发明名称 Mounting arrangement for variable diameter rotor blade assemblies
摘要 A mounting arrangement (100) for a Variable Diameter Rotor blade assembly (16) having an outer blade segment telescopically mounting to a torque tube member (24), and connecting means (70) for transferring centrifugal loads of the outer blade segment (22) to a rotor hub assembly (18). The outer blade segment (22) includes a spar member (30) having a longitudinal axis (26) and defining an internal channel (62) for accepting the torque tube member (24) and the connecting means (70). The mounting arrangement (100) couples the connecting means (70) to the spar member (30) and includes a restraint surface (86) formed within the spar member (30) and a restraint assembly (68) disposed in combination therewith. The restraint surface (86) is disposed inboard of the tip end (90) of the spar member (30) and in a plane oriented transversely of the longitudinal axis (26). The restraint assembly (68) is disposed internally of the spar member (30) and includes a bearing block (102) mounting to the connecting means (70) and having upper and lower transverse slots (104a, 104b) formed therein. The restraint assembly (68) further comprises a load transfer member (106) disposed in combination with the transverse slots (104a, 104b) and the restraint surface (86) for transferring centrifugal loads to the connecting means (70). A sidewall aperture (134) is formed in the spar member (30) and proximal to the restraint surface (86) to facilitate installation of the load transfer member (106) in the transverse slots (104a, 104b).
申请公布号 US5655879(A) 申请公布日期 1997.08.12
申请号 US19950412035 申请日期 1995.03.28
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 KIELY, EDMOND F.;BEATTY, ROBERT D.
分类号 B64C11/00;B64C29/00;(IPC1-7):B64C11/28 主分类号 B64C11/00
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