Flatback insert for turbine blades
    1.
    发明公开
    Flatback insert for turbine blades 有权
    Flachrücken-EinsatzfürTurbinenschaufeln

    公开(公告)号:EP2204577A2

    公开(公告)日:2010-07-07

    申请号:EP09178629.3

    申请日:2009-12-10

    IPC分类号: F03D1/06

    摘要: A blade (108) for use in the generation of power has a leading edge (201) and a trailing edge (203). A first shell portion (301) of the blade (108) extends from the leading edge (201) to the trailing edge (203). A second shell portion (302) of the blade (108) also extends from the leading edge (201) to the trailing edge (203). A root portion (209) of the blade (108) is positioned proximate the wind turbine (100) and a tip portion (207) which extends from the root portion (209) away from the wind turbine (100). A trailing edge insert (220) is positioned between the first shell portion (301) and the second shell portion (302) proximate the root portion (209). The trailing edge insert (220) has a surface (260) which extends between and separates the first shell portion (301) from the second shell portion (302) at the trailing edge (203), such that the insert (220) provides a high lift profile for increased blade efficiency.

    摘要翻译: 用于产生动力的叶片(108)具有前缘(201)和后缘(203)。 叶片(108)的第一壳体部分(301)从前缘(201)延伸到后缘(203)。 叶片(108)的第二壳部分(302)也从前缘(201)延伸到后缘(203)。 叶片(108)的根部(209)位于风力涡轮机(100)附近并且从根部(209)远离风力涡轮机(100)延伸的尖端部分(207)。 后缘插入件(220)位于靠近根部(209)的第一壳部分(301)和第二壳部分(302)之间。 后缘插入件(220)具有在后缘(203)处在第一壳部分(302)之间延伸并在第二壳部分(302)处分离第一壳部分(301)的表面(260),使得插入件(220)提供 高升力轮廓提高叶片效率。

    Flatback insert for turbine blades
    2.
    发明授权
    Flatback insert for turbine blades 有权
    涡轮叶片的平背刀片

    公开(公告)号:EP2204577B1

    公开(公告)日:2018-02-21

    申请号:EP09178629.3

    申请日:2009-12-10

    IPC分类号: F03D1/06

    摘要: A blade (108) for use in the generation of power has a leading edge (201) and a trailing edge (203). A first shell portion (301) of the blade (108) extends from the leading edge (201) to the trailing edge (203). A second shell portion (302) of the blade (108) also extends from the leading edge (201) to the trailing edge (203). A root portion (209) of the blade (108) is positioned proximate the wind turbine (100) and a tip portion (207) which extends from the root portion (209) away from the wind turbine (100). A trailing edge insert (220) is positioned between the first shell portion (301) and the second shell portion (302) proximate the root portion (209). The trailing edge insert (220) has a surface (260) which extends between and separates the first shell portion (301) from the second shell portion (302) at the trailing edge (203), such that the insert (220) provides a high lift profile for increased blade efficiency.

    Flatback insert for turbine blades
    3.
    发明公开
    Flatback insert for turbine blades 有权
    涡轮叶片方回应用

    公开(公告)号:EP2204577A3

    公开(公告)日:2016-07-27

    申请号:EP09178629.3

    申请日:2009-12-10

    IPC分类号: F03D1/06

    摘要: A blade (108) for use in the generation of power has a leading edge (201) and a trailing edge (203). A first shell portion (301) of the blade (108) extends from the leading edge (201) to the trailing edge (203). A second shell portion (302) of the blade (108) also extends from the leading edge (201) to the trailing edge (203). A root portion (209) of the blade (108) is positioned proximate the wind turbine (100) and a tip portion (207) which extends from the root portion (209) away from the wind turbine (100). A trailing edge insert (220) is positioned between the first shell portion (301) and the second shell portion (302) proximate the root portion (209). The trailing edge insert (220) has a surface (260) which extends between and separates the first shell portion (301) from the second shell portion (302) at the trailing edge (203), such that the insert (220) provides a high lift profile for increased blade efficiency.

    Rotor blade for use with a wind turbine
    5.
    发明公开
    Rotor blade for use with a wind turbine 有权
    Rotorschaufel zur Verwendung mit einer风力发电机

    公开(公告)号:EP2341238A3

    公开(公告)日:2014-01-15

    申请号:EP10194832.1

    申请日:2010-12-14

    IPC分类号: F03D1/06

    摘要: A rotor blade (22,100,200,300) for use with a wind turbine (10) is provided. The rotor blade includes a blade sidewall (110,304) at least partially defining a cavity (114,147,160,210,312) extending from a blade root (24,102,218) towards a blade tip (26,104,220) of the rotor blade, the blade sidewall having a leading edge (120) and a trailing edge (122), a structural support assembly (124,324) at least partially positioned within the cavity and extending from the blade root towards the blade tip, the structural support assembly having a root end (126,204) and an opposing tip end (128,206), and at least one support member (134,148,150,172,174,212,326,328) coupled between the blade sidewall and the structural support assembly.

    摘要翻译: 提供了一种与风力涡轮机(10)一起使用的转子叶片(22,100,200,300)。 转子叶片包括至少部分地限定从叶片根部(24,102,218)朝向转子叶片的叶片尖端(26,104,220)延伸的空腔(114,147,160,210,312)的叶片侧壁(110,304),叶片侧壁具有前缘(120)和 至少部分地定位在空腔内并从叶片根部朝向叶片尖端延伸的后缘(122),结构支撑组件(124,324),所述结构支撑组件具有根端(126,204)和相对的末端(128,206) )和联接在叶片侧壁和结构支撑组件之间的至少一个支撑构件(134,148,150,172,174,212,326,328)。

    Rotor blade for use with a wind turbine
    6.
    发明公开
    Rotor blade for use with a wind turbine 有权
    转子叶片用于与风力涡轮机一起使用

    公开(公告)号:EP2341238A2

    公开(公告)日:2011-07-06

    申请号:EP10194832.1

    申请日:2010-12-14

    IPC分类号: F03D1/06

    摘要: A rotor blade (22,100,200,300) for use with a wind turbine (10) is provided. The rotor blade includes a blade sidewall (110,304) at least partially defining a cavity (114,147,160,210,312) extending from a blade root (24,102,218) towards a blade tip (26,104,220) of the rotor blade, the blade sidewall having a leading edge (120) and a trailing edge (122), a structural support assembly (124,324) at least partially positioned within the cavity and extending from the blade root towards the blade tip, the structural support assembly having a root end (126,204) and an opposing tip end (128,206), and at least one support member (134,148,150,172,174,212,326,328) coupled between the blade sidewall and the structural support assembly.