Power conversion technologies for reducing harmonics on the more electric aircraft

SAE Technical Papers

Volumn , Issue , 2006, Pages

  Furmanczyk, Kaz ^a   Stefanich, Mark ^a  

^a ELDEC Corporation

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; ELECTRIC VEHICLES;

CONVERTER TOPOLOGIES; CURRENT HARMONICS; IMPROVING POWER; MORE ELECTRIC AIRCRAFT; POWER CONVERSION; QUALITY REQUIREMENTS; TOTAL DISTORTION;

POWER QUALITY;

EID: 85072418553     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2006-01-3086     Document Type: Conference Paper

References (8)

1. Matheson E., Karimi K.,-"Power Quality Specification Development for more ELECTRIC Airplane Architecture" SAE 2002 Power System Conference, Paper 2002-01-3206.
2. Enviromental Conditions and Test Procedures for Airborne Equipment-RTCA DO-160E, Section 16.
3. Furmanczyk K., Stefanich M., "Demonstration of Very High Power Airbone AC to DC Converter" SAE 2004 Power System Conference, Paper 2004-01-3210.
4. Traver J., "A Multi-Phase Transformer for Shipboard Electronics Systems" Powertechnics Magazine, December 1990.
5. Klumpner C., Blaabjerg F., Thoegersen P., "Evaluation of the Converter Topologies Suited for Integrated Motor Drivers" IEEE Poblication No. 1077-2618/06.
6. Pathak A., Locher R., Mazumdar H., "3-Phase Power Factor Correction, Using Vienna Rectifier Approach and Modular Construction for Improved Overal Performance, Efficiency and Reliability" 2003 Power Electronics Conference, Long Beach, CA.
7. Baumann M., Drofenik U., Kolar J., "New Wide Input Range Three-Phase Unity Power Factor Rectifier Formed by Integration of a Three-Switch Buck-Derived Front End and a DC/DC Boost Converter Output Stage" IEEE International Telecommunications Energy Conference, September 10-14, 2000, Phoenix, AZ.
8. Hammond P. W., "Autotransformer" U.S. Patent 5,619,407, April 8, 1997.