发明名称 Rotor blade track adjustment for helicopters - using control rod coordinated with each rotor blade, with adjustment carried out in flight and indicated in cockpit
摘要 <p>The installation adjusts the running track of helicopter rotor blades. Each rotor blade is coordinated with a length adjustable control rod with an adjusting motor connected to the supply unit for the rotor blade control. The adjustment of each control rod may be carried out during flight by remote control from a command console in the cockpit of the helicopter through a receiver section for the adjustment motor positioned on the rotatable head of the rotor. Indicators are provided which confirm the degree of rotor blade adjsutment on the cockpit instrumentation.</p>
申请公布号 DE2757617(A1) 申请公布日期 1979.06.28
申请号 DE19772757617 申请日期 1977.12.23
申请人 HENSCHEL FLUGZEUG-WERKE AG 发明人 THOM,ELMAR
分类号 B64C27/54;(IPC1-7):64C27/54 主分类号 B64C27/54
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