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公开(公告)号:KR100799122B1
公开(公告)日:2008-01-29
申请号:KR1020070029459
申请日:2007-03-26
Applicant: 한국항공우주연구원
IPC: B64C11/02 , B64C27/473 , B64C27/54
Abstract: A tension-torsion strap and a hub device having the same are provided to reduce the time required for the assembly and construction of the hub device with minimizing the reconstruction of the tension-torsion strap through a simple construction. A hub device(100) having a tension-torsion strap(600) includes a hub flexure(300), and a pitch cage(400). The pitch cage is connected to a blade(500). The hub flexure is fixed at a rotor shaft and has a hollow space inside thereof. The tension-torsion strap is inserted in the hub flexure. The hub flexure is coupled with the tension-torsion strap by a hub flexure connecting pin(310). The pitch cage is mounted on an opposite side of the tension-torsion strap inserted in the hub flexure. The pitch cage fixes the blade and the tension-torsion strap by the pitch cage pin.
Abstract translation: 提供了一种拉力扭力带和具有该拉力扭力带的轮毂装置,以通过简单的结构最小化拉伸扭力带的重建来减少轮毂装置的组装和构造所需的时间。 具有张力扭力带(600)的轮毂装置(100)包括轮毂挠曲件(300)和间距保持架(400)。 节距笼连接到叶片(500)。 轮毂挠曲件固定在转子轴上并且在其内部具有中空空间。 拉力扭力带插入轮毂弯头。 轮毂挠曲通过轮毂挠曲连接销(310)与张力扭力带联接。 间距保持架安装在插入轮毂挠曲件的张力扭力带的相对侧。 节距笼通过俯仰笼销固定刀片和张力扭力带。
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