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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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