26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-6.5.2


A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS

T. Wijekoon, L. Empringham, P. W. Wheeler, J. C. Clare, C. Whitley*, J. Melia*, G. Towers*
Univ. of Nottingham, UK; *GE AVIATION, UK

Keywords: Electric Landing Gear, Electro Mechanical Actuator, BLDC drive, Hysteresis control

This paper describes a dual-output power converter concept where only the large components are shared between two actuators which are used sequentially in the deployment of aircraft landing gear. This mutual component approach combines the advantages of dual-use power converters with the flexibility of one power converter per application.


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