发明名称 Wing assemblies for aircraft
摘要 A rotary wing having a spar that flexes and crosses the axis of t the spar in two or more points. The spar mounts a flying surface extending spanwise and rotatable about the longitudinal axis of the spar without the transmission of flexural movement to the wing sheets. The spar mounts a rib extending chordwise and rotatable about the spar and comprising rib means extending spanwise and positioned such that they can engage a portion of the wing sheets and transmit rotation to the wing sheets without interfering with the relative movement between the wing sheets and the spar. The chordwise rib is adapted to receive power transmission such t that while rotating is capable to transmit rotation to the wing sheets through the spanwise extending ribsmeans. The transmission of rotation to the wing sheets is achieved without transmission of rotation to the spar.
申请公布号 US2005116086(A1) 申请公布日期 2005.06.02
申请号 US20030705529 申请日期 2003.11.12
申请人 ORAZI PAUL 发明人 ORAZI PAUL
分类号 B64C23/02;B64C39/00;(IPC1-7):B64C27/22 主分类号 B64C23/02
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