首页> 外国专利> FUEL NOZZLE, GAS TURBINE COMBUSTOR, FUEL NOZZLE OF GAS TURBINE COMBUSTOR, AND REMODELING METHOD OF GAS TURBINE COMBUSTOR

FUEL NOZZLE, GAS TURBINE COMBUSTOR, FUEL NOZZLE OF GAS TURBINE COMBUSTOR, AND REMODELING METHOD OF GAS TURBINE COMBUSTOR

机译:燃料喷嘴,燃气轮机燃烧室,燃料喷嘴,燃气轮机燃烧室的改造方法

摘要

PROBLEM TO BE SOLVED: To unify a flow rate of the fuel injected from fuel nozzles without impairing atomizing performance of the fuel nozzles respectively disposed on combustors.;SOLUTION: A main nozzle hole for injecting main fuel has a structure of a circular flow channel in parallel with an axial portion of the fuel nozzle, having a linear portion of a constant cross-sectional area of the circular flow channel, to achieve the challenge. According to this invention, deviation in fuel flow rate can be reduced without impairing atomizing performance of the fuel nozzles disposed in the combustors, and the fuel nozzles of high reliability can be provided.;COPYRIGHT: (C)2007,JPO&INPIT
机译:解决的问题:在不损害分别布置在燃烧器上的燃料喷嘴的雾化性能的情况下,统一从燃料喷嘴喷射的燃料的流量;解决方案:用于喷射主燃料的主喷嘴孔具有环形流动通道的结构。与燃料喷嘴的轴向部分平行的,具有圆形流动通道的恒定横截面积的线性部分,以实现挑战。根据本发明,可以在不损害布置在燃烧室中的燃料喷嘴的雾化性能的情况下减小燃料流量的偏差,并且可以提供高可靠性的燃料喷嘴。版权所有:(C)2007,JPO&INPIT

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