期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
A fault-tolerant triple-redundant voice coil motor for direct drive valves:Design, optimization, and experiment 被引量:4
1
作者 Wu Shuai Jiao Zongxia +2 位作者 Yan Liang Yu Juntao Chen Chin-Yin 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第4期1071-1079,共9页
A direct drive actuator (DDA) with direct drive valves (DDVs) as the control device is an ideal solution for a flight actuation system. This paper presents a novel triple-redundant voice coil motor (TRVCM) used ... A direct drive actuator (DDA) with direct drive valves (DDVs) as the control device is an ideal solution for a flight actuation system. This paper presents a novel triple-redundant voice coil motor (TRVCM) used for redundant DDVs. The TRVCM features electrical/mechanical hybrid triple-redundancy by securing three stators along with three moving coils in the same frame. A permanent magnet (PM) Halbach array is employed in each redundant VCM to simplify the system structure. A back-to-back design between neighborly redundancies is adopted to decouple the magnetic flux linkage. The particle swarm optimization (PSO) method is implemented to optimize design parameters based on the analytical magnetic circuit model. The optimization objective function is defined as the acceleration capacity of the motor to achieve high dynamic performance. The optimal geometric parameters are verified with 3D magnetic field finite element analysis (FEA). A research prototype has been developed for experimental purpose. The experimental results of magnetic field density and force output show that the proposed TRVCM has great potential of applications in DDA systems. 展开更多
关键词 Direct drive valve Hydraulic flight control Magnetic field optimization Particle swarm optimization Redundant motor
原文传递
A seventh-order model for dynamic response of an electro-hydraulic servo valve 被引量:8
2
作者 Liu Changhai Jiang Hongzhou 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2014年第6期1605-1611,共7页
In this paper, taking two degrees of freedom on the armature–flapper assembly into account, a seventh-order model is deduced and proposed for the dynamic response of a two-stage electro-hydraulic servo valve from non... In this paper, taking two degrees of freedom on the armature–flapper assembly into account, a seventh-order model is deduced and proposed for the dynamic response of a two-stage electro-hydraulic servo valve from nonlinear equations. These deductions are based on fundamental laws of electromagnetism, fluid, and general mechanics. The coefficients of the proposed seventhorder model are derived in terms of servo valve physical parameters and fluid properties explicitly.For validating the results of the proposed model, an AMESim simulation model based on physical laws and the existing low-order models validated by other researchers through experiments are used to compare with the seventh-order model. The results show that the seventh-order model can reflect the physical behavior of the servo valve more explicitly than the existing low-order models and it could provide guidance more easily for a linear control design approach and sensitivity analysis than the AMESim simulation model. 展开更多
关键词 Hydraulic control systems Nozzle–flapper Servo valve Torque motor Transfer function
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部