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    • 8. 发明授权
    • Gas turbine combustor assembly
    • 燃气轮机燃烧器组件
    • US4426841A
    • 1984-01-24
    • US279960
    • 1981-07-02
    • Walter CorneliusEdward D. Klomp
    • Walter CorneliusEdward D. Klomp
    • F23R3/26F02C7/042
    • F23R3/26
    • An improved gas turbine engine combustor assembly particularly for automotive application including a primary reaction chamber disposed in a pressurized air plenum of the engine, fixed area air flow ports between the reaction chamber and the plenum, a prechamber housing at an upstream end of the reaction chamber having an annular fixed area air passage between the plenum and the reaction chamber, a radially expandable annular partition in the air passage dividing the latter into an inner annular prechamber portion and an outer annular excess air portion, and a fuel nozzle operative to spray fuel into the prechamber portion where it vaporizes and mixes with air passing through the prechamber portion to provide a combustible mixture of properly lean air-fuel ratio in the combustor. The flow areas of the prechamber portion and the excess air portion vary in mutually inverse relationship and combine to always substantially equal the flow area of the air passage.
    • 一种特别用于汽车应用的改进的燃气涡轮发动机燃烧器组件,包括设置在发动机的加压空气通风室中的初级反应室,反应室和增压室之间的固定区域空气流动端口,位于反应室上游端的预室外壳 在通风室和反应室之间具有环形的固定区域空气通道,空气通道中的可径向扩张的环形隔板将空气通道分隔成内部环形预热室部分和外部环形过剩空气部分,以及燃料喷嘴,用于将燃料喷入 预燃室部分,其蒸发并与通过预室部分的空气混合,以提供在燃烧器中适当稀薄空燃比的可燃混合物。 前室部分和过量空气部分的流动面积以相互反比的关系变化,并且总是基本上等于空气通道的流动面积。