A study of aircraft landing gear testing system on PHM

Zhou Yang; Yunxia Chen; Rui Kang

doi:10.1109/PHM.2011.5939549

A study of aircraft landing gear testing system on PHM

Zhou Yang^*
, Yunxia Chen
, Rui Kang

^*Corresponding author for this work

School of Reliability and Systems Engineering

Beihang University

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

3 Scopus citations

Abstract

According to statistics, landing gears play the major role in the failure of aircrafts. However there are no specifically testing systems currently in use. To solve this problem, this paper presented a landing gear testing system based on PHM technology, designed a framework of both hardware and software of this system. A precise reference can be given to the experimenters by the system embodied the idea of PHM. An example proving the feasibility of the system is given at the end of this paper.

Original language	English
Title of host publication	2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011
DOIs	https://doi.org/10.1109/PHM.2011.5939549
State	Published - 2011
Event	2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011 - Shenzhen, China Duration: 24 May 2011 → 25 May 2011

Publication series

Name	2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011

Conference

Conference	2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011
Country/Territory	China
City	Shenzhen
Period	24/05/11 → 25/05/11

Keywords

PHM
landing gear testing system

Access to Document

10.1109/PHM.2011.5939549

Cite this

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title = "A study of aircraft landing gear testing system on PHM",

abstract = "According to statistics, landing gears play the major role in the failure of aircrafts. However there are no specifically testing systems currently in use. To solve this problem, this paper presented a landing gear testing system based on PHM technology, designed a framework of both hardware and software of this system. A precise reference can be given to the experimenters by the system embodied the idea of PHM. An example proving the feasibility of the system is given at the end of this paper.",

keywords = "PHM, landing gear testing system",

author = "Zhou Yang and Yunxia Chen and Rui Kang",

year = "2011",

doi = "10.1109/PHM.2011.5939549",

language = "英语",

isbn = "9781424479511",

series = "2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011",

booktitle = "2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011",

note = "2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011 ; Conference date: 24-05-2011 Through 25-05-2011",

}

Yang, Z, Chen, Y & Kang, R 2011, A study of aircraft landing gear testing system on PHM. in 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011., 5939549, 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011, 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011, Shenzhen, China, 24/05/11. https://doi.org/10.1109/PHM.2011.5939549

TY - GEN

T1 - A study of aircraft landing gear testing system on PHM

AU - Yang, Zhou

AU - Chen, Yunxia

AU - Kang, Rui

PY - 2011

Y1 - 2011

N2 - According to statistics, landing gears play the major role in the failure of aircrafts. However there are no specifically testing systems currently in use. To solve this problem, this paper presented a landing gear testing system based on PHM technology, designed a framework of both hardware and software of this system. A precise reference can be given to the experimenters by the system embodied the idea of PHM. An example proving the feasibility of the system is given at the end of this paper.

AB - According to statistics, landing gears play the major role in the failure of aircrafts. However there are no specifically testing systems currently in use. To solve this problem, this paper presented a landing gear testing system based on PHM technology, designed a framework of both hardware and software of this system. A precise reference can be given to the experimenters by the system embodied the idea of PHM. An example proving the feasibility of the system is given at the end of this paper.

KW - PHM

KW - landing gear testing system

UR - https://www.scopus.com/pages/publications/79960930329

U2 - 10.1109/PHM.2011.5939549

DO - 10.1109/PHM.2011.5939549

M3 - 会议稿件

AN - SCOPUS:79960930329

SN - 9781424479511

T3 - 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011

BT - 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011

T2 - 2011 Prognostics and System Health Management Conference, PHM-Shenzhen 2011

Y2 - 24 May 2011 through 25 May 2011

ER -

A study of aircraft landing gear testing system on PHM

Abstract

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Keywords

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