Converter topology analysis for aircraft application.

Autor: Brombach, J., Jordan, M., Grumm, F., Schulz, D.
Zdroj: International Symposium on Power Electronics Power Electronics, Electrical Drives, Automation & Motion; 1/ 1/2012, p446-451, 6p
Abstrakt: This paper deals with an aircraft weight optimization through an analysis of different load-converter-architectures. A major effort in the development of new aircraft is the reduction of the weight. This results from a direct relationship between aircraft mass and efficiency. At a first step the global onboard converter architecture is analyzed. In addition to the conventional architectures two DC-grid architectures are shown. In the second step a weight reduction through converter optimization is presented. [ABSTRACT FROM PUBLISHER]
Databáze: Complementary Index