A novel rotor dynamic balancing method based on blade tip clearance measurement without the once per revolution sensor-Reference-Cited by-同舟云学术

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A novel rotor dynamic balancing method based on blade tip clearance measurement without the once per revolution sensor

Published:2024-03 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Weibo,WANG Weimin,ZHANG Shuai^ORCID,WANG Jiale,LIN Yulong,LI Tianqing

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference46 articles.

1. Research status and prospect of fault diagnosis for gas turbine aerongine;Lin;Acta Aeronautica et Astronautica Sinica,2022

2. New electromagnetic ring balancer for active imbalance compensation of rotating machinery;Fan;J Sound Vib,2014

3. Dynamic analysis of magnetorheological damper incorporating elastic ring in coupled multi-physical fields;Wang;Mech Syst Signal Pr,2024

4. An equivalent unbalance identification method for the balancing of nonlinear squeeze-film damped rotordynamic systems;Torres Cedillo;J Sound Vib,2016

5. A review of online blade tip clearance measurement technologies for aeroengines;Duan;Acta Aeronautica et Astronautica Sinica,2022

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