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作 者:谢辉松[1] XIE Hui-song(Department of Requirements Engineering,Shanghai Aircraft Design and Research Institute,CACC,Shanghai 201210,China)
机构地区:[1]中国商飞上海飞机设计研究院需求工程与型号发展部,上海201210
出 处:《航空计算技术》2020年第5期27-30,共4页Aeronautical Computing Technique
摘 要:应急撤离是适航要求的一项飞机能力,而通过试验和分析组合的方法验证可以有效降低因全机应急撤离演示带来的高风险、高成本。通过分析影响飞机应急撤离能力的飞机构型要素,结合相似机型已获得的正式的应急撤离演示试验数据,预测某飞机在适航取证条件下的撤离时间。分析方法被适航当局认可,可应用于对飞机应急撤离能力的适航验证,同时,方法对已取证飞机和新研飞机应急撤离相关设计验证均有积极意义。Emergency evacuation is an aircraft capability required by airworthiness,and verification through the combination of test and analysis can effectively reduce the high risks and high costs caused by the full scale emergency evacuation demonstration.The evacuation time of an aircraft under airworthiness certification conditions is predicted by analyzing the aircraft configuration elements that affect the emergency evacuation capability of the aircraft,and combining with the formal emergency evacuation demonstration test data of similar aircraft.This analysis method is approved by airworthiness authority and can be applied to airworthiness verification of aircraft emergency evacuation capability.At the same time,this method is of positive significance to the emergency evacuation design and verification for both the certificated and the newly developed aircraft.
分 类 号:V219[航空宇航科学与技术—航空宇航推进理论与工程]
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