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^*

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Shanghai Aircraft Design and Research Institute
Beihang University

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

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.

Original language	English
Title of host publication	IET Conference Proceedings
Publisher	Institution of Engineering and Technology
Pages	285-290
Number of pages	6
Volume	2020
Edition	3
ISBN (Electronic)	9781839534195
DOIs	https://doi.org/10.1049/icp.2021.0457
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

ANALYSIS
EFFECT
FAILURE CONDITION
LANDING GEAR SYSTEM
VALIDATION

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10.1049/icp.2021.0457

Cite this

@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. in IET Conference Proceedings. 3 edn, vol. 2020, Institution of Engineering and Technology, pp. 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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