Design and testing of a high power piezo pump for hydraulic actuation
Source abstract
Abstract
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-100 W 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 10–100 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 1 kHz. 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.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Hydraulic and Pneumatic Systems · Advanced MEMS and NEMS Technologies · Fuel Cells and Related Materials
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
University of Bath, Bath, UK
Safran Landing Systems, Gloucester, Gloucestershire, UK
Funding
Innovate UK
References (35)
Show source-provided references
1. 10.3390/s1906130110.3390/s19061301 ↗
2. 10.1201/EBK143981808410.1201/EBK1439818084 ↗
3. 10.1119/1.197624010.1119/1.1976240 ↗
4. 10.1186/s10033-018-0217-610.1186/s10033-018-0217-6 ↗
5. 10.1007/s42405-018-0058-710.1007/s42405-018-0058-7 ↗
6. 10.1243/PIME_PROC_1991_205_318_0210.1243/PIME_PROC_1991_205_318_02 ↗
7. 10.1177/095965181351520510.1177/0959651813515205 ↗
8. 10.1115/1.402610610.1115/1.4026106 ↗
9. 10.1177/1045389X1243862810.1177/1045389X12438628 ↗
10. 10.1115/1.403282610.1115/1.4032826 ↗
11. 10.1177/1045389X0403973010.1177/1045389X04039730 ↗
12. 10.1016/j.scriptamat.2015.12.03010.1016/j.scriptamat.2015.12.030 ↗
13. 10.1002/978111933244210.1002/9781119332442 ↗
14. 10.1117/12.35076010.1117/12.350760 ↗
15. 10.1106/HC2A-ABR9-21H8-2TJB10.1106/HC2A-ABR9-21H8-2TJB ↗
16. Nguyen AP · Journal of Aerospace System Engineering · 2018 · 12 · 54
17. Noliac (2022) Piezo actuator drive (PAD). Available at: http://www.noliac.com/tutorials/motorspad/ (accessed 8 April 2022).
18. 10.1177/10453890140043803710.1177/104538901400438037 ↗
19. O’Neill C · US Patent 7 · 2009 · 484 · 940
20. 10.1117/12.71701510.1117/12.717015 ↗
21. Parker Hannafin Corp (2021) Compact eha: Electro-hydraulic actuators for high power density applications. Catalog HY22-3101E 9/20.
22. 10.1016/j.snb.2019.12696110.1016/j.snb.2019.126961 ↗
23. Physik Instrumente LTD (2022) Piezowalk actuators. Available at: https://www.physikinstrumente.co.uk/en/products/linear-actuators/ (accessed 8 April 2022).
24. 10.1243/09596518JSCE22910.1243/09596518JSCE229 ↗
25. 10.1016/j.sna.2016.04.02610.1016/j.sna.2016.04.026 ↗
26. 10.3384/ecp182p27410.3384/ecp182p274 ↗
27. 10.1088/0964-1726/14/1/01010.1088/0964-1726/14/1/010 ↗
28. 10.1109/ACCESS.2018.281401010.1109/ACCESS.2018.2814010 ↗
29. Timoshenko SP · 1959
30. 10.3390/mi1202014010.3390/mi12020140 ↗
31. 10.1061/JMCEA3.000210610.1061/JMCEA3.0002106 ↗
32. 10.1007/s12206-019-0121-810.1007/s12206-019-0121-8 ↗
33. 10.1016/j.sna.2019.11176610.1016/j.sna.2019.111766 ↗
34. 10.1177/1045389X1453343910.1177/1045389X14533439 ↗
35. 10.1111/j.1151-2916.1996.tb08095.x10.1111/j.1151-2916.1996.tb08095.x ↗