Design of a linear electric actuator for an aircraft engine control lever-Reference-Cited by-同舟云学术

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Design of a linear electric actuator for an aircraft engine control lever

Published:2021-11-16 Issue: Volume: Page:
ISSN:
Container-title:2021 International Conference on Electrotechnical Complexes and Systems (ICOECS)
language:
Short-container-title:

Author:

Ismagilov Flyur R.,Vavilov Viacheslav E.,Zherebtsov Aleksey A.,Zharkov Evgeniy O.,Tarasov Nikolay G.,Gusakov Denis V.,Garipov Iskander R.,Kulikov Gennadiy G.

Funder

Ministry of Science and Higher Education of the Russian Federation

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9657193/9657157/09657475.pdf?arnumber=9657475

Reference6 articles.

1. Design of a High- Temperature Linear Electromagnetic Actuator

2. A tubular linear motor structure suitable for large thrust

3. Design and Analysis of a Linear-Rotary Fault-Tolerant Consequent-Pole PM Actuator

4. Proposal of a Three-Degree-of-Freedom Linear-Rotational Resonant Actuator and Inverter Topology

5. A Novel Force Ripple Reduction Method of Tubular Linear Switched Reluctance Actuators based on Multi-stages Translator Poles

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