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IEEE/AIEE 805-1960

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AIEE Proposed Test Procedure for Alternating Current 400 Cycle Per second Aircraft Induction Motors

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Procedure is applicable to aircraft motors which operate from constant-frequency, nominally 400-cycle-per-second, constantvoltage, (nominally 115 volt line to neutral, 3-phase four-wire or 115 volt single-phase) alternating-current aircraft power systems. This aircraft power system is defined by paragraph 3.2.1.3, Type I of Military Specification No. MIL-E-7894. The test methods described herein will be suitable for test of machines of different frequency and voltage ranges. However, test equipment must be chosen suitable for the desired ranges
The purpose of this Procedure is to define uniform acceptable methods for making tests to determine the performance of alternating-current, 400-cycle-per-second, aircraft type, induction electric motors

SDO IEEE: Institute of Electrical and Electronics Engineers
Document Number 805
Publication Date Dec. 31, 1959
Language en - English
Page Count 20
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Dec. 31, 1959 805-1960 Revision