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. 发明申请

US20050129508A1 Cooled turbine blade or vane 有权
标题翻译：冷却涡轮叶片或叶片
公开(公告)号：US20050129508A1
公开(公告)日：2005-06-16
申请号：US10949521
申请日：2004-09-27
申请人： Reinhard Fried , Hans Wettstein
发明人： Reinhard Fried , Hans Wettstein
IPC分类号： F01D5/18 , F01D5/14
CPC分类号： F01D5/187 , F05D2260/607
摘要： A turbine blade or vane (1) has a shell (2), including a first side wall (8) and a second side wall (9), which are connected together at a leading edge (10) and at a trailing edge (11), which extend longitudinally from a root (7) to a tip (6) and which are connected together between leading edge (10) and trailing edge (11) by a plurality of inner ribs (13). In the inner region (12) of the turbine blade/vane (1), the ribs (13) form at least one cooling gas path (15), which guides a cooling gas flow from the root (7) to the tip (6) and, in the process, is deflected a plurality of times in serpentine shape from the outside to the inside and from the inside to the outside. In order to increase the life of the turbine blade/vane (1), at least one bypass opening (18) and/or at least one outlet opening (19) are arranged in the region of at least one rib (13), which deflects the cooling gas flow from the outside to the inside, the bypass opening (18) penetrating the rib (13) at the shell (2) and the outlet opening (19) penetrating the shell (2).
摘要翻译：涡轮叶片或叶片（1）具有壳体（2），包括第一侧壁（8）和第二侧壁（9），它们在前缘（10）和后缘（11）处连接在一起），其从根部（7）纵向延伸到尖端（6），并且通过多个内肋（13）在前缘（10）和后缘（11）之间连接在一起。在涡轮叶片/叶片（1）的内部区域（12）中，肋（13）形成至少一个冷却气体通道（15），其将冷却气体流从根部（7）引导到尖端（6）），并且在该过程中，从外部到内部以及从内部到外部以蛇形形式偏转多次。为了增加涡轮叶片/叶片（1）的寿命，至少一个旁路开口（18）和/或至少一个出口开口（19）布置在至少一个肋（13）的区域中，其中将冷却气流从外部偏转到内部，旁路开口（18）穿过壳体（2）处的肋（13）并穿过壳体（2）的出口开口（19）。

2. 发明授权

US06276140B1 Device to generate energy through a turbo engine 失效
标题翻译：通过涡轮发动机产生能量的装置
公开(公告)号：US06276140B1
公开(公告)日：2001-08-21
申请号：US09486345
申请日：2000-07-07
申请人： Jakob J. Keller , Hans Wettstein
发明人： Jakob J. Keller , Hans Wettstein
IPC分类号： F01K2700
CPC分类号： F02C3/00 , F04F5/08
摘要： An apparatus for the generation of energy by means of a fluid-flow machine is described, for the drive of which a compressor arrangement for compressing a compressible medium, preferably air, is provided, which medium, via a feed-line system, can be fed to the fluid-flow machine directly or after the interposition of a combustion chamber, in which the compressed medium can be ignited with the addition of fuel. The invention is distinguished by the fact that the compressor arrangement provides at least one compressor stage, in which the medium can be compressed isothermally.
摘要翻译：描述了一种通过流体流动机器产生能量的装置，其驱动方式是用于压缩可压缩介质（优选为空气）的压缩机装置，哪种介质可通过进料管线系统直接或在插入燃烧室之后进入流体流动机，其中可以通过添加燃料来点燃压缩介质。本发明的特征在于压缩机装置提供至少一个压缩机级，其中介质可被等压压缩。

3. 发明授权

US5313782A Combined gas/steam power station plant 失效
标题翻译：联合燃气/蒸汽发电站厂房
公开(公告)号：US5313782A
公开(公告)日：1994-05-24
申请号：US127444
申请日：1993-09-10
申请人： Hans U. Frutschi , Alfred Hausermann , Hans Wettstein
发明人： Hans U. Frutschi , Alfred Hausermann , Hans Wettstein
IPC分类号： F01K7/18 , F01D13/00 , F01K23/08 , F01K23/10 , F02C3/14 , F02C6/00 , F02C6/02 , F02C6/18 , F02C7/143
CPC分类号： F01K23/106 , F02C6/003 , F05D2260/211 , Y02E20/16
摘要： In a combined gas/steam power station plant which consists essentially of a fossil-fired gas turbine group and a steam circuit, with an exhaust heat boiler (11) in between, intercooling and reheat are provided to maximize the efficiency. The gas turbine group consists of two compressors (1, 2), of two combustion chambers (7, 9) and of two turbines (8, 10). Downstream of the first compressor (1), there is an intercooler (3) and on the cool side of this is placed an evaporator (4) which is in effective connection with the intercooler. The steam quantity formed in the evaporator (4) is introduced into a turbine (6) of the steam circuit, the result of this being a first improvement in efficiency. Downstream of the first turbine (8), there is a second combustion chamber (9) in which the exhaust gases from the first turbine (8) are processed to produce hot gases for the second turbine (10) . The large calorific potential still present in the exhaust gases from this second turbine (10) flows through the exhaust heat boiler (11) in which a maximized steam power is produced, the result of which is the second improvement in efficiency.
摘要翻译：在基本上由化石燃烧的燃气轮机组和蒸汽回路组成的组合的气体/蒸汽发电站设备中，其间具有排气热锅炉（11），以提供中间冷却和再加热以使效率最大化。燃气轮机组由两个压缩机（1,2），两个燃烧室（7,9）和两个涡轮（8,10）组成。在第一压缩机（1）的下游，存在中间冷却器（3），并且在其冷却侧设置有与中间冷却器有效连接的蒸发器（4）。在蒸发器（4）中形成的蒸汽量被引入到蒸汽回路的涡轮（6）中，其结果是效率的第一改进。在第一涡轮机（8）的下游，存在第二燃烧室（9），其中处理来自第一涡轮机（8）的废气以产生用于第二涡轮机（10）的热气体。来自该第二涡轮机（10）的废气中仍然存在的大的热量潜在地流过其中产生最大蒸汽功率的排热热锅炉（11），其结果是效率的第二改进。

4. 发明申请

US20130036747A1 METHOD FOR COOLING A GAS TURBINE PLANT AND GAS TURBINE PLANT FOR IMPLEMENTING THE METHOD 有权
标题翻译：用于冷却气体涡轮机和用于实施方法的气体涡轮机的方法
公开(公告)号：US20130036747A1
公开(公告)日：2013-02-14
申请号：US13526324
申请日：2012-06-18
申请人： Herbert FUCHS , Anton NEMET , Hans WETTSTEIN
发明人： Herbert FUCHS , Anton NEMET , Hans WETTSTEIN
IPC分类号： F02C7/18 , F02C6/08
CPC分类号： F01D5/187 , F02C7/185 , F05D2260/202 , F05D2260/205
摘要： A method is provided for operating a gas turbine plant, in which compressed air is extracted from a compressor and for cooling is directed in an internal cooling passage through thermally loaded components to the combustion chamber and/or to the turbine, then re-cooled, and added to the compressor main flow in the compressor. At least a portion of the recirculated air is supersaturated, or partially saturated, with drops of water during or before recirculation into the compressor and a cooling mist is created. A gas turbine plant is provided with a closed cooling circuit which, for implementing the method, includes an injection arrangement for introducing water into the recirculated cooling air.
摘要翻译：提供了一种用于操作燃气轮机设备的方法，其中压缩空气从压缩机中抽出，并且用于冷却的内部冷却通道通过热负荷组件被引导到燃烧室和/或涡轮机，然后再冷却，并添加到压缩机中的压缩机主流。再循环空气的至少一部分在再循环进入压缩机期间或之后，在一滴水中过饱和或部分饱和，并产生冷却雾。燃气轮机设置有封闭的冷却回路，用于实施该方法包括用于将水引入再循环的冷却空气中的喷射装置。

5. 发明授权

US07263834B2 Method for cooling a gas turbine system and a gas turbine system for performing this method 有权
标题翻译：用于冷却燃气轮机系统和用于执行该方法的燃气轮机系统的方法
公开(公告)号：US07263834B2
公开(公告)日：2007-09-04
申请号：US09873373
申请日：2001-06-05
申请人： Wilhelm Reiter , Hans Wettstein
发明人： Wilhelm Reiter , Hans Wettstein
IPC分类号： F02C7/18 , F02C7/12
CPC分类号： F01D5/187 , F02C7/185 , F05D2260/202 , F05D2260/205
摘要： A gas turbine system comprises a compressor that takes in suction air on the inlet side and compresses it to compressor end air that is available on the outlet side, a combustor in which a fuel is burned by using the compressor end air while resulting in the formation of hot gas, as well as a turbine in which the hot gas is expanded while providing work output. In a method for cooling this gas turbine system, compressed air is removed from the compressor, is fed as cooling air for cooling inside an internal cooling channel through thermally loaded components of the combustor and/or the turbine, is then compressed and added to the compressor end air. An improved cooling without disadvantage for the efficiency of the system is achieved in that, in the manner of a targeted leakage, a small part of the cooling air is fed for film cooling into the turbine stream through drilled film cooling openings provided on the components.
摘要翻译：燃气轮机系统包括：压缩机，其吸入入口侧的吸入空气并将其压缩到出口侧可用的压缩机端部空气;燃烧器，其中通过使用压缩机端部空气燃烧燃料，同时导致形成的热气体，以及在提供工作输出的同时膨胀热气体的涡轮机。在用于冷却该燃气轮机系统的方法中，压缩空气从压缩机移除，作为冷却空气供入，用于通过燃烧器和/或涡轮机的热负载部件在内部冷却通道内进行冷却，然后被压缩并添加到压缩机末端空气。实现了对系统效率没有缺点的改进的冷却，其特征在于，以目标泄漏的方式，通过设置在部件上的钻孔薄膜冷却开口，将一小部分冷却空气供给到薄膜冷却到涡轮机流中。

6. 发明授权

US07037079B2 Axial-flow thermal turbomachine 有权
标题翻译：轴流热涡轮机
公开(公告)号：US07037079B2
公开(公告)日：2006-05-02
申请号：US10808493
申请日：2004-03-25
申请人： Hans Wettstein , Mohamed Nazmy , Claus Paul Gerdes
发明人： Hans Wettstein , Mohamed Nazmy , Claus Paul Gerdes
IPC分类号： F01D5/30
CPC分类号： F01D5/28 , F01D5/02 , F01D5/30 , F01D11/008 , F05D2300/50 , F05D2300/606
摘要： The invention relates to an axial-flow thermal turbomachine, having a rotor (1) made from a metallic material with a first density (D1), in which rotor blades (3, 3′) and intermediate pieces (4) are mounted alternately in a circumferential groove. It is characterized in that said intermediate pieces (4) consist of a material with a second density (D2), which is lower than the first density (D1). Particularly suitable materials for the intermediate pieces (4) are intermetallic compounds, preferably intermetallic γ-titanium aluminide alloys or intermetallic orthorhombic titanium aluminide alloys, but also titanium alloys.
摘要翻译：本发明涉及一种轴流式热涡轮机，其具有由第一密度（D 1> 1）的金属材料制成的转子（1），其中转子叶片（3,3'）和中间体片（4）交替地安装在周向槽中。其特征在于，所述中间件（4）由低于第一密度（D SUB 1）的第二密度（D 2 2 N）的材料组成。用于中间件（4）的特别合适的材料是金属间化合物，优选金属间化合物的γ-钛铝化物合金或金属间斜方晶钛铝化物合金，也包括钛合金。

7. 发明申请

US20060073019A1 AXIAL-FLOW THERMAL TURBOMACHINE 有权
标题翻译：轴流热涡轮机
公开(公告)号：US20060073019A1
公开(公告)日：2006-04-06
申请号：US10808492
申请日：2004-03-25
申请人： Hans Wettstein , Mohamed Nazmy , Claus Gerdes
发明人： Hans Wettstein , Mohamed Nazmy , Claus Gerdes
IPC分类号： B64C11/16
CPC分类号： F01D5/20 , F01D5/28 , F01D21/04 , F05D2240/30 , F05D2300/50
摘要： The invention relates to an axial-flow thermal turbomachine having a metallic rotor (1), in which rotor blades (3) made of an intermetallic compound are mounted in a circumferential groove to form a row of blades. The invention is characterized in that at least two rotor blades (3′) which are at a uniform distance from one another and are made of a more ductile material are arranged in the said row of blades between the intermetallic rotor blades (3), the rotor blades (3′) made of the more ductile material either being considerably longer than the intermetallic blades (3) or, if they are of the same length, having a different blade tip shape than the intermetallic blades (3).
摘要翻译：本发明涉及一种具有金属转子（1）的轴流式热涡轮机，其中由金属间化合物制成的转子叶片（3）安装在圆周槽中以形成一排叶片。本发明的特征在于，在金属间转子叶片（3）之间的所述一排叶片中布置有至少两个彼此处于相同距离并由更具延展性的材料制成的转子叶片（3'），由更韧性材料制成的转子叶片（3'）比金属间叶片（3）长得多，或者如果它们具有相同长度，则具有与金属间叶片（3）不同的叶片尖端形状。

8. 发明授权

US06886344B2 Method for the operation of a power plant 有权
标题翻译：发电厂运行方法
公开(公告)号：US06886344B2
公开(公告)日：2005-05-03
申请号：US10808487
申请日：2004-03-25
申请人： Hans Ulrich Frutschi , Timothy Griffin , Hans Wettstein , Dieter Winkler
发明人： Hans Ulrich Frutschi , Timothy Griffin , Hans Wettstein , Dieter Winkler
IPC分类号： F02C3/20 , F02C3/34 , F25J3/04 , F02C1/08
CPC分类号： F25J3/04636 , C10J2300/1823 , F02C3/20 , F02C3/34 , F25J3/04533 , F25J2205/80 , F25J2210/50 , F25J2240/70 , Y02E20/344 , Y02P20/129 , Y02P20/152
摘要： In a method for the operation of a power plant with a closed or quasi-closed cycle, the power plant substantially comprises at least one compressor unit (1) or a pump, at least one combustion chamber (2), at least one turbine (3) and at least one heat sink (4). In the combustion chamber (2), a fuel mass flow (14) reacts with at least one oxygen flow (12), the excess combustion products which are formed as a result (CO2, H2O) are removed from the cycle at a suitable location (5, 6), and the oxygen stream (12) fed to the combustion chamber is obtained by means of an air fractionation installation (11). Means (9) for coarse fractionation of the supplied air (8) are connected upstream of the air fractionation installation (11) in order to supply oxygen-enriched air (10) to the air fractionation installation (11).
摘要翻译：在用于操作具有封闭或准闭合循环的发电厂的方法中，发电厂基本上包括至少一个压缩机单元（1）或泵，至少一个燃烧室（2），至少一个涡轮机 3）和至少一个散热器（4）。在燃烧室（2）中，燃料质量流（14）与至少一个氧气流（12）反应，作为结果形成的过量燃烧产物（CO 2，H _{2 O）在合适位置（5,6）从循环中除去，并且通过空气分馏装置（11）获得供给到燃烧室的氧气流（12）。为了向空气分馏装置（11）供给富氧空气（10），在空气分馏装置（11）的上游连接供给空气（8）的粗分馏装置（9）。}

9. 发明授权

US6098009A Method and device for controlling turbomachines 失效
标题翻译：用于控制涡轮机的方法和装置
公开(公告)号：US6098009A
公开(公告)日：2000-08-01
申请号：US956046
申请日：1997-10-22
申请人： Hans Wettstein
发明人： Hans Wettstein
IPC分类号： F01D17/00 , F02C9/00 , F02C9/28 , G05B9/03
CPC分类号： F02C9/28 , F05D2270/053
摘要： A method of controlling turbomachines is specified, a characteristic signal, in particular a performance signal, normally being fed to the controller as a controlled variable, but this performance signal, together with a number of further signals significant of the performance from the plant circuit, forming a signal set in a comparison and selection unit, and the signals from this signal set being compared with one another. The maximum selection among the signals, formed at the same time in the comparison and selection unit 2.1, yields the signal of the controlled variable that is forwarded to the controller 1.1. In addition, monitoring as to whether the performance signal is the maximum signal is performed. In addition, a device for controlling turbomachines according to the method is specified, which device has a control loop 1 for the output of actuating signals for control devices of the plant, the control loop 1 being preceded by a monitoring loop 2 that has a comparison and selection unit 2.1, to which, apart from the performance signal of the control loop 1, at least one further signal significant of the performance is additionally applied, and all these applied signals form a signal set. The comparison and selection unit 2.1 determines the maximum signal from these signal set and the said maximum signal is applied as input signal to a controller 1.1 of the control loop 1 in place of the direct performance signal.
摘要翻译：规定了一种控制涡轮机的方法，特征信号，特别是性能信号，通常作为受控变量馈送到控制器，但是该性能信号连同许多来自工厂电路的性能的进一步信号，在比较和选择单元中形成信号组，并将来自该信号组的信号彼此进行比较。在比较和选择单元2.1中同时形成的信号中的最大选择产生被转发到控制器1.1的受控变量的信号。此外，执行关于性能信号是否是最大信号的监视。此外，规定了根据该方法控制涡轮机的装置，该装置具有用于输出工厂控制装置的致动信号的控制回路1，控制回路1之前是具有比较的监控回路2 和选择单元2.1，除了控制回路1的执行信号之外，附加地施加至少一个对性能有重要影响的另外的信号，并且所有这些应用的信号形成信号组。比较选择单元2.1确定来自这些信号组的最大信号，并且将所述最大信号作为输入信号施加到控制回路1的控制器1.1以代替直接性能信号。

10. 发明授权

US5993155A Cooled gas-turbine blade 失效
标题翻译：冷却燃气轮机叶片
公开(公告)号：US5993155A
公开(公告)日：1999-11-30
申请号：US34231
申请日：1998-03-04
申请人： Wilhelm Endres , Hans Wettstein
发明人： Wilhelm Endres , Hans Wettstein
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/18 , F05D2260/205 , F05D2260/2322
摘要： A gas-turbine blade of solid construction and having cooling passages is specified, which cooling passages run in its interior and through which the cooling medium flows essentially from the blade root through the gas-turbine blade (100), these cooling passages (20) having a relatively small cross section in relation to the blade thickness and being arranged so as to run close to the lateral surface (100.1) of the gas-turbine blade (100), and the cooling-medium feed and discharge being effected in the base (60) of the gas-turbine blade (100).
摘要翻译：规定了具有冷却通道的固体结构并具有冷却通道的燃气轮机叶片，这些冷却通道在其内部运行，冷却介质通过该涡轮叶片叶片根本通过燃气轮机叶片（100）流动，这些冷却通道（20）具有相对于叶片厚度的相对小的横截面并且被布置成靠近燃气轮机叶片（100）的侧表面（100.1）延伸，并且冷却介质进料和排出在基部（60）的燃气轮机叶片（100）。

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