会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明申请
    • COMBUSTION CHAMBER FOR GAS TURBINE
    • 燃气轮机用燃烧室
    • WO99061840A1
    • 1999-12-02
    • PCT/SE1999/000862
    • 1999-05-20
    • F23R3/00F23R3/50F23R3/10F23R3/54
    • F23R3/50F05C2201/04F05C2203/08F05C2253/12F23R3/002
    • A combustion chamber device for a gas turbine comprises a wall member (11) which defines a combustion chamber (5) having an inlet and an outlet end, wherein the wall member (11) comprises an inlet end portion (14), which has at least one opening (7) for receiving a burner member (6), comprised to generate a flame in the combustion chamber (5) and means (16, 17, 19, 39) for conveying a cooling fluid outside the combustion chamber to the inlet end portion (14) of the wall member (11) for cooling thereof. The inlet end portion (14) is substantially closed and defines a barrier against penetration of the cooling fluid into the combustion chamber (5).
    • 一种用于燃气涡轮机的燃烧室装置包括壁构件(11),其限定具有入口和出口端的燃烧室(5),其中所述壁构件(11)包括入口端部(14),所述入口端部 用于接收燃烧器构件(6)的至少一个开口(7),其被包括以在所述燃烧室(5)中产生火焰;以及用于将所述燃烧室外的冷却流体输送到所述入口的装置(16,17,19,39) 壁构件(11)的端部(14)用于冷却。 入口端部(14)基本上是封闭的并且限定了防止冷却流体进入燃烧室(5)的穿透的屏障。