公开(公告)号：US20130174737A1

公开(公告)日：2013-07-11

申请号：US13737414

申请日：2013-01-09

Applicant: ALSTOM Technology Ltd

Inventor： Philippe CHANTEREAU

IPC: B01D53/22

CPC classification number: B01D53/22 ,  B01D53/228 ,  B01D69/02 ,  B01D2258/06 ,  B01D2325/02 ,  B01D2325/022 ,  G21D1/00 ,  G21F9/02 ,  Y02E30/40

Abstract: A membrane for a method for filtration of gas effluents from an industrial installation including a wall having an internal surface and an external surface, the wall having pores of variable dimensions in the radial direction and in the longitudinal direction of the wall.

Abstract translation: 一种用于从包括具有内表面和外表面的壁的工业设备中过滤气体流出物的方法的膜，所述壁具有在径向和纵向方向上具有可变尺寸的孔。

公开(公告)号：US20130174565A1

公开(公告)日：2013-07-11

申请号：US13736980

申请日：2013-01-09

Applicant: ALSTOM Technology Ltd.

Inventor： Susanne Renate Schell ,  Thiemo Meeuwissen

IPC: F02C9/40

CPC classification number: F02C9/40 ,  F02C3/22 ,  F02C3/24 ,  F02C3/30 ,  F05D2270/082 ,  F05D2270/16

Abstract: A method for operating a gas turbine, which is optionally operated with a gaseous fuel (A) having a gaseous mass flow ({dot over (m)}gas)and/or with an oil fuel (B) having an oil mass flow ({dot over (m)}oil), wherein a change between an operating mode with gaseous fuel (A) and an operating mode with oil fuel (B) is undertaken during load operation of the gas turbine, and wherein a water addition of a water mass flow ({dot over (m)}H2O) is provided at least in the operating mode with oil fuel (B). The ratio (Ωnorm) of the added water mass flow ({dot over (m)}H2O) to the fuel mass flow during the change between operating modes is determined according to Ω norm = m . H 2  O · LHV norm m . gas · LHV gas + m . oil · LHV oil .

Abstract translation: 一种用于操作燃气轮机的方法，所述燃气轮机任选地与具有气体质量流（{dot（m）}气体）的气体燃料（A）和/或具有油质量流的油燃料（B） （点）（m）}油），其中在燃气轮机的负载操作期间进行在具有燃料（A）的操作模式与具有油燃料（B）的操作模式之间的变化，并且其中添加水 至少在操作模式下，与油燃料（B）一起提供水质量流量（{dot over（m）} H2O）。 根据Omega norm = m确定在操作模式之间改变期间添加的水质量流量（{dot over（m）} H 2 O）与燃料质量流量的比率（Omeganorm）。 H 2 O·LHV范数m。 气体·LHV气体+ m。 油·LHV油。

公开(公告)号：US20130125547A1

公开(公告)日：2013-05-23

申请号：US13683061

申请日：2012-11-21

Applicant: ALSTOM Technology Ltd

Inventor： Mirko Ruben BOTHIEN ,  Martin Zajadatz ,  Douglas Anthony Pennell

IPC: F23R3/28 ,  F23N1/00 ,  F02C9/26

CPC classification number: F23R3/28 ,  F02C9/26 ,  F05D2270/31 ,  F23N1/00 ,  F23N5/242 ,  F23N2041/20 ,  F23R3/36

Abstract: A method and apparatus are disclosed for operating a combustion device during a transient operation. The combustion device is fed with at least a fuel. The transient operation includes a period having a period length (T) during which the fuel is fed in an amount lower that a designated (e.g., critical) amount (Mc). A limit value (L) is defined for the period length (T), and fuel feed is regulated to keep the period length (T) smaller or equal to the limit value (L).

Abstract translation: 公开了用于在瞬态操作期间操作燃烧装置的方法和装置。 燃烧装置供给至少一种燃料。 瞬态操作包括具有以低于指定（例如临界）量（Mc）的量供给燃料的周期长度（T）的周期。 对于周期长度（T）定义极限值（L），并且调节燃料供给以使周期长度（T）小于或等于极限值（L）。

公开(公告)号：US20130091852A1

公开(公告)日：2013-04-18

申请号：US13649502

申请日：2012-10-11

Applicant: ALSTOM TECHNOLOGY LTD

Inventor： John Philip Wood ,  Madhavan Poyyapakkam ,  Andrea Ciani ,  Khawar Syed ,  Thierry Lachaux ,  Franklin Marie Genin ,  Adnan Eroglu

IPC: F02C9/40

CPC classification number: F01D19/00 ,  F02C3/20 ,  F02C9/34 ,  F02C9/40

Abstract: A gas turbine is operated using a varying blend of a first fuel, preferably natural gas, and a second fuel that is hydrogen. The hydrogen concentration is varied depending on operating conditions in order to reduce emissions of CO and NOx, and/or to mitigate LBO. The fuel mixture is varied using a controller based on a combination of factors in a modular operation concept to address different issues according to relevant load limitations. A method of operating a gas turbine according to this modular operational concept is also provided.

Abstract translation: 燃气轮机使用第一燃料，优选天然气和作为氢的​​第二燃料的变化混合来操作。 氢浓度根据操作条件而变化，以减少CO和NOx的排放，和/或减轻LBO。 使用基于模块化操作概念的因素的组合的控制器来改变燃料混合物，以根据相关的负载限制来解决不同的问题。 还提供了一种根据该模块化操作概念来操作燃气轮机的方法。

公开(公告)号：US20040219012A1

公开(公告)日：2004-11-04

申请号：US10823016

申请日：2004-04-13

Applicant: ALSTOM Technology Ltd

Inventor： Alain Hassan

IPC: F01D001/02

CPC classification number: F01D1/04 ,  F01D15/10 ,  F05D2250/323 ,  F05D2250/324

Abstract: A steam turbine 1 constructed in accordance with the present invention comprises a high-pressure module 2 and a low-pressure module 3, a speed-reducing gearbox 4, and an alternator, and wherein the high-pressure module 2 has a single stage of blades 20. This single stage of blades 20 performs the same function as a multi-stage high-pressure module, but with a blade design that is different from the blade design of multi-stage steam turbines. For example, the pressure ratio between the inlet and the outlet of the high-pressure module 2 may be in the range 3 to 20.

Abstract translation: 根据本发明构造的蒸汽轮机1包括高压模块2和低压模块3，减速齿轮箱4和交流发电机，并且其中高压模块2具有单级 叶片20的单级执行与多级高压模块相同的功能，但是具有与多级蒸汽轮机的叶片设计不同的叶片设计。 例如，高压模块2的入口和出口之间的压力比可以在3至20的范围内。

公开(公告)号：US20040201293A1

公开(公告)日：2004-10-14

申请号：US10794983

申请日：2004-03-05

Applicant: ALSTOM Technology Ltd

Inventor： Kevin Mayor

IPC: H02K009/00 ,  H02K001/24

CPC classification number: H02K3/24 ,  H02K1/32 ,  H02K9/005

Abstract: A turbo-generator includes a rotor body and a rotor winding disposed around the rotor body. The rotor winding including a sub slot, a first axial cooling duct having a first inlet and a first outlet, and a second axial cooling duct disposed adjacent and parallel to the first axial cooling duct for multi-path cooling. The second axial cooling duct has a second inlet and a second outlet. The first inlet is disposed offset from the second inlet and the first outlet is disposed offset from the second outlet.

Abstract translation: 涡轮发电机包括转子体和设置在转子体周围的转子绕组。 包括副槽的转子绕组，具有第一入口和第一出口的第一轴向冷却管道和与第一轴向冷却管道相邻并平行设置的用于多路径冷却的第二轴向冷却管道。 第二轴向冷却通道具有第二入口和第二出口。 第一入口设置成偏离第二入口并且第一出口设置成偏离第二出口。

公开(公告)号：US10907549B2

公开(公告)日：2021-02-02

申请号：US14576712

申请日：2014-12-19

Applicant: ALSTOM Technology Ltd

Inventor： Michael Düsing ,  Adnan Eroglu

IPC: F02C9/28 ,  F02C3/14 ,  F02C6/00 ,  F02C9/34 ,  F02C7/228 ,  F23C6/04

Abstract: The invention concerns a method for a part load CO reduction operation and a low-CO emissions operation of a gas turbine with sequential combustion. The gas turbine essentially includes at least one compressor, a first combustor which is connected downstream to the compressor. The hot gases of the first combustor are admitted at least to an intermediate turbine or directly or indirectly to a second combustor. The hot gases of the second combustor are admitted to a further turbine or directly or indirectly to an energy recovery. At least one combustor runs under a caloric combustion path having a can-architecture, and wherein the air ratio (λ) of the combustion at least of the second combustor is kept below a maximum air ratio (λmax).

公开(公告)号：US10718520B2

公开(公告)日：2020-07-21

申请号：US14061954

申请日：2013-10-24

Applicant: ALSTOM Technology Ltd

Inventor： Mirko Ruben Bothien ,  Jaan Hellat ,  Bruno Schuermans

IPC: F23R3/06 ,  F23R3/34 ,  F23M20/00 ,  F02C6/02 ,  F23R3/00

Abstract: The invention concerns a damper arrangement for reducing combustion-chamber pulsation arising inside a gas turbine, wherein the gas turbine includes at least one compressor, a primary combustor which is connected downstream to the compressor, and the hot gases of the primary combustor are admitted at least to an intermediate turbine or directly or indirectly to a secondary combustor. The hot gases of the secondary combustor are admitted to a further turbine or directly or indirectly to an energy recovery, wherein at least one combustor is arranged in a can-architecture. At least one combustor liner includes air passages, wherein at least one of the air passages is formed as a damper neck. The damper neck being actively connected to a damper volume, and the damper volume is part of a connecting duct extending between a compressor air plenum and the combustor.

公开(公告)号：US10544736B2

公开(公告)日：2020-01-28

申请号：US14245639

申请日：2014-04-04

Applicant: ALSTOM Technology Ltd

Inventor： Madhavan Narasimhan Poyyapakkam ,  Khawar Syed ,  Klaus Knapp ,  Torsten Wind

IPC: F02C7/057 ,  F23N1/02 ,  F23R3/26

Abstract: A combustion chamber including a body with a fuel supply duct for supplying a fuel into the body and a carrier air supply duct for supplying air into the body. An adjusting system adjusts the carrier air mass flow supplied into the body according to the features of the fuel.

公开(公告)号：US10422535B2

公开(公告)日：2019-09-24

申请号：US14260617

申请日：2014-04-24

Applicant: ALSTOM Technology Ltd

Inventor： Klaus Knapp ,  Naresh Aluri ,  Nicolas Tran ,  Ulrich Rathmann ,  Franklin Marie Genin

IPC: F23R3/28 ,  F23R3/14 ,  F23R3/34 ,  F23R3/46

Abstract: The invention relates to a can-combustor for a can-annular combustor arrangement in a gas turbine. The can combustor includes an essentially cylindrical casing with an axially upstream front panel and an axially downstream outlet end. The can combustor further includes a number of premixed burners, extending in an upstream direction from said front panel and having a burner exit, supported by this front panel, for supplying a fuel/air mixture into a combustion zone inside the casing. Up to four premixed burners are attached to the front panel in a substantially annular array. Each burner has a conical swirl generator and a mixing tube to induce a swirl flow of said fuel/air mixture.