A meta network pruning framework for remaining useful life prediction of rocket engine bearings with temporal distribution discrepancy

Author:

Pan Tongyang,Zhang Sui,Li Fudong,Chen Jinglong,Li Aimin

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference36 articles.

1. A supervised framework for recognition of liquid rocket engine health state under steady-state process without fault samples;Lv;IEEE Trans. Instrum. Meas.,2021

2. Application of QGA-BP for fault detection of liquid rocket engines;Xu;IEEE Trans. Aerosp. Electron. Syst.,2019

3. A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump;Tonon;Aerosp. Sci. Technol.,2022

4. R. Glover, B. Kelley, A. Tischer. Studies and analyses of the Space Shuttle Main Engine: SSME failure data review, diagnostic survey and SSME diagnostic evaluation, 1986.

5. Bearings for aerospace applications;Rejith;Tribol. Int.,2023

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