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Enhancement for fuel spray breakup

机译:燃油喷涂的增强

摘要

A combustor or augmentor of a gas turbine engine is provided. The combustor or augmentor includes a wall defining apertures and an interior having an inlet, an outlet and a mixing region between the inlet and the outlet and fuel injectors. The fuel injectors are respectively arrayed along the wall at corresponding apertures to inject fuel into the mixing region. Each fuel injector includes a fuel injector body defining an injection outlet through which fuel exits the fuel injector body toward the mixing region and a pintle. The pintle includes a first end, a second end and a pintle body extending between the first and second ends. At least one of the first and second ends is attachable to the fuel injector body to position the pintle body between the injection outlet and the mixing region.
机译:提供了一种燃气轮机发动机的燃烧器或增强器。燃烧器或增强器包括限定孔的壁和内部,内部具有入口,出口和入口和出口和燃料喷射器之间的混合区域。燃料喷射器分别沿着壁在相应的孔中排列,以将燃料喷射到混合区域中。每个燃料喷射器包括燃料喷射器主体,该燃料喷射器主体限定了喷射出口,燃料通过该喷射出口朝向混合区域和缝隙离开燃料喷射器。叉子包括第一端,第二端和在第一和第二端之间延伸的叉子体。第一和第二端中的至少一个可附接到燃料喷射器主体以定位在喷射出口和混合区域之间的针脚体。

著录项

  • 公开/公告号US10948189B2

    专利类型

  • 公开/公告日2021-03-16

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORPORATION;

    申请/专利号US201816222568

  • 发明设计人 JEFFERY A. LOVETT;

    申请日2018-12-17

  • 分类号F23R3/28;F02C7/22;F02C9/26;F02C9/28;F23R3/34;F23D14/70;

  • 国家 US

  • 入库时间 2022-08-24 17:43:10

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