02230nam 2200373 450 991013650640332120231206165422.01-5044-0447-510.1109/IEEESTD.1960.7438698(CKB)3710000000619067(NjHacI)993710000000619067(EXLCZ)99371000000061906720231206d1960 uy 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierAIEE No 806-1960 AIEE Proposed Test Procedure for Aircraft Alternating Current Generators /IEEE[Place of publication not identified] :IEEE,1960.1 online resourceThe purpose of this procedure to define uniform acceptable test methods for determining the performance and other characteristics of aircraft alternating-current generators. Rotating electric equipment for aircraft is subjected to requirements and operating conditions not normally encountered by commercial generators. For example, conditions of temperature, altitude, humidity, and vibration vary over much wider ranges. Aircraft requirements dictate minimum weight, and yet utmost reliability is essential. Weight reduction is generally achieved by sacrifice of life expectancy commensurate with aircraft practices. The necessity for accurate design requires that direct measurements to insure reliability and adequate life be an important part of this test procedure. It is recognized that there may be acceptable methods of making tests other than those described. Such other methods may be considered as alternative procedures accepted by agreement between interested parties. The tests outlined herein are not necessarily complete for any specific generator; and likewise the requirements in each case will determine the number of tests to be made.AIEE No 806-1960Electric generatorsElectric motorsElectric generators.Electric motors.621.313NjHacINjHaclDOCUMENT9910136506403321AIEE No 806-19603646694UNINA