Title :
The sound field analysis of piezoelectric micromachined ultrasound transducer array
Author :
Xu, Yueping ; Xu, Limei ; Li, Xuesheng ; Miao, Jianmin ; Wang, Zhihong
Author_Institution :
Inst. of Astronaut. & Aeronaut., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
Abstract :
The acoustic boundary element method is applied to solve the Helmholtz boundary integral equation for the sound field problem in the exterior region. Basing on the acoustic boundary element method, the SYSNOISE software is used to numerically calculate the far field sound pressure in the exterior region of piezoelectric micromachined ultrasound transducer array. On the other hand, according to given test conditions, the test platform is putted up, and the frequency response curve chart of the sound pressure level is plotted in the frequency domain. It´s shown that the results obtained by the two methods make a good agreement with each other, and that the acoustic boundary element method with SYSNOISE software in this paper can be used to predict the performance of piezoelectric micromachined ultrasound transducer array at the stage of preliminary design.
Keywords :
acoustic field; boundary integral equations; boundary-elements methods; frequency-domain analysis; piezoelectric transducers; ultrasonic transducer arrays; Helmholtz boundary integral equation; SYSNOISE software; acoustic boundary element method; frequency response curve chart; numerical calculation; piezoelectric micromachined ultrasound transducer array; sound field analysis; sound field problem; Acoustic arrays; Acoustic testing; Acoustic transducers; Boundary element methods; Frequency response; Integral equations; Piezoelectric transducers; Ultrasonic imaging; Ultrasonic transducer arrays; Ultrasonic transducers; boundary element method; fluid mesh model; piezoelectric micromachined ultrasound transducer; test platform;
Conference_Titel :
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location :
Changchun
Print_ISBN :
978-1-4244-2692-8
Electronic_ISBN :
978-1-4244-2693-5
DOI :
10.1109/ICMA.2009.5246131