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热词
    • 6. 发明授权
    • Combustion chamber, especially for gas turbines
    • 燃烧室,特别是燃气轮机
    • US4199934A
    • 1980-04-29
    • US932547
    • 1978-08-10
    • Franz-Josef Meyer
    • Franz-Josef Meyer
    • F23R3/02F23R3/22F23R3/26F23R3/42F02C7/22
    • F23R3/02F23R3/22F23R3/26F23R3/42
    • A combustion chamber having an end-wall at the inlet side and an axial inlet opening, which is adjoined by an essentially cylindrical wall section provided with secondary air inlet openings; the end-wall thereby adjoins the inlet opening approximately hemispherically shaped with a sphere diameter which is larger than the diameter of the cylindrical wall section while the adjoining combustion chamber portion is again reduced to the adjacent cylindrical wall section by way of a combustion chamber wall substantially continuing the sphere shape; the fuel injection device is provided upstream of the inlet opening which injects fuel into the inlet opening, itself covered off by a deflection means.
    • 具有在入口侧的端壁和具有轴向入口的燃烧室,所述轴向入口与由设置有二次空气入口的基本上圆柱形的壁部相邻; 端壁由此邻近大致半球形的入口开口,其球直径大于圆柱形壁部分的直径,同时邻近的燃烧室部分通过燃烧室壁再次被还原到相邻的圆柱形壁部分 继续球形; 燃料喷射装置设置在入口开口的上游,其将燃料喷射到入口开口中,其本身由偏转装置覆盖。