Design and Simulation of Electro-hydrostatic Actuator with a Built-in Power Regulator

Abstract The electro-hydrostatic actuator (EHA) is a kind of power-by-wire (PBW) actuator that converts the electrical power into localized hydraulic power for flight control. By removing the central hydraulic power supply together with hydraulic pipes, an EHA's reliability and efficiency are greatly improved but its frequency width and stiffness decreased. To overcome the drawback, this article proposes a novel structure of EHA associated with a power regulator. Composed of a high-pressure accumulator and a proportional valve, it can store and harness the hydraulic power flexibly according to the changing control requirements. The concept of transferred volume is put forward to estimate the capability of the power regulator. The actuator output position can be kept fixed with a hydraulic lock. The compounded control is specially developed to ensure the actuator system to operate in a correct manner. The simulation results indicate that the new-brand actuator results in efficient expanding of the system frequency width with an optimal power supply.

[1]  R. Alden Flight Demonstration, Evaluation and Proposed Applications for Various All Electric Flight Control Actuation System Concepts , 1993 .

[2]  Wei Li,et al.  Investigation of a High Precision Hydrostatic Actuation System: How Nonlinearities Affect Its Performance , 2007 .

[3]  Zongxia Jiao,et al.  NONLINEAR MODELING AND CONTROL DESIGN OF ELECTRO-HYDROSTATIC ACTUATOR , 2008 .

[4]  Li Jun,et al.  Research on fast response and high accuracy control of an airborne brushless DC motor , 2004, 2004 IEEE International Conference on Robotics and Biomimetics.

[5]  K. Bradley,et al.  A 5-Phase Fault-Tolerant Brushless Permanent Magnet Motor Drive for an Aircraft Thin Wing Surface Actuator , 2007, 2007 IEEE International Electric Machines & Drives Conference.

[6]  Andrew A. Goldenberg,et al.  Design of a new high-performance electrohydraulic actuator , 2000 .

[7]  P.W. Wheeler,et al.  Power supply loss ride-through and device voltage drop compensation in a matrix converter permanent magnet motor drive for an aircraft actuator , 2004, 2004 IEEE 35th Annual Power Electronics Specialists Conference (IEEE Cat. No.04CH37551).

[8]  Johann W. Kolar,et al.  Comparative evaluation of three-phase high-power-factor AC-DC converter concepts for application in future More Electric Aircraft , 2005, IEEE Transactions on Industrial Electronics.

[9]  Bo Gao,et al.  Research on fast response and high accuracy control of an airborne brushless DC motor , 2004, IEEE International Conference on Robotics and Biomimetics.

[10]  Bo Gao,et al.  Research on Dual-Variable Integrated Electro-Hydrostatic Actuator , 2006 .

[11]  Geng Yang,et al.  Finite-Time-Convergent Differentiator Based on Singular Perturbation Technique , 2007, IEEE Transactions on Automatic Control.