DocumentCode :
3662031
Title :
Model development of eddy current brakes for Energy Absorbing System
Author :
Arunesh Kumar Singh; Ibraheem
Author_Institution :
Deptt. of Electr. Eng., Jamia Millia Islamia, New Delhi, India
fYear :
2015
fDate :
3/1/2015 12:00:00 AM
Firstpage :
382
Lastpage :
384
Abstract :
Aircraft Arrester Barrier Systems (AABS) are very important for the purpose of arresting combat aircrafts due to aborted take-off and emergency landings. This system is installed near the end of runways. Energy Absorbing System (EAS) is one of the important subsystems of AABS. There is no control on energy absorption during operation of an aircraft emergency arrestment in conventional EAS. It is highly nonlinear in nature and these are installed as per the capacity of the aircraft. To overcome this problem, we may use the eddy current braking system (ECBS) for the energy absorber. In proposed ECBS, braking torque is high and controllable so that any weight capacity of aircraft can stop. In this paper, the prototype of eddy current brakes has been designed and developed for energy absorbing system of AABS.
Keywords :
"Eddy currents","Aircraft","Brakes","Atmospheric modeling","Torque","Mathematical model","Arresters"
Publisher :
ieee
Conference_Titel :
Recent Developments in Control, Automation and Power Engineering (RDCAPE), 2015 International Conference on
Type :
conf
DOI :
10.1109/RDCAPE.2015.7281429
Filename :
7281429
Link To Document :
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