SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN

Xiyu Wang; Yaoxing Shang; Haiying Hu; Binghui Qiu; Fengjian Teng; Hao Zhang; Zongxia Jiao; Xiaochao Liu

doi:10.1049/icp.2021.0159

SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN

Xiyu Wang
, Yaoxing Shang
, Haiying Hu
, Binghui Qiu
, Fengjian Teng
, Hao Zhang
, Zongxia Jiao
, Xiaochao Liu^*

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
Avic Jiangxi Hongdu Aviation Industry Group Company Ltd
China Aviation Industry Corporation
Aerospace System Engineering Shanghai

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

Abstract

As one of the key and important airborne systems, aircraft braking systems mostly use traditional centralized hydraulic sources. With the new concept of "multi-electric aircraft", the aircraft energy supply system has further branched. This article introduces an integrated hydraulic brake device. It does not require an on-board hydraulic source, and can directly convert the energy of the wheel rotation when the aircraft lands, to complete the braking function. Using Simulink / SimHydraulics module, a corresponding model of aircraft brake integrated hydraulic device was established. The function of this self-feeding hydraulic brake device was verified through simulation and analysis. This method provides a new way to further study the braking system.

Original language	English
Title of host publication	IET Conference Proceedings
Publisher	Institution of Engineering and Technology
Pages	376-381
Number of pages	6
Volume	2020
Edition	3
ISBN (Electronic)	9781839534195
DOIs	https://doi.org/10.1049/icp.2021.0159
State	Published - 2020
Event	2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020 - Virtual, Online Duration: 18 Sep 2020 → 21 Sep 2020

Conference

Conference	2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020
City	Virtual, Online
Period	18/09/20 → 21/09/20

Keywords

AIRCRAFT BRAKES
ENERGY CONVERSION
HYDRAULICS
SIMHYDRAULICS
SIMULATION

Access to Document

10.1049/icp.2021.0159

Cite this

@inproceedings{a4e610a128054cb1bd3b4f9fa699af73,

title = "SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN",

abstract = "As one of the key and important airborne systems, aircraft braking systems mostly use traditional centralized hydraulic sources. With the new concept of {"}multi-electric aircraft{"}, the aircraft energy supply system has further branched. This article introduces an integrated hydraulic brake device. It does not require an on-board hydraulic source, and can directly convert the energy of the wheel rotation when the aircraft lands, to complete the braking function. Using Simulink / SimHydraulics module, a corresponding model of aircraft brake integrated hydraulic device was established. The function of this self-feeding hydraulic brake device was verified through simulation and analysis. This method provides a new way to further study the braking system.",

keywords = "AIRCRAFT BRAKES, ENERGY CONVERSION, HYDRAULICS, SIMHYDRAULICS, SIMULATION",

author = "Xiyu Wang and Yaoxing Shang and Haiying Hu and Binghui Qiu and Fengjian Teng and Hao Zhang and Zongxia Jiao and Xiaochao Liu",

note = "Publisher Copyright: {\textcopyright} 2020 The Institution of Engineering and Technology.; 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020 ; Conference date: 18-09-2020 Through 21-09-2020",

year = "2020",

doi = "10.1049/icp.2021.0159",

language = "英语",

volume = "2020",

pages = "376--381",

booktitle = "IET Conference Proceedings",

publisher = "Institution of Engineering and Technology",

address = "英国",

edition = "3",

}

Wang, X, Shang, Y, Hu, H, Qiu, B, Teng, F, Zhang, H, Jiao, Z & Liu, X 2020, SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN. in IET Conference Proceedings. 3 edn, vol. 2020, Institution of Engineering and Technology, pp. 376-381, 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020, Virtual, Online, 18/09/20. https://doi.org/10.1049/icp.2021.0159

SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN. / Wang, Xiyu; Shang, Yaoxing; Hu, Haiying et al.
IET Conference Proceedings. Vol. 2020 3. ed. Institution of Engineering and Technology, 2020. p. 376-381.

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

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T1 - SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN

AU - Wang, Xiyu

AU - Shang, Yaoxing

AU - Hu, Haiying

AU - Qiu, Binghui

AU - Teng, Fengjian

AU - Zhang, Hao

AU - Jiao, Zongxia

AU - Liu, Xiaochao

PY - 2020

Y1 - 2020

N2 - As one of the key and important airborne systems, aircraft braking systems mostly use traditional centralized hydraulic sources. With the new concept of "multi-electric aircraft", the aircraft energy supply system has further branched. This article introduces an integrated hydraulic brake device. It does not require an on-board hydraulic source, and can directly convert the energy of the wheel rotation when the aircraft lands, to complete the braking function. Using Simulink / SimHydraulics module, a corresponding model of aircraft brake integrated hydraulic device was established. The function of this self-feeding hydraulic brake device was verified through simulation and analysis. This method provides a new way to further study the braking system.

AB - As one of the key and important airborne systems, aircraft braking systems mostly use traditional centralized hydraulic sources. With the new concept of "multi-electric aircraft", the aircraft energy supply system has further branched. This article introduces an integrated hydraulic brake device. It does not require an on-board hydraulic source, and can directly convert the energy of the wheel rotation when the aircraft lands, to complete the braking function. Using Simulink / SimHydraulics module, a corresponding model of aircraft brake integrated hydraulic device was established. The function of this self-feeding hydraulic brake device was verified through simulation and analysis. This method provides a new way to further study the braking system.

KW - AIRCRAFT BRAKES

KW - ENERGY CONVERSION

KW - HYDRAULICS

KW - SIMHYDRAULICS

KW - SIMULATION

UR - https://www.scopus.com/pages/publications/85174649246

U2 - 10.1049/icp.2021.0159

DO - 10.1049/icp.2021.0159

M3 - 会议稿件

AN - SCOPUS:85174649246

VL - 2020

SP - 376

EP - 381

BT - IET Conference Proceedings

PB - Institution of Engineering and Technology

T2 - 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020

Y2 - 18 September 2020 through 21 September 2020

ER -

SIMULATION AND ANALYSIS OF HIGHRELIABILITY BRAKING SYSTEM OF AIRCRAFT BASED ON SELF-FEED ENERGY NONSIMILAR MARGIN

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Keywords

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