Based on the structure of a certain type of aviation axial-piston pump＇s valve plate which adopts a pre-pressurization fluid path （consisting a damping hole, a buffer chamber, and an orifice） to reduce flow ripple,...Based on the structure of a certain type of aviation axial-piston pump＇s valve plate which adopts a pre-pressurization fluid path （consisting a damping hole, a buffer chamber, and an orifice） to reduce flow ripple, a single-piston model of the aviation axial-piston pump is presented. This sin- gle-piston model comprehensively considers fluid compressibility, orifice restriction effect, fluid resistance in the capillary tube, and the leakage flow. Besides, the instantaneous discharge areas used in the single-piston model have been calculated in detail. Based on the single-piston model, a multi-piston pump model has been established according to the simple hydraulic circuit. The sin- gle- and multi-piston pump models have been realized by the S-function in Matlab/Simulink. The developed multi-piston pump model has been validated by being compared with the numerical result by computational fluid dynamic （CFD）. The effects of the pre-pressurization fluid path on the flow ripple and the instantaneous pressure in the piston chamber have been studied and opti- mized design recommendations for the aviation axial-piston pump have been given out.展开更多
研制了一种双斜盘阀配流轴向柱塞式液压电机泵的样机,并阐述了一种依靠改变左右斜盘相对位置角度关系来实现液压泵排量改变的变量方式。研究表明:样机技术指标达到了额定压力20 MPa,输出流量298 m L/min,容积效率达到96%,并验证了新变...研制了一种双斜盘阀配流轴向柱塞式液压电机泵的样机,并阐述了一种依靠改变左右斜盘相对位置角度关系来实现液压泵排量改变的变量方式。研究表明:样机技术指标达到了额定压力20 MPa,输出流量298 m L/min,容积效率达到96%,并验证了新变量方式的可行性和具有余弦规律的变量特性。实验也证明了适当增大吸入阀弹簧预压紧力以抵消配流阀旋转时所受的离心力,与在吸入阀的前腔设计简易的离心增压装置以利用液体离心力等方式是可行的,不仅使得泵在中速(750~1200 r/min)时可保持较好的排量,而且在高速(1200~1500 r/min)时排量降低不显著。展开更多
基金Project supported by the National Natural Science Foundation of China(No.51275450)the National Basic Research Program of China(973 Program)(No.2014CB046403)the Science Fund for Creative Research Groups of National Natural Science Foundation of China(No.51521064)
基金the support of the National Natural Science Foundation of China (No. 51235002)the National Science Foundation for Distinguished Young Scholars (No. 50825502)
文摘Based on the structure of a certain type of aviation axial-piston pump＇s valve plate which adopts a pre-pressurization fluid path （consisting a damping hole, a buffer chamber, and an orifice） to reduce flow ripple, a single-piston model of the aviation axial-piston pump is presented. This sin- gle-piston model comprehensively considers fluid compressibility, orifice restriction effect, fluid resistance in the capillary tube, and the leakage flow. Besides, the instantaneous discharge areas used in the single-piston model have been calculated in detail. Based on the single-piston model, a multi-piston pump model has been established according to the simple hydraulic circuit. The sin- gle- and multi-piston pump models have been realized by the S-function in Matlab/Simulink. The developed multi-piston pump model has been validated by being compared with the numerical result by computational fluid dynamic （CFD）. The effects of the pre-pressurization fluid path on the flow ripple and the instantaneous pressure in the piston chamber have been studied and opti- mized design recommendations for the aviation axial-piston pump have been given out.
