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1. 发明申请

WO2009135721A1 FLUID INTAKE ASSEMBLY 审中-公开
标题翻译：流体吸入装置
公开(公告)号：WO2009135721A1
公开(公告)日：2009-11-12
申请号：PCT/EP2009/053202
申请日：2009-03-18
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F04D29/02 , F04D29/54 , F04D29/70 , F01D9/02 , F02C7/04
CPC分类号： F04D29/541 , F04D29/023 , F04D29/70 , F05B2230/601 , F05B2250/62 , F05C2253/04 , F05C2253/12 , F05D2300/2102 , F05D2300/43 , F05D2300/603
摘要： The present invention relates to a fluid intake assembly (100) adapted for use with a turbo-machine (200). The invention provides an efficient fluid inlet assembly (100) comprising a casing (120) adapted to guide fluid into the turbo-machine (200). The casing (120) comprises an inner wall (130), the inner wall (130) having a lining (140) of a resin infused composite material. The invention also provides a method of producing a fluid intake assembly (100) for use with a turbo-machine (200).
摘要翻译：本发明涉及一种适于与涡轮机（200）一起使用的流体进入组件（100）。本发明提供了一种有效的流体入口组件（100），其包括适于将流体引导到涡轮机（200）中的壳体（120）。壳体（120）包括内壁（130），内壁（130）具有树脂注入复合材料的内衬（140）。本发明还提供一种生产与涡轮机（200）一起使用的流体进料组件（100）的方法。

2. 发明申请

WO2009062793A1 AIR BLEED IN COMPRESSOR WITH VARIABLE GUIDE VANES 审中-公开
标题翻译：压缩机空气压缩机带有可变导向空间
公开(公告)号：WO2009062793A1
公开(公告)日：2009-05-22
申请号：PCT/EP2008/063436
申请日：2008-10-08
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F04D27/02 , F01D17/10
CPC分类号： F02C9/18 , F01D17/162 , F04D27/023 , F04D29/563 , F05D2260/60
摘要： Disclosed is a guide vane (2) for a compressor (1) with an airfoil (7), and a base plate (8) for mounting the guide vane (2) to a compressor casing, wherein the base plate (8) includes an air duct (9) sized and configured to guide compressor air off the airfoil (7) through the air duct (9). Further disclosed is a guide vane arrangement (17).
摘要翻译：公开了一种用于具有翼型件（7）的压缩机（1）的引导叶片（2）和用于将导向叶片（2）安装到压缩机壳体的基板（8），其中基板（8）包括空气管道（9）的尺寸和构造用于通过空气管道（9）将压缩机空气引导到翼型件（7）。进一步公开的是导叶装置（17）。

3. 发明申请

WO2008090202A1 A DIFFUSER FOR DECELERATING A COMPRESSED FLUID 审中-公开
标题翻译：用于减压压缩液的搅拌器
公开(公告)号：WO2008090202A1
公开(公告)日：2008-07-31
申请号：PCT/EP2008/050825
申请日：2008-01-24
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F04D29/54 , F01D9/04
CPC分类号： F04D29/541 , F01D9/041 , F01D9/042 , F05D2250/11 , F05D2250/18 , F05D2250/181 , F05D2250/182 , F05D2250/324 , F05D2250/70 , F05D2260/36
摘要： A diffuser for decelerating a compressed gas, is provided, which includes a ring divided at circumferential positions around the ring into several arcuate sections, the complete ring being assembled from these sections. The ring defines one or more passages, the cross-section of which increases in the direction of travel of a fluid through the diffuser. The interface between adjacent sections is configured in a manner preventing relative movement between the sections. The interface may be configured to have a series of interlocking serrations along the axial length of the diffuser. In a preferred embodiment, there are two arcuate sections involving two interfaces, and the peaks and troughs of the serrations are arranged at an angle to a longitudinal axis of the diffuser. Good immunity to relative movement between the sections is achieved when this angle is of opposite sign at the two interfaces.
摘要翻译：提供了用于使压缩气体减速的扩散器，其包括在环周围的位置分成几个弧形部分的环，该环从这些部分组装。环限定一个或多个通道，其横截面在流体通过扩散器的行进方向上增加。相邻部分之间的界面以防止部分之间相对移动的方式配置。界面可以被配置为沿着扩散器的轴向长度具有一系列互锁锯齿。在优选实施例中，存在两个涉及两个界面的弓形部分，并且锯齿的峰和谷以与扩散器的纵向轴线成一角度的方式布置。当这个角度在两个界面处具有相反的符号时，实现对各部分之间相对运动的良好的抵抗力。

4. 发明申请

WO2012038165A1 GAS TURBINE AND METHOD FOR OPERATING A GAS TURBINE 审中-公开
标题翻译：气体涡轮机和运行气体涡轮机的方法
公开(公告)号：WO2012038165A1
公开(公告)日：2012-03-29
申请号：PCT/EP2011/064308
申请日：2011-08-19
申请人： SIEMENS AKTIENGESELLSCHAFT , JAMES, Richard , TWELL, Philip
发明人： JAMES, Richard , TWELL, Philip
IPC分类号： F01D11/06 , F01D25/16
CPC分类号： F02C7/06 , F01D11/06 , F01D11/08 , F01D25/166
摘要： Gas turbine and method for operating a gas turbine It is described a gas turbine, comprising: a rotor (2) comprising a rotor portion of a fluid bearing (31) for rotatably supporting the rotor; a radially outer stator portion (18); a radially inner stator portion (16) comprising a stator portion of the fluid bearing; a compressor air passage (10) extending between the radially outer stator portion and the radially inner stator portion; an annular gap (14) between the rotor and the radially inner stator portion partially forming an annular air passage in communication with the compressor air passage, wherein along a flow direction (43) of air flowing within the annular air passage a radius (r0,r1,r2,r3,r4) of the air passage decreases in a first portion (20, 26) and then increases in a second portion (22, 28); and a discharge conduit (57, 63) for discharging the air flown through the second portion of the annular air passage, wherein an inlet of the discharge conduit for introducing the air flown through the second portion of the annular air passage is axially arranged between the second portion of the annular air passage and the fluid bearing. Further a method for operating a gas turbine is described.
摘要翻译：燃气轮机和燃气轮机的操作方法描述了一种燃气轮机，包括：转子（2），包括用于可旋转地支撑转子的流体轴承（31）的转子部分; 径向外部定子部分（18）; 径向内部定子部分（16），包括所述流体轴承的定子部分; 在径向外定子部分和径向内定子部分之间延伸的压缩机空气通道（10）所述转子和所述径向内部定子部分之间的环形间隙（14）部分地形成与所述压缩机空气通道连通的环形空气通道，其中沿着在所述环形空气通道内流动的空气的流动方向（43）空气通道的r1，r2，r3，r4）在第一部分（20,26）中减小，然后在第二部分（22,28）中增加; 以及用于排出流过环形空气通道的第二部分的空气的排放管道（57,63），其中用于引导空气流过环形空气通道的第二部分的排放管道的入口被轴向地布置在环形空气通道的第二部分和流体轴承。另外描述了用于操作燃气轮机的方法。

5. 发明申请

WO2012163612A1 EASILY ADAPTABLE COMPRESSOR BLEED SYSTEM DOWNSTREAM OF A VANE PLATFORM 审中-公开
标题翻译：易于适应的压缩机BLEED系统下降的平台
公开(公告)号：WO2012163612A1
公开(公告)日：2012-12-06
申请号：PCT/EP2012/057839
申请日：2012-04-27
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F04D27/02 , F04D29/52 , F01D9/06 , F02C6/08
CPC分类号： F02C9/18 , F01D9/06 , F01D11/005 , F02C6/08 , F04D29/522 , F04D29/526 , F04D29/542
摘要： Discrete bleed behind stator vane platform The present invention relates to a system (100) for bleeding off a working fluid from an inner volume (Vi) of a turbo- machine. The system (100) comprises a vane carrier (104) with an annular rail (105) and a vane device comprising at least one vane element (101), a vane platform (102) and a vane root (103). The vane element (101) is mounted to the vane platform (102) and the vane root (103) is mounted to the annular rail (105). A first annular cavity (106) is formed between the vane platform (102) and the annular rail (105), wherein an annular gap (108) is formed between an edge (110) of the vane platform (102) and the vane carrier (104) such that a part of the working fluid of the turbo-machine is bleedable through the annular gap (108) into the first annular cavity (106). A second annular cavity (107) is formed between the vane root (103), the annular rail (105) and the vane carrier (104), wherein at least one inlet hole (109) is formed into the annular rail (105) for coupling the first annular cavity (106) and the second annular cavity (107).
摘要翻译：定子叶片平台后面的离散泄漏技术领域本发明涉及一种用于从涡轮机的内部容积（Vi）排出工作流体的系统（100）。系统（100）包括具有环形轨道（105）的叶片载体（104）和包括至少一个叶片元件（101），叶片平台（102）和叶根（103）的叶片装置。叶片元件（101）安装在叶片平台（102）上，叶片根部（103）安装在环形轨道（105）上。第一环形空腔（106）形成在叶片平台（102）和环形轨道（105）之间，其中环形间隙（108）形成在叶片平台（102）的边缘（110）和叶片承载件（104），使得所述涡轮机的所述工作流体的一部分可通过所述环形间隙（108）渗出到所述第一环形空腔（106）中。在叶片根部（103），环形轨道（105）和叶片承载件（104）之间形成有第二环形空腔（107），其中至少一个入口孔（109）形成为环形轨道（105），用于联接第一环形空腔（106）和第二环形空腔（107）。

6. 发明申请

WO2011038966A1 AIRFOIL AND CORRESPONDING GUIDE VANE, BLADE, GAS TURBINE AND TURBOMASCHINE 审中-公开
标题翻译：气翼和相应导向叶片，叶片，气体涡轮和涡轮发动机
公开(公告)号：WO2011038966A1
公开(公告)日：2011-04-07
申请号：PCT/EP2010/061553
申请日：2010-08-09
申请人： SIEMENS AKTIENGESELLSCHAFT , SHEPHERD, Andrew , TWELL, Philip
发明人： SHEPHERD, Andrew , TWELL, Philip
IPC分类号： F01D5/20 , F16J15/32 , F01D11/12
CPC分类号： F01D5/20 , F01D11/127 , F16J15/44 , F16J15/4472
摘要： The invention related to an airfoil (27) of a turbomachine, particularly a gas turbine (1), the airfoil (27) suitable for being arranged in a compressor section (5) of the gas turbine (1), the airfoil (27) comprising a platform (25), a pressure surface (42) and a suction surface (43), and a tip region (29). The pressure surface (42) and the suction surface (43), extend substantially perpendicular to the platform (25) along a first direction (D), the first direction (D) being defined as a direction substantially perpendicular to the platform (25) and progressing with a distance to the platform (25). The tip region (29) is located between the pressure (42) and the suction surface (43) opposite to the platform (25) in respect of the pressure (42) and the suction surfaces (43), being a distant end of the airfoil (27) in direction along the first direction (D). The tip region (29) is configured such that the tip region (29) comprises a first surface (70) with a first surface expanse less than a cross sectional plane of the airfoil (27) perpendicular to the first direction (D) and with a first distance (Dl) to the platform (25) along the first direction (D), and a second surface (71) with a second surface expanse and with a second distance (D2) to the platform (25) along the first direction (D), whereas the first distance (Dl) is greater than the second distance (D2) and the first surface (70) and the second surface (71) together build a profiled surface, the profiled surface being a ribbed surface and material of the first surface (70) being deformable such that the material of the first surface (70) will bend away from a direction of rotation of the airfoil (27) during operation.
摘要翻译：本发明涉及一种涡轮机械，特别是燃气轮机（1）的机翼（27），适于布置在燃气轮机（1）的压缩机部分（5）中的翼型件（27），翼型件（27）包括平台（25），压力表面（42）和吸力表面（43）以及尖端区域（29）。压力表面（42）和抽吸表面（43）沿着第一方向（D）基本上垂直于平台（25）延伸，第一方向（D）被定义为基本上垂直于平台（25）的方向，并且与平台（25）的距离前进。尖端区域（29）位于压力（42）和与平台（25）相对的压力（42）的吸力表面（43）之间，相对于压力（42）和吸力表面（43）机翼（27）沿着第一方向（D）的方向。尖端区域（29）构造成使得尖端区域（29）包括具有小于垂直于第一方向（D）的翼型件（27）的横截面的第一表面扩展部的第一表面（70）并且与沿着第一方向（D）到平台（25）的第一距离（D1）和具有第二表面的第二表面（71），并且沿着第一方向与平台（25）具有第二距离（D2）（D），而第一距离（D1）大于第二距离（D2），并且第一表面（70）和第二表面（71）一起构成成型表面，成型表面为肋状表面，并且材料为所述第一表面（70）可变形，使得所述第一表面（70）的材料在操作期间将远离所述翼型件（27）的旋转方向弯曲。

7. 发明申请

WO2011026516A1 A MOUNTING APPARATUS 审中-公开
标题翻译：安装设备
公开(公告)号：WO2011026516A1
公开(公告)日：2011-03-10
申请号：PCT/EP2009/061345
申请日：2009-09-02
申请人： SIEMENS AKTIENGESELLSCHAFT , CANT, Andrew , TWELL, Philip
发明人： CANT, Andrew , TWELL, Philip
IPC分类号： F01D5/30 , F01D25/24 , F01D25/28 , F02K1/80
CPC分类号： F01D25/246 , F01D5/3053 , F01D5/323 , F01D5/326 , F01D25/28 , F02K1/80 , F05B2240/916 , F05B2260/301 , F05D2230/60 , F05D2230/64 , F05D2230/644 , F05D2230/68 , F05D2240/14 , F05D2240/40 , F05D2240/90 , F05D2240/91 , F05D2260/30
摘要： A mounting apparatus comprising: a mounting pin (11) having first and second ends (19, 21); a support (9) having first and second sides (23, 25), the support (9) including a passage (27) between the first and second sides (23, 25) for receiving the mounting pin (11) so that the first end (19) of the pin (11) protrudes from the first side (23) and the second end (21) of the pin (11) protrudes from the second side (25), the second end (21) of the pin (11) being configured to engage an article (7) to be mounted by the mounting apparatus, the first end (19) of the pin (11) being operable to rotate the pin (11) about the axis of the pin (11) to vary the position of a mounted article (7); and a clamping plate (47) for clamping the first end (19) of the mounting pin (11) to the first side (23) of the support (9) for securing the rotational position of the pin (11) with respect to the support (9), wherein: the first end (19) of the pin (11) includes a first locking taper (49) which, with progression along the axis of the pin (11) away from the second end (21) of the pin (11), tapers from a first radial distance from the axis to a second reduced radial distance from the axis; and the clamping plate (47) includes a second locking taper (51) complementary to the first locking taper (49) for locking with the first locking taper (49).
摘要翻译：一种安装设备，包括：安装销（11），其具有第一和第二端（19,21）; 具有第一和第二侧面（23,25）的支撑件（9），所述支撑件（9）包括在所述第一和第二侧面（23,25）之间的通道（27），用于接纳所述安装销（11），使得所述第一销（11）的端部（19）从第一侧（23）突出，销（11）的第二端（21）从第二侧（25）突出，销的第二端（21） 11）构造成接合由安装装置安装的物品（7），销（11）的第一端（19）可操作以使销（11）围绕销（11）的轴线旋转至改变安装的物品（7）的位置; 以及用于将安装销（11）的第一端（19）夹紧到支撑件（9）的第一侧（23）的夹板（47），用于将销（11）的旋转位置相对于支撑件（9），其中：所述销（11）的所述第一端（19）包括第一锁定锥形件（49），所述第一锁定锥形件沿着所述销（11）的轴线远离所述销（11）的第二端部销（11）从距离轴的第一径向距离减小到距离轴的第二减小的径向距离; 并且夹板（47）包括与第一锁定锥（49）互补的第二锁定锥（51），用于与第一锁定锥（49）锁定。

8. 发明申请

WO2012156180A1 DRIVE LEVER ARRANGEMENT 审中-公开
标题翻译：驱动装置
公开(公告)号：WO2012156180A1
公开(公告)日：2012-11-22
申请号：PCT/EP2012/057483
申请日：2012-04-24
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F01D17/16 , F01D17/10
CPC分类号： F04D29/60 , F01D17/10 , F01D17/162 , F05D2260/30 , F05D2260/50 , Y10T29/49321 , Y10T29/49959
摘要： A drive lever arrangement (100) comprising a unison ring (101) which comprises a groove (201); a drive lever (102) comprising connection means for connecting the drive lever (102) to the unison ring (101); a drive lever pin (103) comprising a transversal throughbore hole (206); and a clip, wherein the drive lever pin (103) connects the drive lever (102) to the unison ring (101), and wherein the clip is inserted in the groove (201) through the throughbore hole (206) of the drive lever pin (103), and engages with the groove (201) of the unison ring (101).
摘要翻译： 1.一种驱动杆装置（100），包括具有槽（201）的协调环（101）驱动杆（102），包括用于将驱动杆（102）连接到协调环（101）的连接装置; 驱动杆销（103），包括横向通孔（206）; 和夹子，其中所述驱动杆销（103）将所述驱动杆（102）连接到所述协调环（101），并且其中所述夹子通过所述驱动杆的通孔（206）插入所述凹槽（201）销（103），并与协调环（101）的槽（201）接合。

9. 发明申请

WO2012007248A3 BORE-SCOPE SEALING APPARATUS AND PLUG THEREFOR 审中-公开
公开(公告)号：WO2012007248A3
公开(公告)日：2012-01-19
申请号：PCT/EP2011/060141
申请日：2011-06-17
申请人： SIEMENS AKTIENGESELLSCHAFT , TWELL, Philip
发明人： TWELL, Philip
IPC分类号： F01D21/00 , F01D25/24
摘要： A bore-scope sealing apparatus (1) for removably sealing a bore-scope opening (2, 4) in a turbmachine wall (3, 5) has a plug (6) which is mountable to the bore-scope opening (2, 4) by means of a bayonet coupling (13). The bayonet coupling (13) comprises a projection (14) at the plug (6) and a corresponding recess (18) at the bore-scope opening (2, 4). A resilient retaining means (15) is arranged at the recess (18) being compressed by the projection (14) in a sealing position to retain the plug (6) in the bore-scope opening (2, 4).

10. 发明申请

WO2010031768A3 ADJUSTING DEVICE FOR VARIABLE GUIDE VANES AND METHOD OF OPERATION 审中-公开
公开(公告)号：WO2010031768A3
公开(公告)日：2010-03-25
申请号：PCT/EP2009/061953
申请日：2009-09-15
申请人： SIEMENS AKTIENGESELLSCHAFT , LEITHEAD, Graeme , SMITH, Michael , TWELL, Philip
发明人： LEITHEAD, Graeme , SMITH, Michael , TWELL, Philip
IPC分类号： F01D17/16 , F01D17/20
摘要： The invention relates to a device, system, or method to position variable guide vanes disproportionate. An adjusting device for guide vanes of an axial-flow machine, comprises a plurality of rotatably mounted rings of variable guide vanes (10, 11), a plurality of levers (50; lever1, Iever2, Iever3) which are arranged on the outer sides of a guide vane carrier (30) for rotating the variable guide vanes (10, 11), a plurality of adjusting rings (40, 41, 42, 43), each of the adjustment rings (40, 41, 42, 43) is arranged coaxially to the guide vane carrier (30) and to which a first end (51) of one of the levers (50) is connected, and an adjusting drive with which the adjusting rings (40, 41, 42, 43) can be moved in its peripheral direction. At least one of the levers (lever1) is set up to perform at least partly a disproportionate longitudinal movement of the first end (51) of the at least one lever (lever1).

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