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111.
公开(公告)号:US20190153994A1
公开(公告)日:2019-05-23
申请号:US15818957
申请日:2017-11-21
Applicant: General Electric Company
Inventor: James Robert Tobin , Norman Arnold Turnquist , Stephen Bertram Johnson , Don Conrad Johnson , Thomas Merzhaeuser , Peggy Lynn Baehmann , Stefan Herr , Murray Fisher , Andrew McCalip , Alan M. Walker , Todd Anderson
Abstract: A method for manufacturing a rotor blade panel of a wind turbine includes placing one or more fiber-reinforced outer skins into a mold of the rotor blade panel. The method also includes printing and depositing, via a computer numeric control (CNC) device, a plurality of rib members that form at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more fiber-reinforced outer skins. Further, the grid structure bonds to the one or more fiber-reinforced outer skins as the grid structure is deposited. Moreover, the method includes printing at least one additional feature into the grid structure.
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公开(公告)号:US20190152160A1
公开(公告)日:2019-05-23
申请号:US15819057
申请日:2017-11-21
Applicant: General Electric Company
Inventor: James Robert Tobin , Stephen Bertram Johnson
Abstract: The present disclosure is directed to an apparatus and method 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 machine heads 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 machine heads is moveable along the first axis, the second axis, or both. At least one of the machine heads of the plurality of machine heads is moveable independently of one another along a third axis. A second frame assembly is moveable above the mold along the first axis, the second axis, or both. The second frame assembly includes a holding device. The holding device affixes to and releases from an outer skin to place and displace the outer skin at the mold.
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113.
公开(公告)号:US20190084676A1
公开(公告)日:2019-03-21
申请号:US15707010
申请日:2017-09-18
Applicant: General Electric Company
Inventor: Benjamin Patrick Hallissy , James Robert Tobin , Stefan Herr , Megan Wilson , Andreas Herrig , Matthew Rece
Abstract: A method for providing visual identification of a flow field across one or more wind turbines includes releasing at least one tracer material from at least one predetermined location of the wind turbine. The method also includes synchronizing the releasing of the tracer material with at least one of one or more operating parameters or one or more wind parameters of the wind turbine. Further, the method includes monitoring, via one or more sensors, a resultant flow pattern of the tracer material from one or more uptower locations.
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114.
公开(公告)号:US10213994B2
公开(公告)日:2019-02-26
申请号:US14862216
申请日:2015-09-23
Applicant: General Electric Company
IPC: B29C47/00 , B32B27/12 , B32B5/26 , B32B27/08 , B29C70/46 , B32B7/04 , B32B1/00 , F03D1/06 , B29K101/12 , B29K105/08 , B29K105/00 , B29L9/00 , B29L31/08
Abstract: In one aspect, a method for manufacturing a spar cap for a wind turbine rotor blade may generally include stacking a plurality of plates together to form a plate assembly, wherein each of the plates is formed from a fiber-reinforced composite including a plurality of fibers surrounded by a thermoplastic resin material. The method may also include positioning the plate assembly relative to a mold defining a mold surface, wherein the mold surface is shaped so as to correspond to at least one blade parameter of the wind turbine rotor blade. In addition, the method may include applying pressure to the plate assembly via the mold such that at least a portion of the plate assembly conforms to the shape of the mold surface.
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公开(公告)号:US10113531B2
公开(公告)日:2018-10-30
申请号:US14835998
申请日:2015-08-26
Applicant: General Electric Company
Abstract: The present disclosure is directed a method for repairing a rotor blade of a wind turbine. More specifically, in certain embodiments, the rotor blade may be constructed, at least in part, of a thermoplastic material reinforced with at least one fiber material. Thus, the method includes identifying at least one defect on the rotor blade. For example, in certain embodiments, the defect(s) as described herein may include a crack, creep, void, hole, distortion, deformation, scratch, or any other blade defect. The method also includes applying at least one of heat, pressure, and/or one or more chemicals to the defect(s) for a predetermined time period until the defect is repaired.
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公开(公告)号:US10071532B2
公开(公告)日:2018-09-11
申请号:US14835977
申请日:2015-08-26
Applicant: General Electric Company
CPC classification number: B29D99/0028 , B29C65/02 , B29C65/48 , B29C65/4815 , B29C65/4835 , B29C65/5057 , B29C65/562 , B29C66/1122 , B29C66/524 , B29C66/532 , B29C66/543 , B29C66/636 , B29C66/721 , B29C66/7212 , B29C66/7392 , B29C66/73921 , B29C66/7394 , B29C66/73941 , B29L2031/085 , F03D1/0675 , F03D80/00 , F05B2240/302 , Y02P70/523 , B29K2309/08 , B29K2307/04 , B29K2301/00 , B29K2309/02 , B29K2305/00
Abstract: The present disclosure is directed to a method of assembling a modular rotor blade of a wind turbine. The method includes identifying a main blade structure, constructed at least in part, from at least one of a thermoset or a thermoplastic material. The method also includes identifying at least one blade segment, constructed at least in part, of a thermoplastic material reinforced with at least one of glass fibers or carbon fibers. Thus, the method also includes securing the at least one blade segment to the main blade structure, e.g. via welding.
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公开(公告)号:US10060411B2
公开(公告)日:2018-08-28
申请号:US14805860
申请日:2015-07-22
Applicant: General Electric Company
CPC classification number: F03D1/0675 , B29C66/7392 , B29C66/7394 , F03D1/0658 , F05D2300/42 , F05D2300/433 , F05D2300/436 , F05D2300/603 , Y02E10/721 , Y02P70/523
Abstract: A root assembly for a rotor blade of a wind turbine includes a blade root section having an inner sidewall surface and an outer sidewall surface separated by a radial gap, a plurality of root inserts spaced circumferentially within the radial gap, and a plurality of spacers configured between one or more of the root inserts. Further, each of the root inserts includes at least one bore hole surrounded by a pre-cured or pre-consolidated composite material. In addition, the pultruded spacers are constructed of a pre-cured or pre-consolidated composite material.
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公开(公告)号:US20180223798A1
公开(公告)日:2018-08-09
申请号:US15428620
申请日:2017-02-09
Applicant: General Electric Company
Abstract: The present disclosure is directed methods for manufacturing spar caps for wind turbine rotor blades. In certain embodiments, the method includes forming an outer frame or tray of the spar cap via at least one of three-dimensional (3D) pultrusion, thermoforming, or 3D printing. As such, the outer frame has a varying cross-section that corresponds to a varying cross-section of the rotor blade along a span thereof. The method also includes arranging a plurality of structural materials (e.g. layers of pultruded plates) within the pultruded outer frame of the spar cap and infusing the structural materials and the outer frame together via a resin material so as to form the spar cap. The resulting spar cap can then be easily incorporated into conventional rotor blade manufacturing processes and/or welded or bonded to an existing rotor blade.
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公开(公告)号:US20180223794A1
公开(公告)日:2018-08-09
申请号:US15424055
申请日:2017-02-03
Applicant: General Electric Company
Inventor: James Robert Tobin , Stephen Bertram Johnson , Jamie T. Livingston , Alan M. Walker
CPC classification number: F03D1/0675 , B29D99/0028 , B33Y80/00 , F05B2230/20 , F05B2230/31 , F05B2240/302 , F05B2280/6003 , F05B2280/6013 , Y02E10/721 , Y02P70/523
Abstract: The present disclosure is directed to methods for manufacturing wind turbine rotor blades and components thereof. In one embodiment, the method includes forming an outer surface of a rotor blade panel from one or more fiber-reinforced outer skins. The method also includes printing and depositing at least one reinforcement structure onto an inner surface of the one or more fiber-reinforced outer skins to form the rotor blade panel, wherein the reinforcement structure bonds to the one or more fiber-reinforced outer skins as the reinforcement structure is being deposited.
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公开(公告)号:US09970304B2
公开(公告)日:2018-05-15
申请号:US14805842
申请日:2015-07-22
Applicant: General Electric Company
IPC: F01D5/28 , B29C65/34 , B29C65/00 , B29C45/14 , B29C45/17 , B29C65/02 , B29C45/02 , B29C65/48 , F03D1/06 , B29L31/08 , B29K705/00 , B29K105/20 , B29K101/12
CPC classification number: F01D5/28 , B29C45/02 , B29C45/14065 , B29C45/1701 , B29C65/02 , B29C65/34 , B29C65/48 , B29C66/72 , B29C66/742 , B29K2101/12 , B29K2105/20 , B29K2705/00 , B29L2031/085 , F03D1/0658 , F05B2280/4003 , F05B2280/4006 , F05B2280/4009 , F05D2300/43 , F05D2300/433 , F05D2300/436 , Y02E10/721 , Y02P70/523
Abstract: The present disclosure is directed to a root assembly for a rotor blade of a wind turbine and methods of manufacturing same. The root assembly includes a blade root section having an inner sidewall surface and an outer sidewall surface separated by a radial gap, a plurality of root inserts spaced circumferentially within the radial gap, and a plurality of spacers configured between one or more of the root inserts. Further, each of the root inserts includes at least one bushing surrounded by a pre-cured or pre-consolidated composite material. In addition, the spacers are constructed of a pre-cured or pre-consolidated composite material.
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