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
N1 - Publisher Copyright:
© 2016 IEEE.
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
EP - 272
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 -