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1. 发明申请

WO2008068109A1 TURBINE 审中-公开
标题翻译：涡轮
公开(公告)号：WO2008068109A1
公开(公告)日：2008-06-12
申请号：PCT/EP2007/061191
申请日：2007-10-19
申请人： SIEMENS AKTIENGESELLSCHAFT , SENIOR, Peter
发明人： SENIOR, Peter
IPC分类号： F01D1/02 , F01D9/04 , F01D9/02
CPC分类号： F01D1/023 , F01D9/023 , F01D9/041 , F01D25/24 , F02C3/045 , F05D2220/50 , F05D2250/82 , Y02T50/673 , Y02T50/675
摘要： A turbine (8), comprising a turbine section being surrounded by a turbine casing (22), a turbine rotor (10) with turbine blades (19) extending at least through the turbine section, a turbine stator with stator blades (18), a turbine annulus (21) inside the turbine casing (22) around the turbine rotor (10) and at least two combustors (6) and a corresponding number of exhaust diffuser channels (14), where the stator blades extend over less than 360 degrees and define flowing (20) and non flowing sectors of the annulus with the flowing sectors (20) coinciding with the annular sector over which the stator blades (18) extend, and where the necessary flow area in the turbine annulus (21) for hot gas passing through a turbine blading (18, 19) and driving the turbine (8) is concentrated into said flowing sectors (20) of the annulus (21).
摘要翻译：一种涡轮机（8），包括由涡轮机壳体（22）包围的涡轮机部分，具有至少延伸通过涡轮部分的涡轮机叶片（19）的涡轮机转子（10），具有定子叶片（18）的涡轮机定子，涡轮机壳体（22）内的涡轮机环（21）和涡轮转子（10）周围的至少两个燃烧器（6）和相应数量的排气扩散器通道（14），其中定子叶片延伸超过360度并且限定所述环形的流动（20）和非流动扇区，其中所述流动扇区（20）与所述定子叶片（18）所延伸的所述环形扇区重合，并且所述涡轮机环（21）中用于热的必需流动面积通过涡轮叶片（18,19）并驱动涡轮机（8）的气体被集中到环形空间（21）的所述流动扇区（20）中。

2. 发明申请

WO1998021527A1 COMBUSTOR ARRANGEMENT 审中-公开
标题翻译： COMBUSTOR安排
公开(公告)号：WO1998021527A1
公开(公告)日：1998-05-22
申请号：PCT/GB1997003085
申请日：1997-11-10
申请人： EUROPEAN GAS TURBINES LIMITED , SENIOR, Peter , MAIDHOF, Sebastian
发明人： EUROPEAN GAS TURBINES LIMITED
IPC分类号： F23R03/50
CPC分类号： F23R3/286 , F23R3/12 , F23R3/34 , F23R3/50 , Y02T50/675
摘要： A combustor (30) for a gas turbine engine comprises an annular combustion chamber (31) having radially outer and inner rows of fuel injectors (19 , 20 ) disposed concentrically in the combustor head wall (32). Injectors in one of the rows are in angular registration with spaces between injectors in the other row. Each fuel injector comprises a means for producing a fuel/air mixture having a swirling motion, and a mixing duct located downstream of the means for producing the fuel/air mixture. Each mixing duct opens into the combustion chamber (31) through the combustor head wall (32) and has a length sufficient to allow at least partial mixing of the fuel/air mixture before entry to the combustion chamber as a divergent swirling stream (38, 40). Mixing ducts in the first and second rows of injectors have longitudinal centrelines (L1 , L2 ) oriented to coincide with generating rays of respective first and second imaginary conical sufaces. These conical surfaces intersect at an included angle (2D) within a primary combustion zone in the combustion chamber, whereby injectors (19 , 20 ) located in different rows are angled towards each other in the downstream direction and the divergent swirling streams of fuel/air mixture (38, 40) coming from different rows cross in the combustion chamber in an interdigitating manner. This creates a strong mixing interaction between the streams from different rows and enhances uniformity and rapidity of combustion in the primary combustion zone.
摘要翻译：用于燃气涡轮发动机的燃烧器（30）包括环形燃烧室（31），其具有同心地设置在燃烧器头壁（32）中的径向外排和内排燃料喷射器（19 1，20 1）。一列中的注射器与另一行中的喷射器之间的空间成角度对齐。每个燃料喷射器包括用于产生具有旋动运动的燃料/空气混合物的装置和位于用于产生燃料/空气混合物的装置下游的混合管道。每个混合管道通过燃烧器头壁（32）通入燃烧室（31），并且其长度足以允许燃料/空气混合物在进入燃烧室之前至少部分混合，作为分散的旋流（38， 40）。第一和第二排注射器中的混合管道具有定向成与产生相应的第一和第二虚拟圆锥形表面的射线一致的纵向中心线（L1'，L2'）。这些锥形表面在燃烧室中的主燃烧区内以夹角（2D）相交，由此位于不同行中的喷射器（19 1，20 1）在下游方向上彼此成角度，并且发散来自不同行的燃料/空气混合物（38,40）的回旋流以交叉的方式在燃烧室中交叉。这在来自不同行的流之间产生强烈的混合相互作用，并增强了主燃烧区中燃烧的均匀性和快速性。

3. 发明申请

WO2008037554A3 IMPROVEMENTS IN OR RELATING TO GAS TURBINE ENGINES 审中-公开
标题翻译：燃气涡轮发动机的改进或与之相关的改进
公开(公告)号：WO2008037554A3
公开(公告)日：2008-09-04
申请号：PCT/EP2007059035
申请日：2007-08-30
申请人： SIEMENS AG , SENIOR PETER , WILBRAHAM NIGEL
发明人： SENIOR PETER , WILBRAHAM NIGEL
IPC分类号： F01D9/02 , F02C3/14 , F23R3/60
CPC分类号： F23R3/60 , F01D9/023 , F02C3/14 , F05D2230/60 , F05D2230/61 , F05D2230/70 , F05D2230/80 , F05D2240/40 , F05D2250/411 , F23R2900/00019
摘要： A gas turbine engine includes a number of high-temperature modules, each of which includes a combustion unit and a transition duct. The modules are secured to the engine by means of a displacement mechanism, which enables rapid and easy access to the module and adjacent inner parts of the engine. The displacement mechanism is preferably a pivot arrangement, by means of which the module is rotatably attached to the engine frame. Preferably, the module also includes a stator blading, which is attached to the end of the transition
摘要翻译：燃气涡轮发动机包括多个高温模块，每个高温模块包括燃烧单元和过渡管道。这些模块通过位移机构固定在发动机上，可以快速方便地接近发动机模块和相邻的内部部件。位移机构优选是枢转装置，通过该枢转装置模块可旋转地附接到发动机机架。优选地，模块还包括附接到过渡部的端部的定子叶片

4. 发明申请

WO2008098862A1 FUEL SUPPLY MODULE 审中-公开
标题翻译：燃油供应模块
公开(公告)号：WO2008098862A1
公开(公告)日：2008-08-21
申请号：PCT/EP2008/051440
申请日：2008-02-06
申请人： SIEMENS AKTIENGESELLSCHAFT , SENIOR, Peter
发明人： SENIOR, Peter
IPC分类号： F23R3/28 , F23R3/34
CPC分类号： F23R3/34 , F23R3/28 , F23R2900/00018
摘要： Disclosed is a fuel supply module with a plurality of burner ports (7) for receiving respective burners (2) and a plurality of first fuel supply lines (15), each first fuel supply line (15) integrated into the fuel supply module (1) and connected to one of the burner ports (7) and merging into a common first fuel injection entry (21) for supplying a fuel to the first fuel supply lines (15). Further disclosed is a method of manufacturing a fuel supply module.
摘要翻译：公开了一种具有多个燃烧器端口（7）的燃料供应模块，用于接收相应的燃烧器（2）和多个第一燃料供应管线（15），每个第一燃料供应管线（15）集成到燃料供应模块（1））并且连接到燃烧器端口（7）中的一个并且合并成用于向第一燃料供应管线（15）供应燃料的公共第一燃料喷射入口（21）。进一步公开了一种制造燃料供给模块的方法。

5. 发明申请

WO2008028792A1 TURBINE ENGINE AND METHOD OF OPERATING THE SAME 审中-公开
标题翻译：涡轮发动机及其运行方法
公开(公告)号：WO2008028792A1
公开(公告)日：2008-03-13
申请号：PCT/EP2007/058560
申请日：2007-08-17
申请人： SIEMENS AKTIENGESELLSCHAFT , SENIOR, Peter
发明人： SENIOR, Peter
IPC分类号： F01D5/08 , F01D25/26 , F01D25/24 , F01D25/14 , F01D11/24
CPC分类号： F01D25/26 , F01D5/085 , F01D25/10 , F01D25/12 , F05D2260/205 , F05D2300/505
摘要： A turbine engine with a casing (11) and a rotor (9) extending through the casing (11) is provided. The casing (11) and/or the rotor (9) are/is equipped with fluid channels (43, 51). Moreover, at least one fluid introduction device (49, 55) is present which is designed and arranged such as to introduce a fluid into the fluid channels (43, 51) for flowing there through during a transient engine condition.
摘要翻译：提供具有壳体（11）和延伸穿过壳体（11）的转子（9）的涡轮发动机。壳体（11）和/或转子（9）配备有流体通道（43,41）。此外，存在至少一个流体引入装置（49,55），其被设计和布置成在瞬态发动机状态期间将流体引入到流体通道（43,41）中以在那里流过。

6. 发明申请

WO2007033876A1 AN ARRANGEMENT FOR PREPARATION OF A FUEL FOR COMBUSTION 审中-公开
标题翻译：燃料燃料的制备安排
公开(公告)号：WO2007033876A1
公开(公告)日：2007-03-29
申请号：PCT/EP2006/065353
申请日：2006-08-16
申请人： SIEMENS AKTIENGESELLSCHAFT , NILSSON, Ulf , SENIOR, Peter
发明人： NILSSON, Ulf , SENIOR, Peter
IPC分类号： F23D11/44 , F23R3/32 , F23N1/00
CPC分类号： F23N1/002 , F23D11/443 , F23N2037/14 , F23R3/32
摘要： The invention relates to an arrangement for preparation of a fuel for combustion including a burner, a combustion chamber (8) associated with the burner and in which combustion of a fuel is to take place in use of the arrangement as well as means (12) for supplying liquid fuel to the arrangement through an internal passage (13, 36) in the burner for said combustion, solid portions (1 1 , 19) of the burner body being heated by said combustion in use of the arrangement, wherein said internal passage is located inside said solid portions of the burner body for receiving heat energy evaporating said fuel from these body portions, and that it comprises means (27) for conveying the vaporised fuel to the combustion chamber to take part in the combustion.
摘要翻译：本发明涉及一种用于燃烧燃料的配置的装置，包括燃烧器，与燃烧器相关联的燃烧室（8），并且燃料的燃烧将在该装置的使用中发生，以及装置（12）用于通过用于所述燃烧的燃烧器中的内部通道（13,36）将液体燃料供给到所述装置中，所述燃烧器主体的实心部分（11,19）在使用该装置时被所述燃烧加热，其中所述内部通道位于燃烧器主体的所述固体部分的内部，用于接收从这些主体部分蒸发所述燃料的热能，并且其包括用于将蒸发的燃料输送到燃烧室以参与燃烧的装置（27）。

7. 发明申请

WO1992018164A1 PREPARATION OF DIAGNOSTIC AGENTS 审中-公开
标题翻译：诊断试剂的制备
公开(公告)号：WO1992018164A1
公开(公告)日：1992-10-29
申请号：PCT/GB1992000643
申请日：1992-04-10
申请人： DELTA BIOTECHNOLOGY LIMITED , SUTTON, Andrew, Derek , JOHNSON, Richard, Alan , SENIOR, Peter, James , HEATH, David
发明人： DELTA BIOTECHNOLOGY LIMITED
IPC分类号： A61K49/00
CPC分类号： A61K49/00 , A61K9/1688 , A61K9/1694 , A61K9/5089 , A61K49/223 , A61K49/225 , B01J13/04 , B01J13/043 , B01J13/14 , Y10S516/928
摘要： Microcapsules are prepared by a process comprising the steps of (i) spray-drying a solution or dispersion of a wall-forming material in order to obtain intermediate microcapsules and (ii) reducing the water-solubility of at least the outside of the intermediate microcapsules. Suitable wall-forming materials include proteins such as albumin and gelatin. The microcapsules have walls of 40-500 nm thick and are useful in ultrasonic imaging. The control of median size, size distribution and degree of insolubilisation and cross-linking of the wall-forming material allows novel microsphere preparations to be produced.

8. 发明申请

WO2009121669A1 A COMBUSTOR CASING 审中-公开
标题翻译：一个COMBUSTOR CASING
公开(公告)号：WO2009121669A1
公开(公告)日：2009-10-08
申请号：PCT/EP2009/052199
申请日：2009-02-25
申请人： SIEMENS AKTIENGESELLSCHAFT , BULAT, Ghenadie , SENIOR, Peter
发明人： BULAT, Ghenadie , SENIOR, Peter
IPC分类号： F23R3/00 , F23R3/34
CPC分类号： F23R3/002 , F23R3/346
摘要： Disclosed is a combustor casing (5), with an inner casing (11) and an outer casing (12) and a bimetallic element (15) arranged on an inner side (16) of the inner casing (11). The inner casing (11) comprises a pre-chamber area, where combustion is initiated in a fuel rich state, with an upper end and a lower end, the upper end sized and configured to be connected to a burner head (2). The bimetallic element (15) is located within the pre-chamber area.
摘要翻译：公开了一种燃烧器壳体（5），其具有布置在内壳体（11）的内侧（16）上的内壳体（11）和外壳体（12）和双金属元件（15）。内壳体（11）包括预燃室区域，其中燃料以富燃状态启动，具有上端和下端，上端的尺寸和构造被连接到燃烧头（2）。双金属元件（15）位于预制室内。

9. 发明申请

WO2008107401A1 GUIDE VANE DUCT ELEMENT FOR A GUIDE VANE ASSEMBLY OF A GAS TURBINE ENGINE 审中-公开
标题翻译：导向气缸发动机导向组件的导向导管元件
公开(公告)号：WO2008107401A1
公开(公告)日：2008-09-12
申请号：PCT/EP2008/052518
申请日：2008-02-29
申请人： SIEMENS AKTIENGESELLSCHAFT , HASSELQVIST, Magnus , SENIOR, Peter
发明人： HASSELQVIST, Magnus , SENIOR, Peter
IPC分类号： F01D9/04
CPC分类号： F01D5/143 , F01D9/04 , F01D9/065 , F05D2230/61 , F05D2240/12 , F05D2260/2212 , F05D2260/22141 , F05D2260/60
摘要： An inlet guide vane arrangement for a gas turbine comprises a plurality of guide vane duct elements, the guide vane duct elements comprise a suction side wall (2) and a pressure side wall (3), both walls (2, 3) facing each other, and being designed to be adjoinable to another of said guide vane duct elements (1), such that the pressure side wall (3) of one guide vane duct element (1) cooperates with the suction side wall (2) of the adjacent guide vane duct element (1) thereby forming a guide vane (6), and the guide vane duct element (1) includes features to accept a key element (15) adapted to be arranged between the pressure side wall (3) and the adjacent suction side wall (2), when two guide vane duct elements (1) are adjoining to one another, and to fix together both adjoining guide vane duct elements (1).
摘要翻译：用于燃气轮机的入口引导叶片装置包括多个导叶管道元件，导叶管道元件包括吸力侧壁（2）和压力侧壁（3），两个相互面对的壁（2,3）并且被设计成可与另一个所述导叶管道元件（1）邻接，使得一个导叶管道元件（1）的压力侧壁（3）与相邻引导件的吸入侧壁（2）协作，叶片管道元件（1），从而形成导向叶片（6），并且导叶管道元件（1）包括特征以接受适于布置在压力侧壁（3）和相邻吸力当两个导向叶片管道元件（1）彼此邻接并且将邻接的导叶管道元件（1）固定在一起时，侧壁（2）。

10. 发明申请

WO2007144208A1 A METHOD OF SUBSTITUTING A MATERIAL COMPONENT OF COATINGS OF GAS TURBINE COMPONENTS 审中-公开
标题翻译：取代燃气涡轮机组件涂料的材料成分的方法
公开(公告)号：WO2007144208A1
公开(公告)日：2007-12-21
申请号：PCT/EP2007/051742
申请日：2007-02-23
申请人： SIEMENS AKTIENGESELLSCHAFT , SENIOR, Peter , WILBRAHAM, Nigel
发明人： SENIOR, Peter , WILBRAHAM, Nigel
IPC分类号： F01D5/28 , C23C4/10 , C23C24/04
CPC分类号： F01D5/005 , C23C4/129 , F01D5/286 , F02C7/22 , F05D2230/90
摘要： A method of substituting a material component of coatings of gas turbine components during operation of the gas turbine, in which - the components are charged, - the material component is charged in opposite polarity to the gas turbine components, and - the material component is added to a fluid stream which is led to the gas turbine.
摘要翻译：在燃气轮机的运行期间替代燃气涡轮机部件的涂层的材料成分的方法，其中 - 部件被充电 - 材料部件以与燃气轮机部件相反的极性进行充电，并且 - 添加材料部件被引导到燃气轮机的流体流。

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