Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident

Li Bing; Bai Lu; Zhuangzhuang Wang; Xiaochao Liu

doi:10.1049/icp.2021.0457

Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident

Li Bing
, Bai Lu
, Zhuangzhuang Wang
, Xiaochao Liu^*

^*此作品的通讯作者

自动化科学与电气工程学院

Shanghai Aircraft Design and Research Institute
Beihang University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

This work aims to validate the effect for Failure Condition of landing gear system by case analysis. Based on the real aviation accident data, this paper does the case analysis of failure condition effect for civil aircraft landing gear system. The results obtained in this research include failure condition effects that according to the actual situation and the traceability between theory analysis and real case. This paper provides supporting material for landing gear system Functional Hazard Assessment and supports the safety and certification ofthe aircraft.

源语言	英语
主期刊名	IET Conference Proceedings
出版商	Institution of Engineering and Technology
页	285-290
页数	6
卷	2020
版本	3
ISBN（电子版）	9781839534195
DOI	https://doi.org/10.1049/icp.2021.0457
出版状态	已出版 - 2020
活动	2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020 - Virtual, Online 期限: 18 9月 2020 → 21 9月 2020

会议

会议	2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020
市	Virtual, Online
时期	18/09/20 → 21/09/20

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10.1049/icp.2021.0457

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@inproceedings{18e26c5653b34f0a9b77ce85bd5b26bb,

title = "Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident",

abstract = "This work aims to validate the effect for Failure Condition of landing gear system by case analysis. Based on the real aviation accident data, this paper does the case analysis of failure condition effect for civil aircraft landing gear system. The results obtained in this research include failure condition effects that according to the actual situation and the traceability between theory analysis and real case. This paper provides supporting material for landing gear system Functional Hazard Assessment and supports the safety and certification ofthe aircraft.",

keywords = "ANALYSIS, EFFECT, FAILURE CONDITION, LANDING GEAR SYSTEM, VALIDATION",

author = "Li Bing and Bai Lu and Zhuangzhuang Wang 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.2021.0457",

language = "英语",

volume = "2020",

pages = "285--290",

booktitle = "IET Conference Proceedings",

publisher = "Institution of Engineering and Technology",

address = "英国",

edition = "3",

}

Bing, L, Lu, B, Wang, Z & Liu, X 2020, Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident. 在 IET Conference Proceedings. 3 编辑, 卷 2020, Institution of Engineering and Technology, 页码 285-290, 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020, Virtual, Online, 18/09/20. https://doi.org/10.1049/icp.2021.0457

TY - GEN

T1 - Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident

AU - Bing, Li

AU - Lu, Bai

AU - Wang, Zhuangzhuang

AU - Liu, Xiaochao

PY - 2020

Y1 - 2020

N2 - This work aims to validate the effect for Failure Condition of landing gear system by case analysis. Based on the real aviation accident data, this paper does the case analysis of failure condition effect for civil aircraft landing gear system. The results obtained in this research include failure condition effects that according to the actual situation and the traceability between theory analysis and real case. This paper provides supporting material for landing gear system Functional Hazard Assessment and supports the safety and certification ofthe aircraft.

AB - This work aims to validate the effect for Failure Condition of landing gear system by case analysis. Based on the real aviation accident data, this paper does the case analysis of failure condition effect for civil aircraft landing gear system. The results obtained in this research include failure condition effects that according to the actual situation and the traceability between theory analysis and real case. This paper provides supporting material for landing gear system Functional Hazard Assessment and supports the safety and certification ofthe aircraft.

KW - ANALYSIS

KW - EFFECT

KW - FAILURE CONDITION

KW - LANDING GEAR SYSTEM

KW - VALIDATION

UR - https://www.scopus.com/pages/publications/85174644486

U2 - 10.1049/icp.2021.0457

DO - 10.1049/icp.2021.0457

M3 - 会议稿件

AN - SCOPUS:85174644486

VL - 2020

SP - 285

EP - 290

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 -

Validation for Civil Aircraft Landing Gear Failure Condition by Case Analysis of Aviation incident

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