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    GAS BEARING AND AN ASSOCIATED METHOD THEREOF
    12.
    发明申请
    GAS BEARING AND AN ASSOCIATED METHOD THEREOF 有权
    气体轴承及其相关方法

    公开(公告)号：US20170058951A1

    公开(公告)日：2017-03-02

    申请号：US14836406

    申请日：2015-08-26

    Applicant: General Electric Company

    Inventor： Rodrigo Rodriguez Erdmenger ,  Christopher Edward Wolfe ,  Vittorio Michelassi ,  Quang Tue Nguyen Tran ,  Nathan Evan McCurdy Gibson

    IPC: F16C32/06 ,  F16J15/34 ,  F16C33/72

    CPC classification number: F16C32/0622 ,  F16C32/0607 ,  F16C32/0618 ,  F16C2360/23 ,  F16C2361/00 ,  F16J15/34 ,  F16J15/40

    Abstract: Gas bearing for an aspirating seal assembly is disclosed. The gas bearing includes a bearing body having a bearing surface. The gas bearing further includes a first through-hole disposed in the bearing body, and a plurality of second through-holes spaced apart from each other and disposed around the first through-hole. The first through-hole is characterized by a size, and a first central axis. Each second through-hole is characterized by a size, and a second central axis. The second central axis of each second through-hole in the plurality of second through-holes intersects the first central axis at an angle in a range from about 30 degrees to about 150 degrees or at an angle in a range from about −30 degrees to about −150 degrees. Size of at least one through-hole in the plurality of second through-holes is different from the size of the first through-hole.

    Abstract translation: 公开了用于吸气密封组件的气体轴承。 气体轴承包括具有支承面的轴承体。 气体轴承还包括设置在轴承体中的第一通孔和彼此间隔开并设置在第一通孔周围的多个第二通孔。 第一通孔的特征在于尺寸和第一中心轴线。 每个第二通孔的特征在于尺寸和第二中心轴。 多个第二通孔中的每个第二通孔的第二中心轴与第一中心轴以大约30度至大约150度的角度相交，或者在约-30度到 约-150度。 多个第二通孔中的至少一个通孔的尺寸与第一通孔的尺寸不同。

    SUBSEA FLUID PROCESSING SYSTEM WITH INTERMEDIATE RE-CIRCULATION
    13.
    发明申请
    SUBSEA FLUID PROCESSING SYSTEM WITH INTERMEDIATE RE-CIRCULATION 审中-公开
    具有中间再循环的SUBSEA流体加工系统

    公开(公告)号：US20160138595A1

    公开(公告)日：2016-05-19

    申请号：US14686897

    申请日：2015-04-15

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Guillaume Becquin ,  Rene du Cauze de Nazelle ,  Vittorio Michelassi

    IPC: F04D3/00 ,  F04D15/00

    CPC classification number: F04D3/00 ,  E21B43/01 ,  E21B43/36 ,  F04D13/10 ,  F04D15/0005 ,  F04D15/0027 ,  F04D15/0072 ,  F04D17/14 ,  F04D31/00

    Abstract: A fluid processing system is provided containing a pump and a fluid reservoir. The pump includes a casing, one or more pump stages, a pump inlet, and a pump outlet. The casing includes one or more slots, with at least one slot configured to extract at least a portion of a multiphase fluid flowing within the pump. The fluid reservoir encompasses at least a portion of the casing and is configured to receive and separate the portion of the multiphase fluid into an extracted liquid phase and an extracted gaseous phase. The fluid reservoir includes a re-circulation conduit disposed proximate to the pump inlet and a discharge device coupled to the re-circulation conduit. The discharge device regulates re-circulation of at least a portion of the extracted liquid phase to the pump via the pump inlet for reducing a gas volume fraction of the multiphase fluid being fed to the pump.

    Abstract translation: 提供了一种包含泵和流体储存器的流体处理系统。 泵包括壳体，一个或多个泵级，泵入口和泵出口。 壳体包括一个或多个狭槽，其中至少一个狭槽构造成提取在泵内流动的多相流体的至少一部分。 流体储存器包括壳体的至少一部分并且构造成将多相流体的一部分接收并分离成抽出的液相和萃取的气相。 流体储存器包括靠近泵入口设置的再循环导管和连接到再循环导管的排放装置。 排放装置通过泵入口调节至少部分提取的液相至泵的再循环，以减少供给到泵的多相流体的气体体积分数。

    COUNTER ROTATING HELICO-AXIAL PUMP
    14.
    发明申请
    COUNTER ROTATING HELICO-AXIAL PUMP 有权
    逆转直升机泵

    公开(公告)号：US20140147253A1

    公开(公告)日：2014-05-29

    申请号：US13688613

    申请日：2012-11-29

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Jeremy Daniel Van Dam ,  Vittorio Michelassi ,  René du Cauze de Nazelle ,  Siddharth Navinchandra Ashar ,  Haris Ligata

    IPC: F04D3/00

    CPC classification number: F04D3/00 ,  F04D13/028 ,  F04D19/024 ,  F04D25/028

    Abstract: A counter rotating helico-axial pump is provided, the pump comprising: (a) an inner rotor comprising a plurality of outwardly extending helico-axial impeller vanes; (b) a hollow outer rotor comprising a plurality of inwardly extending helico-axial impeller vanes; (c) a single driving device configured to drive the inner rotor or the hollow outer rotor; and (d) a force transmission coupling joining the inner rotor and the hollow outer rotor and configured to permit rotation of the inner rotor and hollow outer rotor in opposite directions; wherein at least a portion of the inner rotor is disposed within the hollow outer rotor, and wherein the inner rotor, the hollow outer rotor and the helico-axial impeller vanes define a fluid flow path, and wherein the inner rotor and hollow outer rotor are configured such that at least some of adjacent helico-axial impeller vanes are configured to rotate in opposite directions.

    Abstract translation: 提供了一种反向旋转的直轴向泵，所述泵包括：（a）内转子，其包括多个向外延伸的直流叶轮叶片; （b）中空外转子，其包括多个向内延伸的直轴向叶轮叶片; （c）构造成驱动内转子或中空外转子的单个驱动装置; 以及（d）连接所述内转子和所述中空外转子并且构造成允许内转子和中空外转子在相反方向旋转的力传递耦合; 其特征在于，所述内转子的至少一部分设置在所述中空外转子内，并且其中所述内转子，所述中空外转子和所述直流叶轮叶片限定流体流动路径，并且其中所述内转子和中空外转子 被配置成使得至少一些相邻的直叶叶轮叶片构造成沿相反方向旋转。

    CENTRIFUGAL COMPRESSOR AND SYSTEM
    16.
    发明申请
    CENTRIFUGAL COMPRESSOR AND SYSTEM 审中-公开

    公开(公告)号：US20170268528A1

    公开(公告)日：2017-09-21

    申请号：US15075339

    申请日：2016-03-21

    Applicant: General Electric Company

    Inventor： Rodrigo Rodriguez Erdmenger ,  Vittorio Michelassi

    IPC: F04D29/30 ,  F04D29/42 ,  F04D29/28

    CPC classification number: F04D29/30 ,  F04D29/284 ,  F04D29/4206

    Abstract: Centrifugal compressor having flow-control blades in which each of the flow-control blades has a pressure side and an opposite suction side. Each of the flow-control blades includes a main section and an inducer section that project away from an impeller surface. The inducer section is positioned upstream from the main section. The inducer section includes a trailing edge and the main section includes a leading edge that is spaced apart from the trailing edge. The inducer sections are aligned with the respective main sections as the inducer and main sections project from the impeller surface to a designated point above the impeller surface. Each of the trailing edges of the inducer sections and the respective leading edge of the main section form a bleed gap therebetween after the designated point. The bleed gap is configured to permit fluid to flow therethrough from the pressure side to the suction side.

    LIQUID RING FLUID FLOW MACHINE
    17.
    发明申请
    LIQUID RING FLUID FLOW MACHINE 审中-公开
    液体流体流化床

    公开(公告)号：US20160169226A1

    公开(公告)日：2016-06-16

    申请号：US14568564

    申请日：2014-12-12

    Applicant: General Electric Company

    Inventor： Sean Craig Jenkins ,  Vittorio Michelassi

    IPC: F04C19/00

    CPC classification number: F04C19/00 ,  F04C19/004 ,  F04C2230/91

    Abstract: A liquid ring fluid flow machine is presented. The machine includes a stationary annular housing having an outer surface and an inner surface. The inner surface defines a chamber that is arranged to receive a liquid. A rotor having a core and a plurality of radially extending vanes is eccentrically rotatably mounted within the chamber for directing the liquid into a recirculating liquid ring in proximity to the inner surface of the housing within the chamber. The inner surface of the housing that is in contact with the recirculating liquid ring is covered by a hydrophobic coating. The machine further includes a first supply pipe and a second supply pipe, each in fluid communication with the chamber.

    Abstract translation: 提出了一种液环流体流动机。 机器包括具有外表面和内表面的静止环形壳体。 内表面限定了一个被配置成容纳液体的腔室。 具有芯和多个径向延伸的叶片的转子可偏心地可旋转地安装在腔室内，用于将液体引导到腔室内壳体内表面附近的再循环液体环中。 与再循环液体环接触的壳体的内表面被疏水涂层覆盖。 该机器还包括与腔室流体连通的第一供应管和第二供应管。

    CIRCUMFERENTIALLY VARYING AXIAL COMPRESSOR ENDWALL TREATMENT FOR CONTROLLING LEAKAGE FLOW THEREIN
    18.
    发明申请
    CIRCUMFERENTIALLY VARYING AXIAL COMPRESSOR ENDWALL TREATMENT FOR CONTROLLING LEAKAGE FLOW THEREIN 审中-公开
    循环式轴流式压缩机终端处理，用于控制泄漏流量

    公开(公告)号：US20160169017A1

    公开(公告)日：2016-06-16

    申请号：US14572119

    申请日：2014-12-16

    Applicant: General Electric Company

    Inventor： Davide Giacché ,  John David Stampfli ,  Ramakrishna Venkata Mallina ,  Vittorio Michelassi ,  Giridhar Jothiprasad ,  Ajay Keshava Rao ,  Rudolf Konrad Selmeier ,  Sungho Yoon ,  Ivan Malcevic

    IPC: F01D11/00 ,  F02C3/04

    CPC classification number: F01D11/001 ,  F04D27/02 ,  F04D29/526 ,  F04D29/68 ,  F04D29/681 ,  F04D29/685

    Abstract: A compressor for a gas turbine engine including one or more endwall treatments for controlling leakage flow and circumferential flow non-uniformities in the compressor. The compressor includes a casing, a hub, a flow path formed between the casing and the hub, a plurality of blades positioned in the flow path, and one or more circumferentially varying end-wall treatments formed in an interior surface of at least one of the casing or the hub. Each of the one or more circumferentially varying endwall treatments circumferentially varying based on their relative position to an immediately adjacent upstream bladerow. Each of the one or more endwall treatments is circumferentially varied in at least one of placement relative to the immediately adjacent upstream bladerow or in geometric parameters defining each of the plurality of circumferentially varying endwall treatments. Additionally disclosed is an engine including the compressor.

    Abstract translation: 一种用于燃气涡轮发动机的压缩机，其包括用于控制压缩机中的泄漏流动和周向流动不均匀性的一个或多个端壁处理。 压缩机包括壳体，毂，形成在壳体和轮毂之间的流动路径，位于流动路径中的多个叶片，以及形成在至少一个的内表面中的一个或多个周向变化的端壁处理 套管或轮毂。 一个或多个周向变化的端壁处理中的每一个基于它们与紧邻的上游bladerow的相对位置周向地变化。 一个或多个端壁处理中的每一个在相对于直接相邻的上游bladerow的放置中的至少一个中或在限定多个周向变化的端壁处理中的每一个的几何参数中的周向变化。 另外公开了一种包括压缩机的发动机。

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