METHOD OF MANUFACTURING A SPAR CAP FOR A WIND TURBINE BLADE

    公开(公告)号:US20240001632A1

    公开(公告)日:2024-01-04

    申请号:US18039315

    申请日:2021-11-30

    Inventor: Maria ARIAS

    Abstract: The present invention relates to a method of manufacturing a fibre-reinforced spar cap (41) for a wind turbine. The method comprises the steps of providing a mould (62), and fastening a first guide member (64) and a second guide member (66) to the mould for providing a moulding cavity (68) in between the first and second guide members. A fibre material can be arranged within the moulding cavity, such that a first gap (72) is provided between the fibre material and the first guide member, and a second gap (74) is provided between the fibre material and second guide member. First and second inserts (78, 80) are inserted into the gap prior to resin infusion.

    Aeroelastic stable wind turbine blade
    112.
    发明公开

    公开(公告)号:US20230392577A1

    公开(公告)日:2023-12-07

    申请号:US18032939

    申请日:2021-11-19

    CPC classification number: F03D1/0681 F05B2280/6013 F05B2260/964

    Abstract: A wind turbine blade comprising a plurality of spar components extending along the longitudinal axis and providing the main bending stiffness of the wind turbine blade a major principal axis defining a structural pitch angle of at least 1° with respect to a chord line, and including: one or more suction-side spar caps each having a centre line; one or more pressure-side spar caps each having a centre line; and one or more shear webs distributed around a central shear web line and at least one of which being connected to first spar caps, wherein at least one suction-side spar cap centre lines is arranged with a first chordwise distance to the central shear web line, and at least one pressure-side spar cap centre lines is arranged with a second, different, chordwise distance to the central shear web line.

    Turning system for wind turbine blade parts

    公开(公告)号:US11794379B2

    公开(公告)日:2023-10-24

    申请号:US17786184

    申请日:2021-03-16

    CPC classification number: B29C33/26 B29D99/0028 B29C33/306 B29L2031/085

    Abstract: A turning system for turning wind turbine blade shell part carriers between an open position and a closed position about a turning axis, comprising:



    a lower blade shell part carrier having a support surface for receiving and supporting a lower wind turbine blade part;
    an upper blade shell part carrier and having a support surface for receiving and supporting an upper wind turbine blade part; and
    at least one turning device each including:

    a lower hinge element, such as a beam, arranged under the support surface of the lower blade shell part carrier; and
    a turning hinge having a lower hinge part attached to the respective lower hinge element, an upper hinge part attached to the upper blade shell part carrier, and an actuator configured for turning the lower and upper hinge parts relative to each other about the turning axis.

    JOINTED WIND TURBINE ROTOR BLADE HAVING IMPROVED TRANSITIONS BETWEEN VARYING MATERIAL COMBINATIONS

    公开(公告)号:US20230323855A1

    公开(公告)日:2023-10-12

    申请号:US18043183

    申请日:2021-08-31

    CPC classification number: F03D1/0683 F05B2280/6003 F05B2230/60

    Abstract: A method of joining first and second blade components of a rotor blade of a wind turbine includes arranging the first blade component and the second blade component together at an interface. The first and second blade components are formed of different materials having different stiffnesses. The method further includes providing at least one gap at the interface of the blade components. Further, the method includes securing the blade components together by at least partially filling the gap with at least one filler material. Moreover, the method includes further securing the blade components together via an infusion process, wherein, during the infusion process, additional filler material further fills the gap or covers at least a portion of the at least one filler material. In addition, the method includes allowing the filler material(s) to cure. Thus, upon curing, the filler material(s) is configured to smoothly transition a load between the different materials of the blade components, thereby limiting an associated stress at the interface.

    SPECIMEN TEST METHOD
    119.
    发明公开

    公开(公告)号:US20230160797A1

    公开(公告)日:2023-05-25

    申请号:US17916997

    申请日:2021-05-19

    Abstract: Disclosed is a test rig and a method for mechanical load testing of a specimen extending along a longitudinal axis from a first specimen end to a second specimen end and comprising a composite material extending along the longitudinal axis from a first composite end to a second composite end and a primary elongate component extending along the longitudinal axis from a first primary component end to a second primary component end, the first primary component end being the first specimen end, and wherein the composite material encapsulates the primary elongate component along a first interface region extending along the longitudinal axis from the second primary component end to the first composite end. The method comprises applying a load to the specimen resulting in an axial load component and a bending moment being imposed to the specimen.

    RESIN DEGASSING
    120.
    发明公开
    RESIN DEGASSING 审中-公开

    公开(公告)号:US20230150173A1

    公开(公告)日:2023-05-18

    申请号:US17912672

    申请日:2021-03-19

    CPC classification number: B29C37/006 B01D19/0036 B29B2013/005

    Abstract: Disclosed are processes and systems for degassing liquid resin. Resin is provided at a resin inlet and pumped into a first duct using a resin pump to achieve a first absolute pressure of at least 1.6 bar in the first duct; the resin pump and/or a flow control valve are configured to achieve a first pressure drop across the flow control valve of at least 1.5 bar; a second duct communicates the resin from the flow control valve to a storage tank; a gas evacuation system maintains a pressure in the storage tank below 100 mbar at least partly concurrently with pumping resin into the first duct.

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