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Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements.

机译：涡轮飞行器驱动关键性能参数和功能要求。

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The purpose of this paper is to propose specific power and efficiency as the key performance parameters for a turboelectric aircraft power system and investigate their impact on the overall aircraft. Key functional requirements are identified that impact the power system design. Breguet range equations for a base aircraft and a turboelectric aircraft are found. The benefits and costs that may result from the turboelectric system are enumerated. A break-even analysis is conducted to find the minimum allowable electric drive specific power and efficiency that can preserve the range, initial weight, operating empty weight, and payload weight of the base aircraft.

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作者
Jansen, R. H.; Brown, G. V.; Felder, J. L.; Duffy, K. P.;
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年度 2016
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aircraft engines; Turbogenerators; Electric power; Propulsion system configurations; Systems engineering; Functional design specifications; Propulsion system performance; Power efficiency; Propulsive efficiency; Cost analysis;

机译：飞机发动机;汽轮发电机;电力;推进系统配置;系统工程;功能设计规范;推进系统性能;电力效率;推进效率;成本分析;
入库时间 2022-08-29 10:46:13

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1. A Method For Determination And Standardization Of Performance Parameters For Aircrafts With Electric Drives [J] . Miros?aw Nowakowski, Zbigniew Jakielaszek Journal of KONBiN . 2015,第1期

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2. Optimal Voltage and Current Selection for Turboelectric Aircraft Propulsion Networks [J] . Ibrahim Kingsley, Sampath Suresh, Nalianda Devaiah Transportation Electrification, IEEE Transactions on . 2020,第4期

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3. Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches [J] . Brelje Benjamin J., Martins Joaquim R. R. A. Progress in Aerospace Sciences . 2019,第JANa期

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4. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements [C] . Ralph H. Jansen, Gerald V. Brown, James L. Felder, AIAA propulsion and energy forum;AIAA/SAE/ASEE joint propulsion conference . 2015

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5. Concept design theory and model for multi-use space facilities: Analysis of key system design parameters through variance of mission requirements. [D] . Reynerson, Charles Martin. 1997

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7. A Method For Determination And Standardization Of Performance Parameters For Aircrafts With Electric Drives [O] . Jakielaszek Zbigniew, Nowakowski Mirosław 2014

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8. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements. [R] . Jansen, R. H., Brown, G. V., Felder, J. L., 2015

机译：涡轮飞行器驱动关键性能参数和功能要求。

Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements.

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