发明名称 HELICOPTER WITH ROTOR BLADE LOAD CONTROL METHOD AND DEVICE
摘要 <p>Methods and devices are described for reducing the torque and the level of vibration on a helicopter rotor blade by maintaining a constant lift and constant (low) drag on each section of the blade throughout the entire revolution. A rotor system includes a trackway defining a continuous travel circuit, truck members operatively coupled with the trackway wherein the truck members are selectively translatable along the travel circuit, prime movers operatively coupled with the truck member for selectively moving the truck members along the travel circuit, elongate rotor blades having proximal ends operatively coupled with the truck members and opposite free distal ends wherein the rotor blades are carried with the truck members along the travel circuit thereby generating an upward force for lifting associated load-carrying vehicles. The methods and apparatus allow the rotor blades and the transmission to be significantly lighter and easier to manufacture.</p>
申请公布号 WO2012171004(A1) 申请公布日期 2012.12.13
申请号 WO2012US41900 申请日期 2012.06.11
申请人 BLUEBIRDS TECHNOLOGY LLC;WILKINS, JOHN, ANTHONY 发明人 WILKINS, JOHN, ANTHONY
分类号 B64C29/00 主分类号 B64C29/00
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