An Induction Motor Drive Using a Resonant DC Link Inverter.

Abstract

New initiatives to increase the use of electrical power, such as the electric vehicle and the More Electric Airplane, have created a need for improved motor drives. The use of adjustable speed drives has recently received more attention in these applications because new circuit topologies and power components have been developed that have enabled improvements in efficiency, power density and response times. This study reports the design and simulation of an actively clamped resonant dc link inverter that will drive an induction motor based blower. The objective of this study is to design, build and test a resonant dc link (RDCL) inverter and compare the performance of a six-step control strategy with a pulse density modulation strategy in an adjustable speed drive. Comparisons are made between a hard switched pulse width modulation converter and an RDCL inverter. Theoretical and experimental power loss calculations of the RDCL inverter are compared and discussed. The performance of constant voltage/frequency adjustable speed control is presented.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1996
Accession Number
ADA307324

Entities

People

  • Gregory L. Fronista

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Converters
  • Efficiency
  • Frequency
  • Induction Motors
  • Inverters
  • Magnetic Cores
  • Modulation
  • Motors
  • Power Electronics
  • Resonant Circuits
  • Resonant Frequency
  • Simulations
  • Sine Waves
  • Topology

Readers

  • Electrical Engineering
  • Radio communications and signal processing.