Influence of support stiffness on aero-engine coupling vibration quantitative analysis
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This paper investigates the whole aero-engine coupling vibration, as a rotor tester to be the research object. The rotor tester system is composed of two mountings, stator system, support structures and the rotor system. The modal experiment of the whole tester under the condition of mounting in the test room is carried out. The finite element (FE) model of the rotor tester is built, and the model was modified and validated according to the modal test results. A rotor-stator coupling factor and a section rotor-stator rubbing risk coefficient are proposed, the influence of the support stiffness values on the engine vibration characteristics, such as natural frequencies, modal shapes, rotor-stator coupling degree, and stator-rotor rubbing risk degree at compressor and turbine section is quantitative studied. Results show that the support stiffness contributes to the rigid body modal shapes greatly and to the rotor bending ones slightly. The factor and coefficient defined in this study are both reasonable, and they can reflect the corresponding characteristics exactly. Moreover, the effect of the supports stiffness values on the rotor-stator coupling degree and the rotor-stator rubbing risk degree is nonlinear. The rotor-stator coupling factor and the section stator-rotor rubbing risk coefficient proposed in this study provide a new way to quantitatively research the whole engine coupling vibration.Keywords:
Rubbing
This paper introduces the theories of modal analysis,uses modal testing system to identify the frame modal parameters of one motorcycle,conducts modal analysis on this motorcycle frame with finite element software,MSC.Patran/Nastran,and compares simulation results,which demonstrates the agreement of the two analytical methods.
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Experimental modal analysis has developed into a major technology for the study of structural dynamics. Complex structural dynamic responses can be represented using decoupled vibration modes, each of which is a single-degree-of-freedom (DOF) system governed by its natural frequency and mode shape. The study of the dynamic characteristics represented by modal properties, including the natural frequency and mode shape, is referred to as modal analysis. Theoretical modal analysis solves the differential equations of the motion (i.e. the analytical model) of a structure to compute the structure's modal properties. Experimental modal analysis, on the other hand, primarily concerns the determination...
Natural frequency
Structural Dynamics
Mode (computer interface)
Operational Modal Analysis
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In engineering domains, modal analysis is a field that is studied extensively with the goal of better characterizingcomponents or structures. Themodal analysis produces modal parameters, which are essential properties of a system that can be employed for damage identification, vibration analysis, and structural health monitoring. Plated element’s relevance in variousapplications makes it an intriguing vibration study subject. In thisresearch, modal analysis was performed on a square steel plate in free ends condition. This work aimedto provide a complete anatomical description of this complex boundary condition and its implications on modal parameters. Before comparing modal parameters with experimental data, a primary modal analysis was performed using finite element (FE)method. Then experimental analysis was conducted under the operational modal analysis setup (OMA).As the results, six natural frequencies are retrieved and compared amongst the two methods, recording the maximum of 6% percentage difference from the readings. This implied a close values estimated between the methods used. For mode shapes, ninemodes are identified from FE method and discussed according to established free plate vibration studies, while threesimilarly identified modes successfully recognized by using OMA.
Operational Modal Analysis
Square (algebra)
Natural frequency
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This paper deals with modal analysis and estimation of modal parameters of an analyzed structure. An aim of the paper is to verify one of four basic assumptions considered in modal testing. This property is reciprocity. Reciprocity means that the frequency response function measured between two degrees-of-freedom must be the same regardless of which degree-of-freedom is input or output. In the paper the experimental and numerical modal analysis of a cantilever beam are presented. There are described two experimental measurements focused on reciprocity of measurement process. Measured mode shapes are compared to each other using Cross Modal Assurance Criterion. The results of experimental and numerical modal analysis are compared to each other.
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In order to understand the vibration characteristic of a barrel,modal experiments are carried out to get parameters such as natural frequency,damping ratio and vibration pattern.Additionally,the finite element modal analysis of the barrel is conducted to guide modal experiment.The results of modal experiment and finite element analysis are compared,and they are in good agreement.
Natural frequency
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