Optimization of Motor/Gear Drive System for Electric RPV.

Abstract

The goal of Phase I was to prove the feasibility of using a high speed brushless dc motor for propulsion in an RPV application. The electric propulsion system would include a brushless dc motor, electronic controller, and gear reducer that is optimally sized for the cruise condition of an RPV. Performance tests were to be conducted to measure developed power, while driving a propeller loaded at the cruise condition, and to test for the adequacy of heat rejection from the motor in the RPV configuration. The system was to be packaged for minimum size and weight. A complete electric propulsion system consisting of a brushless dc motor, controller, gearbox, and propeller was configured and bench tested. Heat rejection tests were also performed on the brushless dc motor in the RPV configuration. The final system of motor, controller and heat rejection hardware was then packaged for minimum size and weight. In the bench power tests output from the motor was measured to be 5 hp. The heat rejection tests showed that adequate cooling should be attainable through further improvements in a total cooling system.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1986
Accession Number
ADA177492

Entities

People

  • Milton Issacson

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Alternators
  • Assembly
  • Bench Tests
  • Brushless Dc Motors
  • Classification
  • Dc Motors
  • Electric Propulsion
  • Fuel Cells
  • Government Procurement
  • Governments
  • Motors
  • Performance Tests
  • Power Levels
  • Propulsion Systems
  • Security

Readers

  • Aerospace Test and Evaluation
  • Electrical Engineering
  • Neuroscience

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems