专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US06916021B2 Sealing arrangement 有权
标题翻译：密封安排
公开(公告)号：US06916021B2
公开(公告)日：2005-07-12
申请号：US10383735
申请日：2003-03-10
申请人： Alexander Beeck , Bruno Benedetti , Andreas Kieninger , Ulrich Rathmann
发明人： Alexander Beeck , Bruno Benedetti , Andreas Kieninger , Ulrich Rathmann
IPC分类号： F01D5/20 , F01D5/22 , F01D11/08 , F16J15/44
CPC分类号： F16J15/445 , F01D5/225 , F01D11/08 , F16J15/444
摘要： The present invention relates to a sealing arrangement which is formed between a rotating assembly (4, 6) and a static assembly (3, 14, 15). In this sealing arrangement, the rotating assembly (4, 6, 16) has at least one cutting element (1) which engages in a counterpart surface on the static component. The present sealing arrangement is distinguished by the fact that the cutting element (1) is designed as a chipping device with a geometrically determined cutting edge with respect to the counterpart surface (2) or forms a chipping device of this type when the rotating assembly is rotating. The proposed sealing arrangement reduces the wear to the cutting element even in the event of adverse rotation or temperature conditions.
摘要翻译：本发明涉及一种形成在旋转组件（4,6）和静态组件（3,14,15）之间的密封装置。在该密封装置中，旋转组件（4,6,16）具有至少一个切割元件（1），该切割元件（1）与静态部件上的配对表面接合。本密封装置的特征在于，切割元件（1）被设计为具有相对于配对表面（2）几何确定的切割边缘的切屑装置，或者当旋转组件为旋转。所提出的密封装置即使在不利的旋转或温度条件的情况下也减少了对切割元件的磨损。

2. 发明申请

US20050042384A1 Method of altering the frequency of blades for thermal fluid-flow machines 审中-公开
标题翻译：改变热流体流动机叶片频率的方法
公开(公告)号：US20050042384A1
公开(公告)日：2005-02-24
申请号：US10892278
申请日：2004-07-16
申请人： Bruno Benedetti , Andreas Kieninger , Christoph Nagler , Joerg Stengele
发明人： Bruno Benedetti , Andreas Kieninger , Christoph Nagler , Joerg Stengele
IPC分类号： C23C4/00 , F01D5/16 , B05D1/08
CPC分类号： C23C4/00 , F01D5/16 , F05D2230/311 , F05D2230/90
摘要： A method of altering the frequency of blades (1) having an airfoil (2) with a suction side (6), a pressure side (5), a leading edge (10), a trailing edge (7) and a blade tip (9), and including a blade root (3), in particular turbine blades, for thermal fluid-flow machines. A metallic coating (8) formed of a material identical to the parent material is applied to the blade (1), already ready for use, in the region of the blade tip (9), the thickness of the coating (8) tapering continuously at the trailing edge (7) and in the radial direction toward the blade root (3).
摘要翻译：一种改变具有吸力侧（6），压力侧（5），前缘（10），后缘（7）和叶片尖端（6）的翼型（2）的叶片（1）的频率的方法， 9），并且包括用于热流体流动机器的叶片根部（3），特别是涡轮叶片。将由与母体材料相同的材料形成的金属涂层（8）施加到叶片（1），已经准备好使用，在叶片尖端（9）的区域中，涂层（8）的厚度连续地逐渐变细在后缘（7）处并沿径向朝向叶片根部（3）。

3. 发明申请

US20060251519A1 Guide vane ring of a turbomachine and associated modification method 有权
标题翻译：涡轮机导叶环及相关修改方法
公开(公告)号：US20060251519A1
公开(公告)日：2006-11-09
申请号：US11255988
申请日：2005-10-24
申请人： Bruno Benedetti , Andreas Boegli , Christopher Hulme , James Ritchie , Patrick Schnedler
发明人： Bruno Benedetti , Andreas Boegli , Christopher Hulme , James Ritchie , Patrick Schnedler
IPC分类号： F01D5/02
CPC分类号： F01D9/042 , F05D2230/642
摘要： A guide vane ring of a turbomachine, in particular of an axial-throughflow turbine, includes a vane group (6) having a plurality of vanes (2). The vane group (6) has a vane root (11) which has two flanges (12, 13). The vane group (6) is fastened to a vane carrier by means of the flanges (12, 13). In order to reduce stresses in the vanes (2) which occur during deformations of the vane carrier, one flange (13) has on a front end portion (14) and on a rear end portion (15), radially on the inside and radially on the outside, in each case a contact zone (18) which bears against the vane carrier. The other flange (12) has on one end portion (15), radially on the inside, a contact zone (18) which bears against the vane carrier, and is spaced apart from the vane carrier radially on the outside. Moreover, this flange (12) has on the other end portion (14), radially on the outside, a contact zone (18) which bears against the vane carrier, and is spaced apart from the vane carrier radially on the inside. Furthermore, the flanges (12, 13), between their end portions (14, 15), are spaced apart from the vane carrier radially on the inside and radially on the outside.
摘要翻译：涡轮机，特别是轴流式涡轮机的导向叶片环包括具有多个叶片（2）的叶片组（6）。叶片组（6）具有叶片根部（11），其具有两个凸缘（12,13）。叶片组6通过凸缘12,13固定在叶片载体上。为了减小在叶片载体变形期间发生的叶片（2）中的应力，一个凸缘（13）在前端部分（14）和后端部分（15）上具有径向上在内侧和径向上在每个情况下，在外侧具有抵靠叶片承载件的接触区域（18）。另一个凸缘（12）在一个端部（15）的径向上具有抵靠叶片承载件的接触区（18），并且在外侧径向地与叶片承载体间隔开。此外，该凸缘12在径向上具有在另一端部14上的与叶片承载件抵靠的接触区18，并且在内侧径向地与叶片承载体间隔开。此外，其端部（14,15）之间的凸缘（12,13）在径向上在内侧和径向上与外部叶片承载件间隔开。

4. 发明授权

US06732910B2 Device and process for producing a soldered joint between two joining partners which can be by means of a common contact surface 有权
标题翻译：用于在两个连接伙伴之间生产焊接接头的装置和方法，其可以通过公共接触表面
公开(公告)号：US06732910B2
公开(公告)日：2004-05-11
申请号：US10173169
申请日：2002-06-18
申请人： Bruno Benedetti , Christoph Nagler , Joerg Stengele
发明人： Bruno Benedetti , Christoph Nagler , Joerg Stengele
IPC分类号： B23K3102
CPC分类号： B23K1/20 , B23K1/0018 , B23K2101/001 , F05B2240/801 , F05B2260/201 , Y10T29/49321 , Y10T29/49336
摘要： A device for producing a soldered joint between two joining partners which can be joined via a common contact surface (7), using a solder material which can be introduced between the two joining partners. At least one joining partner (1), in the region of the contact surface (7), provides at least one recess, known as a solder reservoir (3), which faces the contact surface and into which the solder material can be introduced, and the solder reservoir (3) is completely delimited and surrounded by the contact surface (7).
摘要翻译：一种用于在两个接合伙伴之间生产焊接接头的装置，其可以通过公共接触表面（7）连接，使用可以在两个接合伙伴之间引入的焊料材料。在接触表面（7）的区域中的至少一个接合配对件（1）提供了至少一个凹槽，称为焊料储存器（3），其面向接触表面并且可以将焊料材料引入到该凹槽中，并且焊料储存器（3）被完全界定并被接触表面（7）围绕。

5. 发明授权

US07458772B2 Guide vane ring of a turbomachine and associated modification method 有权
标题翻译：涡轮机导叶环及相关修改方法
公开(公告)号：US07458772B2
公开(公告)日：2008-12-02
申请号：US11255988
申请日：2005-10-24
申请人： Bruno Benedetti , Andreas Boegli , Christopher Hulme , James Ritchie , Patrick Wolfgang Schnedler
发明人： Bruno Benedetti , Andreas Boegli , Christopher Hulme , James Ritchie , Patrick Wolfgang Schnedler
IPC分类号： F01D25/28
CPC分类号： F01D9/042 , F05D2230/642
摘要： A guide vane ring of a turbomachine, in particular of an axial-throughflow turbine, includes a vane group (6) having a plurality of vanes (2). The vane group (6) has a vane root (11) which has two flanges (12, 13). The vane group (6) is fastened to a vane carrier by means of the flanges (12, 13). In order to reduce stresses in the vanes (2) which occur during deformations of the vane carrier, one flange (13) has on a front end portion (14) and on a rear end portion (15), radially on the inside and radially on the outside, in each case a contact zone (18) which bears against the vane carrier. The other flange (12) has on one end portion (15), radially on the inside, a contact zone (18) which bears against the vane carrier, and is spaced apart from the vane carrier radially on the outside. Moreover, this flange (12) has on the other end portion (14), radially on the outside, a contact zone (18) which bears against the vane carrier, and is spaced apart from the vane carrier radially on the inside. Furthermore, the flanges (12, 13), between their end portions (14, 15), are spaced apart from the vane carrier radially on the inside and radially on the outside.
摘要翻译：涡轮机，特别是轴流式涡轮机的导向叶片环包括具有多个叶片（2）的叶片组（6）。叶片组（6）具有叶片根部（11），其具有两个凸缘（12,13）。叶片组6通过凸缘12,13固定在叶片载体上。为了减小在叶片载体变形期间发生的叶片（2）中的应力，一个凸缘（13）在前端部分（14）和后端部分（15）上具有径向上在内侧和径向上在每个情况下，在外侧具有抵靠叶片承载件的接触区域（18）。另一个凸缘（12）在一个端部（15）的径向上具有抵靠叶片承载件的接触区（18），并且在外侧径向地与叶片承载体间隔开。此外，该凸缘12在径向上具有在另一端部14上的与叶片承载件抵靠的接触区18，并且在内侧径向地与叶片承载体间隔开。此外，其端部（14,15）之间的凸缘（12,13）在径向上在内侧和径向上与外部叶片承载件间隔开。

6. 发明授权

US06945750B2 Turbine blade 有权
标题翻译：涡轮叶片
公开(公告)号：US06945750B2
公开(公告)日：2005-09-20
申请号：US10724091
申请日：2003-12-01
申请人： Bruno Benedetti , Said Jaamei , David Johns , Joerg Krueckels
发明人： Bruno Benedetti , Said Jaamei , David Johns , Joerg Krueckels
IPC分类号： B23H9/10 , F01D5/18 , F01D9/02 , F01D25/12 , F01D9/06
CPC分类号： F01D5/186 , B23H9/10 , F01D5/187 , F01D9/02 , F05D2230/12 , F05D2240/81 , F05D2260/2212
摘要： A turbine blade for a gas turbine has a hollow airfoil extending from a platform. There is a fillet between the airfoil and the platform, both on the pressure side and on the suction side of the airfoil. The fillet contains a cooling bore extending along part of the length of the fillet, having a first end communicating with the interior of the turbine blade for receiving a gaseous coolant and a second end communicating with the exterior of the turbine blade. The cooling may be formed by electro-discharge machining.
摘要翻译：用于燃气轮机的涡轮叶片具有从平台延伸的中空翼型件。在翼型和平台之间都有在翼型的压力侧和吸力侧上的圆角。所述圆角包含沿所述圆角长度的一部分延伸的冷却孔，所述冷却孔具有与所述涡轮机叶片的内部连通的第一端，用于接收气态冷却剂和与所述涡轮叶片的外部连通的第二端。冷却可以通过放电加工形成。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式