Results 291 to 300 of about 1,178,972 (334)
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Lightweight aircraft transformers
Electrical Engineering, 1949THE LARGE a-c electric loads and voltages of airplanes provide such applications for transformers as lighting, instrumentation, control, rectification, and window deicing. Transformer size and weight are determined by the quality of magnetic circuit and temperature limits of the insulation, the a-c frequency being fixed by the aircraft generators. As a
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Transactions of the American Institute of Electrical Engineers, 1943
F. J. Russell, A. P. Charbonneau
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F. J. Russell, A. P. Charbonneau
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Proceedings of the Institute of Radio Engineers, 1920
The application of radio to Naval aircraft is discussed, together with the difficulties of development, standardization, installation, and operation, especially under the stress of war conditions. The first operation of radio on naval aircraft, and the development of the earlier types of sets are described.
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The application of radio to Naval aircraft is discussed, together with the difficulties of development, standardization, installation, and operation, especially under the stress of war conditions. The first operation of radio on naval aircraft, and the development of the earlier types of sets are described.
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Recent developments in advanced aircraft aluminium alloys
, 2014Tolga Dursun, Constantinos Soutis
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Transactions of the American Institute of Electrical Engineers, 1944
The modern fighting airplane requires a large amount of electric power for its successful operation. The aircraft generator provides a reliable source of power at the lowest possible weight. The development of these generators has required close co ordination of design, testing, and interpretation of test results. The tests include raw material, parts,
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The modern fighting airplane requires a large amount of electric power for its successful operation. The aircraft generator provides a reliable source of power at the lowest possible weight. The development of these generators has required close co ordination of design, testing, and interpretation of test results. The tests include raw material, parts,
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Transactions of the American Institute of Electrical Engineers, 1944
Because the selection of aircraft warning devices has not, in most signal installations, provided the pilot with dependable warnings of dangerous conditions, this paper proposes that aircraft signal devices should be designed and stalled in compliance with the pilot's requirements as expressed in three design principles.
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Because the selection of aircraft warning devices has not, in most signal installations, provided the pilot with dependable warnings of dangerous conditions, this paper proposes that aircraft signal devices should be designed and stalled in compliance with the pilot's requirements as expressed in three design principles.
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Aircraft inverter construction
Electrical Engineering, 1943THE word “inverter” is a generic term used to designate any device which receives direct current and delivers alternating current. Such a device may consist of electronic elements, or vibrating contacts, or mechanical choppers, or rotary types. The scope of this paper will be confined to a discussion of rotary-type conversion equipment.
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Aircraft icing: an ongoing threat to aviation safety
, 2018Yihua Cao, Wenyuan Tan, Zhenlong Wu
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