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公开(公告)号：US07192256B2
公开(公告)日：2007-03-20
申请号：US10792708
申请日：2004-03-05
IPC分类号： F01D5/32
CPC分类号： F01D5/32 , F01D5/3038
摘要： The invention relates to a rotor end piece (1) for rotors (2) of thermal turbomachines with a circumferential slot (3), consisting of two end piece halves (4, 4′) having side faces (5, 5′) opposite one another in the installed state and of a wedge (6) which is pushed in between them and which, in the installed state, is anchored in the side faces (5, 5′) of the end piece halves (4, 4′) in a form-fitting manner, the rotor end piece (1) being arranged in the axial direction of the rotor (2) between two moving blades (7, 7′). It is characterized in that each of the end piece halves (4, 4′) is fastened in the axial direction of the rotor (2) to the two adjacent moving blades (7, 7′) by means of one interlocking connection (8, 8′, 9, 9′) each. These four interlocking connections (8, 8′, 9, 9′), instead of the rotor (2), now absorb the axial forces which are caused by the centrifugal force and the caulked wedge (6). In this way, disturbing rotor vibrations are advantageously avoided.
摘要翻译： 本发明涉及一种用于具有圆周槽（3）的热涡轮机的转子（2）的转子端件（1），由两个端部半部（4,4'）组成，两个端部半部（4,4'）具有与其相对的侧面 另一个处于安装状态，并且被推入它们之间的楔形件（6），并且在安装状态下将楔子（6）锚固在端部半部（4,4'）的侧面（5,5'）中 转子端件（1）沿转子（2）的轴向方向布置在两个活动叶片（7,7'）之间。 其特征在于，通过一个互锁连接（8,8）将端部半部（4,4'）中的每一个在转子（2）的轴向方向上紧固到两个相邻的活动叶片（7,7'）上， 8'，9,9'）。 这四个互锁连接（8,8'，9,9'）代替转子（2）现在吸收由离心力和铆接楔（6）引起的轴向力。 以这种方式，有利地避免了干扰转子的振动。
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公开(公告)号：US07351039B2
公开(公告)日：2008-04-01
申请号：US10983225
申请日：2004-11-08
申请人： René Bachofner , Wolfgang Kappis
发明人： René Bachofner , Wolfgang Kappis
IPC分类号： F04D29/38
CPC分类号： F04D29/668 , F01D5/141 , F01D5/16 , F01D5/20 , F04D29/324 , F05D2240/301
摘要： A compressor rotor blade (1) includes a rotor blade (2), a platform (3) that adjoins the rotor blade (2) and blade footing (4) that adjoins the platform (3). The rotor blade (4) is embodied so as to be massive, without an internal cooling system, and exhibits a leading and a trailing edge (5, 6), a suction and a compression side, as well as a blade tip (7). The compressor rotor blade (1) is distinguished by virtue of the fact that the rotor blade (2) of the compressor rotor blade (1) exhibits a recess (8) on the trailing edge (6) of the blade tip (7).
摘要翻译： 压缩机转子叶片（1）包括转子叶片（2），与转子叶片（2）相邻的平台（3）和邻接平台（3）的叶片基部（4）。 转子叶片（4）被实施为具有巨大的，没有内部冷却系统，并且具有前缘和后缘（5,6），吸力和压缩侧以及叶片尖端（7） 。 压缩机转子叶片（1）的特征在于压缩机转子叶片（1）的转子叶片（2）在叶片尖端（7）的后缘（6）上具有凹部（8）。
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公开(公告)号：US07309214B2
公开(公告)日：2007-12-18
申请号：US11530308
申请日：2006-09-08
申请人： René Bachofner , Wolfgang Kappis
发明人： René Bachofner , Wolfgang Kappis
IPC分类号： F01D5/32
CPC分类号： F01D5/3038 , F01D5/32 , F05D2230/232
摘要： A rotor end piece for a rotor of a thermal turbomachine having a circumferential slot includes two end piece halves having side faces opposite one another in the installed state and top surfaces adjoining one another, the side faces of the end piece halves being connected to one another in a form-fitting manner by means of a dovetail interlocking connection, and a whole intermediate end piece having a top surface, the two interlocked end piece halves being firmly connected to the whole intermediate end piece in the region of the top surfaces via a weld.
摘要翻译： 具有圆周槽的热涡轮机的转子的转子端件包括两个端部半部，两个端部半部在安装状态下具有彼此相对的侧面，并且彼此相邻的顶表面，端部半部的侧面彼此连接 通过燕尾形互锁连接的形状配合方式和具有顶表面的整个中间端件，两个互锁的端部件半部通过焊接在顶表面的区域中牢固地连接到整个中间端件 。
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公开(公告)号：US07513747B2
公开(公告)日：2009-04-07
申请号：US11419031
申请日：2006-05-18
申请人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
发明人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
IPC分类号： F01D5/30
CPC分类号： F01D5/3038 , F04D29/322 , F05D2250/29 , F05D2250/291
摘要： A rotor (20) for a compressor, in particular in a gas turbine, has a number of rotor blades (25) which are arranged around the rotation axis of the rotor (20) in the form of a rim and are each held in a circumferential recess (21) on the rotor (20) by a blade root (26), with the blade root (26) having a widening lower part (27) which engages behind two shoulders (24) that are formed on the side walls of the recess (21). In such a rotor, the life is lengthened in that the recess depth (T) of the recess (21) is substantially greater than a minimum recess depth (Tmin) which results in the rotor (20) having sufficient strength in the area of the blade attachment for starting, based on the predetermined material characteristics of the rotor (20) and the operating conditions of the compressor.
摘要翻译： 用于压缩机，特别是燃气轮机的转子（20）具有若干转子叶片（25），其以轮缘的形式围绕转子（20）的旋转轴线布置，并且分别保持在 叶片根部（26）在转子（20）上的圆周凹槽（21）上，叶片根部（26）具有一个加宽的下部（27），后部两个肩部（24） 凹部（21）。 在这种转子中，寿命延长，因为凹部（21）的凹陷深度（T）基本上大于最小凹陷深度（Tmin），这导致转子（20）在 基于转子（20）的预定材料特性和压缩机的操作条件来启动叶片附件。
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公开(公告)号：US07338258B2
公开(公告)日：2008-03-04
申请号：US11276186
申请日：2006-02-17
申请人： René Bachofner , Wolfgang Kappis , Kurt Rubischon
发明人： René Bachofner , Wolfgang Kappis , Kurt Rubischon
IPC分类号： F01D5/32
CPC分类号： F01D5/3038 , F05D2260/30
摘要： A rotor end piece (1) for a rotor of a thermal turbomachine, having at least one circumferential slot (3) in which press blades, intermediate pieces and two end blades (4), between which a residual gap is formed, are fitted, the rotor end piece (1) having two end piece halves (9, 9) and a wedge (7), is characterized in that a clip (8) is arranged in the residual gap, this clip (8) absorbing the forces of the two end piece halves (9, 9) and two shim halves (5, 6) arranged between the end piece halves (9, 9) and restrained with the wedge (7). As a result, the disadvantages of the prior art are avoided and a rotor end piece is provided which exerts no axial forces on the rotor and no forces on adjacent blades in the circumferential direction, so that an occurrence of disturbing rotor vibrations and jamming of adjacent blades is effectively avoided.
摘要翻译： 一种用于热涡轮机的转子的转子端件（1），其具有至少一个周向槽（3），在其中形成有间隙的压制叶片，中间件和两个端部叶片（4） 具有两个端部半部（9,9）和楔形物（7）的转子端部件（1）的特征在于，在剩余间隙中布置有夹子（8），该夹子（8）吸收 两个端部半部（9,9）和布置在端部半部（9,9）之间并被楔形物（7）约束的两个垫片半部（5,6）。 结果，避免了现有技术的缺点，并且提供了转子端件，其在转子上不施加轴向力，并且在圆周方向上不对相邻叶片施加力，使得发生扰动的转子振动和相邻的 叶片被有效地避免。
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公开(公告)号：US06647602B2
公开(公告)日：2003-11-18
申请号：US09996683
申请日：2001-11-30
申请人： René Bachofner , Wolfgang Kappis , Pavel Rihak , Ferdinand Thueringer , Ulrich Waltke , Hans Wettstein
发明人： René Bachofner , Wolfgang Kappis , Pavel Rihak , Ferdinand Thueringer , Ulrich Waltke , Hans Wettstein
IPC分类号： B23P1500
CPC分类号： F01D5/32 , F01D5/3038 , Y10T29/37 , Y10T29/49321 , Y10T29/49323
摘要： Described is a fixation device for blading of a turbo-machine, in which, longitudinally to a mounting groove (1), a plurality of blades (31, 32) is positioned, and in which, between at least two blades (31, 32) positioned adjacent to each other inside the mounting groove (1), a mounting gap is provided, having two insertion elements constructed as collar halves (41, 42) that can be inserted into the mounting gap, and each of which has a width adapted to the width of the mounting gap and which enclose between themselves a gap space (5) into which a wedge element (43) can be inserted that can be wedged in such a way that both collar halves (41, 42) are fixed in a force-derived manner by means of the wedge element (43) inside the mounting groove (1). The invention is characterized in that the wedge element (43) is provided with at least one connecting element (45) towards the side of a blade (31, 32) and that at least one of the two blades (31, 32) adjoining the wedge element (43) is provided with a counter-contour (46) corresponding to the connecting element (45), so that the wedge element (43) and the blade enter (31, 32) into an intimate shape-mated connection with each other.
摘要翻译： 描述了一种用于涡轮机的叶片的固定装置，其中纵向安装槽（1），多个叶片（31,32）被定位，并且其中在至少两个叶片（31,32）之间 ）设置在安装槽（1）内彼此相邻的安装间隙，具有两个插入元件，该插入元件构造成可插入安装间隙中的半环（41,42），并且每个插入元件具有适应的宽度 相对于安装间隙的宽度并且在它们之间包围间隙空间（5），楔形元件（43）能够被插入该间隙空间中，楔形元件可以被插入其中，使得楔形半部（41,42）固定在 通过楔形元件（43）在安装槽（1）内部的力衍生方式。 本发明的特征在于，楔形元件（43）设置有朝向叶片（31,32）的侧面的至少一个连接元件（45），并且两个叶片（31,32）中的至少一个邻接 楔形元件（43）设置有对应于连接元件（45）的相对轮廓（46），使得楔形元件（43）和叶片进入（31,32）成与每个 其他。
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公开(公告)号：US08033784B2
公开(公告)日：2011-10-11
申请号：US11382292
申请日：2006-05-09
申请人： René Bachofner , Wolfgang Kappis , Kurt Rubischon
发明人： René Bachofner , Wolfgang Kappis , Kurt Rubischon
CPC分类号： F04D29/644 , F01D5/06 , F01D25/246 , F05B2260/301 , F05D2230/64
摘要： A compressor has a rotor (13), which rotor (13) has a number of rows of rotor blades (14, 14′) which are at a distance from one another, one behind the other in the axial direction, with a number of thermal barrier segments (10), which are detachably attached to the rotor (13) and are mounted such that they can move in the circumferential direction, being arranged one behind the other in the circumferential direction on the circumference of the rotor (13), and with securing devices (15) being provided on the thermal barrier segments (10), which secure the thermal barrier segments (10) against being moved in the circumferential direction. In the case of such a rotor (13), production and assembly are simplified in that only some of the thermal barrier segments (10) are equipped with the securing devices (15).
摘要翻译： 压缩机具有转子（13），该转子（13）具有多个彼此间隔一定距离的一定数量的转子叶片（14,14'），一个在轴向方向上彼此相隔，多个 隔热片（10），其可拆卸地安装在转子（13）上并且安装成使得它们能够在圆周方向上移动，在圆周方向上在转子（13）的圆周上一个接一个地布置， 并且固定装置（15）设置在热障部分（10）上，其将热障部分（10）固定在周向方向上。 在这样的转子（13）的情况下，制造和组装被简化为只有一些热障部分（10）配备有固定装置（15）。
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公开(公告)号：US07367778B2
公开(公告)日：2008-05-06
申请号：US11276296
申请日：2006-02-23
申请人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
发明人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
IPC分类号： F01D5/32
CPC分类号： F01D5/32 , F01D5/3038
摘要： A rotor end piece (1) for a rotor (6) of a thermal turbomachine, having at least one circumferential slot (3) in which moving blades and intermediate pieces are provided, includes a residual gap (15) formed between an end blade (2) and an end part (11), in which residual gap (15) two end piece halves (4, 4) are arranged which have securing tabs (8, 8) which are in each case connected to the latter in one piece and are in engagement with the end blade (2) and with the end part (11), respectively.
摘要翻译： 一种用于热涡轮机的转子（6）的转子端件（1），其具有至少一个周向槽（3），其中设置有活动叶片和中间件，所述转子端件（1）包括形成在端部叶片 2）和端部（11），其中布置有两个端部半部（4,4）的剩余间隙（15），其具有固定突片（8,8），每个固定突出部分（8,8）分别连接在一起，并且 分别与端部叶片（2）和端部部分（11）接合。
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公开(公告)号：US07048508B2
公开(公告)日：2006-05-23
申请号：US10792707
申请日：2004-03-05
申请人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
发明人： René Bachofner , Pietro Grigioni , Wolfgang Kappis
IPC分类号： F01D5/32
CPC分类号： F01D5/32 , F01D5/3038
摘要： A rotor end piece (1) for rotors (2) of thermal turbormachines is provided with circumferential slot (3), including two end piece halves (4, 4′) having side faces (5, 5′) opposite one another in the installed state and top surfaces (6, 6′) adjoining one another. The rotor end piece (1) side faces (5, 5′) of the end piece halves (4,4′) are connected to one another in a form-fitting manner. To this end, the side faces (5, 5′) are designed in such a way that a dovetail interlocking connection of the two end piece halves (4, 4′) is preferably realized. The interlocked end piece halves are then secured with a weld (8). The firm anchoring of the rotor end piece (1) achieved in this way prevents detachment during operation and damage to the turbomachine caused as a result.
摘要翻译： 一种用于热涡轮机的转子（2）的转子端件（1）设置有周向槽（3），包括两个端部半部（4,4'），所述端部半部（4,4'）在安装 状态和顶表面（6,6'）彼此相邻。 端部半部（4,4'）的转子端部件（1）侧面（5,5'）以形状配合方式彼此连接。 为此，侧面（5,5'）被设计成使得两个端部半部（4,4'）的燕尾形互锁连接最好实现。 然后用焊接（8）固定互锁端部半部。 以这种方式实现的转子端部件（1）的牢固锚固防止了在操作过程中的分离并导致涡轮机械的损坏。
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公开(公告)号：US08449261B2
公开(公告)日：2013-05-28
申请号：US12756729
申请日：2010-04-08
IPC分类号： B64C27/46
CPC分类号： F04D29/32 , F01D5/141 , F01D5/20 , F05D2250/74
摘要： The disclosure provides blades, and the modification thereof, for stages 18-22 of an axial compressor wherein the blades have reduced susceptibility to tip cracking. The blades and blades manufactured by the provided method have a thickened profile that results in reduced stress in response to multi frequency impulses and can have increased frequency response of the chord wise bending mode.
摘要翻译： 本公开为轴向压缩机的级18-22提供叶片及其修改，其中叶片具有降低的尖端开裂敏感性。 通过所提供的方法制造的叶片和叶片具有加厚的轮廓，其导致响应于多频率脉冲而减小的应力，并且可以增加弦弯曲模式的频率响应。
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