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1. 发明申请

US20070231143A1 BLADE WITH SHROUD 有权
标题翻译：刮胡子
公开(公告)号：US20070231143A1
公开(公告)日：2007-10-04
申请号：US11682624
申请日：2007-03-06
申请人： Andreas Boegli , James Ritchie
发明人： Andreas Boegli , James Ritchie
IPC分类号： F01D5/22
CPC分类号： F01D5/225
摘要： A blade for a turbo machine has a blade section and a shroud element terminating the blade section in the blade section longitudinal direction. The blade section has a suction face and a pressure face. The shroud element extends essentially at right angles to the blade section longitudinal direction and has a first platform section projecting beyond the blade section and a second platform section projecting beyond the blade section. The platform sections are asymmetric with respect to one another. At least the first platform section of the shroud element is arranged at an additional inclination angle with respect to a normal alignment of the first platform section, with the additional inclination angle being in the opposite direction to the bending torque which acts on the first platform section during operation.
摘要翻译：用于涡轮机的叶片具有叶片部分和在叶片部分纵向方向上终止叶片部分的护罩元件。叶片部分具有吸力面和压力面。护罩元件基本上与叶片部分纵向方向成直角地延伸，并且具有突出超过叶片部分的第一平台部分和突出超过叶片部分的第二平台部分。平台部分相对于彼此是不对称的。护罩元件的至少第一平台部分相对于第一平台部分的正常对准以额外的倾斜角度布置，附加倾斜角度与作用在第一平台部分上的弯曲扭矩相反的方向在运行期间。

2. 发明授权

US07326033B2 Turbomachine blade 有权
标题翻译：涡轮机刀片
公开(公告)号：US07326033B2
公开(公告)日：2008-02-05
申请号：US11600754
申请日：2006-11-17
申请人： Andreas Boegli , Alexander Mahler , James Ritchie , Slawomir Slowik
发明人： Andreas Boegli , Alexander Mahler , James Ritchie , Slawomir Slowik
IPC分类号： F01D11/02
CPC分类号： F01D5/225 , F05D2230/10 , F05D2240/11
摘要： A turbomachine blade is disclosed having a shroud element, wherein plastic deformations and lifting of the shroud element on one side result during operation under centrifugal load. This load may result in high-temperature creep of the blade. A sealing strip which is arranged on the shroud element can be configured with a thickness varying in a circumferential direction. The mass of the shroud element and thus the asymmetrical centrifugal load and the lifting of the shroud element on one side resulting therefrom can be reduced by material removal at regions lying on the outside in the circumferential direction.
摘要翻译：公开了一种涡轮机叶片，其具有护罩元件，其中在离心载荷下操作期间导致护罩元件在一侧上的塑性变形和提升。该负载可能导致叶片的高温蠕变。布置在护罩元件上的密封条可以被构造成在圆周方向上变化的厚度。护罩元件的质量以及因此不对称的离心载荷和护罩元件在其一侧产生的护罩元件的提升可以通过在圆周方向上位于外侧的区域处的材料去除而减少。

3. 发明授权

US07654797B2 Blade with shroud 有权
标题翻译：带护罩的刀片
公开(公告)号：US07654797B2
公开(公告)日：2010-02-02
申请号：US11682624
申请日：2007-03-06
申请人： Andreas Boegli , James Ritchie
发明人： Andreas Boegli , James Ritchie
IPC分类号： F01D5/22
CPC分类号： F01D5/225
摘要： A blade for a turbo machine has a blade section and a shroud element terminating the blade section in the blade section longitudinal direction. The blade section has a suction face and a pressure face. The shroud element extends essentially at right angles to the blade section longitudinal direction and has a first platform section projecting beyond the blade section and a second platform section projecting beyond the blade section. The platform sections are asymmetric with respect to one another. At least the first platform section of the shroud element is arranged at an additional inclination angle with respect to a normal alignment of the first platform section, with the additional inclination angle being in the opposite direction to the bending torque which acts on the first platform section during operation.
摘要翻译：用于涡轮机的叶片具有叶片部分和在叶片部分纵向方向上终止叶片部分的护罩元件。叶片部分具有吸力面和压力面。护罩元件基本上与叶片部分纵向方向成直角地延伸，并且具有突出超过叶片部分的第一平台部分和突出超过叶片部分的第二平台部分。平台部分相对于彼此是不对称的。护罩元件的至少第一平台部分相对于第一平台部分的正常对准以额外的倾斜角度布置，附加倾斜角度与作用在第一平台部分上的弯曲扭矩相反的方向在运行期间。

4. 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。

5. 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。

6. 发明申请

US20050042092A1 Method of reconditioning a turbine blade 有权
标题翻译：涡轮叶片修复方法
公开(公告)号：US20050042092A1
公开(公告)日：2005-02-24
申请号：US10892136
申请日：2004-07-16
申请人： Andreas Boegli , James Ritchie , Slawomir Slowik , Heinrich Stuessi
发明人： Andreas Boegli , James Ritchie , Slawomir Slowik , Heinrich Stuessi
IPC分类号： F01D5/00 , F01D5/22 , B63H1/00
CPC分类号： B23P6/002 , F01D5/005 , F01D5/225 , F05D2230/10 , F05D2230/23 , F05D2230/30 , F05D2230/80 , F05D2230/90 , F05D2300/611 , Y10T29/49318 , Y10T29/49718 , Y10T29/49719 , Y10T29/49732 , Y10T29/49742 , Y10T29/49746
摘要： A method of reconditioning a rotating blade (1) with a shroud (8) following the operation in a gas turbine, includes the application of a barrier (14) placed on the edge of the shroud (8) facing the edge of a shroud (8) of an adjacent blade having creep deformation. The barrier (14) prevents hot gas ingestion into a shroud cavity (10). It is pre-fabricated or built-up layer-by-layer by welding or laser cladding or other methods. Additionally, the mass of the shroud (8) is reduced in order to re-establish the initial mass of the shroud. A thermal barrier coating (15) is additionally applied to the surfaces of the shroud (8) that are exposed to the hot gas of the turbine. The method significantly increases the lifetime of the blade (1).
摘要翻译：在燃气轮机中的操作之后，用护罩（8）重新调节旋转叶片（1）的方法包括施加位于护罩（8）的面向护罩边缘的边缘（14）上的屏障（14） 8）具有蠕变变形的相邻叶片。阻挡层（14）防止热气体吸入护罩腔（10）。它是通过焊接或激光熔覆或其他方法逐层预制或组装的。此外，为了重新建立护罩的初始质量，护罩（8）的质量被减小。隔热涂层（15）另外施加到暴露于涡轮机的热气体的护罩（8）的表面。该方法显着增加了叶片（1）的寿命。

7. 发明申请

US20080298970A1 Turbo Machine 审中-公开
标题翻译：涡轮机
公开(公告)号：US20080298970A1
公开(公告)日：2008-12-04
申请号：US12045895
申请日：2008-03-11
申请人： Joergen Ferber , James Ritchie , Slawomir Slowik
发明人： Joergen Ferber , James Ritchie , Slawomir Slowik
IPC分类号： F01D5/22
CPC分类号： F01D5/225 , F05B2240/33 , F05D2230/60 , F05D2260/30 , Y02T50/671 , Y02T50/673
摘要： A turbo machine (1, 101), in particular turbine or compressor, includes a rotor (2, 102) which has at least one moving blade row (4, 104) with a plurality of moving blades (5, 105), and a stator (3) which has at least one guide vane row (6, 106) with a plurality of guide vanes (7, 107), at least one moving blade row (4, 104) having a shroud (8, 108). The shroud (8, 108) is designed to be self-supporting in such a way that it can at least partially absorb the centrifugal forces arising during operation and discharge them in the circumferential direction.
摘要翻译：特别是涡轮机或压缩机的涡轮机（1,101）包括具有至少一个具有多个活动叶片（5,105）的活动叶片排（4,104）的转子（2,102），以及定子（3）具有至少一个具有多个导向叶片（7,107）的导向叶片排（6,106），至少一个具有护罩（8,108）的活动叶片排（4,104）。护罩（8,108）被设计成自支撑，使得其可以至少部分地吸收在操作过程中产生的离心力并在圆周方向上排出它们。

8. 发明申请

US20080269237A1 CARBAMIC ACID COMPOUNDS COMPRISING A PIPERAZINE LINKAGE AS HDAC INHIBITORS 有权
标题翻译：包含作为HDAC抑制剂的哌嗪连接物的碳酸化合物
公开(公告)号：US20080269237A1
公开(公告)日：2008-10-30
申请号：US12165686
申请日：2008-07-01
申请人： Clare J. WATKINS , Maria-Rosario Romero-Martin , James Ritchie , Paul W. Finn , Ivars Kalvinsh , Einars Loza , Klara Dikovska , Igor Starchenkov , Daina Lolya , Vija Gailite
发明人： Clare J. WATKINS , Maria-Rosario Romero-Martin , James Ritchie , Paul W. Finn , Ivars Kalvinsh , Einars Loza , Klara Dikovska , Igor Starchenkov , Daina Lolya , Vija Gailite
IPC分类号： A61K31/506 , A61K31/495 , A61P35/00 , C12N9/99 , A61P25/28 , A61P25/16
CPC分类号： C07D213/74 , C07D239/42 , C07D295/185 , C07D295/192 , C07D295/26 , C07D317/58 , C07D333/60
摘要： This invention pertains to certain carbamic acid compounds which inhibit HDAC (histone deacetylase) activity of the following formula: The present invention also pertains to pharmaceutical compositions comprising such compounds, and the use of such compounds and compositions, both in vitro and in vivo, to inhibit HDAC, and in the treatment of conditions mediated by HDAC, cancer, proliferative conditions, psoriasis, etc.
摘要翻译：本发明涉及抑制下式的HDAC（组蛋白脱乙酰酶）活性的某些氨基甲酸化合物：本发明还涉及包含这些化合物的药物组合物，以及这些化合物和组合物在体外和体内的用途抑制HDAC，以及治疗由HDAC，癌症，增殖性病症，牛皮癣等介导的病症。

9. 发明申请

US20060105464A1 Quantitative determination of analyte 审中-公开
标题翻译：分析物的定量测定
公开(公告)号：US20060105464A1
公开(公告)日：2006-05-18
申请号：US10988069
申请日：2004-11-12
申请人： Jorg Friedrich Weber , John Rizzo , James Ritchie , Alan Berry , Allen Godwin
发明人： Jorg Friedrich Weber , John Rizzo , James Ritchie , Alan Berry , Allen Godwin
IPC分类号： G01N33/00
CPC分类号： G01N31/22 , C07C29/16 , Y10T436/200833
摘要： The invention relates to an analytical technique for the quantitative determination of an analyte and a reagent solution useful in said quantitative determination. The analytical technique is conveniently adapted for quantitative determination of carbonyl and even more particularly adapted for finishing an alcohol produced in the Oxo Process.
摘要翻译：本发明涉及用于定量测定所述定量测定中所用分析物和试剂溶液的分析技术。分析技术方便地适用于羰基的定量测定，甚至更特别适用于在Oxo方法中生产的醇。

10. 发明申请

US20050143385A1 Carbamic acid compounds comprising a piperazine linkage as hdac inhibitors 失效
公开(公告)号：US20050143385A1
公开(公告)日：2005-06-30
申请号：US10509732
申请日：2003-04-03
申请人： Clare Watkins , Maria-Rosario Romero-Martin , James Ritchie , Paul Finn , Ivars Kalvinsh , Einars Loza , Klar Dikovska , Igor Starchenkov , Daina Lolya , Vija Gailite
发明人： Clare Watkins , Maria-Rosario Romero-Martin , James Ritchie , Paul Finn , Ivars Kalvinsh , Einars Loza , Klar Dikovska , Igor Starchenkov , Daina Lolya , Vija Gailite
IPC分类号： C07D295/16 , A61K31/495 , A61K31/496 , A61K31/506 , A61P17/06 , A61P35/00 , A61P43/00 , C07D209/14 , C07D209/16 , C07D209/18 , C07D209/42 , C07D213/36 , C07D213/74 , C07D239/42 , C07D241/04 , C07D295/18 , C07D295/185 , C07D295/192 , C07D295/22 , C07D295/26 , C07D317/58 , C07D333/60 , C07D43/02
CPC分类号： C07D213/74 , C07D239/42 , C07D295/185 , C07D295/192 , C07D295/26 , C07D317/58 , C07D333/60
摘要： This invention pertains to certain carbamic acid compounds which inhibit HDAC (histone deacetylase) activity of the following formula: wherein: Cy is independently a cyclyl group; Q1 is independently a covalent bond or cyclyl leader group; the piperazin-1,4-diyl group is optionally substituted; J1 is independently a covalent bond or —C(═;O)—; J2 is independently —C(═O)— or —S(═O)2—; Q2 is independently an acid leader group; wherein: Cy is independently: C3-20carbocyclyl, C3-20heterocyclyl, or C5-20aryl; and is optionally substituted; Q1 is independently: a covalent bond; C1-7alkylene; or C1-7alkylene-X—C1-7alkylene, —X—C1-7alkylene, or C1-7alkylene-X—, wherein X is —O— or —S—; and is optionally substituted; Q2 is independently: C4-8alkylene; and is optionally substituted; and has a backbone length of at least 4 atoms; or: Q2 is independently: C5-20arylene; C5-20arylene-C1-7alkylene; C1-7alkylene-C5-20arylene; or, C1-7alkylene-C5-20arylene-C1-7alkylene; and is optionally substituted; and has a backbone length of at least 4 atoms; or a pharmaceutically acceptable salt, solvate, amide, ester, ether, chemically protected form, or prodrug thereof. The present invention also pertains to pharmaceutical compositions comprising such compounds, and the use of such compounds and compositions, both in vitro and in vivo, to inhibit HDAC, and in the treatment of conditions mediated by HDAC, cancer, proliferative conditions, psoriasis, etc.

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