requirements, which should be followed during material selection, design, manufacture and verification process. Based on this, presented the veriifcation methods for composite aircraft structure, combining with AC20-107B adn other related industry standards.
