Application of pulse excitation for forced vibration of selected eigenmode of blade wheel under rotation. The paper deals with a solution of multipoint electromagnetic pulse excitation of turbine blade wheel under rotation for analysis of its dynamic behaviour. Since a width of electromagnetic pulses should decrease with revolution speed, magnetomotoric forces acting to the blades decrease, too. So, the application of more “high-speed” electromagnets distributed along a circumference of the wheel that multiply the excitation potential seems to be inevitable for such a stiff structure. It, however, requires accurate synchronization of the electromagnets with wheel revolutions and with a dynamic response of the selected blade. Furth...
In this paper a non-contact excitation system based on electromagnets is described. The system aims...
Le pilotage par Modulation de Largeur d’Impulsion (MLI) des moteurs électriques induit des oscillati...
Turbine blades are subjected to nozzle excitation frequencies that can correspond to eigen frequenci...
The procedure for design of blade vibration excitation by synchronous electromagnets is presented. I...
The report analyzes the principle of excitation of turbine wheel vibration by means of magnets switc...
The analytical expressions for description of traveling waves in rotating blade wheels are presented...
The model of the test bladed wheel was mistuned due to the implementation of additional two groups o...
The paper describes the natural frequency identification experiment and results of measuring of blad...
Bladed wheel dynamic characterization is a crucial issue to avoid resonance excitations. The test be...
Development of excitation by magnetic field for a rotating bladed wheel were analyzed and tested on ...
The paper presents an original multiple excitation system based on electromagnets with force control...
The system for active control of the test blade wheel under rotation was designed and realized in th...
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was perfor...
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was perfor...
International audienceRotors of asynchronous machines can be subjected to risk of failure due to vib...
In this paper a non-contact excitation system based on electromagnets is described. The system aims...
Le pilotage par Modulation de Largeur d’Impulsion (MLI) des moteurs électriques induit des oscillati...
Turbine blades are subjected to nozzle excitation frequencies that can correspond to eigen frequenci...
The procedure for design of blade vibration excitation by synchronous electromagnets is presented. I...
The report analyzes the principle of excitation of turbine wheel vibration by means of magnets switc...
The analytical expressions for description of traveling waves in rotating blade wheels are presented...
The model of the test bladed wheel was mistuned due to the implementation of additional two groups o...
The paper describes the natural frequency identification experiment and results of measuring of blad...
Bladed wheel dynamic characterization is a crucial issue to avoid resonance excitations. The test be...
Development of excitation by magnetic field for a rotating bladed wheel were analyzed and tested on ...
The paper presents an original multiple excitation system based on electromagnets with force control...
The system for active control of the test blade wheel under rotation was designed and realized in th...
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was perfor...
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was perfor...
International audienceRotors of asynchronous machines can be subjected to risk of failure due to vib...
In this paper a non-contact excitation system based on electromagnets is described. The system aims...
Le pilotage par Modulation de Largeur d’Impulsion (MLI) des moteurs électriques induit des oscillati...
Turbine blades are subjected to nozzle excitation frequencies that can correspond to eigen frequenci...