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公开(公告)号：US20220221706A1
公开(公告)日：2022-07-14
申请号：US17144435
申请日：2021-01-08
Applicant: General Electric Company , Oliver Crispin Robotics Limited
Inventor： Deepak Trivedi , Grover Andrew Bennett , Stephen Paul Leclerc , Andrew Crispin Graham
IPC: G02B23/24
Abstract: An insertion tool for performing an operation on equipment, the insertion tool including: a plurality of segments, each segment of the plurality of segments including a body including: a first hinge; a second hinge, the first and second hinge members pivotally coupling adjacent segments of the plurality of segments together; and a cavity extending along the body of the segment, the cavity exiting the body at a plurality of exit locations, wherein at least one of the plurality of exit locations is disposed adjacent to the first hinge; and a selectively rigidizable strength member disposed within the cavity.
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公开(公告)号：US10132290B2
公开(公告)日：2018-11-20
申请号：US14887381
申请日：2015-10-20
Applicant: General Electric Company
Inventor： Dmitry Floryovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Fulton Jose Lopez , Daniel Jason Erno , Robert Michael Zirin , Anurag Gupta
IPC: F03D1/06
Abstract: A deployable aerodynamic component configured to be mounted to a wind turbine. The wind turbine includes at least one rotor blade. The deployable aerodynamic component configured to be positioned in front of an inner portion of the at least one rotor blade, and is structurally configured to cover a substantial portion of the inner portion of the at least one rotor blade in a wind direction during deployment of the deployable aerodynamic component and to allow the passage therethrough of an incoming wind when non-deployed. Further described is a wind turbine including the above-described deployable aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine, wherein the method includes mounting the above-described deployable aerodynamic component to a wind turbine.
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3.发明申请公开(公告)号：US20170276141A1
公开(公告)日：2017-09-28
申请号：US15082524
申请日：2016-03-28
Applicant: General Electric Company
Inventor： Swati Saxena , Ajay Keshava Rao , Rudolf Konrad Selmeier , Grover Andrew Bennett , Giridhar Jothiprasad , Corey Bourassa , Byron Andrew Pritchard
CPC classification number: F02C9/18 , F02C6/08 , F04D29/542 , F05D2260/607
Abstract: A compressor assembly for a turbomachine includes a compressor wall including circumferentially spaced stator vanes defining at least one row of stator vanes. The at least one row of stator vanes defines at least one stator passage therein. Each stator vane includes a leading edge, an opposite trailing edge defining an axial chord distance, and a pressure side. The compressor assembly also includes, at least one bleed opening defined within the compressor wall and disposed adjacent the pressure side in the at least one stator passage within a range from approximately 20% the axial chord distance upstream of the leading edge to approximately 20% the axial chord distance downstream of the trailing edge. The compressor assembly further includes at least one bleed arm extending from the at least one bleed opening with at least a portion of compressor airflow extractable through the at least one bleed arm.
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Patent Agency Ranking
公开(公告)号：US10240579B2
公开(公告)日：2019-03-26
申请号：US15007858
申请日：2016-01-27
Applicant: General Electric Company
Inventor： Seyed Gholamali Saddoughi , Matthew Patrick Boespflug , Michael Solomon Idelchik , Grover Andrew Bennett
Abstract: A virtual aerodynamic component for a wind turbine including at least one rotor blade connected to a hub. The at least one rotor blade defines an inner portion and a profiled outer portion. The virtual aerodynamic component includes one or more air-blowing units configured to provide a flow of air substantially opposed to an incoming wind. The flow of air defines the virtual aerodynamic component in front of the inner portion of the at least one rotor blade and provides for redirection of the incoming wind toward the profiled outer portion of the at least one rotor blade in an operational state and allows the incoming wind to flow toward the inner portion of the at least one rotor blade in a non-operational state. Further described is a wind turbine including the above-described virtual aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine.
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公开(公告)号：US20170211545A1
公开(公告)日：2017-07-27
申请号：US15007858
申请日：2016-01-27
Applicant: General Electric Company
Inventor： Seyed Gholamali Saddoughi , Matthew Patrick Boespflug , Michael Solomon Idelchik , Grover Andrew Bennett
CPC classification number: F03D7/022 , F03D1/0666 , F03D7/024 , F03D15/05 , F05B2220/30 , F05B2240/2211 , Y02E10/721 , Y02E10/723
Abstract: A virtual aerodynamic component for a wind turbine including at least one rotor blade connected to a hub. The at least one rotor blade defines an inner portion and a profiled outer portion. The virtual aerodynamic component includes one or more air-blowing units configured to provide a flow of air substantially opposed to an incoming wind. The flow of air defines the virtual aerodynamic component in front of the inner portion of the at least one rotor blade and provides for redirection of the incoming wind toward the profiled outer portion of the at least one rotor blade in an operational state and allows the incoming wind to flow toward the inner portion of the at least one rotor blade in a non-operational state. Further described is a wind turbine including the above-described virtual aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine.
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公开(公告)号：US10227930B2
公开(公告)日：2019-03-12
申请号：US15082524
申请日：2016-03-28
Applicant: General Electric Company
Inventor： Swati Saxena , Ajay Keshava Rao , Rudolf Konrad Selmeier , Grover Andrew Bennett , Giridhar Jothiprasad , Corey Bourassa , Byron Andrew Pritchard
Abstract: A compressor assembly for a turbomachine includes a compressor wall including circumferentially spaced stator vanes defining at least one row of stator vanes. The at least one row of stator vanes defines at least one stator passage therein. Each stator vane includes a leading edge, an opposite trailing edge defining an axial chord distance, and a pressure side. The compressor assembly also includes, at least one bleed opening defined within the compressor wall and disposed adjacent the pressure side in the at least one stator passage within a range from approximately 20% the axial chord distance upstream of the leading edge to approximately 20% the axial chord distance downstream of the trailing edge. The compressor assembly further includes at least one bleed arm extending from the at least one bleed opening with at least a portion of compressor airflow extractable through the at least one bleed arm.
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公开(公告)号：US20220221707A1
公开(公告)日：2022-07-14
申请号：US17144487
申请日：2021-01-08
Applicant: General Electric Company , Oliver Crispin Robotics Limited
Inventor： Deepak Trivedi , Grover Andrew Bennett , Stephen Paul Leclerc , Andrew Crispin Graham
IPC: G02B23/24
Abstract: An insertion tool for performing an operation on equipment, the insertion tool including: a plurality of segments, each segment of the plurality of segments including a body comprising: a first hinge; and a second hinge, the first hinge of a first segment being coupled to the second hinge of a second segment adjacent to the first segment through an interface, wherein the interface comprises a powder gap, a multi-modal interface, a compliance feature, a displace-to-lock configuration, an interference fit, or any combination thereof, wherein the insertion tool is configured to be selectively rigidizable using a strength member interfacing with the plurality of segments.
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8.发明申请APPARATUS AND METHOD FOR AERODYNAMIC PERFORMANCE ENHANCEMENT OF A WIND TURBINE 审中-公开风力涡轮机气动性能提升装置及方法公开(公告)号：US20160040650A1
公开(公告)日：2016-02-11
申请号：US14887381
申请日：2015-10-20
Applicant: General Electric Company
Inventor： Dmitry Floryovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Fulton Jose Lopez , Daniel Jason Erno , Robert Michael Zirin , Anurag Gupta
CPC classification number: F03D1/0625 , F03D1/0691 , F05B2240/12 , Y02E10/721 , Y10T29/49316
Abstract: A deployable aerodynamic component configured to be mounted to a wind turbine. The wind turbine includes at least one rotor blade. The deployable aerodynamic component configured to be positioned in front of an inner portion of the at least one rotor blade, and is structurally configured to cover a substantial portion of the inner portion of the at least one rotor blade in a wind direction during deployment of the deployable aerodynamic component and to allow the passage therethrough of an incoming wind when non-deployed. Further described is a wind turbine including the above-described deployable aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine, wherein the method includes mounting the above-described deployable aerodynamic component to a wind turbine.
Abstract translation: 配置为安装到风力涡轮机的可部署的空气动力学部件。 风力涡轮机包括至少一个转子叶片。 所述可部署空气动力学部件被构造成定位在所述至少一个转子叶片的内部部分的前面，并且在结构上构造成在所述至少一个转子叶片的展开期间在风向方向上覆盖所述至少一个转子叶片的内部部分的大部分 可部署的空气动力学部件，并且当未部署时允许通过其中的风。 进一步描述了一种风力涡轮机，其包括上述可部署的空气动力学部件和用于现有风力涡轮机的空气动力学性能增强的方法，其中所述方法包括将上述可部署空气动力学部件安装到风力涡轮机。
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