发明名称 Gun hardened, rotary winged, glide and descent device
摘要 A payload carrying device which is inserted into a remote area of interest by means of a projectile carrier to obtain data, or the like, from the remote area. The device has counter rotating main blades as well as tail blades carried on a tail rotor. The particular payload is carried in a canister which may also include a power source, a command and control unit and a motor, if hover or lateral flight is desired. The pitch of the tail blades is variable as well as their orientation around an axis, the combination of which generates a thrust vector in a particular direction for controlled lateral flight.
申请公布号 US6347764(B1) 申请公布日期 2002.02.19
申请号 US20000710736 申请日期 2000.11.13
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 BRANDON FRED J.;HOLLIS MICHAEL S. L.
分类号 F42B10/58;(IPC1-7):B64C27/08 主分类号 F42B10/58
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