The paper presents an original multiple excitation system based on electromagnets with force control. The system is specifically designed in order to investigate the dynamics of bladed disks since it mimics the excitation existing in a real engine. Moreover the system is suitable for forced response tests of bladed disks with nonlinear dynamic response like in the case of presence of friction contacts since the amplitude of the exciting force is known with good precision. For this purpose a device called Force Measuring ElectroMagnet (FMEM), was designed and employed during the system calibration. The excitation system is applied to the test rig Octopus (see ASME Turbo Expo GT2010-22879) which includes underplatform dampers (UPDs). Tests we...
Application of pulse excitation for forced vibration of selected eigenmode of blade wheel under rot...
Abstract – This work describes an experimental study using design of experiments applied in magnetic...
A generic method for analysis of nonlinear forced response for bladed disks with friction dampers of...
The paper presents a static test rig called “Octopus” designed for the validation of numerical model...
In this paper a non-contact excitation system based on electromagnets is described. The system aims...
Underplatform dampers (UPDs) are still in use to reduce the vibration amplitude of turbine blades an...
Underplatform dampers (UPDs) are still in use to reduce the vibration amplitude of turbine blades an...
The paper presents the planning, structure and preliminary results of a new test rig for the validat...
This work focuses on efficient modelling and adaptive control of friction damping in bladed disks. T...
In this paper, we present a methodology and results from an experimental investigation of forced vib...
The mechanical design of turbine blades aims at verifying the structural integrity against High Cycl...
The paper presents the experimental activity about the dynamic response of the blades of a gas turbi...
The damping potential of multiple friction contacts in a bladed disk is investigated. Friction conta...
Bladed wheel dynamic characterization is a crucial issue to avoid resonance excitations. The test be...
This work presents dynamic analysis of a bladed disk system with underplatform dampers subjected to ...
Application of pulse excitation for forced vibration of selected eigenmode of blade wheel under rot...
Abstract – This work describes an experimental study using design of experiments applied in magnetic...
A generic method for analysis of nonlinear forced response for bladed disks with friction dampers of...
The paper presents a static test rig called “Octopus” designed for the validation of numerical model...
In this paper a non-contact excitation system based on electromagnets is described. The system aims...
Underplatform dampers (UPDs) are still in use to reduce the vibration amplitude of turbine blades an...
Underplatform dampers (UPDs) are still in use to reduce the vibration amplitude of turbine blades an...
The paper presents the planning, structure and preliminary results of a new test rig for the validat...
This work focuses on efficient modelling and adaptive control of friction damping in bladed disks. T...
In this paper, we present a methodology and results from an experimental investigation of forced vib...
The mechanical design of turbine blades aims at verifying the structural integrity against High Cycl...
The paper presents the experimental activity about the dynamic response of the blades of a gas turbi...
The damping potential of multiple friction contacts in a bladed disk is investigated. Friction conta...
Bladed wheel dynamic characterization is a crucial issue to avoid resonance excitations. The test be...
This work presents dynamic analysis of a bladed disk system with underplatform dampers subjected to ...
Application of pulse excitation for forced vibration of selected eigenmode of blade wheel under rot...
Abstract – This work describes an experimental study using design of experiments applied in magnetic...
A generic method for analysis of nonlinear forced response for bladed disks with friction dampers of...