TY - JOUR
T1 - Design and testing of a high power piezo pump for hydraulic actuation
AU - Sell, Nathan
AU - Feehally, Tom
AU - Plummer, Andrew
AU - Wilson, Peter
AU - Du Bois, Jonathan
AU - Johnston, N
AU - Roesner, Jens
AU - De Bartolomeis, Andrea
AU - Love, Tom
PY - 2023/2/15
Y1 - 2023/2/15
N2 - Traditional valve-controlled hydraulic cylinders are usually very inefficient due to power loss through the control valve. An efficient alternative architecture is to distribute power electrically rather than hydraulically to a group of cylinders and drive each cylinder via individual servomotor-driven pumps. This arrangement is called electrohydrostatic actuation. Such actuators are currently available for power ratings of several hundred watts or greater, but not in the sub-100W range. This paper details the design, simulation and testing of a piezopump which is intended to address this gap. The motivation is for aerospace applications, and in particular accessory actuators used in the landing gear system. The 10\,W-100\,W range is a high-power output for a piezopump, and to achieve this a novel design using disc-style reed valves was developed to allow pumping frequencies above 1kHz. These high frequencies necessitated the development of custom power electronics capable of delivering 950\,V peak-peak sine wave excitation to a largely capacitive load. Experimental results show that the piezopump is capable of delivering over 30\,W of hydraulic power, and at no-load can deliver up to 2\,L/min of flow at 1250\,Hz. Future development includes a transition to multi-cylinder pumps, and improved reed-valve modelling to improve the accuracy of simulated performance.
AB - Traditional valve-controlled hydraulic cylinders are usually very inefficient due to power loss through the control valve. An efficient alternative architecture is to distribute power electrically rather than hydraulically to a group of cylinders and drive each cylinder via individual servomotor-driven pumps. This arrangement is called electrohydrostatic actuation. Such actuators are currently available for power ratings of several hundred watts or greater, but not in the sub-100W range. This paper details the design, simulation and testing of a piezopump which is intended to address this gap. The motivation is for aerospace applications, and in particular accessory actuators used in the landing gear system. The 10\,W-100\,W range is a high-power output for a piezopump, and to achieve this a novel design using disc-style reed valves was developed to allow pumping frequencies above 1kHz. These high frequencies necessitated the development of custom power electronics capable of delivering 950\,V peak-peak sine wave excitation to a largely capacitive load. Experimental results show that the piezopump is capable of delivering over 30\,W of hydraulic power, and at no-load can deliver up to 2\,L/min of flow at 1250\,Hz. Future development includes a transition to multi-cylinder pumps, and improved reed-valve modelling to improve the accuracy of simulated performance.
KW - Piezoelectric
KW - hydraulics
KW - piezoppump
KW - piezoelectric-hydrostatic actuator
M3 - Article
JO - Journal of Intelligent Material Systems and Structures
JF - Journal of Intelligent Material Systems and Structures
SN - 1045-389X
ER -