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91.发明申请ATTACHMENT METHOD AND SYSTEM TO INSTALL COMPONENTS, SUCH AS VORTEX GENERATORS, TO A WIND TURBINE BLADE 有权安装组件的方法和系统，如VORTEX发电机，风力涡轮叶片公开(公告)号：US20160327021A1
公开(公告)日：2016-11-10
申请号：US14706026
申请日：2015-05-07
Applicant: General Electric Company
Inventor： James Robert Tobin , William Max Gobeli , Scott Gabell Riddell , Michael Christopher Booth
CPC classification number: F03D1/0675 , B29C65/4825 , B29C65/483 , B29C65/5057 , B29C65/562 , B29C65/72 , F03D13/10 , F05B2240/122 , Y02E10/721
Abstract: A method for installing an add-on component to a surface of a wind turbine blade includes attaching an adhesive side of strips of a double-sided adhesive tape onto either the surface of the wind turbine blade or a surface of the add-on component, the tape strips having a release liner on an opposite exposed side thereof. The tape strips having an extension tail of the release liner that extends beyond an edge of the add-on component when the add-on component is placed and held at a desired position against the surface of the wind turbine blade. With the add-on component held at the desired position, the extension tail is pulled away at an angle such that that release liner is removed along the length of the tape strip while maintaining the add-on component against the blade surface to attach the exposed adhesive under the release liner to either the surface of the wind turbine blade or the surface of the add-on component.
Abstract translation: 用于将附加部件安装到风力涡轮机叶片的表面的方法包括将双面胶带的条带的粘合剂侧附接到风力涡轮机叶片的表面或附加部件的表面上， 带条在其相对的暴露侧具有释放衬垫。 当附加部件被放置并保持在相对于风力涡轮机叶片的表面的期望位置时，带条具有延伸超过附加部件的边缘的释放衬里的延伸尾部。 随着附加部件保持在期望的位置，延伸尾部以一定的角度拉开，使得沿着带条的长度移除剥离衬垫，同时保持附加部件抵靠刀片表面以附接暴露的 在释放衬垫下方的粘合剂到风力涡轮机叶片的表面或附加部件的表面。
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公开(公告)号：US20150204306A1
公开(公告)日：2015-07-23
申请号：US14157598
申请日：2014-01-17
Applicant: General Electric Company
Inventor： Stefan Herr , James Robert Tobin
CPC classification number: F03D7/022 , B64C3/58 , B64C23/06 , F03D1/0633 , F03D1/0641 , F03D1/0675 , F03D7/0224 , F03D7/0232 , F03D7/024 , F03D7/0252 , F03D80/00 , F05B2240/122 , F05B2240/30 , F05B2240/31 , F05B2240/313 , F05B2260/502 , Y02E10/721 , Y02E10/723 , Y02T50/162
Abstract: The present subject matter directed to a rotor blade assembly for a wind turbine having at least one rotatable aerodynamic surface feature configured thereon. The rotor blade assembly includes a body shell including a pressure side surface and a suction side surface extending between a leading edge and a trailing edge. The aerodynamic surface feature is disposed adjacent to the pressure side surface, the suction side surface, and/or both. In addition, the surface feature may have a generally airfoil-shaped cross section. As such, an actuator can be configured at least partially within an internal volume of the surface feature, the actuator being configured to rotate the surface feature relative to the body shell.
Abstract translation: 本发明涉及用于风力涡轮机的转子叶片组件，其具有构造在其上的至少一个可旋转的空气动力学表面特征。 转子叶片组件包括主体壳体，其包括压力侧表面和在前缘和后缘之间延伸的吸力侧表面。 空气动力学表面特征设置成邻近压力侧表面，吸力侧表面和/或两者。 此外，表面特征可以具有大致翼型的横截面。 因此，致动器可以至少部分地配置在表面特征的内部体积内，致动器被配置为相对于主体壳旋转表面特征。
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公开(公告)号：US20150003985A1
公开(公告)日：2015-01-01
申请号：US13928490
申请日：2013-06-27
Applicant: General Electric Company
Inventor： Christopher Daniel Caruso , James Robert Tobin
IPC: F03D7/02
CPC classification number: F03D7/022 , F03D1/0675 , F03D7/0252 , F05B2240/122 , F05B2240/31 , Y02E10/721 , Y02E10/723
Abstract: Rotor blades for a wind turbines include a shell having a pressure side and a suction side and a plurality of surface features disposed adjacent at least one of the pressure side and the section side. The plurality of surface features is further moveable between a spoiler position and a vortex generator position.
Abstract translation: 用于风力涡轮机的转子叶片包括具有压力侧和吸力侧的壳体以及邻近压力侧和截面侧中的至少一个设置的多个表面特征。 多个表面特征可在扰流器位置和涡流发生器位置之间进一步移动。
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94.发明申请ACTIVE SYSTEMS AND METHODS FOR PRODUCING ULTRASONIC SOUND EMISSIONS FROM WIND TURBINES 有权用于生产来自风力涡轮机的超声波发射的主动系统和方法公开(公告)号：US20140377061A1
公开(公告)日：2014-12-25
申请号：US13926367
申请日：2013-06-25
Applicant: General Electric Company
Inventor： Christopher Daniel Caruso , Kevin Wayne Kinzie , Dongjai Lee , James Robert Tobin , Justin Richard Curtis , Jonathan Henry Zalar
CPC classification number: A01M29/18 , F03D7/0264 , F03D7/04 , F03D17/00 , F03D80/00 , F03D80/10 , Y02E10/72
Abstract: Methods for producing ultrasonic sound emissions from wind turbines, active systems for emitting ultrasonic sounds from wind turbines, and wind turbines are provided. In one embodiment, a method includes operating the wind turbine with an ultrasonic sound emitting device mounted on or within a component of the wind turbine, and receiving in a controller at least one indicator. The method further includes determining if an operating condition exists based on the at least one indicator, and supplying a fluid flow through an outlet of the ultrasonic sound emitting device such that an ultrasonic sound emission is produced by the ultrasonic sound emitting device if the operating condition exists.
Abstract translation: 提供了用于从风力涡轮机产生超声波发射的方法，用于从风力涡轮机发射超声波的主动系统和风力涡轮机。 在一个实施例中，一种方法包括使用安装在风力涡轮机的部件上或内部的超声波发声装置来操作风力涡轮机，以及在控制器中接收至少一个指示器。 所述方法还包括基于所述至少一个指示器来确定是否存在操作条件，以及提供流体流过所述超声波发声装置的出口，使得如果所述操作条件，所述超声波发声装置产生超声波发射 存在
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公开(公告)号：US20140328687A1
公开(公告)日：2014-11-06
申请号：US13886348
申请日：2013-05-03
Applicant: GENERAL ELECTRIC COMPANY
Inventor： James Robert Tobin , Scott Gabell Riddell , Michael Christopher Booth , Megan Michela Wilson
IPC: F04D29/16
CPC classification number: F03D1/0633 , F03D1/0675 , F05B2240/122 , F05B2240/221 , F05B2240/30 , F05B2240/32 , F05B2250/711 , F05B2250/712 , F05B2260/96 , F05B2280/2003 , F05B2280/4004 , Y02E10/721 , Y02E10/726
Abstract: Rotor blade assemblies for wind turbines are provided. A rotor blade assembly includes a rotor blade. In some embodiments, the rotor blade assembly further includes a surface feature configured on an exterior surface of the rotor blade, the surface feature having an exterior mounting surface. At least a portion of the exterior mounting surface has a contour in an uninstalled state that is different from a curvature of the exterior surface of the rotor blade at a mount location of the surface feature on the rotor blade. In other embodiments, the rotor blade assembly further includes a seal member surrounding at least a portion of a perimeter of the surface feature. The seal member contacts and provides a transition between the exterior surface and the surface feature.
Abstract translation: 提供了用于风力涡轮机的转子叶片组件。 转子叶片组件包括转子叶片。 在一些实施例中，转子叶片组件还包括构造在转子叶片的外表面上的表面特征，表面特征具有外部安装表面。 外部安装表面的至少一部分具有处于卸载状态的轮廓，其与转子叶片上的表面特征的安装位置处的转子叶片的外表面的曲率不同。 在其他实施例中，转子叶片组件还包括围绕表面特征的周边的至少一部分的密封构件。 密封构件接触并在外表面和表面特征之间提供过渡。
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Patent Agency Ranking
公开(公告)号：US20240293992A1
公开(公告)日：2024-09-05
申请号：US17768619
申请日：2019-10-15
Applicant: General Electric Company
Inventor： James Robert Tobin
CPC classification number: B32B3/12 , B29D99/0028 , B32B1/00 , B32B5/02 , B32B27/308 , B32B27/365 , B29K2105/08 , B32B2260/021 , B32B2260/046 , B32B2603/00 , F03D1/0675
Abstract: A method for manufacturing a shell includes providing a mold of the shell. The method also includes forming one or more first skins on the mold. Further, the method includes securing at least one three-dimensional (3-D) grid structure onto an inner surface of the one or more first skins. Thus, the method also includes securing one or more reinforcing members to one or more locations of the grid structure so as to locally increase a stiffness of the shell at the one or more locations by creating one or more localized sandwich structures with the grid structure.
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公开(公告)号：US20230234313A1
公开(公告)日：2023-07-27
申请号：US18011233
申请日：2021-06-24
Applicant: General Electric Company
Inventor： James Robert Tobin , Paul Trevor Hayden , Andrew McCalip , Fritz Andres Campo , Boobalan Ayyasamy , Todd Alan Anderson , Raphael Sajous
IPC: B29D99/00 , B33Y10/00 , B33Y30/00 , B33Y80/00 , B33Y40/00 , B29C64/106 , B29C64/209
CPC classification number: B29D99/0028 , B29D99/0014 , B33Y10/00 , B33Y30/00 , B33Y80/00 , B33Y40/00 , B29C64/106 , B29C64/209 , B29C70/30
Abstract: The present disclosure is directed to an apparatus for manufacturing a composite component. The apparatus includes a mold onto which the composite component is formed. The mold is disposed within a grid defined by a first axis and a second axis. The apparatus further includes a first frame assembly disposed above the mold, and a plurality of printheads coupled to the first frame assembly within the grid in an adjacent arrangement along the first axis. At least one of the mold or the plurality of printheads is moveable along the first axis, the second axis, or both. At least one of the printheads of the plurality of printheads is moveable independently of one another along a third axis.
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公开(公告)号：US20230226788A1
公开(公告)日：2023-07-20
申请号：US18011217
申请日：2021-06-24
Applicant: General Electric Company
Inventor： James Robert Tobin , Paul Trevor Hayden , Harald Behmer , Raphael Sajous , Hongyi Zhou
CPC classification number: B29D99/0028 , B33Y80/00 , B29D99/0014 , B33Y10/00
Abstract: In an aspect, the present disclosure is directed to a composite structure. The composite structure includes a three-dimensional (3-D) grid structure and at least one monolithic skin layer at least partially enveloping and securing the grid structure. As such, the grid structure is configured to stabilize the composite structure under at least one of: static local buckling and dynamic global buckling.
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公开(公告)号：US11511457B2
公开(公告)日：2022-11-29
申请号：US17279871
申请日：2018-09-28
Applicant: General Electric Company
Abstract: Methods of manufacturing a cementitious structure, such as a structure for supporting a wind turbine, include additively printing, via an additive printing device, one or more contours that include a cementitious material so as to form a cementitious structure in a layer by layer manner such that a first portion of the plurality of contours comprises a first plurality of contour coupling features that engage with a second plurality of contour coupling features of a second portion of the plurality of contours.
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100.发明申请公开(公告)号：US20220260050A1
公开(公告)日：2022-08-18
申请号：US17627198
申请日：2019-07-16
Applicant: General Electric Company
Inventor： James Robert Tobin , Andrew McCalip , Lauren Laurer Watts , Hongyi Zhou , Huijuan Dai , Collin McKee Sheppard
Abstract: A system for manufacturing a panel includes a support frame, a first caul plate arranged atop the support frame, a second caul plate arranged atop the first caul plate, and a heating assembly having a housing defining an inlet and an outlet. The housing includes one or more heaters. The heater(s) is configured to generate heat and the housing is configured to generate a first pressurized gas film. Thus, one or more layers of material to be consolidated may be placed between the first and second caul plates and drawn through the heating assembly as the heating assembly applies pressure to the one or more layers of material to be consolidated via the first pressurized gas film in combination with applying the heat via the one or more heaters, thereby consolidating the panel.
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