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Premixing chamber for operating an internal combustion engine, a combustion chamber of a gas turbine group or a firing system

机译:用于运行内燃机的预混合室,燃气轮机组的燃烧室或点火系统

摘要

In a premixing burner for the operation of an internal combustion engine, a combustion chamber of a gas turbine group or a firing system, which burner can be used for the combustion of fuels with very different properties, a diffuser (4) is arranged after a swirl generator (1), a convergent part (2) and a throat (3) for the supply of the fuel (9). The convergent part (2), the throat (3) and the diffuser (4) have a rotationally symmetrical configuration and the variation in cross section is adapted in such a way that no flow separation is possible at the wall. Gaseous fuels having a high flame speed are introduced counter to the swirl generated by the swirl generator (1). Gaseous fuels having a low flame speed are introduced in the same direction as the swirl generated by the swirl generator (1).
机译:在用于内燃机,燃气轮机组或燃烧系统的燃烧室的预混合燃烧器中,该燃烧器可用于燃烧性质完全不同的燃料,在燃烧室之后设置扩散器(4)。涡流发生器(1),会聚部分(2)和用于供应燃料(9)的喉部(3)。会聚部分(2),喉部(3)和扩散器(4)具有旋转对称的构造,并且横截面的变化被适配成使得在壁处不可能发生流动分离。与火焰产生器(1)产生的漩涡相反地引入具有高火焰速度的气态燃料。具有低火焰速度的气态燃料沿与旋流发生器(1)产生的旋流相同的方向引入。

著录项

  • 公开/公告号US5673551A

    专利类型

  • 公开/公告日1997-10-07

    原文格式PDF

  • 申请/专利权人 ASEA BROWN BOVERI AG;

    申请/专利号US19960714890

  • 发明设计人 KLAUS DOBBELING;

    申请日1996-09-17

  • 分类号F02G3/00;

  • 国家 US

  • 入库时间 2022-08-22 03:09:17

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