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 代理人
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