Yves Bidaut

Rotordynamic Stability Of A 9500 Psi Reinjection Centrifugal Compressor Equipped With A Hole Pattern Seal-Measurement Versus Prediction Taking Into Account The Operational Boundary Conditions.

Mechanical Development department of MAN Turbo, in Zürich, Switzerland. His job function includes the development and analysis of the components of centrifugal compressors for oil and gas application. He is responsible for providing technical support in rotordynamics and stress analysis. Before joining the site in Switzerland in 2003, he was employed for six years in MAN Turbo, Berlin, where he was involved in the design, finite element analysis, rotordynamic analysis, testing, and development of centrifugal compressors. Mr. Bidaut received his diploma (Mechanical Engineering, 1995) from the University of Valenciennes (France).

Identification of Eigenmodes and Determination of the Dynamical Behaviour of Open Impellers

Whenever an open bladed impeller (without shroud) is implemented in a centrifugal compressor a key issue regarding the reliability of the compressor concerns the dynamical behaviour of this impeller. Due to the absence of the shroud this impeller can be operated at high tip speeds, hence allowing for higher volume flow. However the impeller reacts very sensitive to excitations leading to large blade vibrations with potential considerable dynamic stresses. In order to avoid resonance caused by fluctuating pressure distributions due to rotor-stator interactions special attention must be paid to the natural frequencies of the impeller which shall be determined with the highest accuracy possible.Therefore this paper focuses on the identification of the natural frequencies of the impeller first. To validate the finite-element (FE) model extensive measurements of the natural frequencies are performed at standstill. Especially the set-up and results obtained with the Shaker-Laser vibrometer-tests are described in detail and compared to other measurement methods such as the Laser-Scaning-Vibrometry (LSV) and strain gauges.Furthermore the prediction of the dynamic behaviour of the impeller is of considerable importance in the design of turbo compressors. For this purpose comprehensive measurements of the dynamic stress are carried out on the author’s company’s test rig. The paper describes the test arrangement including numerous strain gauges installed in different positions of the blades.The last part of this paper describes a simplified approach for the evaluation of the dynamic stresses in the impeller blade. A substantial list of comprehensive lectures about coupled CFD–structural analysis to determine the dynamic behaviour of impeller blades is available. However, despite of considerable improvement in software and calculation methods in the last years, such analyses are still expensive and require very large capacities. The presented alternative calculation method is based on a harmonic analysis which is calibrated to the measurements and is the base for a further estimation of the life time of the impeller.Copyright