Research on dual redundancy motor of electro-hydrostatic actuator system

Liang Bo; Li Yuren; Li Bo; Huangfu Yigeng; Zhao Dongdong

doi:10.1109/ITEC.2015.7165751

Research on dual redundancy motor of electro-hydrostatic actuator system

Liang Bo, Li Yuren, Li Bo, Huangfu Yigeng, Zhao Dongdong

School of Automation

Northwestern Polytechnical University Xian

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Scopus citations

Abstract

A new aircraft Electro-Hydrostatic Actuator (EHA) of a certain model fighter was designed to meet the braking system under the Aircraft Anti-skid Braking System development background. The paper describes the principle and features of the EHA, and gives the specific requirements of the EHA. In this paper the selection and performance of the motor, pump and hydraulic cylinder were optimized. It focuses on the motor structures and performances, with dual windings, which played a role as the power driver ofEHA. The operation characteristics of the dual windings motor have investigated under different conditions. Finally, the paper provide modelling and analysis performance of EHA system and beyond a whole aircraft system.

Original language	English
Title of host publication	2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781467367417
DOIs	https://doi.org/10.1109/ITEC.2015.7165751
State	Published - 23 Jul 2015
Event	IEEE Transportation Electrification Conference and Expo, ITEC 2015 - Dearborn, United States Duration: 14 Jun 2015 → 17 Jun 2015

Publication series

Name	2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015

Conference

Conference	IEEE Transportation Electrification Conference and Expo, ITEC 2015
Country/Territory	United States
City	Dearborn
Period	14/06/15 → 17/06/15

Keywords

Aircraft anti-skid braking system
Dual-redundancy brush less DC motor
EHA
Modeling and simulation

Access to Document

10.1109/ITEC.2015.7165751

Cite this

Bo, L., Yuren, L., Bo, L., Yigeng, H., & Dongdong, Z. (2015). Research on dual redundancy motor of electro-hydrostatic actuator system. In 2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015 Article 07165751 (2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ITEC.2015.7165751

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title = "Research on dual redundancy motor of electro-hydrostatic actuator system",

abstract = "A new aircraft Electro-Hydrostatic Actuator (EHA) of a certain model fighter was designed to meet the braking system under the Aircraft Anti-skid Braking System development background. The paper describes the principle and features of the EHA, and gives the specific requirements of the EHA. In this paper the selection and performance of the motor, pump and hydraulic cylinder were optimized. It focuses on the motor structures and performances, with dual windings, which played a role as the power driver ofEHA. The operation characteristics of the dual windings motor have investigated under different conditions. Finally, the paper provide modelling and analysis performance of EHA system and beyond a whole aircraft system.",

keywords = "Aircraft anti-skid braking system, Dual-redundancy brush less DC motor, EHA, Modeling and simulation",

author = "Liang Bo and Li Yuren and Li Bo and Huangfu Yigeng and Zhao Dongdong",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; IEEE Transportation Electrification Conference and Expo, ITEC 2015 ; Conference date: 14-06-2015 Through 17-06-2015",

year = "2015",

month = jul,

day = "23",

doi = "10.1109/ITEC.2015.7165751",

language = "英语",

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Bo, L, Yuren, L, Bo, L, Yigeng, H & Dongdong, Z 2015, Research on dual redundancy motor of electro-hydrostatic actuator system. in 2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015., 07165751, 2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015, Institute of Electrical and Electronics Engineers Inc., IEEE Transportation Electrification Conference and Expo, ITEC 2015, Dearborn, United States, 14/06/15. https://doi.org/10.1109/ITEC.2015.7165751

Research on dual redundancy motor of electro-hydrostatic actuator system. / Bo, Liang; Yuren, Li; Bo, Li et al.
2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015. Institute of Electrical and Electronics Engineers Inc., 2015. 07165751 (2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Research on dual redundancy motor of electro-hydrostatic actuator system

AU - Bo, Liang

AU - Yuren, Li

AU - Bo, Li

AU - Yigeng, Huangfu

AU - Dongdong, Zhao

PY - 2015/7/23

Y1 - 2015/7/23

N2 - A new aircraft Electro-Hydrostatic Actuator (EHA) of a certain model fighter was designed to meet the braking system under the Aircraft Anti-skid Braking System development background. The paper describes the principle and features of the EHA, and gives the specific requirements of the EHA. In this paper the selection and performance of the motor, pump and hydraulic cylinder were optimized. It focuses on the motor structures and performances, with dual windings, which played a role as the power driver ofEHA. The operation characteristics of the dual windings motor have investigated under different conditions. Finally, the paper provide modelling and analysis performance of EHA system and beyond a whole aircraft system.

AB - A new aircraft Electro-Hydrostatic Actuator (EHA) of a certain model fighter was designed to meet the braking system under the Aircraft Anti-skid Braking System development background. The paper describes the principle and features of the EHA, and gives the specific requirements of the EHA. In this paper the selection and performance of the motor, pump and hydraulic cylinder were optimized. It focuses on the motor structures and performances, with dual windings, which played a role as the power driver ofEHA. The operation characteristics of the dual windings motor have investigated under different conditions. Finally, the paper provide modelling and analysis performance of EHA system and beyond a whole aircraft system.

KW - Aircraft anti-skid braking system

KW - Dual-redundancy brush less DC motor

KW - EHA

KW - Modeling and simulation

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DO - 10.1109/ITEC.2015.7165751

M3 - 会议稿件

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T3 - 2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015

BT - 2015 IEEE Transportation Electrification Conference and Expo, ITEC 2015

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - IEEE Transportation Electrification Conference and Expo, ITEC 2015

Y2 - 14 June 2015 through 17 June 2015

ER -

Research on dual redundancy motor of electro-hydrostatic actuator system

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