Small unmanned aircraft

Aeronautics and astronautics – Aircraft power plants – Arrangement

Reexamination Certificate

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C244S105000, C244S903000

Reexamination Certificate

active

07980510

ABSTRACT:
A small unmanned airplane includes; a main wing having a camber airfoil whose under surface is approximately flat, narrowing in the shape of taper to a blade tip, leading edge of which holds sweepback angle, of flying wing type which has an aerodynamic surface of tailless wing type and is low aspect ratio; movable flaps extending approximately extreme breadth in trailing edge part of both left and right sides of the main wing, having a dihedral angle at least in level flight; vertical stabilizers placed at blade tips of left and right of the main wing; and two propellers installed on the top surface of the main wing. This can materialize miniaturization and weight saving of a small unmanned airplane for individual carrying capability and for suitability for such as lift-off by hand throw.

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rl.mite.pdf>. The paper appears to have been given at a conference in 2001; the examiner cannot verify the paper online until Dec. 2003.
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International Search Report for International Application No. PCT/JP2004/006390, Dated Aug. 17, 2004, 2 page(s).

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