DocumentCode :
2618864
Title :
Conducted emission analysis of electric nacelle anti ice system in aircraft
Author :
Qian Zhou ; Nothofer, Angela
Author_Institution :
Dept. of Electr. & Electron. Eng., Univ. of Nottingham, Nottingham, UK
fYear :
2012
fDate :
16-18 Oct. 2012
Firstpage :
1
Lastpage :
5
Abstract :
This paper describes the high frequency behaviour of an Electric Nacelle Anti Ice system (ENAI). In the high frequency range above 150kHz, conducted emissions have to be considered. A silicon-controlled rectifier (SCR) is the main source for conducted emissions. Simulation and measurements are implemented on the ENAI system for comparison and verification. Simulations were verified by measurements and were shown to be a good alternative to measurements to provide quick and reliable predictions, whilst interference in the measurement environment can cause errors.
Keywords :
avionics; thyristors; aircraft; conducted emission analysis; electric nacelle anti ice system; frequency 150 kHz; silicon-controlled rectifier; Current measurement; Electromagnetic interference; Firing; Ice; Load modeling; Switches; Thyristors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Systems for Aircraft, Railway and Ship Propulsion (ESARS), 2012
Conference_Location :
Bologna
ISSN :
2165-9400
Print_ISBN :
978-1-4673-1370-4
Electronic_ISBN :
2165-9400
Type :
conf
DOI :
10.1109/ESARS.2012.6387476
Filename :
6387476
Link To Document :
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