| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed aircraft has top wing located above fuselage, two power internal combustion engines mounted on wing, fuselage and standard control units. Fuselage has case made in form of hull with strong bottom whose skin is profiled for sliding on water, breakwater, stabilizers for obtaining stability in alighting on water: central stabilizer is located along longitudinal axis running through center of gravity and side stabilizers are located in nose section of hull at level of its submergence. Provision is also made for hatches made from transparent material which form upper part of saloon where four rows of seat are arranged. ^ EFFECT: improved visual observation. ^ 2 dwg |
