考虑全电动飞机推进电力系统结构的设计前灵敏度分析工具

2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS) Pub Date : 2015-03-03 DOI:10.1109/ESARS.2015.7101489

C. Jones, P. Norman, S. Galloway, G. Burt, M. Armstrong, A. Bollman

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引用次数: 6

摘要

为混合翼身(HWB) N3-X飞机提出的涡轮电力分布式动力(TeDP)系统是复杂的超导电力网络，必须开发以满足具有挑战性的重量、效率和推进器功率要求。提出了一种集成的系统灵敏度分析工具，可用于支持对TeDP系统的体系结构、保护系统和冗余需求的快速评估研究。使用该工具可以帮助指导未来对TeDP系统的研究，以应对与满足N+3飞机概念设定的严格重量和效率目标相关的关键挑战。

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A pre-design sensitivity analysis tool for consideration of full-electric aircraft propulsion electrical power system architectures

Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An integrated system sensitivity analysis tool is presented, which can be used to support rapid appraisal studies of architectures, protection systems and redundancy requirements for TeDP systems. The use of this tool can help direct future research on TeDP systems towards the key challenges relevant to meeting the stringent weight and efficiency targets set out for N+3 aircraft concepts.

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2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)

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