Light-duty aeroplane

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/10 (2006.01) B64C 39/06 (2006.01) B64C 39/12 (2006.01)

Patent

CA 2125342

The invention relates to the aircraft engineering and in particular, to the design and aerodynamic confi- guration of light-duty multipurpose aeroplanes. The light-duty multipurpose aeroplane comprises a fuselage 1 having a cabin 2 arranged at the centre, at the tail portion of which a pusher propeller is mounted in a ring 3. The front portion of the fuselage is pro- vided with an all-swivelling horizontal empennage of "canard" type 4. The wing of the aeroplane is of arti- culated type and consists of a low-mounted wing 5 and a high-mounted wing 6, which have mutually opposite wing steeps. The tips of the wings are connected with one another by means of an arrow-shaped pylon 8 provided with heading control rudders 9. Owing to the new design, the aeroplane possesses high carrying properties and good stability.

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