Optimization of Shop Visit for Aeroengine Using the Proportional Hazard Model-Reference-Cited by-同舟云学术

Optimization of Shop Visit for Aeroengine Using the Proportional Hazard Model

Published:2020-07 Issue:7 Volume:17 Page:336-345
ISSN:2327-3097
Container-title:Journal of Aerospace Information Systems
language:en
Short-container-title:Journal of Aerospace Information Systems

Author:

Cai Jing¹,Wu Xianbiao¹,Chen Xi¹,Xu Juan¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 211106 Nanjing, People’s Republic of China

Funder

The Fundamental Research Funds for the Central Universities

The Shanghai Sailing Program

The National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering

Reference21 articles.

1. ZhangH. J. “Research on Methods of Performance Synthetic Estimation and CBM Decision-Making Models for Aero-Engine,” Ph.D. Thesis, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, China, 2007.

2. Hybrid PSO–SVM-based method for forecasting of the remaining useful life for aircraft engines and evaluation of its reliability

3. Reduced kernel recursive least squares algorithm for aero-engine degradation prediction

4. Remaining useful life prognostics for aeroengine based on superstatistics and information fusion

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