presenting the fuel injections below a limit fuel flow such that the energy is injected best on sucking part or perhaps the pressure side and/or best through every next or third gasoline nose of a swirl vane and/or that gasoline is only inserted through gas nozzles of every second or 3rd swirl vane on the burner.
14. The axial swirler in accordance with state 1, where the axial swirler is within an annular combustor, can combustors, or just one or reheat engine.
18. The burner according to claim 6, where the energy nozzles is elongated slot nozzles expanding in essence parallel into leading edge regarding the swirl vane.
19. The burner relating to claim 6, when the energy nozzles include an initial nozzle for injection of liquid-fuel, and/or another nozzle for treatment of a gaseous energy and a third nozzle for shot of company air, which encloses initial nozzle and/or the next nozzle.
20. The method according to state 13, where the very reactive gas consists of natural gas fuels, hydrogen rich fuels, and hydrogen gasoline.
These and various other objects are achieved by an axial swirler, specifically for premixing of oxidizer and fuel in gas turbines, containing a series or a plurality of swirl vanes with a streamline cross-section, each swirl vane having a prominent advantage, a trailing edge, and a sucking area and a force part. Continuar leyendo «The sucking area in addition to force part stretch each around mentioned top and trailing borders»