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21. 发明授权

EP3077644B1 VERFAHREN ZUR REGELUNG EINER GASTURBINE 失效转让
公开(公告)号：EP3077644B1
公开(公告)日：2018-05-23
申请号：EP15700375.7
申请日：2015-01-14
申请人： Siemens Aktiengesellschaft
发明人： LARSON, Marco , SAVILIUS, Nicolas
IPC分类号： F02C9/28
CPC分类号： F02C9/28 , F02C3/04 , F02C9/26 , F05D2220/32 , F05D2270/10 , F05D2270/14 , F05D2270/301 , F05D2270/44

22. 发明授权

EP2946096B1 VERFAHREN ZUM BETREIBEN EINER GASTURBINE UNTERHALB IHRER NENNLEISTUNG 有权转让
公开(公告)号：EP2946096B1
公开(公告)日：2017-06-28
申请号：EP14707344.9
申请日：2014-02-12
申请人： Siemens Aktiengesellschaft
发明人： ENGLER, Thorsten , GORYNSKI, Markus , GUTERMUTH, Manuel , KREUTZER, Philipp , LINK, Marco , SAVILIUS, Nicolas , SÜSELBECK, Kai , TERTILT, Marc
IPC分类号： F02C9/22 , F02C9/28
CPC分类号： F02C9/20 , F02C3/04 , F02C9/22 , F02C9/28 , F05D2220/32 , F05D2270/05 , F05D2270/08 , F05D2270/303

23. 发明授权

EP2956630B1 GASTURBINE UND VERFAHREN ZUM BETREIBEN DER GASTURBINE 失效转让
标题翻译：燃气轮机和一种用于运行燃气涡轮机
公开(公告)号：EP2956630B1
公开(公告)日：2017-04-12
申请号：EP14707697.0
申请日：2014-02-20
申请人： Siemens Aktiengesellschaft
发明人： ENGLER, Thorsten , GORYNSKI, Markus , GUTERMUTH, Manuel , KREUTZER, Philipp , LINK, Marco , SAVILIUS, Nicolas , SÜSELBECK, Kai , TERTILT, Marc
IPC分类号： F02C7/057 , F01D25/02 , F01D17/08 , F01D17/16
CPC分类号： F01D17/16 , F01D9/041 , F01D17/08 , F01D17/085 , F01D25/02 , F02C7/04 , F02C7/057 , F05D2220/32 , F05D2240/12 , F05D2270/301 , F05D2270/303 , F05D2270/311

24. 发明公开

EP2964930A1 VERFAHREN ZUR REDUZIERUNG DER CO-EMISSIONEN EINER GASTURBINE SOWIE GASTURBINE 有权转让
公开(公告)号：EP2964930A1
公开(公告)日：2016-01-13
申请号：EP14707726.7
申请日：2014-02-27
申请人： Siemens Aktiengesellschaft
发明人： SAVILIUS, Nicolas
IPC分类号： F02C7/08 , F02C9/00
CPC分类号： F02C7/10 , F02C3/04 , F02C7/08 , F02C9/00 , F05D2220/32 , F05D2270/08 , F05D2270/303 , F05D2270/332 , Y02E20/16
摘要： A method for reducing the CO emissions of a gas turbine (1), having a compressor (6), having a turbine (10) and having an air preheater (22) positioned upstream of the compressor (6), is intended to permit technically simpler regulation without losses in terms of the quality of the reduction of the CO emissions. For this purpose, the heat transfer power of the air preheater (22) is regulated on the basis of a minimum value for the inlet temperature of the compressor (4), wherein the minimum value is predefined as a function of the absolute power of the gas turbine (1).
摘要翻译：一种用于减少具有位于压缩机上游的压缩机，涡轮机和空气预热器的燃气轮机的CO排放的方法，其允许技术上更简单的调节，而在CO排放的减少质量方面没有损失。基于压缩机的入口温度的最小值来调节空气预热器的传热功率，其中最小值被预先定义为燃气轮机的绝对功率的函数。

25. 发明公开

EP2946096A1 VERFAHREN ZUM BETREIBEN EINER GASTURBINE UNTERHALB IHRER NENNLEISTUNG 有权转让
公开(公告)号：EP2946096A1
公开(公告)日：2015-11-25
申请号：EP14707344.9
申请日：2014-02-12
申请人： Siemens Aktiengesellschaft
发明人： ENGLER, Thorsten , GORYNSKI, Markus , GUTERMUTH, Manuel , KREUTZER, Philipp , LINK, Marco , SAVILIUS, Nicolas , SÜSELBECK, Kai , TERTILT, Marc
IPC分类号： F02C9/22 , F02C9/28
CPC分类号： F02C9/20 , F02C3/04 , F02C9/22 , F02C9/28 , F05D2220/32 , F05D2270/05 , F05D2270/08 , F05D2270/303
摘要： The invention relates to a method for operating a gas turbine (10) below the nominal power thereof, comprising the following steps: determining a lower power threshold value (P1@TATK=const. ) of the gas turbine (10) as the power threshold value from which additional lowering of the output gas turbine power causes the gas turbine to leave a CO-emission-compliant partial load range of the gas turbine (10); providing a specified threshold value (p
2 ) for an output gas turbine power, wherein the specified threshold value (p2) is less than the nominal power of the gas turbine; and operating the gas turbine (10) at an output gas turbine power above the specified threshold value (p2) at a constant exhaust gas temperature, wherein the inlet guide blades (13) of a compressor (12) of the gas turbine are closed further in order to reduce the output gas turbine power. In order to avoid larger temperature gradients in the preparation of an especially low partial load operation of the gas turbine (10), a sufficiently large valve is selected for the specified threshold value (p2) that the increases of the primary zone temperature, the combustion temperature, and the exhaust temperature extend over a CO-emission-compliant partial load range of the gas turbine (10) that is as large as possible.
摘要翻译：本发明涉及一种用于在其额定功率以下操作燃气轮机（10）的方法，包括以下步骤：确定燃气轮机（10）的较低功率阈值（P1 @ TATK =常数）作为功率阈值输出燃气轮机功率的额外降低导致燃气轮机离开燃气轮机（10）的符合CO排放的部分负载范围的值; 提供用于输出燃气涡轮机功率的指定阈值（p 2），其中所述指定阈值（p 2）小于所述燃气涡轮机的所述标称功率; 以及在恒定排气温度下以高于所述特定阈值（p2）的输出燃气涡轮机功率操作所述燃气涡轮机（10），其中所述燃气涡轮机的压缩机（12）的所述入口导向叶片（13）进一步关闭以减少输出燃气轮机的功率。为了避免在燃气轮机（10）的特别低的部分负荷运行的准备中出现较大的温度梯度，针对规定的阈值（p2）选择足够大的阀，使得主要区域温度，燃烧温度和排气温度在燃气涡轮机（10）的符合CO排放的部分负荷范围内延伸，所述部分负荷范围尽可能大。

26. 发明公开

EP2809994A2 HITZESCHILDELEMENT FÜR EINEN VERDICHTERLUFTBYPASS UM DIE BRENNKAMMER 有权
标题翻译：挡热元件用于压缩机空气旁通燃烧室
公开(公告)号：EP2809994A2
公开(公告)日：2014-12-10
申请号：EP13712711.4
申请日：2013-03-12
申请人： Siemens Aktiengesellschaft
发明人： BENKLER, Francois , BRANDENBURG, Thomas , DEISS, Olga , GRIEB, Thomas , LINK, Marco , SAVILIUS, Nicolas , VOGTMANN, Daniel , WILKES, Jan
IPC分类号： F23R3/00 , F23M5/00
CPC分类号： F23R3/08 , F23R3/005 , F23R3/007 , F23R3/50 , F23R3/60 , F23R2900/03042
摘要： The invention relates to a heat-shield element (14), in particular for lining a combustion-chamber wall (13), comprising a first wall (17) with a hot side (18) which can be loaded with a hot medium, a cold side (19) which lies opposite the hot side (18), and a circumferential edge (24) which extends on a first (20), a second (21) and a third narrow side (22) of the first wall (17) beyond the cold side (19) substantially as far as a first height (25), wherein the circumferential edge (24) extends on a fourth narrow side (23) as far as a second height (26) which is smaller than the first height (25), and wherein, substantially at the second height (26), a second wall (27) lies opposite the cold side (19) and extends over the width of the fourth narrow side (23) from the fourth narrow side (23) over a part of the length of the narrow sides (20, 22) which adjoin the fourth narrow side (23), wherein the second wall (27) has an edge (29) at the end (28) thereof which faces away from the fourth narrow side (23), which edge (29) extends as far as the first height (25). Furthermore, the invention relates to a combustion chamber and to a gas turbine.

27. 发明授权

EP2588806B1 Brennermodul 有权转让
公开(公告)号：EP2588806B1
公开(公告)日：2014-08-20
申请号：EP11720444.6
申请日：2011-05-16
申请人： Siemens Aktiengesellschaft
发明人： HASE, Matthias , SAVILIUS, Nicolas , SCHNEIDER, Oliver
IPC分类号： F23D14/24 , F23D14/08 , F23R3/28 , F23D14/02
CPC分类号： F23D14/24 , F23D14/02 , F23D2900/00012 , F23R3/286

28. 发明公开

EP2411631A1 DICHTPLATTE UND LAUFSCHAUFELSYSTEM 有权
标题翻译：密封板和刀片系统
公开(公告)号：EP2411631A1
公开(公告)日：2012-02-01
申请号：EP10713877.8
申请日：2010-03-25
申请人： Siemens Aktiengesellschaft
发明人： BUCHAL, Tobias , DUNGS, Sascha , ESSER, Winfried , GRÜGER, Birgit , LÜSEBRINK, Oliver , MILAZAR, Mirko , SAVILIUS, Nicolas , SCHNEIDER, Oliver , SCHRÖDER, Peter , SOCHA, Waldemar
IPC分类号： F01D5/30 , F01D11/00
CPC分类号： F01D5/3015 , F01D11/005 , F05D2230/232
摘要： Sealing plate (40) comprises a number of sheets (50) with two opposite-lying sheets arranged parallel to the plate plane (49). An independent claim is also included for a rotor blade system with the sealing plate; and #Gas turbine with the rotor blade system. Preferred Features: An intermediate sheet (52) with a number of recesses (56) is arranged between the sheets. Each sheet has a number of cooling air holes (58).

29. 发明公开

EP2342427A1 AXIAL SEGMENTIERTER LEITSCHAUFELTRÄGER FÜR EINE GASTURBINE 有权
标题翻译： AXIAL分段式导向叶片的燃气轮机
公开(公告)号：EP2342427A1
公开(公告)日：2011-07-13
申请号：EP09824439.5
申请日：2009-09-10
申请人： Siemens Aktiengesellschaft
发明人： BRYK, Roderich , DUNGS, Sascha , SAVILIUS, Nicolas , HARTMANN, Martin , KAHLSTORF, Uwe , KLEIN, Karl , LÜSEBRINK, Oliver , MILAZAR, Mirko , SCHNEIDER, Oliver , SHENG, Shilun , SHEVCHENKO, Vadim , SIMON, Gerhard , THAMM, Norbert
IPC分类号： F01D9/04 , F01D25/24
CPC分类号： F01D9/041 , F01D25/246
摘要： A guide vane mount (1), in particular for a gas turbine (101), comprising a number of axial segments (24), is to allow a simpler design technically and a more flexible adaptation to the temperature profile present on the guide vane mount in order to maintain operational safety. Therefore, at least one axial segment (24) is to be designed as a grid structure (26).

30. 发明公开

EP2242909A1 TURBOMASCHINENROTOR MIT EINER VORSPANNEINRICHTUNG ZUM VORSPANNEN EINER LAUFSCHAUFEL 有权
标题翻译： TURBOMASCHINEN转子，对于这样的TURBOMASCHINEN转子动叶片对应的汇编方法
公开(公告)号：EP2242909A1
公开(公告)日：2010-10-27
申请号：EP09709892.5
申请日：2009-01-23
申请人： Siemens Aktiengesellschaft
发明人： BENKLER, Francois , BETTENTRUP, Jörn , DEISTER, Frank , KÜPERKOCH, Rudolf , SAVILIUS, Nicolas , SCHNEIDER, Oliver , WISTUBA, Dirk
IPC分类号： F01D5/30
CPC分类号： F01D5/3092 , F01D5/323 , F01D5/326 , Y10T29/49826
摘要： The invention relates to a turbomachine rotor (1) comprising a rotor blade (2) provided with a blade base (4), a wheel disk (16) with a groove (17) in which the blade base (4) engages such that the rotor blade (2) is maintained in the groove in a positive fit in the radial direction, and a pretensioning device (7-14, 19,28) that is supported on the wheel disk as well as on the blade base (4) and that exerts a pretensioning force on the blade base (4) in the radial direction. Said pretensioning device (7-14, 19,28) is designed in such a manner that the pretensioning force can be adjusted when the turbomachine rotor (1) is in the assembled state.

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