DocumentCode :
2812115
Title :
The research of Lightning Protect for aerocraft electro-equipments
Author :
Quan, Xiuqiao ; Wu, Guiqin
Author_Institution :
Meas. Center, Xi´´an Flight Autom. Control Res. Inst., Xi´´an, China
fYear :
2011
fDate :
15-17 July 2011
Firstpage :
4595
Lastpage :
4597
Abstract :
The safety of the aircraft severely affected by lightning, lightning protection is the electro-equipment of aircraft need to be resolved a problem. In this paper,based on the the lightning induced transient susceptibility requirements of RATC/DO 160F,lightning induced pin injection test as an example, introduced the product interface circuit protection method. According to the signal characteristics of the signal transmission line and lightning induction test level, select the appropriate lightning protection devices; for the circuit´s input and output ports, using a variety of protection circuits, the effectiveness of the protection circuit verified by comparing simulation and experiment result.
Keywords :
aerospace components; aerospace safety; avionics; lightning protection; RATC/DO 160F; aerocraft electro-equipments; aircraft safety; lightning induced pin injection test; lightning induced transient susceptibility requirements; lightning induction test level; lightning protection devices; product interface circuit protection method; signal characteristics; signal transmission line; Aerospace control; Aircraft; Atmospheric modeling; Integrated circuit modeling; Lightning protection; Signal resolution; Pin Injection; aerocraft; lightning Induced;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location :
Hohhot
Print_ISBN :
978-1-4244-9436-1
Type :
conf
DOI :
10.1109/MACE.2011.5988031
Filename :
5988031
Link To Document :
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