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公开(公告)号:US20030215323A1
公开(公告)日:2003-11-20
申请号:US10173552
申请日:2002-06-14
发明人: Friedrich B. Prinz , Sangkyun Kang , Tibor Fabian , Georg Brasseur , Jordan Tresser , Francis Holman , Hideki Tsuru , Minoru Matsunaga
IPC分类号: F01D011/22
CPC分类号: F02C3/05 , F01D5/048 , F01D5/284 , F01D11/22 , F01D21/04 , F01D25/16 , F04D29/052 , F05D2220/768 , F05D2270/60 , F05D2300/2283 , H02K1/2726 , H02K7/1823 , Y02T50/673
摘要: In a micro gas turbine engine, a capacitive sensor is used for measuring a tip clearance of a radial compressor section thereof, and an actuator is used for axially displacing a rotor shaft in response to an output from the capacitive sensor. Because the capacitive change gives an accurate measure of the size of the tip clearance, a particularly high sensitivity can be achieved in parts where the tip clearance is small, thereby providing a highly precise tip clearance control.
摘要翻译: 在微型燃气涡轮发动机中,使用电容式传感器来测量其径向压缩机部分的顶端间隙,并且致动器用于响应于电容式传感器的输出轴向移动转子轴。 由于电容变化给出了尖端间隙尺寸的精确测量,所以在顶端间隙小的部分中可以实现特别高的灵敏度,从而提供高精度的顶端间隙控制。
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公开(公告)号:US20020071763A1
公开(公告)日:2002-06-13
申请号:US09995583
申请日:2001-11-29
IPC分类号: F01D011/22
CPC分类号: F01D11/22
摘要: What is described is a device for setting the gap dimension for a turbomachine, in particular a gas turbine, with a multiplicity of moving blades arranged in at least one moving-blade row of a rotor arrangement, with a guide-vane carrier surrounding the rotor arrangement and a turbine casing surrounding the guide-vane carrier, with a multiplicity of heat accumulation segments which are arranged on the guide-vane carrier of the rotor arrangement and at least opposite the moving-blade tips and which, together with the moving-blade tips, enclose a gap, and with at least one drive means which projects radially through the turbine casing and the guide-vane carrier and is operatively connected kinematically to at least one heat accumulation segment and which, when actuated, causes a radial spacing of the heat accumulation segment. The invention is distinguished in that the heat accumulation segment has, in the flow direction of the turbomachine, a conical contour facing the rotor arrangement and is arranged so as to be displaceable parallel to the flow direction, and in that the drive means is connected to the heat accumulation segment directly or via an eccentric unit, in such a way that, when the drive means is actuated, the heat accumulation segment is displaced, with the result that a radial spacing between the heat accumulation segment and the moving-blade tips can be set.
摘要翻译: 所描述的是一种用于设定涡轮机,特别是燃气轮机的间隙尺寸的装置,其具有布置在转子装置的至少一个活动叶片排中的多个活动叶片,围绕转子的导向叶片承载件 布置和围绕导向叶片载体的涡轮机壳体,具有多个热积聚段,其布置在转子装置的导向叶片载体上并且至少与运动叶片尖端相对,并且与运动叶片一起 并且具有至少一个驱动装置,所述至少一个驱动装置径向地突出穿过涡轮壳体和导向叶片载体,并且可动作地连接到至少一个热积聚段,并且当被致动时,该驱动装置使得 热积累段。 本发明的特征在于,热积聚段在涡轮机的流动方向上具有面向转子装置的锥形轮廓,并且被布置成可平行于流动方向移动,并且驱动装置连接到 直接或经由偏心单元的热积聚段,使得当驱动装置被致动时,热积聚段被移位,结果是热积聚段和移动叶片尖端之间的径向间隔可以 被设置。
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公开(公告)号:US20020150469A1
公开(公告)日:2002-10-17
申请号:US10104626
申请日:2002-03-21
发明人: Hans-Thomas Bolms
IPC分类号: F01D011/22 , F01D005/20
CPC分类号: F01D11/22 , F05D2260/56
摘要: The present invention relates to a turbine having a housing (11) and a rotor (12), the housing (11) being provided with a plurality of rows of guide vanes (13) and the rotor (12) being provided with a plurality of rows of rotor blades (14). On the housing (11), there is a guide ring (18) which is provided axially between in each case two rows of guide vanes (13), which guide ring, together with the associated row of rotor blades (14), delimits a gap (21). According to the invention, the guide ring (18) is adjustable in order to change the gap (21). The size of the gap (21) can then be predetermined by adjusting the guide ring (18) and can be optimized according to the specific application.
摘要翻译: 本发明涉及具有壳体(11)和转子(12)的涡轮机,所述壳体(11)设置有多排导叶(13),所述转子(12)设置有多个 一排转子叶片(14)。 在壳体(11)上有一个导向环(18),它们在每个壳体内轴向设置有两排导向叶片(13),导向环与相关联的一排转子叶片(14)一起界定 差距(21)。 根据本发明,引导环(18)是可调节的,以便改变间隙(21)。 然后可以通过调节引导环(18)来预定间隙(21)的尺寸,并且可以根据具体应用进行优化。
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