Title :
An Integrated Approach to Aerospace Motor Design
Author_Institution :
Direct Current Motor and Generator Department General Electric Company
Abstract :
This paper discusses some of the requirements which must be met by motors for aerospace applications, and presents an integrated approach to the design of a complete line of machines to meet these needs. Work carried out during the design study, design integration, and final design phases of the program is described.
Keywords :
DC motors; Design optimization; Electric shock; Frequency; Induction motors; Rotors; Testing; Torque; Vibrations; Voltage;
Journal_Title :
Aerospace, IEEE Transactions on
DOI :
10.1109/TA.1963.4319453
