发明名称 Rotor tip light control
摘要 A control circuit for controlling the intensity of a plurality of lights mounted at the ends of the rotor blades of a helicopter. The control circuit is completely self-contained and is powered by a wind-driven generator mounted to the blades. Commands to alter the intensity of the lights or to switch the lights on or off are transmitted by a pulsed light beam mounted on the helicopter tail boom.
申请公布号 US4066890(A) 申请公布日期 1978.01.03
申请号 US19760726364 申请日期 1976.09.24
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 HAMILTON, CHARLES W.;KLEIDER, ALFRED
分类号 B64D47/06;G08G5/02;H04B10/22;(IPC1-7):H04B9/00 主分类号 B64D47/06
代理机构 代理人
主权项
地址
您可能感兴趣的专利