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    • 1. 发明申请
    • COMBUSTION DEVICE FOR A GAS TURBINE
    • 燃气涡轮机燃烧装置
    • US20110265484A1
    • 2011-11-03
    • US13097221
    • 2011-04-29
    • Andreas HUBERNicolas NoirayBruno SchuermansUrs Benz
    • Andreas HUBERNicolas NoirayBruno SchuermansUrs Benz
    • F23R3/42
    • F23R3/002F23M20/005F23R2900/00014F23R2900/03041F23R2900/03043
    • A combustion device (1) for a gas turbine includes portions (12) having an inner and an outer wall (13, 14) with an interposed noise absorption plate (15) having a plurality of holes (16). The combustion device (1) further has first passages (17) connecting zones between the inner wall (13) and the plate (15) to the inside of the combustion device (1) and second passages (21) for cooling the inner wall (13). The portions (12) also have an inner layer (22) between the inner wall (13) and the plate (15) defining inner chambers (23), each connected to at least a first passage (17), and an outer layer (24) between the outer wall (14) and the plate (15) defining outer chambers (25) connected to the inner chambers (23) via the holes (16) of the plate (15).
    • 一种用于燃气轮机的燃烧装置(1)包括具有内壁和外壁(13,14)的部分(12),其具有带有多个孔(16)的插入式吸声板(15)。 燃烧装置(1)还具有将内壁(13)和板(15)之间的区域连接到燃烧装置(1)的内部的第一通道(17)和用于冷却内壁的第二通道(21) 13)。 部分(12)还在内壁(13)与限定内腔(23)之间的内层(22)之间具有内层(22),每个内层连接至少一第一通道(17)和外层 外壁(14)和板(15)之间通过板(15)的孔(16)限定连接到内室(23)的外室(25)。