发明名称 FLEXBEAM ROTOR ATTACHMENT TO ROTOR BLADE
摘要 A rotor blade assembly includes a flex-beam member and a torque tube surrounding the flex-beam member and extending partially along a rotor blade assembly length. A rotor blade surrounds the flex beam member and extends from the torque tube to a blade tip. A connecting assembly secures the rotor blade and the torque tube at the flex-beam member. The connecting assembly includes a first connecting member extending at least partially into the rotor blade assembly through the rotor blade from a first rotor blade side and a second connecting member located at a second rotor blade side. A clamping load between the first connecting member and the second connecting member secures the rotor blade and torque tube to the flex-beam member.
申请公布号 US2016176521(A1) 申请公布日期 2016.06.23
申请号 US201514702081 申请日期 2015.05.01
申请人 Sikorsky Aircraft Corporation 发明人 Parsons Eric S.;Nussenblatt Eric Lucien;Thomas Justin;Casey Ryan Thomas;Hunter David H.
分类号 B64C27/473;B64C27/04;B64C27/12;B64C27/33;B64C27/48 主分类号 B64C27/473
代理机构 代理人
主权项
地址 Stratford CT US