| contributor author | Zaipeng Man | |
| contributor author | Fan Ding | |
| contributor author | Chuan Ding | |
| contributor author | Shuo Liu | |
| date accessioned | 2017-05-08T22:24:40Z | |
| date available | 2017-05-08T22:24:40Z | |
| date copyright | November 2015 | |
| date issued | 2015 | |
| identifier other | 44253285.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/80082 | |
| description abstract | To guarantee the reliability of hydraulic systems, it is of vital importance to do impulse testing for hydraulic components. A hydraulic impulse-testing system with pressure difference feedback from a second-stage valve is studied. A mathematical model of the system is built, and it shows that the inner closed-loop damping ratio of the system is influenced by the pressure difference feedback of the control chambers of the second-stage valve. And by changing the pressure difference feedback gain, various damping ratios can be achieved, which is a key factor affecting the system overshoot. The results of both the simulation and experiment show that with the same square wave input the system overshoot can be freely controlled between 0 and 50% by adjusting the pressure difference feedback gain, which is a new method to obtain both peak wave impulse pressure cycle and square wave impulse pressure cycle utilizing the same system and the same input. | |
| publisher | American Society of Civil Engineers | |
| title | Hydraulic Impulse-Testing System with Pressure Difference Feedback from a Second-Stage Valve | |
| type | Journal Paper | |
| journal volume | 28 | |
| journal issue | 6 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000492 | |
| tree | Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006 | |
| contenttype | Fulltext | |