DocumentCode :
2617256
Title :
Unified coil solenoid actuator for aerospace application
Author :
Narayanswamy, Renukaprasad ; Mahajan, Deepak P. ; Bavisetti, Siva
Author_Institution :
Aerosp. Electron. Hardware, Honeywell Technol. Solutions, Bangalore, India
fYear :
2012
fDate :
16-18 Oct. 2012
Firstpage :
1
Lastpage :
5
Abstract :
Solenoid is an electromagnetically operated actuator. One of the typical applications of solenoid is to operate valves in aircraft engine under harsh environmental conditions and high endurance requirements. Solenoid coil is wound around an insulator (e.g. PTFE / Polyimide/ Nomex etc) which is generally called as bobbin. Classical bobbin construction reduces the available window area for the coil winding. This successively reduces the number of turns that can be accommodated in the reduced window area. MMF (Magneto Motive Force) is the product of the number of turns and the magnitude of the coil current. Due to reduction in the MMF, the magnetic field strength of the solenoid reduces and the force generated by the solenoid gets decreased. The proposed topology of the solenoid eliminates the bobbin for reducing the size of solenoid coils or in other words more window area is available against the classical bobbin designs. The proposed method aims at generating higher force for the constrained size or generating the same force with less size and weight of the solenoid.
Keywords :
aerospace engines; electromagnetic actuators; insulators; machine windings; solenoids; PTFE; aerospace application; aircraft engine; bobbin construction; coil winding; electromagnetically operated actuator; harsh environmental conditions; high endurance requirements; insulator; magnetic field strength; magneto motive force; nomex; polyimide; reduced window area; unified coil solenoid actuator; Cable insulation; Coils; Solenoids; Springs; Stacking; Welding; actuator; aerospace; finite element methods; solenoid;
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.2012.6387392
Filename :
6387392
Link To Document :
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