Title :
Flight performance of micro-wings rotating in an alternating magnetic field
Author :
Miki, N. ; Shimoyama, I.
Author_Institution :
Mechano-Inf., Tokyo Univ., Japan
Abstract :
The flight mechanism that gains thrust by rotating magnetic wings in an alternating magnetic field is proposed. Through the analysis and the experiments with large-sized models whose wing length is from 3 mm to 8.6 mm, some hints for the design of micro-sized models whose wing length is around 1 mm were shown. That is, the wings should be flat, the angle of attack should be over 25 degrees, and the take-off frequency is estimated to be 600 Hz. We made micro-sized models using MEMS technology. The wings are made of electroplated nickel, and a thin glass rod is attached to the center as an axis of rotation. The glass rod is inserted into a small glass tube which works as an outer bearing. The 900 /spl mu/m long micro-wings succeed in flying up at a rotating frequency of 570 Hz. The thrust generated by the wings at 570 Hz can be regarded as the weight of the micro-wings.
Keywords :
attitude control; drag; electromagnetic actuators; electroplating; microactuators; microfluidics; micromachining; microrobots; torque; 3 to 8.6 mm; 570 Hz; 900 mum; MEMS technology; Ni; alternating magnetic field; angle of attack; attitude control; drag forces; electroplated nickel; fabrication; flight mechanism; flight performance; flying microrobots; large-sized models; lift forces; low Reynolds number flow; micro-sized models design; microfluidics; outer bearing; polyimide residual stress; rotating magnetic wings; rotating micro-wings; scale effect; small glass tube; take-off frequency; thin glass rod; thrust gain; torque; wing length; Fluid dynamics; Frequency estimation; Glass; Magnetic analysis; Magnetic fields; Magnetic materials; Micromechanical devices; Nickel; Performance gain; Viscosity;
Conference_Titel :
Micro Electro Mechanical Systems, 1999. MEMS '99. Twelfth IEEE International Conference on
Conference_Location :
Orlando, FL, USA
Print_ISBN :
0-7803-5194-0
DOI :
10.1109/MEMSYS.1999.746794