公开(公告)号：EP3396169A1

公开(公告)日：2018-10-31

申请号：EP17168535.7

申请日：2017-04-27

申请人： Cryostar SAS

发明人： DARRY, Marina

IPC分类号： F04D17/12 ,  F04D17/14 ,  F04D27/02

CPC分类号： F04D27/0207 ,  F04D17/122 ,  F04D17/14 ,  F04D27/0269 ,  F04D27/0276 ,  F05D2270/10 ,  F05D2270/3011 ,  F05D2270/3013 ,  F05D2270/303

摘要： Method for controlling a plural stage compressor comprising at least a first stage (10), a second stage (20) and a first inter-stage line (12) between the first stage (10) and the second stage (20), comprising the steps of:
a- measuring the temperature at the inlet of the compressor,
b- measuring the ratio between the outlet pressure (Pout) and the inlet pressure (Pin) of the first stage (10) of the compressor,
c- calculating a coefficient (Ψ) based at least on the value of the inlet temperature (Tin) and on the measured pressure ratio (Pout/Pin),
d- if the calculated coefficient (Ψ)is in a predetermined range, acting on a control valve (70; 76; 92) mounted in a line (4; 8) supplying the inlet of the first stage (10) of the compressor or in a gas recycle line (74) which opens into the first inter-stage line (12).

公开(公告)号：EP3396117A1

公开(公告)日：2018-10-31

申请号：EP18168803.7

申请日：2018-04-23

申请人： Doosan Heavy Industries & Construction Co., Ltd.

发明人： CHOI, Byung Hee

IPC分类号： F01D25/02 ,  F02C9/20

CPC分类号： F02C7/047 ,  F01D25/02 ,  F02C3/04 ,  F02C9/20 ,  F02C9/26 ,  F05D2220/32 ,  F05D2270/303 ,  F05D2270/304

摘要： A gas turbine system, and a control apparatus (100) and method thereof, can control the amount of compressed air supplied to each of a combustor and an anti-icing unit (70) in order to improve the droop control performance of the gas turbine system. The control apparatus of the gas turbine system may include a sensing unit (110) to measure a rotor speed of the turbine; and a compressed air distribution unit (120) to adjust a distribution ratio of the compressed air supplied to the combustor to the compressed air supplied to the anti-icing unit, based on the measured rotor speed. The control apparatus can increase the amount of compressed air supplied to the combustor even though the revolution number of the turbine connected with a system frequency may be significantly lowered.

公开(公告)号：EP3168428B1

公开(公告)日：2018-09-12

申请号：EP16190765.4

申请日：2016-09-27

申请人： Rolls-Royce plc

发明人： Holt, Jonathan ,  Lewis, Leo

IPC分类号： F01D11/24 ,  F01D21/12 ,  F01D17/02 ,  F01D5/02 ,  F01D21/00 ,  F01D25/12 ,  F01D25/14 ,  F01D25/24 ,  F02C7/18 ,  F02C9/18

CPC分类号： F02C9/18 ,  F01D5/02 ,  F01D11/24 ,  F01D17/02 ,  F01D21/003 ,  F01D21/12 ,  F01D25/12 ,  F01D25/14 ,  F01D25/24 ,  F02C7/18 ,  F05D2220/32 ,  F05D2260/20 ,  F05D2270/112 ,  F05D2270/303

摘要： A case cooling calibration system for a gas turbine engine comprises a rotor casing, and a rotor stage, rotatably mounted within the rotor casing. The rotor casing comprises in series fluid communication, a duct, a flow control valve, and a manifold. The valve is operable to regulate an air flow through the duct to the manifold, with the manifold arranged radially outwardly around the casing radially coplanar with the rotor stage. A temperature sensing apparatus is positioned on the rotor casing, radially outwardly of the rotor stage. A controller is operable to regulate the valve in a stepwise manner to provide a variable cooling air flow to the rotor casing. A processor is operable to calculate a correction characteristic in dependence on a comparison between the rotor casing temperature and a predicted rotor casing temperature for a given engine power condition. An engine controller is operable to control the valve in dependence on the correction characteristic to maintain a predetermined operational radial clearance between the rotor stage and the rotor casing.

公开(公告)号：EP3311277A2

公开(公告)日：2018-04-25

申请号：EP16852222.5

申请日：2016-06-14

申请人： Sikorsky Aircraft Corporation

发明人： LEFEVRE, Brian D.

IPC分类号： G06F11/30

CPC分类号： B64F5/60 ,  B64D15/04 ,  F02C9/18 ,  F05D2260/80 ,  F05D2260/85 ,  F05D2270/303 ,  F05D2270/304 ,  G07C5/006

摘要： A method for diagnosing the function of an anti-ice/start bleed valve (AISBV) includes determining an operating mode of an engine and retrieving current engine system data associated with the operating mode. The method includes indicating whether the AISBV is functioning properly based on the current engine system data. An AISBV assessment system includes an AISB V assessment module configured to be operatively connected to a plurality of sensors. The AISBV assessment module includes a processor operatively connected to a memory, wherein the memory includes instructions recorded thereon that, when read by the processor, cause the processor to determine an operating mode of an engine, retrieve current engine system data associated with the operating mode, and indicate whether an AISBV is functioning properly based on the current engine system data.

公开(公告)号：EP2674594A3

公开(公告)日：2018-04-04

申请号：EP13171409.9

申请日：2013-06-11

申请人： General Electric Company

发明人： Liotta, Gary Charles ,  Miranda, Carlos Miguel

IPC分类号： F02C9/16 ,  F02C9/26 ,  F02C9/28 ,  F01D17/08 ,  F02C7/18 ,  F01D5/08

CPC分类号： F01D17/085 ,  F01D5/081 ,  F02C7/18 ,  F02C9/16 ,  F02C9/26 ,  F02C9/28 ,  F05D2260/20 ,  F05D2270/303

摘要： A thermally actuated assembly (10) for a gas turbine assembly for a gas turbine system includes a heat transfer component (20) having a first portion (22) and a second portion (24), wherein the first portion (22) is disposed within a first cavity (14) having a first temperature and the second portion (24) is disposed in a second cavity (16) having a second temperature, wherein the heat transfer component (20) extends through a cavity wall, wherein the first temperature is greater than the second temperature. Also included is a temperature sensitive element (26) disposed within the second cavity (16) and in operable communication with the heat transfer component (20). Further included is a flow manipulating device (30,32) disposed within the second cavity (16) and configured to displace in response to a temperature change in the first cavity (14).

摘要翻译： 一种用于燃气涡轮机系统的燃气涡轮机组件的热致动组件（10）包括具有第一部分（22）和第二部分（24）的传热部件（20），其中第一部分（22）设置在 具有第一温度的第一腔体（14），并且所述第二部分（24）设置在具有第二温度的第二腔体（16）中，其中所述传热部件（20）延伸穿过腔体壁，其中所述第一温度是 大于第二温度。 还包括设置在第二腔体（16）内并且与传热部件（20）可操作连通的温度敏感元件（26）。 还包括布置在第二腔体（16）内并配置为响应于第一腔体（14）中的温度变化而位移的流量控制装置（30,32）。

公开(公告)号：EP3296825A1

公开(公告)日：2018-03-21

申请号：EP17190799.1

申请日：2017-09-13

申请人： General Electric Company

发明人： ZHANG, Hua ,  CARDENAS, Manuel ,  TRAYHAN, David

IPC分类号： G05B17/02 ,  F02C9/28 ,  G05B13/04 ,  G05B23/02

CPC分类号： F02C9/28 ,  F02C9/40 ,  F05D2220/32 ,  F05D2270/07 ,  F05D2270/301 ,  F05D2270/303 ,  F05D2270/44 ,  F05D2270/71 ,  G05B13/041 ,  G05B17/02 ,  G05B23/0294 ,  G06F17/5009

摘要： A system 50 for predicting performance of a liquid fuel system includes a processor 58 and a memory 60 communicatively coupled to the processor, wherein the memory stores instructions which when executed by the processor perform operations. The operations include establishing a baseline parameter for at least one physical parameter of a nozzle or a valve associated with at least one combustor of the liquid fuel system 16 with at least one time. The operations also include obtaining one or more operational parameters associated with the liquid fuel system from one or more sensors 62 during operation of a gas turbine engine 22. The operations further include utilizing an operational model of a fuel flow divider to output an action associated with the liquid fuel system based at least on the baseline parameter and the one or more operational parameters.

摘要翻译： 用于预测液体燃料系统的性能的系统50包括处理器58和通信地耦合到处理器的存储器60，其中存储器存储当由处理器执行时执行操作的指令。 操作包括用至少一次建立与液体燃料系统16的至少一个燃烧器相关联的喷嘴或阀的至少一个物理参数的基线参数。 这些操作还包括在燃气涡轮发动机22的操作期间从一个或多个传感器62获得与液体燃料系统相关联的一个或多个操作参数。操作还包括利用燃料分流器的操作模型来输出与 液体燃料系统至少基于基线参数和一个或多个操作参数。

公开(公告)号：EP3290654A1

公开(公告)日：2018-03-07

申请号：EP17188214.5

申请日：2017-08-28

申请人： General Electric Technology GmbH

发明人： REIGL, Martin

IPC分类号： F01D17/14 ,  F01D21/00

CPC分类号： F01D21/003 ,  F01D17/145 ,  F01D17/20 ,  F05D2220/31 ,  F05D2230/80 ,  F05D2260/80 ,  F05D2270/11 ,  F05D2270/303 ,  F05D2270/332 ,  F05D2270/334 ,  G01M15/14

摘要： The present application provides a method of evaluating inspection intervals in a turbine (100) by a data acquisition system (710). The method may include the steps of receiving a number of operating parameters from a number of sensors (380), wherein the operating parameters may include steam pressure, steam temperature, metal temperature, and valve spindle position, comparing one or more of the operating parameters to predetermined values, and shortening an inspection interval if the one or more of the operating parameters exceed the predetermined values for longer than a predetermined duration.

摘要翻译： 本申请提供了一种通过数据采集系统（710）评估涡轮机（100）中的检查间隔的方法。 该方法可以包括以下步骤：从多个传感器（380）接收多个操作参数，其中操作参数可以包括蒸汽压力，蒸汽温度，金属温度和阀主轴位置，将一个或多个操作参数 到预定值，并且如果一个或多个操作参数超过预定值的时间长于预定持续时间，则缩短检查间隔。

公开(公告)号：EP2538023A3

公开(公告)日：2018-02-28

申请号：EP12172490.0

申请日：2012-06-18

申请人： General Electric Company

发明人： Miranda, Carlos Miguel ,  Cummings, Edward William

IPC分类号： F01D5/08 ,  F01D25/12 ,  F02C7/141

CPC分类号： F02C7/141 ,  F01D5/082 ,  F01D25/12 ,  F05D2270/301 ,  F05D2270/303

摘要： A pressure and temperature actuation system is provided having a high-temperature low-pressure zone, a low-temperature high-pressure zone, a boundary, a pressure actuated mechanism, and a temperature mechanism. A gas located in the high-temperature low-pressure zone has a greater gas temperature than the gas located in the low-temperature high-pressure zone. The gas located in the low-temperature high-pressure zone has a greater gas pressure than the gas located in the high-temperature low-pressure zone. The boundary separates the high-temperature low-pressure zone from the low-temperature high pressure zone. The pressure actuated mechanism is located within the boundary and is configured for opening at a specified gas pressure in either the high-temperature low-pressure zone or the low-temperature high-pressure zone. The temperature actuated mechanism is located within the boundary and is configured for opening at a specified gas temperature in either the high-temperature low-pressure zone or the low-temperature high-pressure zone.

摘要翻译： 提供了具有高温低压区，低温高压区，边界，压力致动机构和温度机构的压力和温度致动系统。 位于高温低压区域的气体比位于低温高压区域的气体具有更高的气体温度。 位于低温高压区域的气体比位于高温低压区域的气体具有更大的气体压力。 边界将高温低压区与低温高压区分开。 压力驱动机构位于边界内，并配置为在高温低压区域或低温高压区域中的特定气体压力下打开。 温度启动机构位于边界内，并配置为在高温低压区域或低温高压区域中的特定气体温度下打开。

公开(公告)号：EP2843211B1

公开(公告)日：2017-12-27

申请号：EP14174900.2

申请日：2014-06-30

申请人： Ansaldo Energia Switzerland AG

发明人： Ferreira-Providakis, Theodoros ,  Singla, Ghislain ,  Meeuwissen, Thiemo ,  Lipari, Sebastian ,  Margari, Nektaria-Ourania

IPC分类号： F02C6/00 ,  F02C7/228 ,  F02C9/20 ,  F02C9/28 ,  F23R3/34

CPC分类号： F02C6/003 ,  F01N3/18 ,  F02C7/22 ,  F02C7/228 ,  F02C9/20 ,  F02C9/28 ,  F05D2270/08 ,  F05D2270/112 ,  F05D2270/303 ,  F23N1/022 ,  F23N5/022 ,  F23N2025/08 ,  F23N2037/02 ,  F23N2041/20 ,  F23R3/346 ,  F23R2900/03341

摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the opening of the row of variable compressor inlet guide vanes (14) is controlled depending on the temperatures of the operative burners (9) of the second combustor (15) and simultaneously the number of operative burners is kept at a minimum. This leads to low CO emissions at partial load of the gas turbine.

公开(公告)号：EP3247909A1

公开(公告)日：2017-11-29

申请号：EP15876240.1

申请日：2015-12-30

申请人： Delta T Corporation

发明人： JOHNSON, Jerrill Scott ,  REED, Alex Christopher ,  BORDERS, Marcus Landon ,  LESSER, Thomas James ,  FIZER, Jason Hunt ,  TUCKER, Adam Glenn ,  HARPER, Stephen Alexander ,  NOBLE, Ernest John ,  TAN, Ken Siong ,  LING, Jon Jet ,  CHAN, Seng Rui

IPC分类号： F04D25/08 ,  F04D27/00

CPC分类号： F04D25/088 ,  F04D27/004 ,  F05D2270/303 ,  F24F7/10 ,  F24F11/30 ,  F24F11/77 ,  F24F13/32 ,  F24F2110/00 ,  F24F2110/10 ,  F24F2110/20

摘要： A system for controlling thermal comfort in a space is provided with a variable mode of operation. The system may include a conditioner for conditioning air in the space, and a sensor for measuring a temperature in the space. A controller is provided for controlling the conditioner based on the temperature sensed by the sensor, and a fan for circulating air within the space is regulated based on the temperature sensed by the sensor. A related system for controlling a fan based on height is also provided, as is a system and method for easily and efficiently determining the height of a fan using a simple camera, such as one on a “smart” phone. A further aspect pertains to a controller, such as for example a portable handheld device, having a user interface adapted for suggesting an increase in a set point temperature of a thermostat based on the selected speed of the fan.