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    • 25. 发明授权
    • Gas turbine combustion chamber with impingement cooling tubes
    • 具有冲击冷却管的燃气轮机燃烧室
    • US5388412A
    • 1995-02-14
    • US151797
    • 1993-11-15
    • Burkhard Schulte-WerningRoger Suter
    • Burkhard Schulte-WerningRoger Suter
    • F02C7/18F23R3/00F23R3/04F23R3/54F23R3/02
    • F23R3/002F23R3/54F05B2260/201F23R2900/03044
    • In a gas turbine combustion chamber (1) cooled by means of impingement cooling, the height of the cooling duct (5) formed by the perforated plate (3) and the impingement surface (4) increases continuously in the transverse flow direction to correspond with the supply of cooling air. Tubes (7) are arranged in the cooling duct (5) on the holes (6) of the perforated plate (3) in such a way that the impingement air meets the impingement surface (4) at right angles, the height of the tubes (7) increasing in the transverse flow direction in such a way that the distance between the tubes (7) and the impingement surface (4) is constant over the complete length of the cooling duct (5). By this means, the heat transfer coefficient remains constant along the impingement cooling section and uniform removal of heat is made possible. The cooling effect can be specifically controlled by a suitable choice of the diameter of the holes (6) and the height of the tubes (7).
    • 在通过冲击冷却冷却的燃气轮机燃烧室(1)中,由多孔板(3)和冲击表面(4)形成的冷却管道(5)的高度在横向流动方向上连续增加,以对应于 供应冷却空气。 管(7)以多孔板(3)的孔(6)的方式布置在冷却管道(5)中,使得冲击空气以直角与冲击表面(4)相交,管的高度 (7)在横向流动方向上增加,使得管(7)和冲击表面(4)之间的距离在冷却管道(5)的整个长度上是恒定的。 通过这种方式,传热系数沿着冲击冷却部分保持恒定,并且可以均匀地除去热量。 可以通过孔(6)的直径和管(7)的高度的适当选择来具体控制冷却效果。
    • 30. 发明授权
    • Method and arrangement for carrying out repair and/or maintenance work in the inner casing of a multishell turbomachine
    • 在多壳涡轮机的内壳中进行维修和/或维护工作的方法和装置
    • US06189211B1
    • 2001-02-20
    • US09307735
    • 1999-05-10
    • Roger Suter
    • Roger Suter
    • B23P1500
    • F01D25/285F01D25/26F05D2230/70Y10T29/49318Y10T29/49723
    • A relatively simple, effort-saving and cost-saving arrangement and a corresponding method for repair and/or maintenance work in the inner casing of a multishell turbomachine is provided. To this end, after a tool carrier is put into the outer casing of a turbinemachine, the connecting elements of top part and bottom part of the inner casing are slackened. The top part of the inner casing is then lifted in the outer casing to such an extent that the tool carrier can reach into the inner casing. To this end, at least one locating fixture for a lifting device is arranged on the top part. A radial distance is formed between the at least one outer casing and the inner casing, the radial distance corresponding to at least the radial extent of a tool carrier to be introduced into the inner casing.
    • 提供了一种相对简单,省力和节省成本的布置以及用于多壳涡轮机的内壳中的维修和/或维护工作的相应方法。 为此,在将工具架放入涡轮机的外壳之后,内壳的顶部和底部的连接元件松弛。 然后将内壳的顶部在外壳中提升到使刀架能够到达内壳的程度。 为此,在顶部设置至少一个用于提升装置的定位夹具。 在所述至少一个外壳和所述内壳之间形成径向距离,所述径向距离至少对应于将被引入到所述内壳中的工具托架的径向长度。