Design of hybrid-electric aircraft with fault-tolerance considerations

作     者：Valerio MARCIELLO Francesco OREFICE Fabrizio NICOLOSI Danilo CILIBERTI Pierluigi DELLA VECCHIA Valerio MARCIELLO;Francesco OREFICE;Fabrizio NICOLOSI;Danilo CILIBERTI;Pierluigi DELLA VECCHIA

作者机构：Department of Industrial EngineeringUniversity of Naples"FedericoⅡ"Naples 80125Italy 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2023年第36卷第2期

页      面：160-178页

核心收录：

学科分类：082502[工学-航空宇航推进理论与工程] 08[工学] 0825[工学-航空宇航科学与技术] 

基　　金：The ELICA project leading to this application has received funding from the Clean Sky 2 Joint Undertaking(JU)(No.864551) The JU receives support from the European Union’s Horizon 2020 research and innovation programme 

主　　题：Distributed electric propulsion Failure management Fault-tolerance analysis Hybrid-electric aircraft Lateral-directional controllability 

摘      要：The potential benefits of hybrid-electric or all-electric propulsion have led to a growing interest in this topic over the past *** design of propulsion systems and innovative configurations has been extensively discussed in literature,but steps towards higher levels of technological readiness,optimisation algorithms based on reliable weight estimation and simulationbased mission analysis are *** paper focuses on the integration of a method for evaluating the lateral-directional controllability of an aircraft within a design chain that integrates aero-propulsive interactions,accurate modelling of the fuel system,and mid-fidelity estimation of the structural ***,the present work proposes a strategy for powerplant management in scenarios with an inoperative chain *** of hybrid-electric propulsion on the design of the vertical tail plane are evaluated involving the analysis of multiple failure scenarios and certification *** proposed application concerns a commuter aircraft.