scholarly journals Thermal Behavior of a Magnetically Levitated Spindle for Fatigue Testing of Fiber Reinforced Plastic

Actuators ◽  
2019 ◽  
Vol 8 (2) ◽  
pp. 37
Author(s):  
Daniel Franz ◽  
Maximilian Schneider ◽  
Michael Richter ◽  
Stephan Rinderknecht

This article discusses the critical thermal behavior of a magnetically levitated spindle for fatigue testing of cylinders made of fiber reinforced plastic. These cylinders represent the outer-rotor of a kinetic energy storage. The system operates under vacuum conditions. Hence, even small power losses in the rotor can lead to a high rotor temperature. To find the most effective way to keep the rotor temperature under a critical limit in the existing system, first, transient electromagnetic finite element simulations are evaluated for the active magnetic bearings and the electric machine. Using these simulations, the power losses of the active components in the rotor can be derived. Second, a finite element simulation characterizes the thermal behavior of the rotor. Using the power losses calculated in the electromagnetic simulation, the thermal simulation provides the temperature of the rotor. These results are compared with measurements from an experimental spindle. One effective way to reduce rotational losses without major changes in the hardware is to reduce the bias current of the magnetic bearings. Since this also changes the characteristics of the magnetic bearings, the dynamic behavior of the rotor is also considered.

2003 ◽  
Vol 17 (08n09) ◽  
pp. 1959-1964 ◽  
Author(s):  
Nam Seo Goo ◽  
K. Joon Yoon

This paper has focused on the analysis of newly proposed Lightweight Piezo-composite Curved Actuator. LIPCA was born from the idea that the heavy metal layers of THUNDERTM were replaced by lightweight fiber reinforced plastic layers. Several combinations of composites and PZT wafer have been tested and finally two types are chosen: LIPCA-C1 and C2. Finite element code, developed in the previous work, has been used for the investigation of their static and dynamic behaviors. The maximum actuation displacements and fundamental frequency with respect to the design parameters are presented.


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