发明名称 Rotor blade internal damper
摘要 A load absorbing elastic member or members is incorporated in the design of a rotor blade to assist in reducing flapwise and chordwise bending moments, torsional loading, and to reduce or eliminate the control system loads induced by rotor blade moment stall. In all its embodiments, the load absorbing elastic member has operatively associated therewith a constraining member which serves as a strain amplifier permitting the load absorbing elastic member to achieve its purpose effectively.
申请公布号 US4329119(A) 申请公布日期 1982.05.11
申请号 US19790040364 申请日期 1979.05.16
申请人 THE BOEING COMPANY 发明人 BASKIN, JOSEPH M.
分类号 B64C27/473;B64C27/51;(IPC1-7):B64C27/46 主分类号 B64C27/473
代理机构 代理人
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