Abstract:In order to realize a stator structure with large thrusttoweight ratio and better profit for miniaturization,an inplane longitudinalbending compound linear ultrasonic motor was designed and developed in this study. The working principle of this type of motor and the forming condition of the elliptical locus of the driving foot of the stator were discussed,and the stator structure was optimized by using the finite element analysis software. A motor prototype was fabricated,the feasibility and rationality of the motor design were verified,and the experimental study on the vibration performance of the stator driving foot and the output performance of the motor were carried out. The results showed that under the conditions of the peaktopeak excitation voltage of 200 V,the prepressure of 20 N,the excitation frequency of 45.7 kHz,and the phase difference of 90°, the noload speeds of the motor in the left and right directions are 0.25 m/s and 0.22 m/s,respectively, and the maximum thrust was 3.4 N and the thrusttoweight ratio was 47 (the stator mass was 7.36 g).Compared with the prototype of the inplane longitudinalbending linear ultrasonic motor, the amplitude of driving foot of the slotted stator was increased, and the output speed and thrust of the motor were increased significantly (the noload speed was increased by 51.5% and the maximum thrust was increased by 36%),which is beneficial to the miniaturization of linear ultrasonic motor.