首页> 外国专利> GAS TURBINE COMBUSTOR FOR COAL GAS, CAPABLE OF REDUCING POWER GENERATION COST BY DECREASING COAL FUEL

GAS TURBINE COMBUSTOR FOR COAL GAS, CAPABLE OF REDUCING POWER GENERATION COST BY DECREASING COAL FUEL

机译:煤制燃气轮机燃烧器,可通过减少煤燃料降低发电成本

摘要

PURPOSE: A gas turbine combustor for coal gas is provided to increase the availability and the reliability of IGCC(Integrated Gasification Combined Cycle) plant by stably burning coal gas by considering the combustion property of coal gas.;CONSTITUTION: A gas turbine combustor for coal gas comprises a housing(10), a pilot nozzle(20) and a swirler(30). The pilot nozzle is installed at the center of the housing. The swirler is installed at the front of the pilot nozzle. The swirler comprises first and second swirling units(40,50). A group of jetting holes(42) of the first swirling unit are arranged at the circumferencial surface with a constant distance among the holes. The second swirling unit is arranged at the front of the first swirling unit. The second swirling unit comprises a central pilot fuel jetting hole(52) and a plurality of swirl groove s(54). The swirl grooves are formed within a certain distance from the pilot fuel jetting hole.;COPYRIGHT KIPO 2010
机译:目的:提供一种燃气轮机燃烧器,通过考虑煤气的燃烧特性稳定地燃烧燃气,以提高IGCC(整体气化联合循环)装置的可用性和可靠性。;构成:一种燃气轮机燃烧器气体包括壳体(10),导向喷嘴(20)和旋流器(30)。导向喷嘴安装在外壳的中心。旋流器安装在先导喷嘴的前面。旋流器包括第一和第二旋流单元(40,50)。第一回旋单元的一组喷射孔(42)布置在圆周表面上,其中孔之间的距离恒定。第二回旋单元布置在第一回旋单元的前部。第二回旋单元包括中央引燃燃料喷射孔(52)和多个回旋槽s(54)。旋流槽形成在距引燃燃料喷射孔一定距离的范围内。; COPYRIGHT KIPO 2010

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