Redundancy design of a new electrically powered actuator for aerospace application

Jiankang Zhi; Binghui Qiu; Xiaoye Qi; Yongling Fu; Jian Fu

doi:10.1109/ICMA.2018.8484622

Redundancy design of a new electrically powered actuator for aerospace application

Jiankang Zhi
, Binghui Qiu
, Xiaoye Qi
, Yongling Fu
, Jian Fu

School of Mechanical Engineering and Automation

Beihang University
Equipment Department of China PLA Air Force

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

Abstract

Electro-Mechanical-Hydrostatic Actuator (EMHA) is a new type of electrically powered actuator that acts on thrust vector control system (TVC). The reliability of the redundancy system was researched, and the fault tree method was used to analyze the fault of the EMHA system, and task reliability was also calculated; then, the redundancy design of the EMHA system was carried out from the point of the overall redundancy, and the switch valve block that is the key role in the EMHA system was analyzed in detail. Finally, the redundancy design of the EMHA system was carried out from the point of the component redundancy. The ideas and suggestions of EMHA system redundancy scheme was given based on the above procedures.

Original language	English
Title of host publication	Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1009-1014
Number of pages	6
ISBN (Electronic)	9781538660720
DOIs	https://doi.org/10.1109/ICMA.2018.8484622
State	Published - 5 Oct 2018
Event	15th IEEE International Conference on Mechatronics and Automation, ICMA 2018 - Changchun, China Duration: 5 Aug 2018 → 8 Aug 2018

Publication series

Name	Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018

Conference

Conference	15th IEEE International Conference on Mechatronics and Automation, ICMA 2018
Country/Territory	China
City	Changchun
Period	5/08/18 → 8/08/18

Keywords

Electro mechanical-hydrostatic actuator
Redundancy technology reliability
Switching valve block system
Thrust vector control system

Access to Document

10.1109/ICMA.2018.8484622

Cite this

Zhi, J., Qiu, B., Qi, X., Fu, Y., & Fu, J. (2018). Redundancy design of a new electrically powered actuator for aerospace application. In Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018 (pp. 1009-1014). Article 8484622 (Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMA.2018.8484622

Zhi, Jiankang ; Qiu, Binghui ; Qi, Xiaoye et al. / Redundancy design of a new electrically powered actuator for aerospace application. Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018. Institute of Electrical and Electronics Engineers Inc., 2018. pp. 1009-1014 (Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018).

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title = "Redundancy design of a new electrically powered actuator for aerospace application",

abstract = "Electro-Mechanical-Hydrostatic Actuator (EMHA) is a new type of electrically powered actuator that acts on thrust vector control system (TVC). The reliability of the redundancy system was researched, and the fault tree method was used to analyze the fault of the EMHA system, and task reliability was also calculated; then, the redundancy design of the EMHA system was carried out from the point of the overall redundancy, and the switch valve block that is the key role in the EMHA system was analyzed in detail. Finally, the redundancy design of the EMHA system was carried out from the point of the component redundancy. The ideas and suggestions of EMHA system redundancy scheme was given based on the above procedures.",

keywords = "Electro mechanical-hydrostatic actuator, Redundancy technology reliability, Switching valve block system, Thrust vector control system",

author = "Jiankang Zhi and Binghui Qiu and Xiaoye Qi and Yongling Fu and Jian Fu",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 15th IEEE International Conference on Mechatronics and Automation, ICMA 2018 ; Conference date: 05-08-2018 Through 08-08-2018",

year = "2018",

month = oct,

day = "5",

doi = "10.1109/ICMA.2018.8484622",

language = "英语",

series = "Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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Zhi, J, Qiu, B, Qi, X, Fu, Y & Fu, J 2018, Redundancy design of a new electrically powered actuator for aerospace application. in Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018., 8484622, Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018, Institute of Electrical and Electronics Engineers Inc., pp. 1009-1014, 15th IEEE International Conference on Mechatronics and Automation, ICMA 2018, Changchun, China, 5/08/18. https://doi.org/10.1109/ICMA.2018.8484622

Redundancy design of a new electrically powered actuator for aerospace application. / Zhi, Jiankang; Qiu, Binghui; Qi, Xiaoye et al.
Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018. Institute of Electrical and Electronics Engineers Inc., 2018. p. 1009-1014 8484622 (Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018).

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

TY - GEN

T1 - Redundancy design of a new electrically powered actuator for aerospace application

AU - Zhi, Jiankang

AU - Qiu, Binghui

AU - Qi, Xiaoye

AU - Fu, Yongling

AU - Fu, Jian

PY - 2018/10/5

Y1 - 2018/10/5

N2 - Electro-Mechanical-Hydrostatic Actuator (EMHA) is a new type of electrically powered actuator that acts on thrust vector control system (TVC). The reliability of the redundancy system was researched, and the fault tree method was used to analyze the fault of the EMHA system, and task reliability was also calculated; then, the redundancy design of the EMHA system was carried out from the point of the overall redundancy, and the switch valve block that is the key role in the EMHA system was analyzed in detail. Finally, the redundancy design of the EMHA system was carried out from the point of the component redundancy. The ideas and suggestions of EMHA system redundancy scheme was given based on the above procedures.

AB - Electro-Mechanical-Hydrostatic Actuator (EMHA) is a new type of electrically powered actuator that acts on thrust vector control system (TVC). The reliability of the redundancy system was researched, and the fault tree method was used to analyze the fault of the EMHA system, and task reliability was also calculated; then, the redundancy design of the EMHA system was carried out from the point of the overall redundancy, and the switch valve block that is the key role in the EMHA system was analyzed in detail. Finally, the redundancy design of the EMHA system was carried out from the point of the component redundancy. The ideas and suggestions of EMHA system redundancy scheme was given based on the above procedures.

KW - Electro mechanical-hydrostatic actuator

KW - Redundancy technology reliability

KW - Switching valve block system

KW - Thrust vector control system

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M3 - 会议稿件

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T3 - Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018

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BT - Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 15th IEEE International Conference on Mechatronics and Automation, ICMA 2018

Y2 - 5 August 2018 through 8 August 2018

ER -

Zhi J, Qiu B, Qi X, Fu Y , Fu J. Redundancy design of a new electrically powered actuator for aerospace application. In Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018. Institute of Electrical and Electronics Engineers Inc. 2018. p. 1009-1014. 8484622. (Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018). doi: 10.1109/ICMA.2018.8484622

Redundancy design of a new electrically powered actuator for aerospace application

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