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Retrofit body for a rotor blade of a wind turbine, retrofitted rotor blade and method for retrofitting the rotor blade

机译:用于风力涡轮机的转子叶片的改装体,改装的转子叶片以及改装该转子叶片的方法

摘要

A retrofit body for a rotor blade (2) of a wind power plant has a retrofit body tip (11) and a coupling side (12) arranged away from the retrofit body tip (11) and adapted for molding the retrofit body (7) to the rotor blade tip (6), such that when the retrofit body (7) is molded onto the rotor blade tip (6), the retrofit body tip (11) protrudes from the rotor blade tip (6) by a predetermined span extension (16) in the spanwise direction of the rotor blade (2), the retrofit body (7) a profile lug (9) which forms the front of the retrofit body (7) seen in the direction of flow of the rotor blade (2) and which has the retrofit body leading edge (8) and away from the retrofit body tip (11) beyond the coupling side by a predetermined length protrudes with its leading edge extension portion (13), which, when the retrofit body (7) is integrally formed on the rotor blade tip (6) t, facing the rotor blade root (5) and covering an outer region of the rotor blade leading edge (3) seen in the spanwise direction, the profile nose (9) being parallel to the retrofit body leading edge (8) arranged a plurality of juxtaposed and protruding from the profile nose (9) Having projections (18) whose heights and / or their distances from each other and / or their offset away from the Nachrüstkörpervorderkante (8) in the flow direction are dimensioned such that the buoyancy-reducing effect of the projections (18) only at those Anstellwinkeln (24) of the retrofitted rotor blade (1) equal to or greater than a design pitch angle (24) of the original rotor blade (2).
机译:用于风力发电设备的转子叶片(2)的改装体具有改装体尖端(11)和布置成远离改装体尖端(11)并适于模制改装体(7)的联接侧(12)。这样,当改装体(7)模制到转子叶片尖端(6)上时,改装体尖端(11)从转子叶片尖端(6)伸出预定的跨度(16)在转子叶片(2)的翼展方向上,改型体(7)的轮廓凸耳(9)从转子叶片(2)的流动方向看形成了改型体(7)的前部),其具有改型车身前缘(8),并从改型车身末端(11)超出联接侧一预定长度,并以其前缘延伸部分(13)突出,当改型车身(7)时整体地形成在转子叶片尖端(6)t上,面向转子叶片根部(5),并覆盖SPA中看到的转子叶片前缘(3)的外部区域在n方向上,平行于改型主体前缘(8)的轮廓鼻部(9)布置成从轮廓鼻部(9)并列并突出,并具有突起(18),所述突起的高度和/或它们彼此的距离和/或在流动方向上偏离Nachrüstkörpervorderkante(8)的尺寸确定为使得仅在改造后的转子叶片(1)的Anstellwinkeln(24)处,突起(18)的降低浮力的作用原始转子叶片(2)的设计俯仰角(24)。

著录项

  • 公开/公告号DE102017107464A1

    专利类型

  • 公开/公告日2018-10-11

    原文格式PDF

  • 申请/专利权人 TEG TUBERCLE ENGINEERING GROUP GMBH;

    申请/专利号DE201710107464

  • 发明设计人 ACHIM FISCHER;

    申请日2017-04-06

  • 分类号F03D1/06;

  • 国家 DE

  • 入库时间 2022-08-21 12:34:10

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