System for a tower segment of a tower, a respective tower segment, and a wind turbine having a tower segment

    公开(公告)号:US11802577B2

    公开(公告)日:2023-10-31

    申请号:US17541652

    申请日:2021-12-03

    IPC分类号: F15D1/10 F03D13/20

    摘要: A system for a tower segment of a tower is presented, wherein the tower segment is configured for forming at least partially a part of a tower for carrying a structure, in particular for supporting a nacelle of a horizontal-axis wind turbine or a machine house of a vertical-axis wind turbine. The system is configured to be attached, arranged, and/or mounted to the tower segment and comprises at least an airflow manipulation arrangement and a support arrangement. The airflow manipulation arrangement includes an airflow manipulator which is configured for affecting an airflow around the tower segment. The support arrangement is configured for supporting the airflow manipulation arrangement and for mounting the airflow manipulation arrangement to the tower segment. The airflow manipulation arrangement and the support arrangement are configured such, when mounted to the tower segment, that the airflow manipulator projects a tower diameter in radial direction by at least 5%, in particular at least 10%, preferred at least 15%, in particular not more than 30%, further in particular not more than 20%, of the tower diameter, or that the airflow manipulator is essentially parallel to the tower segment. By this, an effective measure against vortex shedding effects is put in place.

    WIND CHANNELLING AND DIRECTING STRUCTURES
    83.
    发明公开

    公开(公告)号:US20230287910A1

    公开(公告)日:2023-09-14

    申请号:US18007220

    申请日:2021-07-05

    IPC分类号: F15D1/10

    CPC分类号: F15D1/10

    摘要: A structure (1) for channelling and directing incident wind is described. The structure includes a hollow pipe (2) having a downstream end (2a) that defines at least one outlet and an upstream end (2b). A rotatably mounted intake (4) is positioned at the upstream end (2b) of the pipe (2) and is adapted to direct incident wind into the pipe.

    AIR CONDUCTION ELEMENT FOR REDUCING AIR RESISTANCE OF A LOAD-CARRYING VEHICLE

    公开(公告)号:US20180154951A1

    公开(公告)日:2018-06-07

    申请号:US15576026

    申请日:2016-06-08

    IPC分类号: B62D35/00 F15D1/10 F15D1/14

    摘要: An air conduction element for reducing the air resistance of a load-carrying vehicle having a load space structure. The air conduction element can be externally mounted in the rear region of the load space structure and includes an air conduction duct with a front air inlet opening and a rear air outlet opening, front and rear being in relation to the direction of travel (x). The air inlet opening overlaps the load space structure in the direction of travel (x) and the air outlet opening is arranged behind the load space structure within the cross-sectional contour thereof. The air conduction element has a cover which delimits the air conduction duct. It was therefore the aim to devise an air conduction element which does not increase the dimensions of the load space structure when the vehicle is driving slowly or is at a standstill. For this purpose, the cover is produced from a flexible flat material.

    Fairing
    87.
    发明授权
    Fairing 有权

    公开(公告)号:US09725961B2

    公开(公告)日:2017-08-08

    申请号:US14783758

    申请日:2013-04-12

    发明人: Kjetil Skaugset

    摘要: A fairing device for the reduction of vortex-induced vibrations or motions and the minimization of drag about a substantially cylindrical element immersed in a fluid medium, comprising; a cylindrical element, a fairing rotatably mounted about the cylindrical element, the fairing comprising a shell with a cylindrical cross-sectional shape with an outer diameter (D) following the outer diameter of the cylindrical element from an upward stagnation point of 0 degrees to at least +/−90 degrees, and which at +/−90 degrees continues as two fin-like portions in an aft direction and defining a chord length (C), further comprising that the fin-like portions are convexly curved aft of +/−90 degrees thus tapering towards each other and defining a tail end opening or gap less than the fairing standoff height.