公开(公告)号：WO2012150139A1

公开(公告)日：2012-11-08

申请号：PCT/EP2012/057343

申请日：2012-04-23

Applicant: SIEMENS AKTIENGESELLSCHAFT ,  NILSSON, Ulf

Inventor： NILSSON, Ulf

IPC: F23D11/28 ,  F23R3/34

CPC classification number: F23R3/28 ,  F23D11/28 ,  F23R3/343

Abstract: A device (100) for injecting fuel into a combustion chamber of a gas turbine, comprising a distribution section (103) to which a first fuel channel (101), a second fuel channel (102) and an injection channel (104) are coupled. The first fuel channel (101) and the second fuel channel (102) are arranged such that a) fuel is transportable by one of the first fuel channel (101) and the second fuel channel (102) to the distribution section (103), and b) a first quantity of fuel is transportable by the other one of the first fuel channel (101) and the second fuel channel (102) out of the distribution section (103). The injection channel (104) is arranged such that a second quantity of fuel is injectable from the distribution section (103) into the combustion chamber. The device (100) further comprises an end cap (113) with a protrusion (201) having the injection channel (104) inside, and extending inside the inner tube (110).

Abstract translation: 一种用于将燃料喷射到燃气涡轮机的燃烧室中的装置（100），包括分配部分（103），第一燃料通道（101），第二燃料通道（102）和注射通道（104）与所述分配部分 。 第一燃料通道（101）和第二燃料通道（102）被布置成使得燃料可以通过第一燃料通道（101）和第二燃料通道（102）之一运送到分配部分（103） 以及b）第一数量的燃料可由第一燃料通道（101）和第二燃料通道（102）中的另一个运送到分配部分（103）之外。 喷射通道（104）被布置成使得第二量的燃料可以从分配部分（103）喷射到燃烧室中。 装置（100）还包括具有在内部具有注入通道（104）并且在内管（110）内延伸的突出部（201）的端盖（113）。

公开(公告)号：WO2012110315A1

公开(公告)日：2012-08-23

申请号：PCT/EP2012/051652

申请日：2012-02-01

Applicant: SIEMENS AKTIENGESELLSCHAFT ,  NILSSON, Ulf

Inventor： NILSSON, Ulf

IPC: F23R3/04 ,  F23R3/28 ,  F23M5/02

CPC classification number: F23R3/343 ,  F23D2214/00 ,  F23D2900/00016 ,  F23M5/025 ,  F23R3/04 ,  F23R3/283 ,  F23R2900/00004 ,  F23R2900/03042 ,  F23R2900/03043

Abstract: The present invention relates to a combustion chamber (100) for a gas turbine. The combustion chamber (100) comprises a wall section (101) and a brim element (103). The wall section (101) comprises an inlet aperture (102) for injecting a cooling medium into the combustion chamber (100). The brim element (103) is mounted to an inner face (104) of the wall section (101), wherein the brim element (103) is formed in such a way that a projected area of the brim element (103) onto the inner face (104) along a direction of a normal (n) of the inner face (104) at least partially covers the inlet channel (102).

Abstract translation: 本发明涉及燃气轮机的燃烧室（100）。 燃烧室（100）包括壁部（101）和边缘元件（103）。 壁部分（101）包括用于将冷却介质注入到燃烧室（100）中的入口孔（102）。 边缘元件（103）安装到壁部分（101）的内表面（104）上，其中边缘元件（103）形成为使得边缘元件（103）的投影面积到内部 面（104）沿着内表面（104）的法线（n）的方向至少部分地覆盖入口通道（102）。

公开(公告)号：WO2012084347A2

公开(公告)日：2012-06-28

申请号：PCT/EP2011/070245

申请日：2011-11-16

Applicant: SIEMENS AKTIENGESELLSCHAFT ,  NILSSON, Ulf

Inventor： NILSSON, Ulf

IPC: F23K5/10 ,  B01F3/04

CPC classification number: F02C7/22 ,  B01F3/0446 ,  B01F5/0463 ,  F02C3/24 ,  F02C7/222 ,  F02C7/2365 ,  F05D2260/85 ,  F23K5/10 ,  F23K2301/103 ,  F23K2900/05084 ,  F23R3/28

Abstract: The present invention relates to gas turbine comprising a combustion system with several burners, a conduit system with a fuel manifold for providing the burners with liquid fuel and a system for aerating the liquid fuel with gas. According to the invention said system for aerating the liquid fuel (53) with gas (54) is located upstream to said fuel manifold (51).

Abstract translation: 本发明涉及包括具有多个燃烧器的燃烧系统的燃气轮机，具有用于为燃烧器提供液体燃料的燃料歧管的导管系统以及用于使气体对液体燃料充气的系统。 根据本发明，用于用气体（54）对液体燃料（53）进行充气的所述系统位于所述燃料歧管（51）的上游。

公开(公告)号：WO2011149406A1

公开(公告)日：2011-12-01

申请号：PCT/SE2011/050571

申请日：2011-05-06

Applicant: ATLAS COPCO ROCK DRILLS AB ,  NILSSON, Ulf ,  WALTER, Magnus

Inventor： NILSSON, Ulf ,  WALTER, Magnus

IPC: B25D17/00 ,  B25D17/08 ,  E21B6/00

CPC classification number: E21B1/00 ,  E21B6/00

Abstract: The invention relates to a rock drilling machine comprising a front part (1a), a removable cartridge (5) arranged in the front part (1a), a shank adapter (3) and a stop ring (4) for the shank adapter (3). According to the invention, the diameter of the removable cartridge (5) is at least as great as the diameter of the stop ring (4), such that it is possible during demounting of the removable cartridge (5) to mount or demount the stop ring (4), without removing the front part (1 a) from the rock drilling machine. The invention also relates to a removable cartridge (5), a stop ring (4) and a drilling rig incorporating the drilling machine.

Abstract translation: 本发明涉及一种凿岩机，包括前部（1a），布置在前部（1a）中的可移除筒（5），柄适配器（3）和用于柄适配器（3）的止动环（4） ）。 根据本发明，可移除的盒（5）的直径至少与止动环（4）的直径一样大，使得可拆卸的可拆卸的盒（5）可以在安装或拆卸止动件 环（4），而不用从凿岩机中移除前部（1a）。 本发明还涉及一种可移除的盒（5），一个止动环（4）和一个结合钻机的钻机。

公开(公告)号：WO2010040750A1

公开(公告)日：2010-04-15

申请号：PCT/EP2009/062976

申请日：2009-10-06

Applicant: NYSTRÖM, Jenny ,  BUVALL, Lisa ,  NILSSON, Ulf ,  HARALDSSON, Börje

Inventor： NYSTRÖM, Jenny ,  BUVALL, Lisa ,  NILSSON, Ulf ,  HARALDSSON, Börje

IPC: A61K31/444 ,  A61P35/00

CPC classification number: A61K31/444

Abstract: Methods are provided of treating renal cancer by administration of certain 3,3',4,4'- tetrahydroxy-2,2'-bipyridine-N,N'-dioxide compounds, especially 3,3',4,4'-tetrahydroxy-2,2'-bipyridine-N,N'-dioxide (Orellanine), using particular administration protocols and dosing regimens, as well as pharmaceutical compositions suitable for use in the treatment methods that are provided.

Abstract translation: 提供了通过施用某些3,3'，4,4'-四羟基-2,2'-联吡啶-N，N'-二氧化物化合物，特别是3,3'，4,4'-四羟基 -2,2'-联吡啶-N，N'-二氧化物（Orellanine），使用特定的给药方案和给药方案，以及适用于所提供的治疗方法的药物组合物。

公开(公告)号：WO2009139719A9

公开(公告)日：2009-11-19

申请号：PCT/SE2009/050560

申请日：2009-05-18

Applicant: FORSKARPATENT I SYD AB ,  NILSSON, Ulf

Inventor： NILSSON, Ulf

IPC: C07H1/00 ,  C07H15/04 ,  C07H15/18 ,  C07H19/056 ,  C07H3/04 ,  C07H5/06 ,  C07H5/10

Abstract: The present invention relates to novel synthesis routes for preparation of thiodigalactosides of the general formula (12). The method comprises the use of a 3-azido-galactosyl thiouronium salt derivative, which is activated to the corresponding thiol in situ , which in turn is directly reacted with a 3-azido-galactosyl bromide resulting in the 3,3'-di-azido-thio-di-galactoside before the thiol has a chance to reduce the azido 10 group. Hence, in situ formation of the 3-azido-galactosyl thiol from the thiouronium salt is essential in the synthesis procedure, because any other method that generate the thiol separately results in extensive unwanted azide reduction.

公开(公告)号：WO2009139719A1

公开(公告)日：2009-11-19

申请号：PCT/SE2009050560

申请日：2009-05-18

Applicant: FORSKARPATENT I SYD AB ,  NILSSON ULF

Inventor： NILSSON ULF

IPC: C07H1/00 ,  C07H3/04 ,  C07H5/06 ,  C07H5/10 ,  C07H15/04 ,  C07H15/18 ,  C07H19/056

CPC classification number: C07H5/10 ,  C07H19/056

Abstract: The present invention relates to novel synthesis routes for preparation of thiodigalactosides of the general formula (12). The method comprises the use of a 3-azido-galactosyl thiouronium salt derivative, which is activated to the corresponding thiol in situ, which in turn is directly reacted with a 3-azido-galactosyl bromide resulting in the 3,3'-di-azido-thio-di-galactoside before the thiol has a chance to reduce the azido 10 group. Hence, in situ formation of the 3-azido-galactosyl thiol from the thiouronium salt is essential in the synthesis procedure, because any other method that generate the thiol separately results in extensive unwanted azide reduction.

Abstract translation: 本发明涉及用于制备通式（12）的硫二糖苷的新型合成路线。 该方法包括使用3-叠氮基 - 半乳糖基硫脲盐衍生物，其被原位活化到相应的硫醇上，其又与3-叠氮基 - 半乳糖基溴直接反应，得到3,3'-二 - 硫代二硫代双半乳糖苷之前硫醇有机会减少叠氮基10组。 因此，在合成过程中，从β-硫脲鎓盐中原位形成3-叠氮基 - 半乳糖基硫醇是必需的，因为分别产生硫醇的任何其它方法导致广泛的不希望的叠氮化物还原。

公开(公告)号：WO2009109429A1

公开(公告)日：2009-09-11

申请号：PCT/EP2009/050998

申请日：2009-01-29

Applicant: SIEMENS AKTIENGESELLSCHAFT ,  KAY, Peter ,  NILSSON, Ulf ,  SENIOR, Peter

Inventor： KAY, Peter ,  NILSSON, Ulf ,  SENIOR, Peter

IPC: F01C1/344 ,  F01C11/00 ,  F04C18/344 ,  F02B29/00 ,  F02C3/22 ,  F02M37/06

CPC classification number: F01C11/008 ,  F01C1/3442 ,  F04C18/3442 ,  F04C25/00

Abstract: A method for compressing gaseous fuel is disclosed, which comprises the steps: a) ingesting gaseous fuel into a chamber; b) ingesting air into the chamber and mixing the gaseous fuel with the air; c) igniting and partially combusting the resulting mixture of gaseous fuel and air in a confined space such that a predominant fraction of the gaseous fuel is not combusted, causing an increased temperature and therefore an increased pressure of the fraction of the gaseous fuel which is not combusted; and d) discharging the resulting compressed gaseous fuel. Moreover, a compressor (1) is provided, comprising a casing (2), a rotor (3) with at least three vanes (6), at least one inlet (7) for gaseous fuel, at least one outlet (11) for gaseous fuel, at least one air inlet (9) and at least one igniter (14). The rotor (3) is placed in the casing (2) such that at least three variable-volume chambers (15, 16, 17) part-bounded by the vanes (6) are formed during a rotor revolution, the inlet (7) for gaseous fuel is placed in the casing (2) such that the inlet (7) for gaseous fuel is connected to a first location where a chamber (15) has an increasing volume during a revolution of the rotor (3), the air inlet (9) and the igniter (14) are placed in the casing (2) in a second location where a chamber (16) has an increasing, decreasing or constant volume during a revolution of the rotor (3), and the outlet (11) for gaseous fuel is placed in the casing in a third location where a chamber (17) has a decreasing volume during a revolution of the rotor (3). Furthermore, a gas turbine comprising an inventive compressor (1) is disclosed.

Abstract translation: 公开了一种压缩气体燃料的方法，其包括以下步骤：a）将气体燃料吸入室中; b）将空气吸入室内并将气体燃料与空气混合; c）点燃和部分燃烧所产生的气态燃料和空气的混合物在密闭空间中，使得主要部分的气体燃料不燃烧，导致升高的温度，因此不增加气态燃料部分的压力 燃烧; 和d）排出所得到的压缩气体燃料。 此外，提供了一种压缩机（1），包括壳体（2），具有至少三个叶片（6）的转子（3），用于气体燃料的至少一个入口（7），至少一个用于 气体燃料，至少一个空气入口（9）和至少一个点火器（14）。 转子（3）被放置在壳体（2）中，使得在转子旋转期间形成由叶片（6）部分界定的至少三个可变容积的室（15,16,17），入口（7） 气体燃料被放置在壳体（2）中，使得用于气体燃料的入口（7）连接到在转子（3）的转动期间室（15）具有增加的体积的第一位置，空气入口 （9）和点火器（14）在转子（3）的转动期间在室（16）具有增加的，减小的或恒定的体积的第二位置处放置在壳体（2）中，并且出口（11） ）用于气体燃料的第三位置放置在壳体内，在第三位置，在转子（3）的转动期间室（17）具有减小的体积。 此外，公开了一种包括本发明的压缩机（1）的燃气涡轮机。

公开(公告)号：WO2009089921A2

公开(公告)日：2009-07-23

申请号：PCT/EP2008053586

申请日：2008-03-27

Applicant: SIEMENS AG ,  NILSSON ULF

Inventor： NILSSON ULF

IPC: F02C7/224

CPC classification number: F02C7/224 ,  F01D15/08 ,  F02C6/10 ,  F02C7/12

Abstract: A gas turbine engine (100) with - a compressor section (105), - a combustor section (106) comprising at least one combustor (107, 110), - a turbine section (112), - at least one gaseous fuel supply conduit (22) with an upstream section (23) and a downstream section (25) the downstream section (25) being connected to the combustor (107, 110) for delivering gaseous fuel and - a fuel booster located in the gaseous fuel supply conduit, the fuel booster (1) having a driving expander (9) with a driving fluid inlet (11) that is in flow connection with a compressed air outlet (116) of the gas turbine engine's compressor, for receiving compressed air and a driving fluid outlet (13) for discharging expanded air and a fuel compressor (17) with a low pressure fuel inlet (19) connected to the upstream section (23) of the gaseous fuel supply conduit (22) and a high pressure fuel outlet (21) connected to the downstream section (25) of the gaseous fuel supply conduit (22), characterised in that a heat exchanger (3) is present which is located such between the unexpanded driving fluid or the expanded driving fluid on the one side and the low pressure gaseous fuel or the high pressure gaseous fuel on the other side that a heat transfer between the air and the gaseous fuel is possible.

Abstract translation: 一种具有压缩机部分（105）的燃气涡轮发动机（100）， - 包括至少一个燃烧器（107,110）的燃烧器部分（106）， - 涡轮部分（112）， - 至少一个气体燃料供应管道 （22）具有上游部分（23）和下游部分（25），所述下游部分（25）连接到用于输送气体燃料的燃烧器（107,110）和 - 位于所述气体燃料供应管道中的燃料增压器， 燃料助力器（1）具有驱动膨胀器（9），其具有与燃气涡轮发动机的压缩机的压缩空气出口（116）流动连接的驱动流体入口（11），用于接收压缩空气和驱动流体出口 用于排放膨胀空气的燃料压缩机（13）和连接到气体燃料供应管道（22）的上游部分（23）的低压燃料入口（19）的燃料压缩机（17）和连接到气体燃料供应管道 到达气体燃料供应管道（22）的下游部分（25），其特征在于热量 存在交换器（3），其位于一侧的未膨胀的驱动流体或膨胀的驱动流体之间，另一侧上的低压气态燃料或高压气体燃料之间，空气和气体之间的热传递 燃料是可能的。

公开(公告)号：WO2008128954A1

公开(公告)日：2008-10-30

申请号：PCT/EP2008/054656

申请日：2008-04-17

Applicant: SIEMENS AKTIENGESELLSCHAFT ,  HEYES, Francis ,  NILSSON, Ulf

Inventor： HEYES, Francis ,  NILSSON, Ulf

IPC: F01D5/04 ,  F04D29/02 ,  F04D29/28

CPC classification number: F01D5/046 ,  F01D5/288 ,  F01D11/02 ,  F04D29/023 ,  F04D29/284 ,  F05D2220/40 ,  F05D2230/31 ,  F05D2230/90 ,  F05D2300/2112 ,  F05D2300/43

Abstract: An impeller (12) is provided with a back surface that is at least partly coated with a thermal barrier coating (14) comprising an anodised layer, polymer or polymer-based ceramics.

Abstract translation: 叶轮（12）设置有至少部分地涂覆有包含阳极氧化层，聚合物或聚合物基陶瓷的热障涂层（14）的后表面。