在设计初期确定全电动飞机起飞质量的方法

Q3 Earth and Planetary Sciences

Aerospace Systems Pub Date : 2023-09-08 DOI:10.1007/s42401-023-00242-5

Denis Dukhnovskiy

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引用次数: 0

摘要

本文介绍了全电动飞机（AEA）设计初期起飞质量技术的开发成果。文中描述了确定飞机电池相对质量的过程。通过比较从开发的表达式中获得的数值和现有 AEA 的数值，对该技术进行了验证。开发并描述了确定 AEA 动力装置质量的方法。就如何应用所获得的表达式设计 AEA 提出了一般性建议。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Methodology for determining the takeoff mass of all-electric aircraft at the early stages of design

The paper presents the results of the development of the takeoff mass technique for all-electric aircraft (AEA) at the early stages of design. The process of determining the relative mass of aircraft batteries is described. The technique was verified by comparing the values obtained from the developed expressions with the values of existing AEA. A method for determining the mass of the AEA power plant was developed and described. General recommendations are given on the application of the obtained expressions for the design of AEA.

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来源期刊

Aerospace Systems Social Sciences-Social Sciences (miscellaneous)

CiteScore

1.80

自引率

0.00%

发文量

期刊介绍： Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion