A remaining useful life prediction method for airborne fuel pump after maintenance. (December 2019)

• Record Type: Journal Article
• Authors: Li, Juan; Jing, Bo; Dai, Hongde; Sheng, Zengjin; Jiao, Xiaoxuan; Liu, Xiaodong
• Is Part Of: Proceedings of the Institution of Mechanical Engineers. Volume 233:Number 15(2019)
• Page Start: 5660
• Page End: 5673
• Publication Date: 2019-12
• Subjects: Fuel pump -- smooth transition auto-regression -- degradation modeling -- remaining useful life -- Wiener process -- Bayesian; Aeronautics -- Periodicals; Astronautics -- Periodicals; Airplanes -- Design and construction -- Periodicals; Aerospace industries -- Periodicals; 629.1
• DOI: 10.1177/0954410019853995
• Languages: English
• ISSNs: 0954-4100

Abstract

Remaining useful life prediction is the core of condition-based maintenance under the technology framework of prognostic and health management. But the remaining useful life of airborne fuel pump after maintenance is difficult to predict because of the multi-stage noise and small data size. A new method is proposed to solve the remaining useful life prediction of repaired fuel pump. Firstly, an alternative smooth transition auto-regression model logistic smooth transition auto-regression or exponential smooth transition auto-regression is proposed to reduce the multi-stage noise. Secondly, random effect Wiener process is utilized to model the de-noised degradation data, and the posterior parameters of remaining useful life prediction after maintenance are derived by the Bayesian method based on the parameters before maintenance. Finally, the method proposed above is compared with the methods which neglect the multi-stage noise and information before maintenance, comparative results show that the proposed method can improve the remaining useful life prediction accuracy significantly.