Title of article :
A fault-tolerant triple-redundant voice coil motor for direct drive valves: Design, optimization, and experiment
Author/Authors :
Wu، نويسنده , , Shuai and Jiao، نويسنده , , Zongxia and Yan، نويسنده , , Liang and Yu، نويسنده , , Juntao and Chen، نويسنده , , Chin-Yin، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2013
Pages :
9
From page :
1071
To page :
1079
Abstract :
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.
Keywords :
Magnetic Field Optimization , Redundant motor , particle swarm optimization , Direct drive valve , Hydraulic flight control
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2013
Journal title :
Chinese Journal of Aeronautics
Record number :
2265335
Link To Document :
بازگشت