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71. 发明公开

EP1654440A1 GASTURBINE MIT EINEM DICHTUNGSELEMENT ZWISCHEN LEITSCHAUFELKRANZ UND LAUFSCHAUFELKRANZ DES TURBINENTEILS 有权
标题翻译：与所述叶片环的密封元件或动涡轮部件的叶片环GEAR燃气轮机
公开(公告)号：EP1654440A1
公开(公告)日：2006-05-10
申请号：EP04740664.0
申请日：2004-07-05
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D11/00 , F01D25/12
CPC分类号： F01D11/001 , F01D11/005
摘要： The invention relates to a gas turbine (1). The aim of the invention is to provide an axial sealing between a vane ring (11) and a moving blade ring (13), which has an excellent sealing effect, is easy to install and inexpensive to produce. For this purpose, a sealing element (35) is used that extends across at least a fourth of the hot gas channel circumference. Preferably, said sealing element extends across approximately half the circumference and is inserted in grooves of the vane support (79) and the vane platforms.

72. 发明公开

EP1636526A1 BRENNKAMMER 有权
公开(公告)号：EP1636526A1
公开(公告)日：2006-03-22
申请号：EP04729621.5
申请日：2004-04-27
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： HUTH, Michael , TIEMANN, Peter
IPC分类号： F23R3/00
CPC分类号： F23R3/005
摘要： The invention relates to a combustion chamber (4) of a gas turbine (1), inside of which a supplied fuel is reacted with supplied combustion air in order to produce a working medium (M). The inside of the combustion chamber wall (24) is provided with a lining formed from a number of heat shield elements (26). The or each heat shield element (26), together with the combustion chamber wall (24), forms an interior space (27) that can be subjected to the action of a coolant (K). The aim of the invention is to provide a combustion chamber with a comparatively simple design that has a high system efficiency. To this end, the invention provides that a flow element (49) is placed in the respective interior space (27) while serving to effect a locally specific control of the flow of coolant.
摘要翻译：燃气轮机（1）的燃烧室（4）技术领域本发明涉及一种燃气轮机（1）的燃烧室（4），在该燃烧室内供给的燃料与供给的燃烧空气反应以产生工作介质（M）。燃烧室壁（24）的内部设置有由多个隔热元件（26）形成的衬里。该或每个热屏元件（26）与燃烧室壁（24）一起形成能够经受冷却剂（K）的作用的内部空间（27）。本发明的目的是为燃烧室提供具有高系统效率的相对简单的设计。为此，本发明提供了一种流量元件（49），其被放置在相应的内部空间（27）中，同时用于实现对冷却剂流的局部特定控制。

73. 发明公开

EP1423586A1 BRENNKAMMERZWISCHENSTÜCK FÜR GASTURBINE 有权
标题翻译：燃烧ZWISCHENSTÜCK燃气轮机
公开(公告)号：EP1423586A1
公开(公告)日：2004-06-02
申请号：EP02797639.8
申请日：2002-08-28
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D9/02
CPC分类号： F01D9/023 , Y02T50/675
摘要： The invention relates to a gas turbine (1) having a combustion chamber arrangement and a turbine chamber (2) connected downstream of said combustion chamber arrangement, wherein the combustion chamber arrangement includes a plurality of individual combustion chambers (3) formed by input areas (4) and transition areas (5) converging in an annular gap leading to the turbine chamber and wherein the longitudinal axes (B) of the individual combustion chambers are placed at an angle relative to an engine axis (M) that is defined by the axial extension of the turbine chamber (2). In order to improve said gas turbine by visibly reducing the thermal and mechanical loads of the individual combustion chambers in the transition area so that cooling requirements can be lowered in said area, the transition area (5) of at least one individual combustion chamber (3) and a corresponding input area (9) of the turbine chamber (2) are embodied in such a way that the gas flow running from the at least one individual combustion chamber (3) into the turbine chamber (2) is deflected in the direction of the engine axis (M) and substantially in the input area (9) of the turbine chamber (2).

74. 发明授权

EP1276972B1 TURBINE 有权
标题翻译：涡轮
公开(公告)号：EP1276972B1
公开(公告)日：2004-04-14
申请号：EP01911696.1
申请日：2001-02-23
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D11/00 , F01D5/22
CPC分类号： F01D11/005 , F01D5/22
摘要： The invention relates to a turbine (6), especially a gas turbine. According to the invention, a sealing element (44) with a receiving area (50) is provided for sealing the guide blades (18) which are adjacent to each other in the peripheral direction (36) of the turbine (6). The foot plates (21) of the guide blades (18) extend into said receiving area. The edge area of the foot plates (21) does not have to be reinforced compared to a conventional seal, which enables the entire foot plate to be cooled homogeneously. A closed cooling system (62) can therefore be used for cooling, especially with steam.
摘要翻译：本发明涉及一种涡轮机（6），特别是燃气涡轮机。根据本发明，提供具有容纳区域（50）的密封元件（44），用于密封在涡轮机（6）的周向方向（36）上彼此相邻的导向叶片（18）。导向叶片（18）的脚踏板（21）延伸到所述接收区域中。与常规密封件相比，脚踏板（21）的边缘区域不必被增强，这使得整个脚踏板能够被均匀地冷却。封闭的冷却系统（62）因此可以用于冷却，特别是用于蒸汽。

75. 发明授权

EP1165939B1 KÜHLMITTELDURCHSTRÖMTE, GEGOSSENE GASTURBINENSCHAUFEL SOWIE VORRICHTUNG UND VERFAHREN ZUR HERSTELLUNG EINES VERTEILERRAUMS DER GASTURBINENSCHAUFEL 有权
标题翻译：冷却剂流经，CAST燃气轮机叶片和器件及其制造方法的燃气涡轮叶片分布的区域
公开(公告)号：EP1165939B1
公开(公告)日：2003-08-13
申请号：EP00920564.2
申请日：2000-03-23
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D5/08
CPC分类号： F01D5/3007 , F01D5/087
摘要： The invention relates to a cast gas turbine blade (1) that is flown through by a coolant. Said gas turbine blade (1) comprises a footing of the blades (2) which is provided with several supply channels (4) and a distribution chamber (5). A coolant can be fed to the supply channels (4) by means of a feeding channel (6) of the disc (3). The feeding channel (6) communicates with the supply channels (4) via the distribution chamber (5). The aim of the invention is to optimise the flow and the production of said gas turbine blade (1). To this end, a cast distribution chamber (5) is provided that has supply channels (4) which are provided with rounded or flattened admission openings (7). The cast distribution chamber (5) is produced by a one-piece casting core.

76. 发明公开

EP1320661A1 GASTURBINENSCHAUFEL 有权
公开(公告)号：EP1320661A1
公开(公告)日：2003-06-25
申请号：EP01980405.3
申请日：2001-09-18
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F05D2260/201
摘要： The invention relates to a gas turbine blade (1) having a combined convective cooling effected by a meandering cooling channel (21) and having an impact cooling effected via an impact cooling insert (37). The impact cooling insert (37) is arranged inside a first partial section (23) of the meandering cooling channel (21) extending along the front edge (8) of the blade pan. The impact cooling insert (37) tapers along this first partial section (23).
摘要翻译：本发明涉及一种燃气涡轮机叶片（1），其具有由弯曲冷却通道（21）实现的组合对流冷却并且具有经由冲击冷却插入件（37）实现的冲击冷却。冲击冷却插入件（37）布置在沿着刀盘的前边缘（8）延伸的曲折冷却通道（21）的第一局部区段（23）内。冲击冷却插入件（37）沿着该第一局部区段（23）渐缩。

77. 发明公开

EP1292760A1 KONFIGURATION EINER KÜHLBAREN TURBINENSCHAUFEL 有权
标题翻译：配置的冷却的涡轮叶片
公开(公告)号：EP1292760A1
公开(公告)日：2003-03-19
申请号：EP01949387.3
申请日：2001-06-08
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter , STRASSBERGER, Michael
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , B22C9/10 , F05D2260/20 , F05D2260/22141
摘要： The invention relates to a turbine blade (1) through which cooling liquid flows and which comprises several flow channels (4, 5, 6) that are adjacently arranged in the flowing-off direction (2) of the working fluid (3). Said flow channels (4, 5, 6) extend between inflow openings (7, 8, 9), which are located on a radially inner blade foot (10), and outflow openings (11, 12, 13), which are situated opposite the blade foot in a more radially outer manner. The flow channels (4, 5, 6) extend such that the local radial flow components (15) of the resulting cooling fluid stream (14) are directed outward in a, for the most part, predominantly radial manner. A flow channel (4), which is in the front when viewing in the flowing-off direction (2), is provided whose outflow openings (11) are placed inside a touching edge (16) of the turbine blade (1). In addition, at least one rear edge channel (5, 6) is provided whose associated resulting cooling fluid stream (14) additionally comprises local cross-flow components (17) and whose outflow openings (12, 13) are placed inside a rear edge (16) of the turbine blade (1).

78. 发明公开

EP1257373A1 VORRICHTUNG UND VERFAHREN ZUM GIESSEN EINES WERKSTÜCKS UND WERKSTÜCK 有权
标题翻译：装置和方法用于铸造工件和工作
公开(公告)号：EP1257373A1
公开(公告)日：2002-11-20
申请号：EP01921269.5
申请日：2001-01-31
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： B22C9/10
CPC分类号： B22C9/10 , B22D25/005
摘要： The invention relates to a device for casting a workpiece, especially a turbine blade with inner cooling, comprising a casting cavity (1) in which casting cores (2) which produce channels (3) that pass through the workpiece are provided. The aim of the invention is to improve a device of this type in such a way that there are no poorly cooled areas present in the workpiece. To this end, the casting cores (2) are placed in the casting cavity (1) in such a way that they rest against each other loosely.

79. 发明授权

EP1000224B1 KÜHLLUFTVERTEILUNG IN EINER TURBINENSTUFE EINER GASTURBINE 失效
标题翻译：冷却配风涡轮级的燃气涡轮机
公开(公告)号：EP1000224B1
公开(公告)日：2002-10-02
申请号：EP98947313.7
申请日：1998-07-20
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter , MILAZAR, Mirko
IPC分类号： F01D5/08
CPC分类号： F01D11/24 , F01D25/12 , F02C7/18
摘要： The invention relates to a cooling device for cooling a first stage (2) of a gas turbine (1) with a first guide blade (3) and a first moving blade (4), using air. The inventive device comprises a first cooling air supply (15) which is located on the guide blade (3) to be cooled and a second cooling air supply (17) for cooling the first stage, said second cooling air supply (17) being located downstream from the first cooling air supply (15).

80. 发明公开

EP1165939A1 KÜHLMITTELDURCHSTRÖMTE, GEGOSSENE GASTURBINENSCHAUFEL SOWIE VORRICHTUNG UND VERFAHREN ZUR HERSTELLUNG EINES VERTEILERRAUMS DER GASTURBINENSCHAUFEL 有权
标题翻译：冷却剂流经，CAST燃气轮机叶片和器件及其制造方法的燃气涡轮叶片分布的区域
公开(公告)号：EP1165939A1
公开(公告)日：2002-01-02
申请号：EP00920564.2
申请日：2000-03-23
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： TIEMANN, Peter
IPC分类号： F01D5/08
CPC分类号： F01D5/3007 , F01D5/087
摘要： The invention relates to a cast gas turbine blade (1) that is flown through by a coolant. Said gas turbine blade (1) comprises a footing of the blades (2) which is provided with several supply channels (4) and a distribution chamber (5). A coolant can be fed to the supply channels (4) by means of a feeding channel (6) of the disc (3). The feeding channel (6) communicates with the supply channels (4) via the distribution chamber (5). The aim of the invention is to optimise the flow and the production of said gas turbine blade (1). To this end, a cast distribution chamber (5) is provided that has supply channels (4) which are provided with rounded or flattened admission openings (7). The cast distribution chamber (5) is produced by a one-piece casting core.

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