Method for manufacturing a preform for a wind turbine blade

    公开(公告)号:US20250050596A1

    公开(公告)日:2025-02-13

    申请号:US18718935

    申请日:2023-02-03

    Abstract: The present invention relates to a method of manufacturing a part, such as a preform, for a wind turbine blade. One or more channel members (72) are fastened to the mould surface of a preform mould, and a fibre material (85) and a binding agent is arranged on the mould surface (87). The fibre material, the binding agent and the one or more channel members are covered with a vacuum bag, and negative pressure is applied to the fibre material and binding agent via the one or more channel members for consolidating the preform. Each of the channel members (72) comprises a plurality of slits (77) extending between its inner surface and its outer surface, the slits having an orientation that is substantially transverse to the longitudinal axis of the channel member.

    SYSTEM FOR ASSEMBLING A WIND TURBINE BLADE SHELL

    公开(公告)号:US20250026090A1

    公开(公告)日:2025-01-23

    申请号:US18713156

    申请日:2022-11-29

    Abstract: The present invention relates to a system for assembling a wind turbine blade shell. The system comprises a first support structure comprising a stationary portion and a moveable portion, the moveable portion being adapted to support a first wind turbine blade shell half; a second support structure adapted to support a second wind turbine blade shell half; moving means attached to the moveable portion and configured to move the moveable portion between: i) a first position in which the moveable portion is positioned above the stationary structure, and ii) a second position in which the moveable portion is positioned above the second support structure, wherein when the moveable portion is in the second position, a first wind turbine blade shell half supported by the moveable portion and a second wind turbine blade shell half supported by the second support structure are assembled, forming the wind turbine blade shell.

    Noise reduction element and a wind turbine blade comprising a noise reduction element

    公开(公告)号:US12188451B2

    公开(公告)日:2025-01-07

    申请号:US17794071

    申请日:2021-02-23

    Abstract: A noise reduction element extends between a first end and a second end in a first direction. The noise reduction element extends between a third end and a fourth end in a second direction perpendicular to the first direction. The noise reduction element includes a base part configured to be attached to a trailing edge of a wind turbine blade. The base part has a first base part surface and a second base part surface. The base part extends between the first end and a first position in the first direction. The noise reduction element includes a first serration part having a serration pressure surface and a serration suction surface and extending in the first direction between the first position and the second end. The first serration part has a thickness in a third direction between the serration pressure surface and the serration suction surface.

    MANDREL DEVICE FOR MANUFACTURING A SEGMENTED WIND TURBINE BLADE

    公开(公告)号:US20240391199A1

    公开(公告)日:2024-11-28

    申请号:US18686277

    申请日:2022-08-24

    Abstract: A mandrel device (50) for manufacturing a hollow spar beam (30) for a segmented wind turbine blade (10) in a mould (100), the mandrel device comprising: a plurality of mandrel elements (52, 53, 54, 55, 56, 57, 58, 59) each comprising a substantially rigid material, and a plurality of attachment devices (60) configured for detachably attaching adjacent mandrel elements, wherein the mandrel device has an assembled configuration and a detached configuration, wherein: in the assembled configuration, the plurality of attachment devices is engaged so that the plurality of mandrel elements is detachably attached to each other, and the plurality of mandrel elements extends along a longitudinal axis of the mandrel device so that the mandrel device has a substantially box shaped cross-section that varies along the longitudinal axis, and in the detached configuration, the plurality of attachment devices is disengaged so that the plurality of mandrel elements is detached from each other, and the plurality of mandrel elements is inwardly collapsible.

    Method of manufacturing wind turbine blade with core member and wind turbine blade with structural member

    公开(公告)号:US12138866B2

    公开(公告)日:2024-11-12

    申请号:US18037303

    申请日:2021-11-16

    Abstract: The present invention relates to a method of manufacturing a wind turbine blade (10), comprising the steps of placing a fibre lay-up including one or more fibre layers on the mould surface of a blade mould (60), arranging a load-bearing structure (45) and a core member (62) on the fibre lay-up such that the core member (62) is arranged between the load-bearing structure (45) and the leading edge (18) and/or between the load-bearing structure (45) and the trailing edge (20), and infusing resin into the blade mould to impregnate the fibre lay-up. The core member (62) comprises a first hole (64) with a circular cross section, a first cylindrical insert (70) rotatably arranged within the first hole (64) of the core member (62), the first cylindrical insert (70) having a central axis (71). A recess (80) is formed in the first cylindrical insert (70), wherein the recess (80) is arranged eccentrically with respect to the central axis (71) of the first cylindrical insert (70).

    SEGMENTED WIND TURBINE BLADE
    7.
    发明公开

    公开(公告)号:US20240352917A1

    公开(公告)日:2024-10-24

    申请号:US18687457

    申请日:2022-10-24

    Inventor: Rama RAZEGHI

    CPC classification number: F03D1/0677 F03D1/0681 F05B2230/23 F05B2240/302

    Abstract: The present disclosure relates to a method for manufacturing a blade segment for a segmented wind turbine blade, and a resulting segment for a segmented wind turbine blade as well as the segmented wind turbine blade. In particular, the blade segment comprises a female spar part defining an inner cavity and having a longitudinal inner end and an opposite longitudinal open end towards an end face of the blade segment, a first spar cap connected to an inner surface of a first shell portion and comprising a first primary spar cap portion. The blade segment further comprises a first secondary spar cap portion affixed to a first outer surface of the female spar part. The first secondary spar cap portion is glued to the inner surface of the first shell portion and/or to the first primary spar cap portion forming a glue interface between the first secondary spar cap portion and the inner surface of the first shell portion and/or the first primary spar cap portion.

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