| 摘要 |
PROBLEM TO BE SOLVED: To provide an aircraft which enables low-speed flight by using wings that gain sufficient lift and is not affected by cross wind even in low-speed flight.SOLUTION: Sub-fuselages 12 are arranged in parallel on both sides of a main fuselage 1. A front horizontal stabilizer 13 and a rear horizontal stabilizer 15 in which their centers are fixed to the main fuselage 1 and both ends are fixed to the sub-fuselages 12 are provided. A main wing 14 in which its center is fixed to the main fuselage 1 and intermediate parts are fixed to the sub-fuselages 12 is provided. Two pairs of posture controlling propellers 18 in total in which rotation shafts are directed in a longitudinal direction of the wing are provided for a front end part and a rear end part of both sub-fuselages 12. Two pairs of vertical floating propellers 16 in total in which rotation shafts are directed in a direction penetrating the wing are provided for both end parts of the front horizontal stabilizer 13 and the rear horizontal stabilizer 15. The posture controlling propellers 18 make it possible to take off and land without being affected by cross wind even in low-speed flight. |
