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公开(公告)号：US20160356805A1
公开(公告)日：2016-12-08
申请号：US14819903
申请日：2015-08-06
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Carsten Michael Schneider , Vittorio Michelassi , Andreas Herrig , Erik Mele , Nathaniel David Varano , Brent David Michalowski , Kenton Travis Shonhor
CPC classification number: G01P13/02 , G01D5/145 , G01D5/3473
Abstract: A flow angle probe is provided comprising: (a) a probe vane configured to contact a moving fluid within a fluid conduit; (b) an optional probe mounting mechanically coupled to the probe vane; (c) a rotary shaft coupled either to the optional probe mounting or the probe vane; (d) a rotary encoder coupled to the rotary shaft; (e) a sensor hermetically isolated from the probe vane and configured to sense a change in position of the rotary encoder; and (f) a probe housing encompassing at least a portion of the rotary shaft, the rotary encoder and the sensor. The novel flow angle probes disclosed herein may be used in a wide variety of turbomachines and fluid processing systems, and applications, including turbomachine design and operational control, as well as in flow assurance.
Abstract translation: 提供了一种流角探针，包括：（a）探针叶片，其构造成接触流体导管内的运动流体; （b）机械耦合到探针叶片的可选探头安装件; （c）连接到可选探头安装件或探针叶片的旋转轴; （d）联接到旋转轴的旋转编码器; （e）传感器，其与所述探针叶片气密隔离并且构造成感测所述旋转编码器的位置变化; 和（f）包围所述旋转轴的至少一部分，所述旋转编码器和所述传感器的探针壳体。 本文公开的新型流角探头可用于各种涡轮机和流体处理系统以及应用，包括涡轮机设计和操作控制以及流量保证。
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公开(公告)号：US09500122B2
公开(公告)日：2016-11-22
申请号：US13931191
申请日：2013-06-28
Applicant: General Electric Company
Inventor： Cathal Clancy , Daniel Edward Loringer , Rodrigo Rodriguez Erdmenger , Vittorio Michelassi
IPC: F02B37/24 , F02B37/013 , F02B37/00 , F01D17/16 , F01D5/14
CPC classification number: F02B37/24 , F01D5/146 , F01D17/162 , F01D17/167 , F02B37/004 , F02B37/013 , F05D2220/40 , Y02T10/144
Abstract: The method includes moving at least one of a first support and a second support to vary a position of the plurality of main blades and tandem blades relative to each other to control one or more flow control characteristics across the turbine. The turbine includes a nozzle having the plurality of main blades and tandem blades. The plurality of main blades are coupled to the first support and the plurality of tandem blades are coupled to the second support disposed spaced apart from the first support.
Abstract translation: 该方法包括移动第一支撑件和第二支撑件中的至少一个以改变多个主叶片和串联叶片相对于彼此的位置，以控制跨越涡轮机的一个或多个流量控制特性。 涡轮机包括具有多个主叶片和串联叶片的喷嘴。 多个主叶片联接到第一支撑件并且多个串联叶片联接到与第一支撑件间隔开设置的第二支撑件。
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公开(公告)号：US20160138762A1
公开(公告)日：2016-05-19
申请号：US14568759
申请日：2014-12-12
Applicant: General Electric Company
Inventor： Guillaume Becquin , Siddharth Navinchandra Ashar, JR. , Vittorio Michelassi , Rosa Castane Selga , Rene DU CAUZE DE NAZELLE
IPC: F17D3/01
CPC classification number: E21B43/017 , B01D53/00 , E21B43/01 , E21B43/122 , E21B43/36 , E21B43/385 , F04D31/00 , F17D1/065 , F17D3/01 , Y10T137/2076 , Y10T137/85954 , Y10T137/86027 , Y10T137/86171
Abstract: A subsea fluid processing system is provided containing a liquid reservoir, an inlet tank, a pump, an outlet system, and a fluid re-circulation loop. The liquid reservoir circulates a primer liquid stream to the inlet tank via the fluid re-circulation loop. The inlet tank further receives a first production fluid stream and mixes it with the primer liquid stream to produce thereby a second production fluid stream having a reduced gas volume fraction (GVF) relative to the first production fluid stream. The pump receives the second production fluid stream from the inlet tank and increases its pressure. Further, the outlet system containing the liquid reservoir receives the second production fluid stream from the pump and separates at least a portion of the primer liquid stream from a principal production stream. The primer liquid includes at least one exogenous liquid not derived from the first production fluid stream.
Abstract translation: 提供了一种海底液体处理系统，其包含液体储存器，入口箱，泵，出口系统和流体再循环回路。 液体储存器通过流体再循环回路将底漆液体流循环到入口箱。 入口箱还接收第一生产流体流并将其与底漆液体流混合以产生相对于第一生产流体流具有降低的气体体积分数（GVF）的第二生产流体流。 泵从入口箱接收第二生产流体流并增加其压力。 此外，包含液体储存器的出口系统接收来自泵的第二生产流体流，并将至少一部分底漆液体流与主生产流分离。 底漆液体包括至少一种不是从第一生产流体流中得到的外源性液体。
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公开(公告)号：US10218247B2
公开(公告)日：2019-02-26
申请号：US14729405
申请日：2015-06-03
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Vittorio Michelassi , Siddharth Navinchandra Ashar , Ismail Hakki Sezal , Rene du Cauze de Nazelle , Egidio Marotta , Ravishankar Balasubramanian , Mohamed Osama
IPC: F04D1/06 , H02K9/19 , F04D31/00 , H02K1/27 , F04D29/06 , F04D13/06 , H02K16/00 , F04D13/10 , H02K7/14 , H02K17/16 , H02K21/22 , H02K19/10
Abstract: An electric pump powered by an electric motor having a stator disposed within a hollow rotor is provided. Impellers on the rotor outer surface extend into a fluid flow path defined by the pump. One or more torque-producing rotor sections are driven by a plurality of independently controllable stator sections disposed within the rotor cavity. The relative positions of the rotor and stator are maintained by a plurality of bearings configured to allow rotation of the rotor and defining a bearing span. The pump is configured such that the stator and rotor share the same bearing span. Such an arrangement reduces motor windage losses relative to conventional motors in which the rotor is disposed within the stator, owing to a reduction in the diameter of the air gap between the stator and the rotor. In addition, the peripheral speed of the pump is increased owing to an increase in the rotor diameter.
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公开(公告)号：US09574562B2
公开(公告)日：2017-02-21
申请号：US13961680
申请日：2013-08-07
Applicant: General Electric Company
Inventor： Jeremy Daniel Van Dam , Vittorio Michelassi , Ismail Hakki Sezal , Xuele Qi , Rene du Cauze de Nazelle , Vishal Gahlot , Scott Richard Erler
CPC classification number: F04D3/02 , F04D29/183
Abstract: A pump for pumping a multiphase fluid includes a housing and a rotor with an outer surface. A plurality of inducer vanes are attached to the rotor hub, each having a leading edge and a trailing edge where the leading edge of one inducer vane overlaps the trailing edge of an adjacent inducer vane by a first overlap angle. A plurality of impeller vanes are also attached to the hub. The impeller vanes each have a leading edge and a trailing edge where the leading edge of one impeller vane overlaps the trailing edge of an adjacent impeller vane by a second overlap angle larger than the first overlap angle. The pump includes a rotor flow channel extending between the hub outer surface and the housing inner surface. The rotor flow channel has an inlet area and an outlet area, whereby the outlet area is smaller than the inlet area.
Abstract translation: 用于泵送多相流体的泵包括壳体和具有外表面的转子。 多个导流叶片附接到转子轮毂，每个导轮叶片具有前缘和后缘，其中一个导流叶片的前缘与相邻的导流叶片的后缘重叠第一重叠角。 多个叶轮叶片也附接到轮毂。 叶轮叶片各自具有前缘和后缘，其中一个叶轮叶片的前缘与相邻叶轮叶片的后缘重叠大于第一重叠角的第二重叠角。 泵包括在轮毂外表面和壳体内表面之间延伸的转子流动通道。 转子流动通道具有入口区域和出口区域，由此出口面积小于入口区域。
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Patent Agency Ranking
6.发明申请公开(公告)号：US20160153465A1
公开(公告)日：2016-06-02
申请号：US14556452
申请日：2014-12-01
Applicant: General Electric Company
Inventor： Sungho Yoon , John David Stampfli , Ramakrishna Venkata Mallina , Vittorio Michelassi , Giridhar Jothiprasad , Ajay Keshava Rao , Rudolf Konrad Selmeier , Davide Giacché , Ivan Malcevic
CPC classification number: F04D29/526 , F04D29/321 , F04D29/522 , F04D29/685
Abstract: An axial compressor for a gas turbine engine including one or more endwall treatments for controlling leakage flow in the compressor. The one or more endwall treatments having a height formed in an interior surface of a compressor casing or a compressor hub and configured to return a flow adjacent a plurality of rotor blade tips or a plurality of stator blade tips to a cylindrical flow passage upstream of a point of removal of the flow. Each of the endwall treatments defining a front wall, a rear wall, an outer wall extending between the front wall and the rear wall, an axial overhang, an axial overlap, an axial lean angle and a tangential lean angle. The axial overhang extending upstream to overhang at least one of the at least one set of rotor blades or the at least one set of stator blades. The axial overlap extending downstream to overlap at least one of the at least one set of rotor blades or the at least one set of stator blades.
Abstract translation: 一种用于燃气涡轮发动机的轴向压缩机，包括用于控制压缩机中的泄漏流的一个或多个端壁处理。 所述一个或多个端壁处理具有形成在压缩机壳体或压缩机毂的内表面中的高度，并且被配置为将邻近多个转子叶片尖端或多个定子叶片尖端的流返回到一个圆柱形流动通道 清除流量点。 每个端壁处理限定了前壁，后壁，在前壁和后壁之间延伸的外壁，轴向突出，轴向重叠，轴向倾斜角和切向倾斜角。 所述轴向突出部在所述至少一组所述转子叶片或所述至少一组定子叶片中的至少一个的上游延伸。 在下游延伸的轴向重叠与所述至少一组转子叶片或至少一组定子叶片中的至少一个重叠。
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公开(公告)号：US09127679B2
公开(公告)日：2015-09-08
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
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。
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公开(公告)号：US20150044027A1
公开(公告)日：2015-02-12
申请号：US13961680
申请日：2013-08-07
Applicant: General Electric Company
Inventor： Jeremy Daniel Van Dam , Vittorio Michelassi , Ismail Hakki Sezal , Xuele Qi , Rene du Cauze de Nazelle , Vishal Gahlot , Scott Richard Erler
IPC: F04D3/02
CPC classification number: F04D3/02 , F04D29/183
Abstract: A pump for pumping a multiphase fluid includes a housing and a rotor with an outer surface. A plurality of inducer vanes are attached to the rotor hub, each having a leading edge and a trailing edge where the leading edge of one inducer vane overlaps the trailing edge of an adjacent inducer vane by a first overlap angle. A plurality of impeller vanes are also attached to the hub. The impeller vanes each have a leading edge and a trailing edge where the leading edge of one impeller vane overlaps the trailing edge of an adjacent impeller vane by a second overlap angle larger than the first overlap angle. The pump includes a rotor flow channel extending between the hub outer surface and the housing inner surface. The rotor flow channel has an inlet area and an outlet area, whereby the outlet area is smaller than the inlet area.
Abstract translation: 用于泵送多相流体的泵包括壳体和具有外表面的转子。 多个导流叶片附接到转子轮毂，每个导轮叶片具有前缘和后缘，其中一个导流叶片的前缘与相邻导流叶片的后缘重叠第一重叠角。 多个叶轮叶片也附接到轮毂。 叶轮叶片各自具有前缘和后缘，其中一个叶轮叶片的前缘与相邻叶轮叶片的后缘重叠大于第一重叠角的第二重叠角。 泵包括在轮毂外表面和壳体内表面之间延伸的转子流动通道。 转子流动通道具有入口区域和出口区域，由此出口面积小于入口区域。
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公开(公告)号：US10539154B2
公开(公告)日：2020-01-21
申请号：US15531992
申请日：2014-12-10
Applicant: General Electric Company
Inventor： Ramakrishna Venkata Mallina , Sungho Yoon , Vittorio Michelassi , Ivan Malcevic
Abstract: A compressor is provided including a compressor end-wall having a casing and a hub. The compressor further includes at least one set of rotor blades, one set of stator blades, and a plurality of end-wall treatments spaced apart from each other, formed in an interior surface of at least one of the casing and hub, and facing a tip of the rotor blade or stator blade. Each end-wall treatment includes a forward recess portion extending along a first axis and an aft recess portion extending along a second axis different than the first axis. The aft recess portion is joined to the corresponding forward recess portion via an intersection portion which is inclined relative to at least one of the first axis, and the second axis. The aft recess portion and/or the forward recess portion are bent from the intersection portion and inclined relative to an axial direction of the compressor.
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10.发明授权公开(公告)号：US10047620B2
公开(公告)日：2018-08-14
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
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.
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