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SYSTEM AND PROCESS FOR STARTING FLIGHT OF POWER WING AIRFOILS, IN PARTICULAR FOR WIND GENERATOR

机译:风力机特别是动力翼型机翼飞行的系统和过程

摘要

FIELD: wind turbines.;SUBSTANCE: invention relates to a system for starting the flight of wing air foils for a wind power generator. System (1) for starting the flight of wing air foils (7) for wind power generator (5), comprising: at least one wing profile (7), operatively connected through control tie-rods (9), to winches, at least one autonomous towing aircraft (11) adapted to be connected through disengageable connecting means (13) to at least one wing profile (7) and to transport in flight said wing profile (7), said disengageable connecting means (13) being composed of at least one dragging cable (15) having a first end connected to said autonomous towing aircraft (11), and a second opposite end connected to said first end equipped with at least one controlled engaging/disengaging device (17) adapted to be engaged/disengaged to and from a respective engagement element arranged on said wing profile (7). Controlled engaging/disengaging device (17) is at least one electromagnetic hook and said engagement element arranged on said wing profile (7) is a related element made of metallic material adapted to be magnetically connected to said electromagnetic hook, and said wing profile (7) comprises at least one measuring system (19), preferably of ultrasound type (21), adapted to high frequency triangulate the relative positions of said autonomous towing aircraft (11) and of said wing profile (7).;EFFECT: invention is aimed at providing an autonomous take-off or flight of wing profiles at low wind speeds.;6 cl, 4 dwg
机译:技术领域本发明涉及一种用于启动风力发电机的机翼空气箔片飞行的系统。用于开始风力发电机(5)的机翼空气箔(7)飞行的系统(1),包括:至少一个机翼轮廓(7),其通过控制拉杆(9)可操作地连接至绞盘,至少一架自动牵引飞机(11),其适于通过可分离的连接装置(13)连接至至少一个机翼轮廓(7),并在飞行中运输所述机翼轮廓(7),所述可分离的连接装置(13)包括至少一根拖缆(15),其第一端连接到所述自主牵引飞机(11),第二相对端连接到所述第一端,装备有至少一个适于接合/分离的受控接合/分离装置(17)往返于布置在所述机翼轮廓(7)上的相应的接合元件。受控的接合/脱离装置(17)是至少一个电磁钩,并且布置在所述机翼轮廓(7)上的所述接合元件是由金属材料制成的相关元件,所述相关材料适于磁性地连接到所述电磁机钩,并且所述机翼轮廓(7) )包括至少一个测量系统(19),优选为超声类型(21),该测量系统适于高频地三角测量所述自主牵引飞行器(11)和所述机翼轮廓(7)的相对位置。在低风速下自动起飞或飞行机翼轮廓; 6 cl,4 dwg

著录项

  • 公开/公告号RU2655432C2

    专利类型

  • 公开/公告日2018-05-28

    原文格式PDF

  • 申请/专利权人 KAJT DZHEN RESERCH S.R.L.;

    申请/专利号RU20160100190

  • 发明设计人 IPPOLITO MASSIMO (IT);

    申请日2014-06-05

  • 分类号F03D5;

  • 国家 RU

  • 入库时间 2022-08-21 12:35:33

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