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    • 2. 发明申请
    • PITCH DRIVE APPARATUS OF WIND GENERATOR AND WIND GENERATOR
    • 风力发电机和风力发电机的俯仰驱动装置
    • US20120025525A1
    • 2012-02-02
    • US12600494
    • 2009-04-17
    • Tomohiro Numajiri
    • Tomohiro Numajiri
    • F03D7/04H02P9/04
    • F03D7/0224F05B2260/76F05B2260/79Y02E10/721Y02E10/723
    • The present invention provides a pitch drive apparatus of a wind generator and the wind generator constituted not to affect a main shaft or a gear box, and capable of preventing reliability from being deteriorated. The pitch drive apparatus includes a wind turbine blade (6) having a base portion (21) mounted so as to be turnable around an axis center L with respect to a rotor head (4), an electric drive member having an output shaft (19) mounted on the rotor head (4) so as to extend in a direction along the axis center (L), a lever (15) having one end fixed to the output shaft (19) and extending in a direction intersecting with the output shaft (19), and a connecting link (17) disposed so as to extend in a direction intersecting with the output shaft (19). One end of the connecting link (17) is rotatably mounted on a free end of the lever (15) and the other end of the connecting link (17) is rotatably mounted on a drive position P of the wind turbine blade (6).
    • 本发明提供了一种风力发电机的变桨驱动装置和风力发电机,其不影响主轴或齿轮箱,并且能够防止可靠性劣化。 变桨驱动装置包括:风力涡轮机叶片(6),具有安装成相对于转子头(4)围绕轴线中心L旋转的基部(21),具有输出轴(19)的电驱动构件 )安装在所述转子头(4)上以沿着所述轴线中心(L)的方向延伸;杆(15),其一端固定到所述输出轴(19)并沿与所述输出轴 (19),以及连接杆(17),其设置成在与输出轴(19)相交的方向上延伸。 连接杆(17)的一端可旋转地安装在杠杆(15)的自由端上,并且连接杆(17)的另一端可旋转地安装在风力涡轮机叶片(6)的驱动位置P上。
    • 6. 发明申请
    • TURBINE ROTOR
    • 涡轮转子
    • US20150300178A1
    • 2015-10-22
    • US14692451
    • 2015-04-21
    • MITSUBISHI HEAVY INDUSTRIES
    • Katsuyuki OSAKOAtsushi MATSUOTakao YOKOYAMA
    • F01D5/14F01D25/24F01D5/02
    • F01D5/141F01D5/02F01D5/043F01D5/048F01D5/20F01D25/24F05D2240/30F05D2250/71
    • A turbine rotor of a turbine includes a hub that serves as an axis of rotation, and a plurality of turbine blades. The turbine blades each have a line extending along a shroud-side edge of the turbine blade from the inlet to the outlet as a shroud line. The shroud line includes an entrance-side shroud line La that makes a small change from the inlet toward the outlet in a blade angle with respect to the axis of rotation, a center shroud line Lb that extends from the outlet side of the entrance-side shroud line La and makes a greater change than that of the entrance-side shroud line La, and an exit-side shroud line Lc that extends from the outlet side of the center shroud line Lb to the outlet and makes a smaller change than that of the center shroud line Lb.
    • 涡轮机的涡轮机转子包括用作旋转轴线的轮毂和多个涡轮机叶片。 涡轮机叶片各自具有沿着涡轮机叶片的护罩侧边缘从入口延伸到出口的线作为护罩线。 护罩线包括入口侧护罩线La,该入口侧护罩线La相对于旋转轴线以相对于入口朝向出口的角度稍微改变,中心护罩线Lb从入口侧的出口侧延伸 护罩线La并且比入口侧护罩线La更大的变化,以及从中心护罩线Lb的出口侧到出口延伸的出口侧护罩线Lc,并且比从 中心护罩线Lb。
    • 9. 发明授权
    • Gas turbine rotor blade
    • 燃气轮机转子叶片
    • US6099253A
    • 2000-08-08
    • US203680
    • 1998-12-01
    • Ichiro FukueEiji AkitaKiyoshi SuenagaYasuoki Tomita
    • Ichiro FukueEiji AkitaKiyoshi SuenagaYasuoki Tomita
    • F01D5/18F01D5/20F02C7/18
    • F01D5/225F01D5/187Y02T50/676
    • A gas turbine rotor blade has a plurality of first cooling holes for the flow of a cooling gas bored in a blade portion along its lengthwise direction and a plurality of second cooling holes for flow of the cooling gas bored in a shroud along its plane direction so as to communicate with the first cooling holes, and is constructed such that the cooling gas can flow in a uniform distribution. The plurality of the first cooling holes 3 for flow of the cooling gas are bored in the blade portion 2 and the plurality of the second cooling holes 5 for flow of the cooling gas are bored in the shroud 1 along its plane direction. The second cooling holes 5 communicate with the first cooling holes 3, hole to hole, via two-step holes 4, and the second cooling holes 5 are bored alternately on the dorsal side and the ventral side of the rotor blade.
    • 燃气轮机转子叶片具有多个第一冷却孔,用于沿其长度方向在叶片部分中钻出的冷却气体的流动,以及多个用于沿着其平面方向在护罩中钻出的冷却气体的流动的第二冷却孔, 与第一冷却孔连通,并且被构造成使得冷却气体能够以均匀的分布流动。 多个用于冷却气体流动的第一冷却孔3在叶片部分2中钻孔,并且用于冷却气体流动的多个第二冷却孔5沿其平面方向在护罩1中钻孔。 第二冷却孔5通过两步孔4与第一冷却孔3,孔对孔连通,第二冷却孔5在转子叶片的背侧和腹侧交替地钻孔。