Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump

Xingjian Wang; Siru Lin; Shaoping Wang

doi:10.1109/AUS.2016.7748057

Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump

School of Automation Science and Electrical Engineering

Beihang University

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

9 Scopus citations

Abstract

In order to realize condition-based maintenance of aircraft and therefore ensure flight safety, it is significant to timely and accurately determine of remaining useful life (RUL) of the aviation hydraulic piston pump. Failure resulting from hydraulic oil contamination is the main failure mode of piston pump, thus a life prediction model based on contaminant sensitivity is established for the aviation hydraulic piston pump in this study. The mathematically explicit relationship between oil contamination and useful life of the piston pump is deduced by utilizing the contaminant sensitivity theory of hydraulic system. The experimental method for measuring contaminant sensitivity of the aviation hydraulic piston pump is proposed based on the contaminant sensitivity model. Useful life of the piston pump under certain contaminant conditions is then predicted utilizing a group of experimental data, verifying the effectiveness of the proposed contaminant-based life prediction model.

Original language	English
Title of host publication	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	266-272
Number of pages	7
ISBN (Electronic)	9781509010875
DOIs	https://doi.org/10.1109/AUS.2016.7748057
State	Published - 17 Nov 2016
Event	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016

Publication series

Name	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/Territory	China
City	Beijing
Period	10/10/16 → 12/10/16

Keywords

aircraft hydraulic system
contaminant sensitivity
piston pump
remaining useful life (RUL)

Access to Document

10.1109/AUS.2016.7748057

Cite this

Wang, X., Lin, S., & Wang, S. (2016). Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems (pp. 266-272). Article 7748057 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AUS.2016.7748057

Wang, Xingjian ; Lin, Siru ; Wang, Shaoping. / Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump. AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 266-272 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

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title = "Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump",

abstract = "In order to realize condition-based maintenance of aircraft and therefore ensure flight safety, it is significant to timely and accurately determine of remaining useful life (RUL) of the aviation hydraulic piston pump. Failure resulting from hydraulic oil contamination is the main failure mode of piston pump, thus a life prediction model based on contaminant sensitivity is established for the aviation hydraulic piston pump in this study. The mathematically explicit relationship between oil contamination and useful life of the piston pump is deduced by utilizing the contaminant sensitivity theory of hydraulic system. The experimental method for measuring contaminant sensitivity of the aviation hydraulic piston pump is proposed based on the contaminant sensitivity model. Useful life of the piston pump under certain contaminant conditions is then predicted utilizing a group of experimental data, verifying the effectiveness of the proposed contaminant-based life prediction model.",

keywords = "aircraft hydraulic system, contaminant sensitivity, piston pump, remaining useful life (RUL)",

author = "Xingjian Wang and Siru Lin and Shaoping Wang",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 ; Conference date: 10-10-2016 Through 12-10-2016",

year = "2016",

month = nov,

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doi = "10.1109/AUS.2016.7748057",

language = "英语",

series = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

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

pages = "266--272",

booktitle = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

address = "美国",

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Wang, X, Lin, S & Wang, S 2016, Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump. in AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems., 7748057, AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, Institute of Electrical and Electronics Engineers Inc., pp. 266-272, 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016, Beijing, China, 10/10/16. https://doi.org/10.1109/AUS.2016.7748057

Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump. / Wang, Xingjian; Lin, Siru; Wang, Shaoping.
AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. p. 266-272 7748057 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

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

TY - GEN

T1 - Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump

AU - Wang, Xingjian

AU - Lin, Siru

AU - Wang, Shaoping

PY - 2016/11/17

Y1 - 2016/11/17

N2 - In order to realize condition-based maintenance of aircraft and therefore ensure flight safety, it is significant to timely and accurately determine of remaining useful life (RUL) of the aviation hydraulic piston pump. Failure resulting from hydraulic oil contamination is the main failure mode of piston pump, thus a life prediction model based on contaminant sensitivity is established for the aviation hydraulic piston pump in this study. The mathematically explicit relationship between oil contamination and useful life of the piston pump is deduced by utilizing the contaminant sensitivity theory of hydraulic system. The experimental method for measuring contaminant sensitivity of the aviation hydraulic piston pump is proposed based on the contaminant sensitivity model. Useful life of the piston pump under certain contaminant conditions is then predicted utilizing a group of experimental data, verifying the effectiveness of the proposed contaminant-based life prediction model.

AB - In order to realize condition-based maintenance of aircraft and therefore ensure flight safety, it is significant to timely and accurately determine of remaining useful life (RUL) of the aviation hydraulic piston pump. Failure resulting from hydraulic oil contamination is the main failure mode of piston pump, thus a life prediction model based on contaminant sensitivity is established for the aviation hydraulic piston pump in this study. The mathematically explicit relationship between oil contamination and useful life of the piston pump is deduced by utilizing the contaminant sensitivity theory of hydraulic system. The experimental method for measuring contaminant sensitivity of the aviation hydraulic piston pump is proposed based on the contaminant sensitivity model. Useful life of the piston pump under certain contaminant conditions is then predicted utilizing a group of experimental data, verifying the effectiveness of the proposed contaminant-based life prediction model.

KW - aircraft hydraulic system

KW - contaminant sensitivity

KW - piston pump

KW - remaining useful life (RUL)

UR - https://www.scopus.com/pages/publications/85006789270

U2 - 10.1109/AUS.2016.7748057

DO - 10.1109/AUS.2016.7748057

M3 - 会议稿件

AN - SCOPUS:85006789270

T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

SP - 266

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BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016

Y2 - 10 October 2016 through 12 October 2016

ER -

Wang X, Lin S, Wang S. Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc. 2016. p. 266-272. 7748057. (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). doi: 10.1109/AUS.2016.7748057

Remaining useful life prediction model based on contaminant sensitivity for aviation hydraulic piston pump

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