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  • 1
    Publication Date: 2019-06-27
    Description: Two methods of starting the Brayton power system have been considered: (1) using the alternator as a motor to spin the Brayton rotating unit (BRU), and (2) spinning the BRU by forced gas injection. The first method requires the use of an auxiliary electrical power source. An alternating voltage is applied to the terminals of the alternator to drive it as an induction motor. Only gas-injection starts are discussed in this report. The gas-injection starting method requires high-pressure gas storage and valves to route the gas flow to provide correct BRU rotation. An analog computer simulation was used to size hardware and to determine safe start and shutdown procedures. The simulation was also used to define the range of conditions for successful startups. Experimental data were also obtained under various test conditions. These data verify the validity of the start and shutdown procedures.
    Keywords: AUXILIARY SYSTEMS
    Type: NASA-TN-D-6938 , E-6996
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: A study of the motor starting of a Brayton cycle power system was conducted to provide estimates of system sensitivity to several controllable parameters. These sensitivity estimates were used as a basis for selection of an optimum motor-start scheme to be implemented on the 2- to 10-kilowatt Brayton power system designed and presently under test. The studies were conducted with an analog simulation of the Brayton power system and covered a range of frequencies from 400 Hz (33 percent design) to 1200 Hz (design), voltage-to-frequency ratios of 0.050 (50 percent design) to 0.100 (design), turbine-inlet temperatures of 800 K (1440 R, 70 percent design) to 1140 K (2060 deg R, design), and prestart pressure levels of 14.5 psia to 29.0 psia. These studies have shown the effect of selected system variables on motor starting. The final selection of motor-start variables can therefore be made on the basis of motor-start inverter complexity, battery size and weight, desired steady-state pressure level after startup, and other operational limitations. In general, the study showed the time required for motor starting to be inversely proportional to motor frequency, voltage, turbine-inlet temperature, and pressure level. An increase in any of these parameters decreases startup time.
    Keywords: AUXILIARY SYSTEMS
    Type: NASA-TM-X-2432 , E-6548
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: Motor starting techniques for 2-15 kW Brayton space power system
    Keywords: NUCLEAR ENGINEERING
    Type: NASA-TM-X-67819
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-13
    Description: Analog computer simulation of single shaft Brayton cycle system dynamics, including startup and shutdown transients
    Keywords: AUXILIARY SYSTEMS
    Type: AMERICAN INST. OF CHEMICAL ENGINEERS, INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE; Sep 22, 1969 - Sep 26, 1969; WASHINGTON, DC
    Format: text
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  • 5
    Publication Date: 2019-07-13
    Description: Motor starting techniques for 2-15 kW Brayton space power system with turbine driven radial flow compressor and Lundell type alternator
    Keywords: AUXILIARY SYSTEMS
    Type: INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE; Aug 03, 1971 - Aug 05, 1971; BOSTON, MA
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