| 某型直升机重要改装设计批准符合性验证研究 |
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| 引用本文： | 郑庆,李艳军,曹愈远,王小明.某型直升机重要改装设计批准符合性验证研究[J].滨州师专学报,2013(6):48-52. |
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| 作者姓名： | 郑庆 李艳军 曹愈远 王小明 |
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| 作者单位： | 南京航空航天大学民航学院,江苏南京211106 |
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| 摘 要： | 基于对中国民用航空规章CCAR27部正常类旋翼航空器适航规定条款的深入研究，确定某型直升机重要改装设计批准（MDA）的审定基础，提出了重要改装挂架在极限惯性载荷作用下的适航符合性验证方法，为某型直升机取得重要改装设计批准提供技术支持．
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| 关 键 词： | 适航审定 符合性验证 极限载荷 |
Research on Compliance Verification and Design Modification Approval for a Certain Type of Helicopter |
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| ZHENG Qing,LI Yan-jun,CAO Yu-yuan,WANG Xiao-ming.Research on Compliance Verification and Design Modification Approval for a Certain Type of Helicopter[J].Journal of Binzhou Teachers College,2013(6):48-52. |
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| Authors: | ZHENG Qing LI Yan-jun CAO Yu-yuan WANG Xiao-ming |
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| Institution: | (College of Civil Aviation, Nanjing University of aeronautics and Astronautics Nanjing 211106 ,China) |
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| Abstract: | Based on the research of airworthiness terms of normal class rotor aircraft under the China Civil Aviation Regulations CCAR 27,the approval basis of a certain type of helicopter Modification Design Approval （MDA） is determined and the modified mounts,under the action of ultimate load of airworthiness compliance verification method are pur forward,and the technical support for a certain type of helicopter＇s design modification approval is provided. |
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| Keywords: | airworthiness approval compliance verification ultimate load |
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