发明名称 |
JOINT ASSEMBLY FOR ROTOR BLADE SEGMENTS OF A WIND TURBINE |
摘要 |
The present subject matter is directed to a rotor blade assembly and/or a joint assembly for a wind turbine blade. In one embodiment, the rotor blade assembly includes at least first and second blade segments connected together at a chord-wise extending joint, one or more shear-loaded pins configured through the chord-wise extending joint, and an anti-rotation locking feature. As such, the rotor blade assembly includes a maintenance-free bolted joint. The first blade segment has a body shell defining a generally aerodynamic profile. The body shell includes a suction side surface and a pressure side surface. The shear-loaded pin may extend in a generally flap-wise direction (i.e. from the suction side surface to the pressure side surface of the body shell) or in a generally chord-wise direction (i.e. from the pressure side to the suction side of the body shell). |
申请公布号 |
US2015240780(A1) |
申请公布日期 |
2015.08.27 |
申请号 |
US201414188756 |
申请日期 |
2014.02.25 |
申请人 |
General Electric Company |
发明人 |
Leonard Jay F.;Judge Paul William |
分类号 |
F03D1/06 |
主分类号 |
F03D1/06 |
代理机构 |
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代理人 |
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主权项 |
1. A rotor blade assembly for a wind turbine, the rotor blade assembly comprising:
a first blade segment comprising:
a body shell defining a generally aerodynamic profile, the body shell comprising a suction side surface and a pressure side surface; a second blade segment connected to the first blade segment at a maintenance-free chord-wise extending joint; at least one shear-loaded pin configured through the chord-wise extending joint, the shear-loaded pin extending in a generally flap-wise direction; and, an anti-rotation locking feature configured with the at least one shear-loaded pin, the locking feature configured to secure the shear-loaded pin within the body shell. |
地址 |
Schenectady NY US |