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Systems and methods for modifying a modal oscillation in connection with a turbine

机译:用于改变与涡轮机有关的模态振荡的系统和方法

摘要

Jacket arrangements are described (214) and a method (1100) for changing at least a modal oscillation frequency of an inner shell (700) of an overcoat device (214) in a turbine (100). A shroud (214) has an inner jacket (700) and an outer jacket (304) on. The inner jacket (700) comprises a body (702) with a first end portion (708), a the first end portion opposite second end portion (710), an upper surface (704) and a lower surface (706), wherein the lower surface adjacent to a number of rotating turbine blades (204) is arranged. The inner jacket (700) further contains at least two strips (712a, 712b). A method (1100) to prevent an undesirable modal excitations in the inner shell (700) uses at least two strips (712a, 712b) ") which, on the upper surface (704) and extending between the first end portion (708) and the second end portion (710), between the at least two strips (712a, 712b) an impact cooling surface (716) is defined. In addition, the inner shell (700) at least one transverse strut (718) which, on the upper surface (704) and is formed in a direction which extends transversely to the at least two strips (712a, 712b) runs.
机译:描述了外套装置(214)和用于改变涡轮机(100)中的罩面装置(214)的内壳(700)的至少模态振荡频率的方法(1100)。护罩(214)上具有内护套(700)和外护套(304)。内护套(700)包括具有第一端部(708),与第二端部(710)相对的第一端部,上表面(704)和下表面(706)的主体(702),其中下表面邻近多个旋转的涡轮叶片(204)布置。内护套(700)还包含至少两个条带(712a,712b)。防止内壳(700)中的不期望的模态激励的方法(1100)使用至少两个条(712a,712b)”,其在上表面(704)上并在第一端部部分(708)和第二端部(708)之间延伸。在第二端部710上,在至少两个条带712a,712b之间限定了冲击冷却表面716;此外,内壳700还包括至少一个横向支柱718,在其上上表面(704)并沿横向于至少两个条带(712a,712b)延伸的方向形成。

著录项

  • 公开/公告号DE102009025796A1

    专利类型

  • 公开/公告日2010-01-14

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE20091025796

  • 发明设计人

    申请日2009-05-13

  • 分类号F01D25/24;F02C7/00;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:19

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