| 摘要 |
<p>A blade joint (125) for joining a first blade segment (100) and a second blade segment (100), each having an aerodynamic profile, in a rotor blade (22) is disclosed. The blade joint (125) includes a firstjoint segment (130) and a secondjoint segment (130) each having an outer surface (132), an inner surface (134), and a thickness (136) therebetween. The outer surface (132) of each joint segment (130) has an aerodynamic profile. The firstjoint segment (130) and the secondjoint segment (130) each further have a joint interface end (142), a blade interface end (144), and a length (146) therebetween. The joint interface end (142) of the first joint segment (130) and the joint interface end (142) of the second joint segment (130) are configured to couple the first joint segment (130) and second joint segment (130) together.</p> |
