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    • 3. 发明授权
    • Shroud assembly with discourager
    • 护罩装配与沮丧者
    • US08303245B2
    • 2012-11-06
    • US12576386
    • 2009-10-09
    • Gregory Thomas FosterAndres Jose Garcia CrespoHerbert Chidsey Roberts
    • Gregory Thomas FosterAndres Jose Garcia CrespoHerbert Chidsey Roberts
    • F01D11/08
    • F01D25/265F01D9/04F01D11/00F05D2240/11Y02T50/672
    • A turbine shroud assembly is disclosed, the shroud assembly including an outer shroud, at least one inner shroud attached to the outer shroud, and at least one discourager enclosed within the inner shroud. The discourager prevents the hot gas or steam in the turbine from having a direct line of access to the outer shroud. In one embodiment, one inner shroud is provided for the shroud assembly, with one discourager enclosed within the inner shroud, the discourager positioned offset from the inner shroud so as to extend past the inner shroud and into an inner shroud of a neighboring shroud assembly. In another embodiment, a plurality of inner shrouds are provided, each inner shroud enclosing a discourager, the discouragers being adjacent to each other within the inner shrouds and positioned offset from the inner shrouds so as to cover a gap between the inner shrouds.
    • 公开了一种涡轮机护罩组件,护罩组件包括外护罩,附接到外护罩的至少一个内护罩和封闭在内护罩内的至少一个挡板。 防火墙防止涡轮机中的热气体或蒸汽直接进入外护罩。 在一个实施例中,为护罩组件提供一个内护罩,其中一个气囊封闭在内护罩内,捣毁器定位成偏离内护罩,以便延伸穿过内护罩并进入相邻护罩组件的内护罩。 在另一个实施例中,提供多个内护罩,每个内护罩包围一个挡板,该挡板在该内护罩内彼此相邻并且与该内护罩相偏离,以便覆盖该内护罩之间的间隙。