公开(公告)号：EP2730751A3

公开(公告)日：2017-07-19

申请号：EP13191938.3

申请日：2013-11-07

Applicant: Rolls-Royce Deutschland Ltd & Co KG

Inventor： Klauke, Dr.-Ing. Thomas ,  Mojem, Mats ,  Rajaratnam, Nishanth

IPC: F01D17/16 ,  F02C9/20

CPC classification number: F01D9/045 ,  F01D17/162 ,  F02C9/20 ,  F04D29/563 ,  F05D2260/50

Abstract: Die vorliegende Erfindung betrifft eine Leitschaufelverstellvorrichtung einer Gasturbine mit einer Vielzahl von jeweils um eine radiale Achse 44 schwenkbaren Leitschaufeln 20, welche in zumindest zwei Radialebenen angeordnet sind, sowie mit zumindest einem Leitschaufelverstellring 29, welcher mit den jeweiligen Leitschaufeln 20 gekoppelt ist und mittels zumindest einer Betätigungsvorrichtung 30 in Umfangsrichtung drehbar ist, wobei die Betätigungsvorrichtung 30 ein Kurbelwellenelement 31 umfasst, welches mittels eines Aktuators 32 um eine ortsfeste Drehachse 33 verschwenkbar ist, dadurch gekennzeichnet, dass an dem Leitschaufelverstellring 29 gelenkig ein erster Hebel 34 angelenkt ist, dessen freies Ende gelenkig 35 mit einem mittleren Bereich eines zweiten Hebels 36 verbunden ist, wobei der zweite Hebel 36 an seinem einen Ende an einem ortsfesten Drehpunkt 37 gelagert ist und an seinem anderen Ende gelenkig 38 mit einem dritten Hebel 39 gekoppelt ist, welcher an seinem freien Ende gelenkig 40 an dem Kurbelwellenelement 31 gelagert ist.

Abstract translation: 本发明涉及一种Leitschaufelverstellvorrichtung具有在每种情况下绕径向的多个轴，其被布置在至少两个径向平面枢转的叶片20，以及与至少一个Leitschaufelverstellring 29，其被耦合到相应的导向44的燃气涡轮机叶片20和经由至少一个致动装置 30，其特征在于所述致动装置30包括曲柄件31，这是通过围绕固定的旋转致动器32的装置轴线33枢转，其特征在于，第一杆设置在Leitschaufelverstellring 29铰接铰接34，铰接35的自由端在圆周方向上旋转，与 被连接到第二杆36的中央部，第二杆安装在其一端以固定的枢转点37和36连接在其另一端铰接到38的第三杆39在其自由端克 元件40安装在曲轴构件31上。

公开(公告)号：EP2672089A4

公开(公告)日：2017-06-28

申请号：EP11857457

申请日：2011-02-04

Applicant: MITSUBISHI HITACHI POWER SYS

Inventor： KIM EUNKYEONG ,  KOYAMA KAZUHITO ,  HATAMIYA SHIGEO ,  KATAGIRI YUKINORI ,  YOSHIDA TAKUYA ,  KUSUMI NAOHIRO ,  TAKAHASHI KAZUO

IPC: F02C3/30 ,  F02C9/20

CPC classification number: F02C9/00 ,  F02C3/30 ,  F02C7/1435 ,  F02C9/20

Abstract: A controller is intended for use in a gas turbine power plant that includes: a compressor 1 that compresses combustion air; a water atomization cooling apparatus 3 that sprays water drops of atomized water supplied via a water atomization flow rate regulating valve 13 over a flow of air drawn in the compressor 1; a combustor 2 that mixes the compressed combustion air with fuel to thereby burn a fuel-air mixture and generate combustion gas at high temperature and performs combustion switching during operation; a turbine 4 that uses the combustion gas to drive the compressor 1 and a generator; the water atomization flow rate regulating valve 13 that controls a flow rate of the atomized water; and a compressor inlet inner blade 11 that controls a flow rate of air drawn in the compressor 1. The controller includes control means 24 that calculates a fuel-air ratio correction command signal for compensating for reduction in a fuel-air ratio in the combustor 2 occurring during the combustion switching and, based on the fuel-air ratio correction command signal, controls an opening amount of the compressor inlet inner blade 11 or/and an opening amount of the water atomization flow rate regulating valve 13.

Abstract translation: 控制器旨在用于燃气涡轮发电设备，该燃气涡轮发电设备包括：压缩燃烧空气的压缩机1; 该喷射的通过水雾化流量调节阀13在压缩机1吸入的空气的流动供给雾化水水滴水雾化冷却装置3; 燃烧器2，其将压缩的燃烧空气与燃料混合以由此燃烧燃料 - 空气混合物并在高温下产生燃烧气体并且在操作期间执行燃烧切换; 使用燃烧气体驱动压缩机1和发电机的涡轮机4; 控制雾化水的流量的水雾化流量调节阀13， 和压缩机入口内刀片11，其控制在所述压缩机1的控制器包括控制吸入的空气的流动速率装置24计算用于在燃烧器2来补偿减少在燃料 - 空气比的燃料 - 空气比的校正指令信号 燃烧切换时发生的和，基于所述燃料 - 空气比的校正指令信号，控制压缩机的开启量入口内刀片11和/或水雾化流量调节阀13的开口量。

公开(公告)号：EP3181859A1

公开(公告)日：2017-06-21

申请号：EP16200648.0

申请日：2016-11-25

Applicant: General Electric Company

Inventor： CONCHIERI, John Anthony

IPC: F02C3/34 ,  F02C6/18 ,  F02C9/50 ,  F02C3/107

CPC classification number: F02C9/20 ,  F01D25/30 ,  F02C3/04 ,  F02C3/107 ,  F02C3/34 ,  F02C6/18 ,  F02C9/50 ,  F05D2220/32 ,  F05D2220/72 ,  F05D2270/053 ,  Y02E20/14 ,  Y02E20/16

Abstract: A system and method for controlling gas turbine 12 exhaust energy for a gas turbine 12 power plant 10 is disclosed herein. The system includes a gas turbine 12 having a combustor 16 downstream from a compressor 14, a turbine 18 disposed downstream from the combustor 16 and an exhaust duct 44 downstream from an outlet of the turbine 18. An exhaust gas damper 64 is operably connected to a downstream end 66 of the exhaust duct 44 and a compressed gas supply 68 is in fluid communication with the exhaust duct 44 downstream from the turbine outlet and upstream from the exhaust gas damper 64. During operation of the gas turbine 12, the exhaust gas damper 64 and the compressed gas supply 68 increase backpressure at the turbine outlet and restrict axial exit velocity of the exhaust gas 42 exiting the turbine outlet.

Abstract translation: 一种用于燃气涡轮机发电厂12 10控制燃气涡轮机12的废气能量的系统和方法开始是游离缺失盘。 该系统包括从压缩机14中，从燃烧器16和下游设置在涡轮18的排气阻尼器64的出口到排气管44从下游的涡轮18具有燃烧器16的燃气涡轮机12的下游可操作地连接到一个 排气管44和压缩气体供给68的下游端66与排气管44从涡轮机出口下游和上游从排气阻尼器64的流体连通。在燃气涡轮机12，排气阻尼器64的操作 并且在涡轮机出口的压缩气体供给68背压的上升，限制离开涡轮机出口处的排气42的轴向出口速度。

公开(公告)号：EP2971598A4

公开(公告)日：2017-04-19

申请号：EP14801625

申请日：2014-02-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DO LOGAN H ,  SYKES RICHARD L

IPC: F01D17/16 ,  F01D9/04 ,  F02C7/04 ,  F02C9/22

CPC classification number: F01D17/12 ,  F01D9/02 ,  F01D17/02 ,  F01D17/162 ,  F02C9/20 ,  F04D27/0246 ,  F05D2220/3216 ,  F05D2240/12 ,  F05D2270/44

Abstract: A method of controlling a variable vane assembly includes the steps of sensing a first angular deflection of a first array of variable vanes about a first vane axis, and a second angular deflection of a second array of variable vanes about a second vane axis, the first array of variable vanes axially spaced from the second array of variable vanes, and adjusting the angular deflection of one of the first and second arrays of variable vanes, based on the sensed angular deflections from the other of the first and second arrays of variable vanes. A compressor including the variable vane assembly and a method of operating the variable vane assembly for a compressor are also disclosed.

公开(公告)号：EP3141725A1

公开(公告)日：2017-03-15

申请号：EP16178599.3

申请日：2016-07-08

Applicant: United Technologies Corporation

Inventor： HANRAHAN, Paul H. ,  KUPRATIS, Daniel Bernard

IPC: F02C9/22

CPC classification number: F02C9/20 ,  F02C9/22 ,  F05D2270/708

Abstract: A method of controlling a variable area gas turbine engine (10) includes, running the variable area turbine engine (10) at initial settings, monitoring two sets of operating parameters of the engine at the initial settings, and deducing vane angles of adjustable vanes (106) without directly measuring the vane angles from mapped data of the two sets of operating parameters of a similar engine operated while direct vane angle measurements were being recorded.

Abstract translation: 控制可变区的燃气涡轮发动机（10）包括，运行在初始设置的可变截面涡轮发动机（10），在初始设定监测两组的所述发动机的运行参数，并推导可调叶片的叶片角度的方法（ 106），而不脱离两组而正在记录直接叶片角测量操作的类似发动机的操作参数的映射图化数据直接测量叶片角。

公开(公告)号：EP3099911A1

公开(公告)日：2016-12-07

申请号：EP15712838.0

申请日：2015-03-19

Applicant: Siemens Aktiengesellschaft

Inventor： WILKE, Martin

IPC: F02C7/10 ,  F01D25/24

CPC classification number: F01D9/023 ,  F01D25/24 ,  F02C3/04 ,  F02C3/14 ,  F02C3/145 ,  F02C7/08 ,  F02C7/10 ,  F02C7/18 ,  F02C9/18 ,  F02C9/20 ,  F04D29/541 ,  F05D2220/32 ,  F05D2230/80 ,  F05D2240/35 ,  F23R3/002 ,  F23R3/60 ,  F23R2900/03342 ,  Y02E20/16

Abstract: The invention relates to a gas turbine (1) which comprises a compressor (2), a central housing (12), at least one combustion chamber (28), an expansion turbine (26), and a heat exchanger (68). Each combustion chamber (28) is fluidically connected to the expansion turbine (26) via an inner housing (24) which is guided through the interior (10) of the central housing (12). The compressor (2) is fluidically separated from the interior (10) of the central housing (12) by an annular collection chamber (16) which is connected to an outlet (8) of the compressor (2) and which has a number of discharge lines (20) which are connected to the cold side (72) of the heat exchanger (68) during operation. Each combustion chamber is designed as a silo combustion chamber (22), and each silo combustion chamber (28) has an inner wall (30), which delimits a combustion chamber (34), and an outer wall (40), and the outer wall (40) surrounds the inner wall (30), thereby forming a cavity (38). The inner wall (30) transitions into the inner housing (24), and the cavity (38) transitions into the interior (10) of the central housing (12).

Abstract translation: 燃气轮机具有压缩机，中央壳体，至少一个燃烧室，膨胀涡轮机和热交换器。 每个燃烧室通过内部壳体流体地连接到膨胀涡轮机，该内部壳体被引导通过中央壳体的内部。 压缩机通过连接到压缩机的出口的环形收集室与中央壳体的内部流体地分离，并且在操作期间具有连接到热交换器的冷侧的多个排出管线。 每个燃烧室被设计为筒仓燃烧室，并且每个筒仓燃烧室具有限定燃烧室的内壁和外壁，并且外壁围绕内壁，从而形成空腔。 内壁转变到内壳体中，腔体转变到中心壳体的内部。

公开(公告)号：EP3098510A1

公开(公告)日：2016-11-30

申请号：EP16168454.3

申请日：2016-05-04

Applicant: Honeywell International Inc.

Inventor： COFFEY, Scot ,  CHAPMAN, Gregory J. ,  XIONG, Yufei

IPC: F23N3/06 ,  F02C9/18 ,  F02C9/22 ,  F23N5/24

CPC classification number: F02C9/20 ,  F02C9/18 ,  F02C9/22 ,  F02C9/263 ,  F05B2270/101 ,  F05B2270/1011 ,  F05B2270/107 ,  F05D2270/02 ,  F05D2270/051 ,  F05D2270/09 ,  F05D2270/304 ,  F23N3/06 ,  F23N5/242

Abstract: A system and method of accommodating an uncontrolled high thrust condition in a turbofan gas turbine engine includes processing engine data from the turbofan gas turbine engine to determine when a potential for an uncontrolled high thrust condition exists. When the potential for an uncontrolled high thrust condition exists, the engine data are processed to determine whether corrective action for the uncontrolled high thrust condition should be implemented by varying turbofan gas turbine engine effective geometry to (i) increase turbofan gas turbine engine rotational speed or (ii) decrease turbofan gas turbine engine rotational speed. The determined corrective action is automatically implemented.

Abstract translation: 在涡轮风扇燃气涡轮发动机在不受控制的高推力条件收容的系统和方法包括从涡轮风扇燃气涡轮发动机确定性矿当高推力条件不受控制的电势存在处理引擎的数据。 当不受控制的高推力条件为潜在存在，发动机数据被处理以确定矿无论是不受控制的高推力条件校正动作应该由涡轮风扇燃气涡轮发动机的有效几何形状变化被实现（ⅰ）增加涡扇燃气涡轮发动机转速或 （ⅱ）减少涡轮风扇燃气涡轮发动机的旋转速度。 确定性开采纠正措施自动执行。

公开(公告)号：EP2809924A4

公开(公告)日：2016-07-06

申请号：EP13744405

申请日：2013-01-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WEHMEIER ERIC J

IPC: F02C9/16 ,  B05B1/00 ,  F02C7/26

CPC classification number: F02C9/20 ,  F02K1/1207 ,  F02K1/165 ,  F05D2260/85 ,  F05D2270/092

公开(公告)号：EP2984315A4

公开(公告)日：2016-05-18

申请号：EP14840394

申请日：2014-02-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： IZQUIERDO FELIX

IPC: F02C7/042 ,  F01D17/16 ,  F02C9/20 ,  F02K3/075 ,  F02K3/077

CPC classification number: F02C9/20 ,  F01D17/162 ,  F02C3/107 ,  F02K3/075 ,  F02K3/077

Abstract: An annular airflow control system for a gas turbine engine includes a sync ring rotatable to move a multiple of contra-rotating variable vanes between an open position and a closed position to throttle an airflow through said multiple of contra-rotating variable vanes.

公开(公告)号：EP3014088A1

公开(公告)日：2016-05-04

申请号：EP14739015.7

申请日：2014-06-24

Applicant: ExxonMobil Upstream Research Company

Inventor： THATCHER, Jonathan Carl ,  WEST, James A. ,  VOREL, Aaron Lavene

IPC: F02C3/34 ,  F02C6/18 ,  F02C1/08 ,  F01D17/14 ,  F02C7/042 ,  F02C7/057 ,  F02C9/20 ,  F02C1/06 ,  F02C9/22 ,  F02C9/54

CPC classification number: F02C9/00 ,  F01D17/141 ,  F02C1/06 ,  F02C1/08 ,  F02C3/04 ,  F02C3/30 ,  F02C3/34 ,  F02C6/18 ,  F02C7/042 ,  F02C7/057 ,  F02C9/20 ,  F02C9/22 ,  F02C9/54 ,  F05D2240/40 ,  Y02E20/16

Abstract: A method of controlling an exhaust gas recirculation (EGR) gas turbine system includes adjusting an angle of a plurality of inlet guide vanes of an exhaust gas compressor of the EGR gas turbine system, wherein the plurality of inlet guide vanes have a first range of motion defined by a minimum angle and a maximum angle, and wherein the angle is adjusted based on one or more monitored or modeled parameters of the EGR gas turbine system. The method further includes adjusting a pitch of a plurality of blower vanes of a recycle blower disposed upstream of the exhaust gas compressor, wherein the plurality of blower vanes have a second range of motion defined by a minimum pitch and a maximum pitch, and the pitch of the plurality of blower vanes is adjusted based at least on the angle of the plurality of inlet guide vanes.

Abstract translation: 废气再循环（EGR）燃气涡轮机系统的控制的方法，包括调节所述EGR气体涡轮机系统的排气气体压缩机的进口导向叶片的多个角度的，worin入口导向叶片的多元性具有运动的第一范围 由最小角和最大角限定，并且worin的角度是基于所述EGR气体涡轮机系统的一个或多个被监控或建模参数进行调整。该方法还包括调节设置在再循环鼓风机的鼓风机叶片的多个桨距 废气压缩机，worin鼓风机叶片的多元性具有由最小间距和最大桨距，及送风机叶片的多个间距定义的运动的第二范围的上游至少基于的多个角度调整 入口导向叶片。