Research on Parameters Matching of Ultralight Electric Aircraft Propulsion System

Gui Wen Kang; Yu Hu; Ya Dong Li; Wen Hui Jiang

doi:10.4028/www.scientific.net/AMR.732-733.1212

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 732-733Research on Parameters Matching of Ultralight...

Research on Parameters Matching of Ultralight Electric Aircraft Propulsion System

Abstract:

The propulsion system of ultralight electric aircraft is one of the general aviation technology development directions. It has the advantages such as light pollution, low noise, high energy utilization ratio, simple structure, easy maintenance, high reliability, less heat radiation, little operation cost and so on. Combined with the certain type of ultralight aircraft design parameters, the layout of aircraft electric propulsion, the principles and steps of the parameter matching of electric propulsion system were presented. The method of parameter matching and performance verification of electric propulsion system was put forward. The feasibility of the system is verified from the point of dynamic property. The study of parameter matching of electric propulsion system could not only provide basis for the integrated optimization for electric power system, but also evaluate the performance of the system simulation as reference.

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Periodical:

Advanced Materials Research (Volumes 732-733)

Pages:

1212-1215

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.732-733.1212

Citation:

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Online since:

August 2013

Authors:

Gui Wen Kang, Yu Hu, Ya Dong Li, Wen Hui Jiang

Keywords:

Electric Propulsion System, Environmental Protection, Parameter Matching, Performance Verification, Uiltralight Aircraft

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