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SAE ARP1480 - GROUND ELECTRICAL POWER UNIT BRUSHLESS, SYNCHRONOUS, ELECTRIC MOTOR-DRIVEN 400 HERTZ, 3-PHASE OUTPUT Organization: SAE
Date: 1998-09-01
IET - SMALL ELECTRIC MOTORS - SMALL ELECTRIC MOTORS Organization: IET
Date: 1998-01-01
Description: The various types of motor, together with their differing characteristics and their relationship to small drives are covered. Developments such as brushless DC motors and stepper motors are discussed, as well as the use of electronic control which widens the spectrum of small motor applications.
NASA-LLIS-0893 - LESSONS LEARNED – SELECTION OF ELECTRIC MOTORS FOR AEROSPACE APPLICATION Organization: NASA
Date: 2000-03-06
Description: The following factors are considered in electric motor design: application, environment, thermal, efficiency, weight, volume, life, complexity, torque, speed, torque ripple, power source, envelope, duty cycle, and controllability. Brushless direct current motors have been proven to be the best all-around type of motors for aerospace applications because of their long life, high torque, high efficiency, and low heat dissipation.
SAE J2867 - LABORATORY TESTING OF LIGHT DUTY VEHICLE ELECTRIC COOLING FAN ASSEMBLIES FOR AIRFLOW PERFORMANCE Organization: SAE
Date: 2014-08-01
Description: In the case of brushless motor technology, the controller is an integral part of the motor where it also performs the commutation process electronically.
SAE/TP - 2010-01-1753 - ACTUATOR REMAINING LIFE ESTIMATION UNDER FAULT TOLERANT OPERATION Organization: SAE/TP
Date: 2010-11-02
Description: Consequently, operation in the fault tolerant mode has a growing interest and potential wide-spread application. The modern actuator mainly consists of a brushless DC motor (BLDC) that is composed of stator winding, a permanent magnet rotor and Hall Effect sensors.

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