混合动力飞机技术和设计综述:关键分析和新解决方案

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Karim Abu Salem , Giuseppe Palaia , Alessandro A. Quarta
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引用次数: 7

摘要

减少温室气体排放已成为民用运输航空的优先事项。当前航空研究所研究的可能解决方案之一是引入电力推进,这将大大减少与飞行相关的温室气体排放。本文深入探讨了这一主题;这部作品分为两个相互交织的部分。第一个涉及对现有技术的广泛审查,从分析航空应用的电气技术推动因素开始,并对当前的飞机概念设计提案进行调查,包括中短程和区域级。本综述部分采用了一种关键方法,为论文第二部分的技术框架定义提供了相关指示,其中提出了一种新型混合动力电动飞机的概念开发。具体而言,对现有技术的分析结果表明,混合动力电动飞机应属于区域类别,应考虑机身的节能解决方案。此外,还详细介绍了集成混合电力推进的潜力和局限性,并为拟议飞机的设计选择了未来十年合理现实的技术水平。箱翼机身结构已被采用,因为它有可能在增加载荷运输能力的同时最大限度地减少诱导的空气动力学阻力,从而代表了一种空气动力学高效的解决方案。开发了一个设计和优化框架,以评估混合动力电动推进与箱翼提升系统的集成。这两种技术的结合,加上飞机设计方法的范式变化,可以确定在整个典型的区域任务范围内最大限度地减少燃料消耗的概念解决方案,从而产生潜在的无排放区域飞机。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Review of hybrid-electric aircraft technologies and designs: Critical analysis and novel solutions

Reducing greenhouse gas emissions has become a priority for civil transport aviation. One of the possible solutions investigated by current aeronautics research is the introduction of electric propulsion, which would drastically reduce greenhouse gas emissions related to flight. This paper addresses this topic in depth; the work is structured in two intertwined parts. The first relates to an extensive review of the state of the art, starting with the analysis of electrical technology enablers for aviation applications, and leading to the investigation of current proposals of aircraft conceptual designs, both for short-medium range and regional class. This review section, which is presented with a critical approach, provides the relevant indications for the definition of the technical framework of the second part of the paper, in which the conceptual development of a novel hybrid-electric aircraft is proposed. Specifically, the outcomes from the analysis of the state of the art suggest that the hybrid-electric aircraft should belong to the regional category, and that energy efficient solutions for the airframe should be considered. Moreover, potentials and limitations of integrating hybrid-electric propulsion are carefully detailed, and reasonably realistic technology levels for the next decade have been selected for the design of the proposed aircraft. A box-wing airframe architecture has been adopted as it has the potential to minimize induced aerodynamic drag while increasing the load transport capacity, thus representing an aerodynamic efficient solution. A design and optimization framework has been developed to evaluate the integration of the hybrid-electric propulsion with the box-wing lifting system. The coupling of these two technologies, together with a paradigm change in the aircraft design approach, allow to identify conceptual solutions that minimize fuel consumption throughout the typical regional mission envelope, leading to a potential emission-free regional aircraft.

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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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