Electric Drive with Magnetic Reduction of the Helicopter Main Rotor

A. Yu. Afanas’ev; N. A. Berezov; N. A. Rybushkin

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Electric Drive with Magnetic Reduction of the Helicopter Main Rotor

机译：电动驱动直升机主转子的磁力减少

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摘要

The design and main calculation relations are presented for the driving electric motor with magnetic gear box to drive the helicopter main rotor. The design advantages in terms of volume and reliability are noted.

机译：为磁力齿轮箱驱动电动机提供了设计和主要计算关系，以驱动直升机主转子。注意到在体积和可靠性方面的设计优势。

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来源
《Russian Aeronautics》 |2019年第2期|共6页
作者
A. Yu. Afanas’ev; N. A. Berezov; N. A. Rybushkin;
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作者单位

Tupolev Kazan National Research Technical University;

Tupolev Kazan National Research Technical University;

Tupolev Kazan National Research Technical University;

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
helicopter; synchronous electric motor; laminated lattice magnetic conductor; permanent magnets; magnetic gear box;

机译：直升机;同步电动机;层压晶格磁导体;永磁体;磁齿轮箱;

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专利

1. Electric Drive with Magnetic Reduction of the Helicopter Main Rotor [J] . A. Yu. Afanas’ev, N. A. Berezov, N. A. Rybushkin Russian Aeronautics . 2019,第2期

机译：电动驱动直升机主转子的磁力减少
2. Design and application of an Electric Tail Rotor Drive Control (ETRDC) for helicopters with performance tests [J] . Yuwen ZHANG, Chen JIANG, Yunjie WANG, 中国航空学报（英文版） . 2018,第009期

机译：具有性能测试的直升机电动尾桨驱动控制（ETRDC）的设计和应用
3. Variable-speed tail rotors for helicopters with variable-speed main rotors [J] . Han D., Barakos G. N. The Aeronautical Journal . 2017,第1238期

机译：带有可变速主旋翼的直升机的可变速尾旋翼
4. Modelling and Design of a High Performance Electric Drive for an Unmanned Helicopter Main Rotor [C] . S. J. Nall, P. H. Mellor, P. C. Bunniss UAVs Eighteenth International Conference Mar 31-Apr 2, 2003 Bristol, United Kingdom . 2003

机译：无人机主旋翼高性能电传动的建模与设计
5. A comprehensive aeroelastic analysis of helicopter main rotors with trailing edge flaps for vibration reduction. [D] . Milgram, Judah Henry. 1997

机译：具有后缘襟翼的直升机主旋翼的全面气动弹性分析，可减少振动。
6. Influence of Rotor Dynamic Scattering on Helicopter Radar Cross-Section [O] . Zeyang Zhou, Jun Huang 2020

机译：旋翼动态散射对直升机雷达截面的影响
7. A Comparison of Helicopter Main Rotor Features Due to Stiffness of Rotor Blade-Hub Connection [O] . Jarosław Stanisławski 2018

机译：转子叶片 - 轮毂连接刚度引起的直升机主转子特征的比较

Electric Drive with Magnetic Reduction of the Helicopter Main Rotor

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