Calculation of Damping Ratio and Analysis of Damping Effect of Turbine Blade Dry Friction Damper in Rotating State

The vibration of turbine blades during the operation of jet engines is a serious and complex issue that has garnered significant attention. In practical jet engines, dry friction damping is commonly used to suppress blade vibrations due to its reliability and efficiency. The equivalent damping ratio of dry friction dampers is a crucial metric for evaluating their performance. However, calculating dry friction dampers’ damping ratio for actual structures involves nonlinear vibration calculations, which are challenging and often lack precision. A method combining simulation and experimentation to calculate the equivalent damping ratio of a structure is proposed. In a laboratory setting, the vibration response of turbine blades under centrifugal load and the damping effect of under-platform dampers were analyzed using oil excitation. The research results indicate that this method can effectively calculate the equivalent damping ratio of actual structures. The findings provide robust support for the design of under-platform dampers and the vibration analysis of turbine blades.

Authors

Institutions

Publication Details

Journal
Aerospace
Published
2024-11-25
DOI
https://doi.org/10.3390/aerospace11120968
Citations
1
Primary Topic
Bladed Disk Vibration Dynamics
Type
article
Field-Weighted Citation Impact
0.26
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Calculation of Damping Ratio and Analysis of Damping Effect of Turbine Blade Dry Friction Damper in Rotating State

Kun Qiao, Di Li, Hongguang Li, Guang Meng et al.
1 citations
Aerospace
Bladed Disk Vibration Dynamics
0.26
article

Calculation of Damping Ratio and Analysis of Damping Effect of Turbine Blade Dry Friction Damper in Rotating State

Kun Qiao, Di Li, Hongguang Li, Guang Meng, Han Le, Dasheng Wei
article en
1 citations

Abstract

The vibration of turbine blades during the operation of jet engines is a serious and complex issue that has garnered significant attention. In practical jet engines, dry friction damping is commonly used to suppress blade vibrations due to its reliability and efficiency. The equivalent damping ratio of dry friction dampers is a crucial metric for evaluating their performance. However, calculating dry friction dampers’ damping ratio for actual structures involves nonlinear vibration calculations, which are challenging and often lack precision. A method combining simulation and experimentation to calculate the equivalent damping ratio of a structure is proposed. In a laboratory setting, the vibration response of turbine blades under centrifugal load and the damping effect of under-platform dampers were analyzed using oil excitation. The research results indicate that this method can effectively calculate the equivalent damping ratio of actual structures. The findings provide robust support for the design of under-platform dampers and the vibration analysis of turbine blades.

AerospaceVol. 11(12)
Shanghai Jiao Tong University (CN), Aero Engine Corporation of China (China) (CN), Beihang University (CN)
Affordable and clean energy
Openalex Percentile: Top 43%
Bladed Disk Vibration Dynamics
0.26
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.