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    • 6. 发明公开
    • Condition measurement apparatus and method
    • Bedingungsmessvorrichtung und -verfahren
    • EP2484977A2
    • 2012-08-08
    • EP12154281.5
    • 2012-02-07
    • General Electric Company
    • Kwanwoo, KimMyers, Geoffrey DavisNarra, VenkateswarluSrinivasan, Shiva Kumar
    • F23N5/16
    • F23N5/16F23N2041/20F23R2900/00013
    • A condition measurement apparatus (10) is provided and includes a gas turbine engine combustor (20) having an end cover (210), a liner (22) defining a liner interior (220) and a fuel nozzle (23) communicative with the liner interior (220), the end cover (210) being formed to separate a cold side thereof, which is a relatively low temperature environment, from a hot side thereof, which is a relatively high temperature environment in which the liner (22) and the fuel nozzle (23) are disposed, the combustor (20) being formed to define a fuel flow path extending through piping (30) disposed at the cold side of the end cover (210) by which fuel is deliverable to the fuel nozzle (23), and a condition sensing device (40) operably mounted on the piping (30).
    • 提供了一种条件测量装置(10),其包括具有端盖(210)的燃气涡轮发动机燃烧器(20),限定衬套内部(220)的衬套(22)和与衬套相通的燃料喷嘴(23) 内部(220),所述端盖(210)形成为将相对较低温度环境的冷侧从其较热的侧面分离,所述热侧是相对较高的温度环境,其中所述衬套(22)和 燃料喷嘴(23)被设置,燃烧器(20)形成为限定了延伸通过设置在端盖(210)的冷侧的配管(30)的燃料流路,燃料可以通过燃料喷射到燃料喷嘴(23) )和可操作地安装在管道(30)上的条件感测装置(40)。