首页> 外国专利> PILOT MIXER FOR MIXER ASSEMBLY OF GAS TURBINE ENGINE COMBUSTOR INCLUDING PRIMARY FUEL INJECTOR AND A PLURALITY OF SECONDARY FUEL INJECTION PORTS

PILOT MIXER FOR MIXER ASSEMBLY OF GAS TURBINE ENGINE COMBUSTOR INCLUDING PRIMARY FUEL INJECTOR AND A PLURALITY OF SECONDARY FUEL INJECTION PORTS

机译:用于燃气轮机燃烧室混合器的先导混合器,包括主燃料喷射器和多个二次燃料注入口

摘要

PROBLEM TO BE SOLVED: To reduce discharge of harmful combustion components in a wide operating state of a gas turbine.;SOLUTION: The pilot mixer 102 includes: an annular pilot housing 108 having a hollow interior; the primary fuel injector 110 mounted inside the pilot housing 108 for supplying fuel droplets to the hollow interior of the pilot housing 108; a plurality of axial swirlers 112, 114 disposed upstream of the primary fuel injector 110; and the plurality of secondary fuel injection ports 134 for introducing fuel into the hollow interior of the pilot housing 108. A main mixer 104 further includes: a main housing 124 surrounding the pilot housing 108 and forming an annular hollow 126; a plurality of fuel injection ports 128 for introducing fuel into the hollow 126; and at least one swirler 130 disposed upstream of the plurality of fuel injection ports 128.;COPYRIGHT: (C)2009,JPO&INPIT
机译:解决的问题:在燃气轮机的宽工作状态下,减少有害燃烧成分的排放。主燃料喷射器110安装在引燃器壳体108内,用于将燃料滴供应到引燃器壳体108的中空内部。多个轴向旋流器112、114设置在主燃料喷射器110的上游;主混合器104还包括:主壳体124,其包围引燃器壳体108并形成环形中空部126;以及主壳体124,该主壳体124包围引燃器壳体108的中空。多个燃料喷射口128用于将燃料引入中空部分126中。至少一个旋流器130布置在多个燃料喷射口128的上游。版权所有:(C)2009,JPO&INPIT

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号