Motoring Characteristics of a 2- to 10-kilowatt Brayton Rotating Unit
Author : Robert C. Evans
Publisher :
Page : 34 pages
File Size : 22,75 MB
Release : 1971
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Author : Robert C. Evans
Publisher :
Page : 34 pages
File Size : 22,75 MB
Release : 1971
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Author : Robert C. Evans
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Page : 20 pages
File Size : 12,12 MB
Release : 1971
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Author :
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Page : 224 pages
File Size : 18,55 MB
Release : 1973
Category : Aeronautics
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Author :
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Page : 378 pages
File Size : 16,11 MB
Release : 1971
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Author : Robert J. Frye
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Page : 28 pages
File Size : 21,57 MB
Release : 1972
Category : Brayton cycle
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The design of a three-phase, 400-Hz, 15-kVA static inverter for motor-starting the 2- to 15-kWe Brayton electrical space power system is described. The inverter operates from a nominal 56-V dc source to provide a 28-V, rms, quasi-square-wave output. The inverter is capable of supplying a 200-A peak current. Integrated circuitry is used to generate the three-phase, 400-Hz reference signals. Performance data for a drive stage that improves switching speed and provides efficient operation over a range of output current and drive supply voltage are presented. A transformerless, transistor output stage is used.
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Page : 20 pages
File Size : 45,71 MB
Release : 1971
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Author : United States. Congress. Senate. Committee on Commerce
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Page : 290 pages
File Size : 14,41 MB
Release : 1968
Category : Air
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Author : United States. Congress. Senate. Commerce
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Page : 360 pages
File Size : 16,38 MB
Release : 1968
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Author : J. E. Davis
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Page : 396 pages
File Size : 40,46 MB
Release : 1972
Category : Brayton cycle
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The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, and demonstrated for use in a closed Brayton cycle space power conversion system. The BRU uses a binary mixture of xenon and helium (molecular weight, 83.8) as the cycle working fluid and bearing lubricating medium and was designed to produce from 2.25 to 10.5 kw sub e of 1200 Hz three-phase electrical power. The single-shaft rotating assembly operates at a design speed of 36,000 rpm and comprises a radial single-stage compressor, a four-pole Rice alternator rotor, and a radial inflow turbine. Four units, a dynamic simulator and three component research packages, were supplied to the NASA Lewis Research Center for performance testing and further development.
Author : United States. Congress. Senate. Committee on Commerce
Publisher :
Page : 830 pages
File Size : 42,36 MB
Release : 1968
Category : Legislative hearings
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