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    HEAT EXCHANGER FOR COOLED COOLING AIR
    101.
    发明申请
    HEAT EXCHANGER FOR COOLED COOLING AIR 审中-公开
    用于冷却冷却空气的热交换器

    公开(公告)号：US20170044982A1

    公开(公告)日：2017-02-16

    申请号：US14826871

    申请日：2015-08-14

    Applicant: United Technologies Corporation

    Inventor： Paul W. Duesler ,  Frederick M. Schwarz

    IPC: F02C7/18 ,  F02C7/141

    CPC classification number: F02C7/185 ,  F01D25/12 ,  F02C7/141 ,  F02C7/32 ,  F05D2220/32 ,  F05D2240/91 ,  F05D2250/42 ,  F05D2260/213 ,  F05D2260/232 ,  F05D2260/30 ,  F05D2260/941 ,  F28F9/002 ,  F28F2265/26 ,  Y02T50/675

    Abstract: A heat exchanger (HEX) for cooling air in a gas turbine engine is provided. The HEX may comprise an intake manifold in fluid communication with a compressor section and configured to receive air from the compressor section, an outtake manifold in fluid communication with the intake manifold via a tube, and a cooling air flow path defined by at least one of an outer surface of the tube, an outer surface of the intake manifold, and an outer surface of the outtake manifold, wherein the cooling air flow path is orthogonal to said tube. The air from the intake manifold may travel through the tube to the outtake manifold and from the outtake manifold to a portion of the gas turbine engine.

    Abstract translation: 提供一种用于在燃气涡轮发动机中冷却空气的热交换器（HEX）。 HEX可以包括与压缩机部分流体连通并被配置为从压缩机部分接收空气的进气歧管，经由管与进气歧管流体连通的出口歧管和由至少一个 管的外表面，进气歧管的外表面和出口歧管的外表面，其中冷却空气流动路径与所述管正交。 来自进气歧管的空气可以通过管移动到出口歧管，并且从出口歧管移动到燃气涡轮发动机的一部分。

    HEAT EXCHANGER FOR COOLED COOLING AIR WITH ADJUSTABLE DAMPER
    102.
    发明申请
    HEAT EXCHANGER FOR COOLED COOLING AIR WITH ADJUSTABLE DAMPER 审中-公开
    热交换器用于冷却冷却空气与可调节阻尼器

    公开(公告)号：US20170044980A1

    公开(公告)日：2017-02-16

    申请号：US15062400

    申请日：2016-03-07

    Applicant: United Technologies Corporation

    Inventor： Paul W. Duesler ,  Frederick M. Schwarz

    IPC: F02C7/18 ,  F28F9/013 ,  F28D1/047 ,  F28F9/02 ,  F28F9/00

    CPC classification number: F02C7/18 ,  F02C7/141 ,  F02K3/115 ,  F04D29/5826 ,  F05D2260/213 ,  F28D1/0475 ,  F28D7/06 ,  F28D2021/0021 ,  F28D2021/0026 ,  F28F9/0268 ,  F28F9/24 ,  Y02T50/675

    Abstract: A heat exchanger (HEX) for cooling air in a gas turbine engine is provided. An adjustable damper is provided. The adjustable damper may be for damping a movement of the HEX relative to the gas turbing engine. An adjustable damper may comprise: a first tube; a second tube located at least partially within the first tube; a housing coupled to the second tube; a moveable member, the moveable member comprising a contacting surface in contact with the second tube; an adjusting member adjustably coupled to the housing; and a spring member located between the moveable member and the adjusting member, the spring member configured to at least one of compress or decompress in response to adjusting member moving relative to the housing.

    Abstract translation: 提供一种用于在燃气涡轮发动机中冷却空气的热交换器（HEX）。 提供可调节阻尼器。 可调阻尼器可以用于阻止HEX相对于气体涡流发动机的运动。 可调节阻尼器可以包括：第一管; 至少部分地位于第一管内的第二管; 联接到所述第二管的壳体; 可移动构件，所述可移动构件包括与所述第二管接触的接触表面; 可调节地联接到所述壳体的调节构件; 以及位于所述可移动构件和所述调节构件之间的弹簧构件，所述弹簧构件构造成响应于调节构件相对于所述壳体移动而被压缩或减压中的至少一个。

    AIR SUPPLY AND CONDITIONING SYSTEM FOR A GAS TURBINE
    104.
    发明申请
    AIR SUPPLY AND CONDITIONING SYSTEM FOR A GAS TURBINE 有权
    用于气体涡轮机的空气供应和调节系统

    公开(公告)号：US20170002739A1

    公开(公告)日：2017-01-05

    申请号：US14755406

    申请日：2015-06-30

    Applicant: General Electric Company

    Inventor： Juan Leonardo Soria Ramirez ,  Ismael Orozco Arciga ,  Luis Alberto Aguado Mandujano ,  Humberto Sanchez Moreno

    IPC: F02C7/141 ,  F02C7/052

    CPC classification number: F02C7/141 ,  B01D53/26 ,  F02C6/08 ,  F02C7/052 ,  F02C7/055 ,  F05D2220/32 ,  F05D2260/209 ,  F05D2260/607 ,  F25B9/04 ,  Y02T50/675

    Abstract: An air supply and conditioning system for an inlet system of a gas turbine includes an air processing unit having an inlet configured to receive compressed air from a compressor of the gas turbine. The air processing unit includes a heat exchanger that is downstream from the inlet. A vortex cooler is disposed downstream from the inlet of the air processing unit. The vortex cooler is in fluid communication with the heat exchanger and with an outlet of the air processing unit. The system further includes a self-cleaning filter that is disposed within a duct of the inlet system. The self-cleaning filter is in fluid communication with at least one of the outlet of the air processing unit or an outlet of the vortex cooler.

    Abstract translation: 用于燃气轮机的入口系统的空气供应和调节系统包括空气处理单元，其具有被配置为从燃气轮机的压缩机接收压缩空气的入口。 空气处理单元包括在入口下游的热交换器。 涡流冷却器设置在空气处理单元的入口的下游。 涡流冷却器与热交换器和空气处理单元的出口流体连通。 该系统还包括设置在入口系统的管道内的自清洁过滤器。 自清洁过滤器与空气处理单元的出口或涡流冷却器的出口中的至少一个流体连通。

    POWER GENERATION SYSTEM EXHAUST COOLING
    106.
    发明申请
    POWER GENERATION SYSTEM EXHAUST COOLING 有权
    发电系统排风冷却

    公开(公告)号：US20160376991A1

    公开(公告)日：2016-12-29

    申请号：US14753066

    申请日：2015-06-29

    Applicant: General Electric Company

    Inventor： Lewis Berkley Davis, JR. ,  Parag Prakash Kulkarni ,  Robert Joseph Reed

    IPC: F02C7/141 ,  F02C7/18 ,  F02C3/04 ,  F02C6/08

    CPC classification number: F02C7/141 ,  F01D25/305 ,  F01N3/2066 ,  F02C6/08 ,  F02C7/18 ,  F02C9/18 ,  F02K3/00 ,  F05D2270/082

    Abstract: An airflow control system for a gas turbine according to an embodiment includes: an airflow generation system for attachment to a rotatable shaft of a gas turbine system, the airflow generation system drawing in an excess flow of air through an air intake section; a mixing area for receiving an exhaust gas stream of the gas turbine system; an air extraction system for: extracting at least a portion of the excess flow of air generated by the airflow generation system to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.

    Abstract translation: 根据实施例的用于燃气轮机的气流控制系统包括：用于附接到燃气轮机系统的可旋转轴的气流产生系统，所述气流产生系统通过进气部分吸入空气过量; 用于接收燃气轮机系统的废气流的混合区域; 空气提取系统，用于：提取由气流发生系统产生的空气过剩的至少一部分，以提供旁路空气; 并将旁路空气转移到混合区域中以降低废气流的温度; 以及用于处理降温废气流的废气处理系统。

    GAS TURBINE POWER GENERATION EQUIPMENT, AND DEVICE AND METHOD FOR DRYING GAS TURBINE COOLING AIR SYSTEM
    107.
    发明申请
    GAS TURBINE POWER GENERATION EQUIPMENT, AND DEVICE AND METHOD FOR DRYING GAS TURBINE COOLING AIR SYSTEM 审中-公开
    气体涡轮发电设备，以及用于干燥气体涡轮机冷却空气系统的装置和方法

    公开(公告)号：US20160326963A1

    公开(公告)日：2016-11-10

    申请号：US15111093

    申请日：2015-01-21

    Applicant: MITSUBISHI HITACHI POWER SYSTEMS, LTD.

    Inventor： Shinichi YAMAZAKI ,  Jiro ASAKUNO

    IPC: F02C7/30 ,  F02C7/14 ,  F02C3/107

    CPC classification number: F02C7/30 ,  F01D25/32 ,  F02C3/107 ,  F02C7/14 ,  F02C7/141 ,  F02C7/185 ,  F02C7/32 ,  F05D2210/12 ,  F05D2220/32 ,  F05D2260/211 ,  F05D2260/232 ,  F05D2260/608

    Abstract: The occurrence of corrosion on the inner surfaces of pipes is to be minimized in a cooling air system of a gas turbine. Specifically, this gas turbine power generation equipment has: a gas turbine including a turbine connected to a generator, a combustor that supplies combustion gas to the turbine, and a compressor that supplies compressed air to the combustor; a cooling air system that supplies compressed air bled from the compressor to the turbine, the cooling air system being connected at a first end side to an intermediate stage or an outlet of the compressor and connected at a second end side to the turbine; and a drying air system that supplies drying air into the cooling air system when the gas turbine is stopped, the drying air system being connected to the cooling air system.

    Abstract translation: 在燃气轮机的冷却空气系统中，要使管子内表面的腐蚀发生最小化。 具体而言，该燃气轮机发电设备具有：燃气轮机，其包括与发电机连接的涡轮机，将燃料气体供给到涡轮机的燃烧器和向燃烧器供给压缩空气的压缩机; 将从压缩机排出的压缩空气供给到涡轮机的冷却空气系统，所述冷却空气系统在第一端侧连接到所述压缩机的中间台或出口并在第二端侧连接到所述涡轮机; 以及干燥空气系统，其在燃气轮机停止时向干燥空气系统供给干燥空气，所述干燥空气系统与所述冷却风系统连接。

    HEAT PIPE TEMPERATURE MANAGEMENT SYSTEM FOR A TURBOMACHINE
    108.
    发明申请
    HEAT PIPE TEMPERATURE MANAGEMENT SYSTEM FOR A TURBOMACHINE 有权
    涡轮管热管温度管理系统

    公开(公告)号：US20160290233A1

    公开(公告)日：2016-10-06

    申请号：US14676936

    申请日：2015-04-02

    Applicant: General Electric Company

    Inventor： Sanji Ekanayake ,  Joseph Paul Rizzo ,  Alston Ilford Scipio ,  Timothy Tahteh Yang ,  Thomas Edward Wickert

    IPC: F02C7/141 ,  F02C6/08 ,  F01K23/02 ,  F02C7/224

    CPC classification number: F02C7/141 ,  F01D5/082 ,  F01D5/088 ,  F01D5/18 ,  F01D5/181 ,  F01D9/065 ,  F01D25/125 ,  F01K23/02 ,  F02C6/08 ,  F02C6/18 ,  F02C7/14 ,  F02C7/143 ,  F02C7/224 ,  F05D2260/208 ,  Y02E20/16

    Abstract: A turbomachine includes a compressor having an inter-stage gap between adjacent rows of rotor blades and stator vanes. A combustor is connected to the compressor, and a turbine is connected to the combustor. An intercooler is operatively connected to the compressor, and includes a first plurality of heat pipes that extend into the inter-stage gap. The first plurality of heat pipes are operatively connected to a first manifold, and the heat pipes and the first manifold are configured to transfer heat from the compressed airflow from the compressor to heat exchangers. A cooling system is operatively connected to the turbine, and includes a second plurality of heat pipes located in the turbine nozzles. The second plurality of heat pipes are operatively connected to a second manifold, and the heat pipes and the second manifold are configured to transfer heat from the turbine nozzles to the heat exchangers.

    Abstract translation: 涡轮机包括压缩机，其具有在相邻的转子叶片和定子叶片之间的间隔间隙。 燃烧器连接到压缩机，并且涡轮连接到燃烧器。 中间冷却器可操作地连接到压缩机，并且包括延伸到级间间隙中的第一多个热管。 第一多个热管可操作地连接到第一歧管，并且热管和第一歧管被配置为将热量从压缩空气流从压缩机传递到热交换器。 冷却系统可操作地连接到涡轮机，并且包括位于涡轮喷嘴中的第二多个热管。 第二多个热管可操作地连接到第二歧管，并且热管和第二歧管被配置为将热量从涡轮喷嘴传递到热交换器。

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