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  • Journal of Jet Propulsion > New Patents
    Jump-type flow divider for gas turbine power plant fuel system (2,770,945).
  • CR4 - Thread: Frame 6B GE Gas Turbine Power Load Hunting During Fuel Changeover
    Frame 6B GE gas turbine power load hunting or Flow divider ceased problem during manual fuel change over from Gas to Liquid or During Mix fuel (GAS + Liquid ) to 100% GAS Fuel.
  • CR4 - Thread: COMBUSTION IN GAS TURBINE
    SOME OF GAS TURBINES ,(EX. MODEL MW701D WESTINGHOUSE TYPE, MADE BY MITSUBISHI)DOES NOT HAVE A MECHANICAL FLOW DIVIDER NEITHER FOR "FUEL OIL" NOR FOR "FUEL GAS".
  • CR4 - Thread: Combustion dynamics
    SOME OF GAS TURBINES ,(EX. MODEL MW701D WESTINGHOUSE TYPE, MADE BY MITSUBISHI)DOES NOT HAVE A MECHANICAL FLOW DIVIDER NEITHER FOR "FUEL OIL" NOR FOR "FUEL GAS".
  • Rotary wave-ejector enhanced pulse detonation engine
    The numeri- cal code, originally developed [43–45] at NASA has been applied to a broad range of non-unsteady flow devices such as pressure dividers [46], wave augmented diffusers [47 … … 49], pulsejets [36,50], premixed gas turbine combustors [51,52], PDEs …
  • Sustainable Energy Systems and Applications
    LEGEND 1 – SOFC stack 2 – combustion chamber 3 – turbine 4 – air compressor 5 – natural gas compressor 6 – air pre-heater 7 – … … 13 – mixer 14 – mixer 15 – flow divider valve 16 – flow …
  • Electrical engineering and electronics
    … magnetic 29, 30 photodetector 365 photoelement 171 photo thyristor 172 phototransistor 171 Francisturbine 306 freewheeling diode 190 freewheeling effect 184 overhead line 343 foreign excitation of the direct current machine 236 frequency 103 frequency measurement 363 frequency divider 210 frequency converters 191 … Fork coupler 174 gas pressure cables 166 gate circuit 156 gate voltage 157 gate 203, 326 gas turbine power plant 302 gate 155, Gaussian number plane 101 mutual induction 49 mutual inductance 53 .
  • NEXT GENERATION TURBINE PROGRAM
    The modulating valve meters fuel in response to a signal from the elec- tronic gas turbine control. The fuel then flows through two fuel shutoff valves and a flow divider , into the manifold and through the liquid fuel nozzles.
  • Generic turbine design study. Final report
    Also, the need for the accurate subdivision of the fuel oil to the several nozzles will not be required and the flow divider system and all of its components will be … … oil manifold, similar in function to the fuel gas manifold. … possible because the combustor outlet gasses will be thoroughly mixed prior to being introduced into the turbine .
  • Journal of Thermophysics and Heat Transfer > Flow Structure in a U-Shaped Channel
    … ” International Journal of Rotating Machinery, Vol. 4, No. 3, 1998, pp. 175–188. doi:10.1155/S1023621X98000153 [3] Liou, T.-M., Tzeng, Y.-Y., and Chen, C.-C., “Fluid Flow in a 180 Deg … … Turning Duct with Different Divider Thicknesses,” Journal of … … pp. 243–258. doi:10.1016/j.ijheatfluidflow.2005.08.010 [7] Metzger, D. E., Plevich, C. W., and Fan, C. S., “Pressure Loss Through Sharp 180 Deg Turns in Smooth Rectangular Channels,” Journal of Engineering for Gas Turbines and Power, Vol. 106 …