Design theory for vibration characterisation experiments on real turbine blades with underplatform damper
DOI:
https://doi.org/10.54097/hzb1dt09Keywords:
Aero-engine, blade vibration, vibration reduction, dry friction damping, underplatform damper, structural design, parameter optimization, vibration reduction experiment.Abstract
One of the main causes of turbine rotor blade failures is high-frequency fatigue caused by blade resonance, and the vibration of turbine blades can be effectively suppressed through the reasonable design of dry friction damping structure. In order to understand the vibration characteristics of the blade-disc system and to check whether the damping effect meets the technical specifications, it is necessary to design and carry out dry friction damping blade vibration characteristics experiment. This paper takes a certain type of underplatform damped turbine blade in production as an example, and briefly describes the design idea and design process of such blade vibration characteristic experiments under the premise of the experiment blade structure, material and other physical parameters.
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