LEADING EDGE PROTECTION WITH REDUCED NOISE IMPACT

    公开(公告)号:US20240133358A1

    公开(公告)日:2024-04-25

    申请号:US18278262

    申请日:2022-02-14

    申请人: LM WIND POWER A/S

    IPC分类号: F03D1/06

    摘要: The present invention relates to a leading edge protection for a wind turbine blade, wherein a leading edge axis of the leading edge protection is configured to be fitted on at least part of a leading edge of a wind turbine blade and the leading edge protection is configured to extend between the leading edge and a first edge downstream a first side of the wind turbine blade as well as between the leading edge and a second edge downstream a second side of the wind turbine blade, wherein the leading edge protection comprises a first part and wherein the first edge is configured to be non-parallel with the leading edge of the wind turbine blade along the first part of the leading edge protection. The present invention further relates to a wind turbine blade comprising the leading edge protection and a wind turbine comprising the wind turbine blade. Finally, the present invention relates to a method for protecting a leading edge of a wind turbine blade arranged on a wind turbine and a leading edge protection obtainable by that method.

    Trailing edge modifications for wind turbine airfoil

    公开(公告)号:US09670901B2

    公开(公告)日:2017-06-06

    申请号:US14221726

    申请日:2014-03-21

    IPC分类号: F03D1/06

    摘要: A wind turbine blade airfoil trailing edge (TE) with a first waveform profile (44B, 44C, 44E) as seen from behind, formed by ruffles or alternating ridges (21) and valleys (22) formed on the airfoil (20) and ending at the trailing edge. The trailing edge may further include a second waveform profile (48B, 48C, 48E) as seen from above, resulting from serrations formed by an oblique termination plane (32B) of the trailing edge or by other geometry. The ridges and/or serrations may be asymmetric (44E, 48E) to increase a stall fence effect of the ridges on the suction side (SS) of the trailing edge. The first and second waveforms may have the same period (44B, 48B) or different periods (44C, 48C).

    Vortex generators aligned with trailing edge features on wind turbine blade
    15.
    发明授权
    Vortex generators aligned with trailing edge features on wind turbine blade 有权
    风力发电机与风力涡轮机叶片上的后缘特征对齐

    公开(公告)号:US09476406B2

    公开(公告)日:2016-10-25

    申请号:US14251943

    申请日:2014-04-14

    IPC分类号: F03B3/12 F03D1/06

    摘要: A wind turbine blade (80, 82) having a spanwise series of vortex generators (26, 28, 26P, 28P, 64, 66) and having a trailing edge (42) defining a waveform. The vortex generators are aligned with a predetermined position or phase (44, 46) of a respective period of the trailing edge waveform. Each vortex generator may be designed to create a vortex (27, 29) that crosses the trailing edge at an angle of less than 30 degrees from parallel to the trailing edge. The blade may include alternating ridges (52) and troughs (54) that end at the waveform trailing edge. A front end of each trough may form a V-shaped drop-off in the suction side of the blade that forms a pair (64, 66) of vortex generators to create counter-rotating vortices within the trough that entrain energy to the bottom of the trough.

    摘要翻译: 具有翼展式涡旋发生器(26,28,26P,28P,64,66)并且具有限定波形的后缘(42)的风力涡轮机叶片(80,82)。 涡流发生器与后缘波形的相应周期的预定位置或相位(44,46)对齐。 每个涡流发生器可被设计成产生以与后缘平行的小于30度的角度穿过后缘的涡流(27,29)。 叶片可以包括在波形后缘处结束的交替的脊(52)和槽(54)。 每个槽的前端可在叶片的吸入侧形成V形脱落物,形成涡流发生器的一对(64,66),以在槽内形成反向旋转的旋涡,其将能量夹带到 槽。

    WIND TURBINE BLADE
    16.
    发明申请
    WIND TURBINE BLADE 有权
    风力涡轮叶片

    公开(公告)号:US20140286784A1

    公开(公告)日:2014-09-25

    申请号:US14360125

    申请日:2012-11-15

    发明人: Ashish Singh

    IPC分类号: F03D1/06

    摘要: A wind turbine blade is described having noise reduction features. The blade has a plurality of projecting serrations provided at the blade trailing edge to reduce the scattering noise produced during operation of the blade, wherein the serrations have a plurality of through-going apertures defined in the serration body. The apertures act to provide a pressure equalisation effect at the serrations between the suction and pressure sides. This pressure equalisation provides for improved noise reduction performance, as well as a reduction in mechanical stresses and strains which may be experienced by the serrations, increasing serration lifetime.

    摘要翻译: 描述了具有降噪特征的风力涡轮机叶片。 叶片具有设置在叶片后缘处的多个突出锯齿,以减少在叶片操作期间产生的散射噪声,其中锯齿具有限定在锯齿体中的多个贯穿孔。 这些孔用于在吸力侧和压力侧之间的锯齿处提供压力平衡效果。 这种压力均衡提供了改进的降噪性能,以及锯齿可能经历的机械应力和应变的降低,增加了锯齿寿命。

    CORRUGATED PANEL FOR WIND POWER GENERATOR BLADE
    17.
    发明申请
    CORRUGATED PANEL FOR WIND POWER GENERATOR BLADE 审中-公开
    风力发电机叶片变压板

    公开(公告)号:US20140017088A1

    公开(公告)日:2014-01-16

    申请号:US14007314

    申请日:2012-01-06

    IPC分类号: F01D5/14

    摘要: A corrugated panel for a wind power generator blade is provided. The corrugated panel for a wind power generator blade includes: a plurality of wrinkles that are coupled to one surface or the other surface of the wind power generator blade having an airfoil transverse section and that are formed in a length direction of the blade, wherein a gap and a height at a predetermined position of the plurality of wrinkles each have a value of a predetermined ratio to a chord length of the airfoil transverse section of the blade at the predetermined position, when the plurality of wrinkles are coupled to the blade.

    摘要翻译: 提供了一种用于风力发电机叶片的波纹板。 用于风力发电机叶片的波纹板包括:多个皱纹,其耦合到风力发电机叶片的具有翼型横截面并且沿着叶片的长度方向形成的一个表面或另一个表面,其中, 多个褶皱的预定位置处的间隙和高度各自具有与预定位置处的叶片的翼型件横截面的弦长的预定比率的值,当多个褶皱联接到叶片上时。

    Wind turbine blade with anti-noise devices
    19.
    发明授权
    Wind turbine blade with anti-noise devices 有权
    具有防噪声装置的风力发电机叶片

    公开(公告)号:US08157532B2

    公开(公告)日:2012-04-17

    申请号:US12154570

    申请日:2008-05-23

    IPC分类号: F03D1/06

    摘要: A wind turbine comprising at least a blade (11) having an aerodynamic profile with a leading edge (13), a trailing edge (15) and suction and pressure sides between the leading edge (13) and the trailing edge (15) that includes an anti-noise device (31) placed on the suction side formed by elements (33) that modify the frequency spectra of the boundary layer noise. Preferably the anti-noise device (31) is placed on the suction side between two sections corresponding to chord positions in the range of 40%-95% of the chord length, measured from the leading edge (13).

    摘要翻译: 一种风力涡轮机,包括具有前缘(13)的空气动力学轮廓的至少一个叶片(11),在前缘(13)和后缘(15)之间的后缘(15)和吸力和压力侧, 放置在由元件(33)形成的吸入侧的抗噪声装置(31),其改变边界层噪声的频谱。 优选地,抗噪声装置(31)被放置在从前缘(13)测量的对应于弦长的40%-95%范围内的和弦位置的两个部分之间的吸力侧。