公开(公告)号：US20060245910A1

公开(公告)日：2006-11-02

申请号：US11413871

申请日：2006-04-28

申请人： Tobias Buchal ,  Gerhard Hulsemann ,  Mirko Milazar ,  Dierer Minninger ,  Michael Neubauer ,  Harald Nimptsch ,  Heinrich Putz ,  Kang Qian ,  Arnd Reichert ,  Volker Vosberg

发明人： Tobias Buchal ,  Gerhard Hulsemann ,  Mirko Milazar ,  Dierer Minninger ,  Michael Neubauer ,  Harald Nimptsch ,  Heinrich Putz ,  Kang Qian ,  Arnd Reichert ,  Volker Vosberg

IPC分类号： F04D27/02

CPC分类号： F01D11/24 ,  F01D19/02

摘要： The invention relates a method for improving the hot-starting behavior of a turbomachine. By virtue of the setting of a radial gap formed between a brushing edge of a blade profile and a guide face lying opposite this, in which setting a guide ring forming the guide face can be acted upon with a coolant, the hot-starting behavior can be improved, in that the guide ring is cooled before the start of the machine.

摘要翻译： 本发明涉及一种改善涡轮机热启动行为的方法。 由于在叶片轮廓的刷牙边缘和与其相反的引导面之间形成的径向间隙的设定，其中形成引导面的导向环可以用冷却剂作用，热启动行为可以 因为引导环在机器启动之前被冷却。

公开(公告)号：US07766611B2

公开(公告)日：2010-08-03

申请号：US11413871

申请日：2006-04-28

申请人： Tobias Buchal ,  Gerhard Hülsemann ,  Mirko Milazar ,  Dieter Minninger ,  Michael Neubauer ,  Harald Nimptsch ,  Heinrich Pütz ,  Kang Qian ,  Arnd Reichert ,  Volker Vosberg

发明人： Tobias Buchal ,  Gerhard Hülsemann ,  Mirko Milazar ,  Dieter Minninger ,  Michael Neubauer ,  Harald Nimptsch ,  Heinrich Pütz ,  Kang Qian ,  Arnd Reichert ,  Volker Vosberg

IPC分类号： F01D11/08

CPC分类号： F01D11/24 ,  F01D19/02

摘要： The invention relates a method for improving the hot-starting behavior of a turbomachine. By virtue of the setting of a radial gap formed between a brushing edge of a blade profile and a guide face lying opposite this, in which setting a guide ring forming the guide face can be acted upon with a coolant, the hot-starting behavior can be improved, in that the guide ring is cooled before the start of the machine.

摘要翻译： 本发明涉及一种改善涡轮机热启动行为的方法。 由于在叶片轮廓的刷牙边缘和与其相反的引导面之间形成的径向间隙的设定，其中形成引导面的导向环可以用冷却剂作用，热启动行为可以 因为引导环在机器启动之前被冷却。

公开(公告)号：US20100287949A1

公开(公告)日：2010-11-18

申请号：US12844919

申请日：2010-07-28

申请人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

发明人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

IPC分类号： F02C7/20

CPC分类号： F01D5/081 ,  F05D2230/642 ,  F05D2240/55 ,  F05D2250/182 ,  F05D2260/30 ,  F16L41/001

摘要： A fastening arrangement of a pipe is provided. The fastening arrangement is coaxial to a longitudinal axis, on a shaft step, which is rotatably mounted around the longitudinal axis, for connecting of the two component parts, with a coaxial circumferential surface located on the shaft step, upon which circumferential surface at least partially lies the inner side of the pipe end which faces the shaft step. In order to disclose the creation of a fastening arrangement which is especially simple and inexpensive to manufacture and also free of wear during operation, it is proposed that the pipe end has notches distributed over the circumference, and an encompassing annular slot on the inner side of the pipe in the region of the notches, with a sleeve which is installed in the annular slot, covers the notches, and at least partially lies on the circumferential surface of the shaft step.

摘要翻译： 提供管道的紧固装置。 所述紧固装置与纵向轴线同轴，所述轴台阶可围绕所述纵向轴线可旋转地安装，用于将所述两个部件连接到位于所述轴台阶上的同轴圆周表面，所述圆周表面至少部分地 位于管端的面向轴台阶的内侧。 为了公开产生紧凑装置，其特别简单且制造成本低廉，并且在操作期间也没有磨损，因此提出管端在圆周上分布有凹口，在内侧的包围环形槽 凹槽区域中的管道，其中安装有环形槽的套筒覆盖切口，并且至少部分地位于轴台阶的圆周表面上。

公开(公告)号：US07080513B2

公开(公告)日：2006-07-25

申请号：US10767835

申请日：2004-01-29

申请人： Arnd Reichert

发明人： Arnd Reichert

IPC分类号： F02C1/00 ,  F02G3/00

CPC分类号： F01D11/005 ,  F01D9/023 ,  F05D2230/642 ,  F05D2250/182 ,  F16J15/0893 ,  F16J15/121 ,  Y02T50/675

摘要： The invention pertains to a seal element for sealing a gap, in particular within a turbo-machinery, between a first component and a second components spaced apart from each other, said first component having a first surface and said second component having an opposing second surfaces. The seal element comprises a support structure and a sealing structure covering at least partially said support structure. The support structure comprises at least two contacting members, each contacting member serves for putting a portion of the sealing structure in contact with one of the surfaces and being capable of following a deformation of said surface. The invention further pertains to a combustion turbine, wherein a gap is formed between a first surface and a second surface, which gap is sealed off by said seal element.

摘要翻译： 本发明涉及用于密封第一部件和彼此间隔开的第二部件之间的间隙，特别是在涡轮机械内的密封元件，所述第一部件具有第一表面，所述第二部件具有相对的第二表面 。 密封元件包括支撑结构和至少部分地覆盖所述支撑结构的密封结构。 支撑结构包括至少两个接触构件，每个接触构件用于使密封结构的一部分与其中一个表面接触并能够跟随所述表面的变形。 本发明还涉及一种燃气轮机，其中在第一表面和第二表面之间形成间隙，该间隙被所述密封元件密封。

公开(公告)号：US07559741B2

公开(公告)日：2009-07-14

申请号：US10586795

申请日：2005-01-19

申请人： Arnd Reichert ,  Bernd Stöcker

发明人： Arnd Reichert ,  Bernd Stöcker

IPC分类号： F01D11/18

CPC分类号： F01D11/02 ,  F01D11/22 ,  F04D29/052 ,  F04D29/164 ,  F05D2250/312 ,  F05D2250/314

摘要： The invention relates to a compressor, which is axially flowed through, for a gas turbine having an axially displaceable rotor. An annular flow channel, which narrows in an axial direction, is formed between a rotationally fixed outer delimiting surface and an inner delimiting surface on the rotor. A stationary ring comprised of guide profiles and at least one ring comprised of moving profiles attached to the rotor are placed inside said annular flow channel. The end of each moving or guide blade is located opposite an axial section of one of both delimiting surfaces while forming a radial gap. The aim of the invention is to provide a non-positive-displacement machine having an axially displaceable rotor whose velocity losses are at least not increased during an axial displacement of the rotor. To this end, the invention provides that the size of the radial gap between the end of each moving or guide blade and the opposite axial section of the delimiting surface is constant at least over the path of displacement of the rotor, and the radial gap extends parallel to the rotation axis of the rotor.

摘要翻译： 本发明涉及一种用于具有可轴向移动的转子的燃气轮机的轴向流过的压缩机。 在旋转固定的外部限定表面和转子上的内部限定表面之间形成有在轴向方向上变窄的环形流动通道。 包括导向轮廓的固定环和由连接到转子的移动轮廓组成的至少一个环被放置在所述环形流动通道内。 每个移动或引导刀片的端部与形成径向间隙的两个限定表面之一的轴向部分相对。 本发明的目的是提供一种具有轴向移位的转子的非正排量机械，其在转子的轴向位移期间速度损失至少不增加。 为此，本发明规定，每个移动或引导叶片的端部与限定表面的相对的轴向部分之间的径向间隙的尺寸至少在转子的位移路径上是恒定的，并且径向间隙延伸 平行于转子的旋转轴线。

公开(公告)号：US06565322B1

公开(公告)日：2003-05-20

申请号：US09979678

申请日：2002-03-05

申请人： Dirk Lieser ,  Arnd Reichert ,  Micheal Strassberger ,  Peter Tiemann

发明人： Dirk Lieser ,  Arnd Reichert ,  Micheal Strassberger ,  Peter Tiemann

IPC分类号： F01D530

CPC分类号： F01D11/006

摘要： The invention relates to a turbo-machine (1) comprising a rotor (25) that extends along a rotational axis (15). Said rotor (25) has a peripheral surface (31) which is defined by the outer radial delimitation surface of the rotor (25) and has a receiving structure (33) as well as a first moving blade (13A) and a second moving blade (13B). Each moving blade comprises a blade footing (43A, 43B) and a blade platform (17A, 17B). The blade platform (17A) of the first moving blade (13A) and the blade platform (17B) of the second moving blade (13B) border one another, and a gap (49) is formed between the blade platforms (17A, 17B) and the peripheral surface (31). A sealing system (51) is provided in the gap (49) on the peripheral surface (31).

摘要翻译： 本发明涉及一种包括沿旋转轴线（15）延伸的转子（25）的涡轮机（1）。 所述转子（25）具有由转子（25）的外部径向限定表面限定的周边表面（31），并且具有接收结构（33）以及第一动叶片（13A）和第二动叶片 （13B）。 每个动叶片包括叶片基脚（43A，43B）和叶片平台（17A，17B）。 第一活动叶片（13A）的叶片平台（17A）和第二活动叶片（13B）的叶片平台（17B）彼此相交，并且在叶片平台（17A，17B）之间形成间隙（49） 和周边表面（31）。 密封系统（51）设置在外周表面（31）上的间隙（49）中。

公开(公告)号：US20070108762A1

公开(公告)日：2007-05-17

申请号：US11594588

申请日：2006-11-07

申请人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

发明人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

IPC分类号： F16L21/06

CPC分类号： F01D5/081 ,  F05D2230/642 ,  F05D2240/55 ,  F05D2250/182 ,  F05D2260/30 ,  F16L41/001

摘要： The invention relates to a fastening arrangement of a pipe, which is coaxial to a longitudinal axis, on a shaft step, which is rotatably mounted around the longitudinal axis, for connecting of the two component parts, with a coaxial circumferential surface located on the shaft step, upon which circumferential surface at least partially lies the inner side of the pipe end which faces the shaft step. In order to disclose the creation of a fastening arrangement which is especially simple and inexpensive to manufacture and also free of wear during operation, it is proposed that the pipe end has notches distributed over the circumference, and an encompassing annular slot on the inner side of the pipe in the region of the notches, with a sleeve which is installed in the annular slot, covers the notches, and at least partially lies on the circumferential surface of the shaft step.

摘要翻译： 本发明涉及一种与纵向轴线同轴的管道的紧固装置，该轴台阶可围绕纵向轴线可旋转地安装，用于将两个部件连接起来，该同轴圆周表面位于轴上 其中圆周表面至少部分地位于面向轴台阶的管端的内侧。 为了公开产生紧凑装置，其特别简单且制造成本低廉，并且在操作期间也没有磨损，因此提出管端在圆周上分布有凹口，在内侧的包围环形槽 凹槽区域中的管道，其中安装有环形槽的套筒覆盖切口，并且至少部分地位于轴台阶的圆周表面上。

公开(公告)号：US06749395B1

公开(公告)日：2004-06-15

申请号：US10048810

申请日：2002-01-29

申请人： Arnd Reichert ,  Dirk Lieser

发明人： Arnd Reichert ,  Dirk Lieser

IPC分类号： F01D700

CPC分类号： F01D25/12 ,  F01D17/14 ,  F15C1/16

摘要： An apparatus for controlling a cooling air flow, in particular a gas turbine cooling air flow, is for the control, specific to requirement, of a cooling air flow using low-maintenance. A control fluid flow is introduced into the cooling air flow in the region of the flow duct with a flow component transverse to the flow direction of the cooling air flow through the flow duct. As such, the flow rate of the cooling air flow is adjustable as a function of control parameters of the control fluid flow and/or other parameters.

摘要翻译： 用于控制冷却空气流的装置，特别是燃气轮机冷却空气流，用于使用低维护来控制冷却空气流的具体要求。 控制流体流在流动管道的区域中被引入冷却空气流中，其流动分量横向于通过流动管道的冷却空气流的流动方向。 因此，作为控制流体流动的控制参数和/或其他参数的函数，可以调节冷却空气流的流量。

公开(公告)号：US06427448B1

公开(公告)日：2002-08-06

申请号：US09701850

申请日：2001-02-09

申请人： Arnd Reichert

发明人： Arnd Reichert

IPC分类号： F02C500

CPC分类号： F01D25/12 ,  F01D5/081 ,  F01D5/18 ,  Y02T50/676

摘要： The invention relates to a gas turbine (4) having a turbine stage (24) which has a guide blade (26) and a feed (32) for cooling air (K) with a cooling-air outlet (34). The turbine stage (24) can be cooled by the cooling air (K), the cooling-air feed (32) having means via which a predeterminable pressure of the cooling air (K) can be set at the cooling-air outlet (34).

摘要翻译： 本发明涉及一种具有涡轮级（24）的燃气轮机（4），该涡轮级具有导向叶片（26）和用冷却空气出口（34）冷却空气（K）的进料（32）。 涡轮级（24）可以由冷却空气（K）冷却，冷却空气供给装置32具有可以在冷却空气出口（34）处设置冷却空气（K）的可预定压力的装置 ）。

公开(公告)号：US08062000B2

公开(公告)日：2011-11-22

申请号：US12844919

申请日：2010-07-28

申请人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

发明人： Axel Buschmann ,  Markus Kunze ,  Arnd Reichert

IPC分类号： B63H1/28 ,  B63H5/00 ,  B63H7/00 ,  B63H13/00 ,  B63H15/00 ,  B64C11/14 ,  B64C27/32 ,  F01D5/00 ,  F01D25/00 ,  F03B1/02 ,  F03B11/00 ,  F03D11/00 ,  F04D29/00

CPC分类号： F01D5/081 ,  F05D2230/642 ,  F05D2240/55 ,  F05D2250/182 ,  F05D2260/30 ,  F16L41/001

摘要： A fastening arrangement of a pipe is provided. The fastening arrangement is coaxial to a longitudinal axis, on a shaft step, which is rotatably mounted around the longitudinal axis, for connecting of the two component parts, with a coaxial circumferential surface located on the shaft step, upon which circumferential surface at least partially lies the inner side of the pipe end which faces the shaft step. In order to disclose the creation of a fastening arrangement which is especially simple and inexpensive to manufacture and also free of wear during operation, it is proposed that the pipe end has notches distributed over the circumference, and an encompassing annular slot on the inner side of the pipe in the region of the notches, with a sleeve which is installed in the annular slot, covers the notches, and at least partially lies on the circumferential surface of the shaft step.

摘要翻译： 提供管道的紧固装置。 所述紧固装置与纵向轴线同轴，所述轴台阶可围绕所述纵向轴线可旋转地安装，用于将所述两个部件连接到位于所述轴台阶上的同轴圆周表面，所述圆周表面至少部分地 位于管端的面向轴台阶的内侧。 为了公开创建紧凑装置，其特别简单且制造成本低廉并且在操作期间也没有磨损，因此提出管端在圆周上分布有凹口，并且在内侧的包围环形槽 凹槽区域中的管道，其中安装有环形槽的套筒覆盖了切口，并且至少部分地位于轴台阶的圆周表面上。