公开(公告)号：US06533547B2

公开(公告)日：2003-03-18

申请号：US09796309

申请日：2001-02-28

Applicant: Dirk Anding ,  Burkhard Bischoff-Beiermann ,  Hans-Thomas Bolms ,  Michael Scheurlen ,  Thomas Schulenberg ,  Peter Tiemann

Inventor： Dirk Anding ,  Burkhard Bischoff-Beiermann ,  Hans-Thomas Bolms ,  Michael Scheurlen ,  Thomas Schulenberg ,  Peter Tiemann

IPC: F04D2958

CPC classification number: F01D5/188

Abstract: The turbine blade has an internal space through which a coolant fluid is guided and in which stiffening ribs are formed to reinforce and support the external walls. Coolant screens that reduce the cooling of the stiffening ribs, are arranged in front of the stiffening ribs in order to reduce thermal stresses. The turbine blade is preferably a gas turbine blade.

Abstract translation: 涡轮叶片具有内部空间，冷却剂流体通过该内部空间被引导，并且其中形成有加强肋以加强和支撑外壁。 减少加强筋的冷却的冷却液筛被布置在加强筋的前面，以减少热应力。 涡轮叶片优选为燃气轮机叶片。

公开(公告)号：US06641362B1

公开(公告)日：2003-11-04

申请号：US10030236

申请日：2001-12-28

Applicant: Dirk Anding ,  Hans-Thomas Bolms ,  Michael Scheurlen ,  Michael Strassberger ,  Peter Tiemann

Inventor： Dirk Anding ,  Hans-Thomas Bolms ,  Michael Scheurlen ,  Michael Strassberger ,  Peter Tiemann

IPC: F01D508

CPC classification number: F01D5/187 ,  F05D2260/2212

Abstract: A component can be subjected to hot gas. At least one duct is provided which can be subjected to a cooling fluid. The duct is bounded by two first walls opposite to one another. The walls include turbulators with the same direction of inclination. In order to avoid constrictions, the turbulators of the first wall have a different angle of inclination relative to a flow direction of the cooling fluid to the turbulators of the second wall.

Abstract translation: 组分可以经受热气体。 提供至少一个可以经受冷却流体的管道。 管道由彼此相对的两个第一壁限定。 墙壁包括具有相同倾斜方向的扰流器。 为了避免收缩，第一壁的紊流器相对于冷却流体流向第二壁的湍流器的流动方向具有不同的倾斜角。

公开(公告)号：US06631561B1

公开(公告)日：2003-10-14

申请号：US10129850

申请日：2002-08-12

Applicant: Dirk Anding ,  Michael Scheurlen ,  Peter Tiemann

Inventor： Dirk Anding ,  Michael Scheurlen ,  Peter Tiemann

IPC: B23P1500

CPC classification number: F01D5/18 ,  B22C9/10 ,  B22C21/14 ,  F01D5/187 ,  Y10T29/49339 ,  Y10T29/49341

Abstract: A method is for producing a turbine blade, in particular, a gas turbine blade, comprising a head, a foot, and a blade section, in addition to an internal canalization system, including individual channels through which coolant gas can pass along a flow path within the turbine blade. The turbine blade also includes a throttle device which influences the passage of the coolant gas without impairing the flow of the coolant gas in the intake area. The throttle device is located in the rear section of the flow path, and is positioned upstream of the exit openings.

Abstract translation: 一种除了内部管道系统之外，还包括一个头部，一个脚部和一个叶片部分的涡轮机叶片，特别是一种燃气轮机叶片的方法，该内部管道系统包括单独的通道，冷却剂气体可以通过该通道沿流动路径 在涡轮叶片内。 涡轮机叶片还包括节流装置，其影响冷却剂气体的通过，而不损害进气区域中的冷却剂气体的流动。 节流装置位于流路的后部，并且位于出口的上游

公开(公告)号：US06755986B2

公开(公告)日：2004-06-29

申请号：US10204693

申请日：2002-08-23

Applicant: Dirk Anding ,  Michael Strassberger ,  Peter Tiemann

Inventor： Dirk Anding ,  Michael Strassberger ,  Peter Tiemann

IPC: F01D518

CPC classification number: F01D5/081 ,  F01D5/147 ,  F01D5/187 ,  F01D5/3007

Abstract: A moving turbine blade includes a blade profile with inner cooling which extends out from a blade platform adjoined by a blade foot, the blade foot engaging with a turbine disk and having a radial cross-section with an area whose width increases towards the blade platform. A moving turbine blade of this type is configured in such a way as to enable the moving blade profile to be lengthened. To this end, the blade foot has a hollowed-out section which opens out in the direction facing away from the platform side and which has a widened cross section in the area of the blade foot whose width increases.

Abstract translation: 移动涡轮机叶片包括具有内部冷却的叶片轮廓，其从与叶片脚相邻的叶片平台延伸出来，叶片脚与涡轮盘接合并具有径向横截面，其宽度朝向叶片平台增加。 这种类型的移动涡轮机叶片被构造成能够延长移动的叶片轮廓。 为此，叶片脚具有一个中空部分，该部分在远离平台侧的方向上敞开，并且在叶片的宽度增加的区域中具有加宽的横截面。

公开(公告)号：US09004856B2

公开(公告)日：2015-04-14

申请号：US12866077

申请日：2008-11-03

Applicant: Christoph Lange ,  Henning Ressing ,  Fikri Aynacioglu ,  Dirk Anding ,  Karl-Heinz Dreyer

Inventor： Christoph Lange ,  Henning Ressing ,  Fikri Aynacioglu ,  Dirk Anding ,  Karl-Heinz Dreyer

IPC: F01D25/16 ,  F04D29/059 ,  F01D9/06 ,  F04D19/02 ,  F04D29/52 ,  F04D29/64 ,  F04D29/66

CPC classification number: F04D29/059 ,  F01D9/065 ,  F01D25/162 ,  F04D19/02 ,  F04D29/063 ,  F04D29/522 ,  F04D29/644 ,  F04D29/668

Abstract: An inlet connection piece for an axial compressor, particularly for a turbocompressor, includes an inlet housing (1) in which is arranged a bearing housing (2) with a bearing (3), particularly a radial and/or axial bearing, for a rotor. The bearing housing (2) is connected to the inlet housing (1) by an inlet strut (4) which is connected to the inlet housing in a front cross section. The center of the bearing (3) is arranged axially in the flow direction of a fluid to be compressed behind the area center of the front cross section by at least 0.1-times, particularly at least 0.15-times, particularly at least 0.2-times, particularly at least 0.25-times, the chord length of the front cross section. In addition or alternatively, a fluid passage (5, 6) is formed in the inlet strut (4), and at least portions of this fluid passage (5, 6) form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.

Abstract translation: 用于轴向压缩机的入口连接件，特别是用于涡轮压缩机的入口连接件包括入口壳体（1），其中布置有用于转子的轴承（3），特别是径向和/或轴向轴承的轴承壳体（2） 。 轴承壳体（2）通过入口支柱（4）连接到入口壳体（1），入口支柱（4）以前横截面连接到入口壳体。 轴承（3）的中心轴向地被布置在待压缩流体的流动方向后面的前横截面的区域中心的至少0.1倍，特别是至少0.15倍，特别是至少0.2倍 ，特别是至少0.25倍的前横截面的弦长。 另外或替代地，在入口支柱（4）中形成流体通道（5,6），并且该流体通道（5,6）的至少一部分与正常平面相对于纵向轴线的纵向轴线形成锐角 入口连接件。

公开(公告)号：US20140341745A1

公开(公告)日：2014-11-20

申请号：US14276602

申请日：2014-05-13

Applicant: Klaus Hörmeyer ,  Bernhard Eisenberg ,  Roland Emmrich ,  Dirk Anding

Inventor： Klaus Hörmeyer ,  Bernhard Eisenberg ,  Roland Emmrich ,  Dirk Anding

IPC: F04D29/18

CPC classification number: F04D29/181 ,  F01D5/02 ,  F01D5/282 ,  F04D29/18 ,  F04D29/324 ,  F04D29/384

Abstract: A rotor blade of an axial compressor includes: a blade root; and a blade leaf. The blade leaf has: a flow inlet edge, a flow outlet edge, a pressure side extending between the flow inlet edge and the flow outlet edge and a suction side extending between the flow inlet edge and the flow outlet edge, which together define a blade profile of the blade leaf in Cartesian coordinate values x, y and z such that first and second profile coordinates, or the coordinates x and y when joining via continuous arcs, each describe a smooth profile section on a radial section height along a third profile coordinate, or the coordinate value z, and the joining of the radial profile sections with a smoothing function describe the blade profile of the blade leaf.

Abstract translation: 轴向压缩机的转子叶片包括：叶根; 和叶片叶。 叶片叶片具有：流入口边缘，流出口边缘，在流入口边缘和流出口边缘之间延伸的压力侧和在流入口边缘和流出口边缘之间延伸的吸力侧，其一起限定叶片 以笛卡尔坐标值x，y和z为基准，使得第一和第二轮廓坐标或通过连续弧连接时的坐标x和y各自描绘沿着第三轮廓坐标的径向截面高度上的平滑轮廓截面 或坐标值z，并且具有平滑功能的径向轮廓部分的接合描述叶片的叶片轮廓。

公开(公告)号：US20100329861A1

公开(公告)日：2010-12-30

申请号：US12866077

申请日：2008-11-03

Applicant: Christoph Lange ,  Henning Ressing ,  Fikri Aynacioglu ,  Dirk Anding ,  Karl-Heinz Dreyer

Inventor： Christoph Lange ,  Henning Ressing ,  Fikri Aynacioglu ,  Dirk Anding ,  Karl-Heinz Dreyer

IPC: F04D29/059 ,  F04D29/52 ,  F04D29/64 ,  F04D29/66

CPC classification number: F04D29/059 ,  F01D9/065 ,  F01D25/162 ,  F04D19/02 ,  F04D29/063 ,  F04D29/522 ,  F04D29/644 ,  F04D29/668

Abstract: An inlet connection piece for an axial compressor, particularly for a turbocompressor, includes an inlet housing (1) in which is arranged a bearing housing (2) with a bearing (3), particularly a radial and/or axial bearing, for a rotor. The bearing housing (2) is connected to the inlet housing (1) by an inlet strut (4) which is connected to the inlet housing in a front cross section. The center of the bearing (3) is arranged axially in the flow direction of a fluid to be compressed behind the area center of the front cross section by at least 0.1-times, particularly at least 0.15-times, particularly at least 0.2-times, particularly at least 0.25-times, the chord length of the front cross section. In addition or alternatively, a fluid passage (5, 6) is formed in the inlet strut (4), and at least portions of this fluid passage (5, 6) form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.

Abstract translation: 用于轴向压缩机的入口连接件，特别是用于涡轮压缩机的入口连接件包括入口壳体（1），其中布置有具有用于转子的轴承（3），特别是径向和/或轴向轴承的轴承壳体（2） 。 轴承壳体（2）通过入口支柱（4）连接到入口壳体（1），入口支柱（4）以前横截面连接到入口壳体。 轴承（3）的中心轴向地被布置在待压缩流体的流动方向后面的前横截面的区域中心的至少0.1倍，特别是至少0.15倍，特别是至少0.2倍 ，特别是至少0.25倍的前横截面的弦长。 另外或替代地，在入口支柱（4）中形成流体通道（5,6），并且该流体通道（5,6）的至少一部分与正常平面相对于纵向轴线的纵向轴线形成锐角 入口连接件。

公开(公告)号：US10012235B2

公开(公告)日：2018-07-03

申请号：US14276602

申请日：2014-05-13

Applicant: Klaus Hörmeyer ,  Bernhard Eisenberg ,  Roland Emmrich ,  Dirk Anding

Inventor： Klaus Hörmeyer ,  Bernhard Eisenberg ,  Roland Emmrich ,  Dirk Anding

IPC: F04D29/18 ,  F04D29/32 ,  F01D5/28 ,  F04D29/38 ,  F01D5/02

CPC classification number: F04D29/181 ,  F01D5/02 ,  F01D5/282 ,  F04D29/18 ,  F04D29/324 ,  F04D29/384

Abstract: A rotor blade of an axial compressor includes: a blade root; and a blade leaf. The blade leaf has: a flow inlet edge, a flow outlet edge, a pressure side extending between the flow inlet edge and the flow outlet edge and a suction side extending between the flow inlet edge and the flow outlet edge, which together define a blade profile of the blade leaf in Cartesian coordinate values x, y and z such that first and second profile coordinates, or the coordinates x and y when joining via continuous arcs, each describe a smooth profile section on a radial section height along a third profile coordinate, or the coordinate value z, and the joining of the radial profile sections with a smoothing function describe the blade profile of the blade leaf.

公开(公告)号：US09752584B2

公开(公告)日：2017-09-05

申请号：US14495501

申请日：2014-09-24

Applicant: Klaus Hörmeyer ,  Roland Emmrich ,  Bernhard Eisenberg ,  Dirk Anding ,  Henning Ressing

Inventor： Klaus Hörmeyer ,  Roland Emmrich ,  Bernhard Eisenberg ,  Dirk Anding ,  Henning Ressing

IPC: F04D17/02 ,  F01D5/14 ,  F02C3/08 ,  F04D29/66 ,  F02C3/14

CPC classification number: F04D17/025 ,  F01D5/143 ,  F02C3/08 ,  F02C3/14 ,  F04D29/666

Abstract: A compressor arrangement has a common shaft, an axial compressor having at least a single-stage, and a radial compressor having at least single-stage. Assemblies of the, or each, axial compressor stage on the rotor side and assemblies of the, or each, radial compressor stage on the rotor side are attached to a common shaft (4). A ratio between a maximum diameter of the shaft (4) in the region of the axial compressor (2) and a minimum radial impeller seat diameter of the shaft (4) in the region of the radial compressor (3) is between 1.5 and 3.0.

公开(公告)号：US20150139788A1

公开(公告)日：2015-05-21

申请号：US14495501

申请日：2014-09-24

Applicant: Klaus Hörmeyer ,  Roland Emmrich ,  Bernhard Eisenberg ,  Dirk Anding ,  Henning Ressing

Inventor： Klaus Hörmeyer ,  Roland Emmrich ,  Bernhard Eisenberg ,  Dirk Anding ,  Henning Ressing

IPC: F04D17/02

CPC classification number: F04D17/025 ,  F01D5/143 ,  F02C3/08 ,  F02C3/14 ,  F04D29/666

Abstract: A compressor arrangement has a common shaft, an axial compressor having at least a single-stage, and a radial compressor having at least single-stage. Assemblies of the, or each, axial compressor stage on the rotor side and assemblies of the, or each, radial compressor stage on the rotor side are attached to a common shaft (4). A ratio between a maximum diameter of the shaft (4) in the region of the axial compressor (2) and a minimum radial impeller seat diameter of the shaft (4) in the region of the radial compressor (3) is between 1.5 and 3.0.

Abstract translation: 压缩机装置具有公共轴，具有至少单级的轴向压缩机和至少具有单级的径向压缩机。 转子侧的或每个轴向压缩机级的组件或转子侧上的每个或径向压缩机级的组件都附接到公共轴（4）。 轴向压缩机（2）区域中的轴（4）的最大直径与径向压缩机（3）区域中的轴（4）的最小径向叶轮座直径之间的比率在1.5和3.0之间 。