DocumentCode :
2757374
Title :
A study of design process of BLDC motor for aircraft hybrid drive
Author :
Bogusz, Piotr ; Korkosz, Mariusz ; Prokop, Jan
Author_Institution :
Fac. of Electr. & Comput. Eng., Rzeszow Univ. of Technol., Rzeszow, Poland
fYear :
2011
fDate :
27-30 June 2011
Firstpage :
508
Lastpage :
513
Abstract :
A study of the design process of BLDC motor designated as a power source for an Unmanned Aerial Vehicle (UAV). It was assumed that the UAV would be powered by a hybrid system, where electric power source operates in parallel to a combustion engine. Geometry of the electric motor being designed is presented as well as how the shape and magnetizing method influence cogging torque and average torque of the motor. Regulation characteristics, instantaneous currents, voltages and electromagnetic torque values are presented. Motor performance was analyzed as well as losses versus deliberately selected control parameters.
Keywords :
aerospace robotics; brushless DC motors; mobile robots; remotely operated vehicles; BLDC motor; UAV; aircraft hybrid drive; cogging torque; combustion engine; electric power source; electromagnetic torque value; geometry; hybrid system; instantaneous current; instantaneous voltage; magnetizing method; unmanned aerial vehicle; Brushless DC motors; Forging; Magnetic flux; Permanent magnet motors; Torque;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial Electronics (ISIE), 2011 IEEE International Symposium on
Conference_Location :
Gdansk
ISSN :
Pending
Print_ISBN :
978-1-4244-9310-4
Electronic_ISBN :
Pending
Type :
conf
DOI :
10.1109/ISIE.2011.5984077
Filename :
5984077
Link To Document :
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