发明名称 ELASTOMERIC HELICOPTER LOAD REACTION SYSTEM
摘要 <p>ELASTOMERIC HELICOPTER ROTOR LOAD REACTION SYSTEM A helicopter rotor having one or more blades mounted for rotation with the rotor hub and each supported therefrom by an elastomeric bearing, and having a lead-lag damper connected to the blade and the hub and extending substantially parallel to the blade axis, and including the improvement of apparatus for preventing tension loading of the elastomeric bearing as the blade moves radially inwardly as a result of rotor braking.</p>
申请公布号 CA1110604(A) 申请公布日期 1981.10.13
申请号 CA19790326994 申请日期 1979.05.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FERRIS, DONALD L.;HIBYAN, EDWARD S.;FAIZ, ROBERT L.
分类号 B64C27/32;B64C27/35;B64C27/48;(IPC1-7):64C11/06;64C27/04 主分类号 B64C27/32
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