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民用飞机电源系统对25.1309条款的符合性验证研究 被引量:3

Compliance Verification Research of Airworthiness Regulation 25.1309 for Electrical Power System of Civil Aircraft
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摘要 通过对适航条款25.1309的分析,结合AC 25.1309、SAE ARP 4761和AC 25.1709,分析了民用飞机电源系统设计中需考虑的来自适航条款25.1309的需求,并初步研究了用于表明系统设计和安装对25.1309符合性的验证思路和方法。 Based on the analysis of airworthiness regulation 25.1309 combined with AC 25.1309, SAE ARP 4761 and AC 25.1709, this paper analyzes which requirements allocated from 25.1309 shall be considered in the design of Electrical Power System of Civil Aircraft. Electrical Power System compliance veriifcation approach and means for 25.1309 is also preliminarily researched in this paper.
作者 郑建 沈飞
出处 《航空科学技术》 2014年第7期23-26,共4页 Aeronautical Science & Technology
关键词 符合性验证 电源系统 系统安全性 25.1309条款 compliance veriifcation electrical power system system safety 25.1309 regulation
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参考文献5

  • 1刘剑锋.中国民用航空规章第25部:运输类飞机适航标准[S].中国民用航空总局,2001.
  • 2CS Part 25 Airworthiness Standards: Transport CategoryAirplanes[S], EASA.
  • 3AC 25.1309-1A System Design and Analysis [Z]. 1988.
  • 4SAE ARP 4761 Guidelines and Methods for Conducting the SafetyAssessment Process on Civil Airborne Systems and Equipment [Z].1996.
  • 5AC25.1701-1 Certification of Electrical Wiring InterconnectionSystems on Transport Category Airplanes[Z]. 2007.

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