GASTURBINE UND DICHTUNGSMITTEL FÜR EINE GASTURBINE
    4.
    发明公开
    GASTURBINE UND DICHTUNGSMITTEL FÜR EINE GASTURBINE 有权
    环形带密封胶燃气轮机

    公开(公告)号:EP1664489A1

    公开(公告)日:2006-06-07

    申请号:EP04764907.4

    申请日:2004-09-07

    发明人: MILAZAR, Mirko

    IPC分类号: F01D11/00 F16J15/08

    摘要: A gas turbine (1), with a fixed inner housing (37), arranged concentric to the rotor (3), with a throughflow of working medium, is disclosed. The housing comprises at least two serial rings (25, 26) with an annular gap (23) left between two directly adjacent rings (25, 26), whereby an annular sealing means is arranged in at least one peripheral groove (31) for sealing the annular gap (23). According to the invention, a sealing means is provided which permits a greater movement of both components forming the gap, whereby the annular gap (23) is formed by partly overlapping rings (25, 26), running against the flow direction of the working fluid (20) in the radial sense and the frontmost of the two rings (25), in the sense of the flow direction, comprises a locating annular surface (32) for the sealing means embodied as an annular spring element (24) on which the spring element (24) rests under tension such as to seal the annular gap (23).

    DICHTELEMENT ZUR DICHTUNG EINES SPALTES SOWIE GASTURBINENANLAGE
    5.
    发明授权
    DICHTELEMENT ZUR DICHTUNG EINES SPALTES SOWIE GASTURBINENANLAGE 失效
    密封件用于密封GAP和燃气轮机电厂

    公开(公告)号:EP0852659B1

    公开(公告)日:2002-04-03

    申请号:EP96942252.6

    申请日:1996-09-27

    IPC分类号: F01D11/00 F16J15/08

    CPC分类号: F01D11/005

    摘要: The invention pertains to a sealing element (1) for sealing a gap (5) which can form between two components (2a, 2b) liable to move relative to one another as a result of thermal action and each provided with an opposing groove (3a, 3b). The sealing element (1) in one cross-section is substantially perpendicular to a main line (21) along a median line (4). It has a first end (6a), a second end (6b) opposite the first end, and a central region (10) between the two ends, and is provided with teeth. The sealing element (1) is especially suitable for use in sealing a gap (5) between guide vanes (12) at high temperatures in a gas-turbine facility (22) as a means of preventing gas flow from a cool gas region (8) to a hot gas region (11).

    GASTURBINE MIT EINEM RINGFÖRMIGEN DICHTUNGSMITTEL
    8.
    发明授权
    GASTURBINE MIT EINEM RINGFÖRMIGEN DICHTUNGSMITTEL 有权
    环形带密封胶燃气轮机

    公开(公告)号:EP1664489B1

    公开(公告)日:2007-07-11

    申请号:EP04764907.4

    申请日:2004-09-07

    发明人: MILAZAR, Mirko

    IPC分类号: F01D11/00 F16J15/08

    摘要: A gas turbine (1), with a fixed inner housing (37), arranged concentric to the rotor (3), with a throughflow of working medium, is disclosed. The housing comprises at least two serial rings (25, 26) with an annular gap (23) left between two directly adjacent rings (25, 26), whereby an annular sealing means is arranged in at least one peripheral groove (31) for sealing the annular gap (23). According to the invention, a sealing means is provided which permits a greater movement of both components forming the gap, whereby the annular gap (23) is formed by partly overlapping rings (25, 26), running against the flow direction of the working fluid (20) in the radial sense and the frontmost of the two rings (25), in the sense of the flow direction, comprises a locating annular surface (32) for the sealing means embodied as an annular spring element (24) on which the spring element (24) rests under tension such as to seal the annular gap (23).