scholarly journals Modeling and Dynamic Characteristics Analysis of a Continuously Variable Damper with Electro-Hydraulic Pressure Control Valve

2002 ◽  
Vol 8 (2) ◽  
pp. 158-166
Author(s):  
Jerry R. Boza ◽  
Kapseong Ro

Electro-hydraulic pressure-control valves are used in many applications, such as manufacturing equipment, agricultural machinery, and aircrafts to name a few. A traditional electro-hydraulic pressure-control valve regulates an output pressure for a corresponding input current by balancing solenoid force, spring force, and regulated pressure force. This results in a repeatable steady-state pressure output that is nearly proportional to the input current. This is helpful in open loop applications when one wants to achieve a consistent output pressure for a corresponding input current. The transient pressure response, however, is highly sensitive to the component tolerances and manufacturing processes as well as the fluid properties in the regulated volume, such as bulk modulus, viscosity, density, and aeration. These properties are often unknown in a system and can vary significantly from system to system and also during use in a typical application, making controllability difficult. Since there is variation in the steady-state pressure output for a given valve population, these valves are often calibrated in the end system to better achieve the desired output. This helps, but there is variation in this process, and also variation within a single valve over life. So although various attempts are made to minimize steady-state error, it will always exist and therefore closed loop control is desirable. Unfortunately, attempts at closed loop control of a traditional pressure-control valve often yield unacceptable and inconsistent performance. This is due to the sensitivity of the transient response to system characteristics, primarily fluid and mechanical properties of the regulated control port volume. The transient performance sensitivity of the valve can be reduced by de-coupling the regulated pressure dynamics from the spool dynamics. This will conversely increase the sensitivity of the steady state performance; however this can be solved through the implementation of a closed loop controller. In this paper a dynamic model is developed for a traditional pressure-control valve and different pressure-control valves without the traditional pressure balancing force. The new valve models are validated experimentally and then used to compare the performance characteristics of the valves. Linear analysis is performed on the validated models to further illustrate the impact of the system properties. The objective of this work is to develop a pressure-control valve with more consistent transient performance characteristics that are less sensitive to the system parameters so that a closed loop controller can be developed for the valve.


Author(s):  
J Ruan ◽  
R Burton ◽  
P Ukrainetz ◽  
Y. M. Xu

The two-dimensional pressure control valve is a piloted control valve which functions by using both linear and rotary motions of a single spool. A groove on the spool land, incorporating a sensing channel, forms the pilot stage to control the pressure of a spool chamber, while the load pressure is fed to the other spool chamber. To sustain the balance of the force across the spool, the load pressure must follow the change of pressure variation along the groove while the spool is in rotary motion. The geometric parameters of the groove and the spool-to-sleeve clearance have significant effects on both the static and dynamic characteristics of the valve. Increasing the sectional size of the groove results in a large Reynolds number and the static property of the valve thus changes from that of linearity owing to the entrance effect. The linearity of the static property is also affected by the leakage through the spool-to-sleeve clearance. The dynamic characteristics of the valve are dependent upon both the structural parameters and the tune constant of the load. The stability and dynamic response were investigated under different structural parameters and time constants of the load using both linear theory and simulation methods. Experiments were designed to obtain the static and dynamic characteristics of the valve and the leakage through the pilot. A balance should be made between the linearity of the static property and the response speed; it was found that both fairly linear static and desired dynamic characteristics could be simultaneously maintained for the two-dimensional pressure control valve.


2012 ◽  
Vol 263-266 ◽  
pp. 615-619
Author(s):  
Zhong Wei Sui ◽  
Jian Xiang Guo ◽  
Guo You Gao ◽  
Jia Wen Qiang

Self-operating differential pressure control valves has been widely used in HVAC system because of its unique control functions .For the research and development of the valves, a large number of performance parameters such as flow-resistance and controlled pressure difference are required.This paper proposed a multi-functional fluid apparatus on the basis of virtual instrument technology and variable frequency technology which can achieve continuous sampling of the test point.The measurement method and valve characteristics analysis are also practised.


Author(s):  
Liu Ruiwei ◽  
Hongwei Guo ◽  
Zhang Qinghua ◽  
Rongqiang Liu ◽  
Tang Dewei

Balancing stiffness and weight is of substantial importance for antenna structure design. Conventional fold-rib antennas need sufficient weight to meet stiffness requirements. To address this issue, this paper proposes a new type of cable-rib tension deployable antenna that consists of six radial rib deployment mechanisms, numerous tensioned cables, and a mesh reflective surface. The primary innovation of this study is the application of numerous tensioned cables instead of metal materials to enhance the stiffness of the entire antenna while ensuring relatively less weight. Dynamic characteristics were analyzed to optimize the weight and stiffness of the antenna with the finite element model by subspace method. The first six orders of natural frequencies and corresponding vibration modes of the antenna structure are obtained. In addition, the effects of structural parameters on natural frequency are studied, and a method to improve the rigidity of the deployable antenna structure is proposed.


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