An Electromechanically Actuated Nose Landing Gear Using a Dual-Output Motor Control Unit

Paper #:
  • 2010-01-1744

Published:
  • 2010-11-02
Citation:
Wheeler, P., Empringham, L., and Clare, J., "An Electromechanically Actuated Nose Landing Gear Using a Dual-Output Motor Control Unit," SAE Technical Paper 2010-01-1744, 2010, https://doi.org/10.4271/2010-01-1744.
Pages:
5
Abstract:
This paper describes the design, construction and testing of a dual-output power converter concept where the large components, such as the DC link capacitor and heat-sink, 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. Practical results of the converter operating are presented for a range of test conditions in order to validate the simulation study.
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