Water surface aircraft with high marine adaptability and short-distance low-speed take-off and landing
The embodiment of the invention discloses a water surface aircraft with high marine adaptability and short-distance low-speed take-off and landing. The water surface aircraft comprises a fuselage 1, wings 2, an empennage, a turbofan engine 5 and double hulls 6, the wings 2 are arranged to be upper s...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The embodiment of the invention discloses a water surface aircraft with high marine adaptability and short-distance low-speed take-off and landing. The water surface aircraft comprises a fuselage 1, wings 2, an empennage, a turbofan engine 5 and double hulls 6, the wings 2 are arranged to be upper single wings, the wings 2 and the fuselage 1 are arranged to be of an integrated highly-fused structure, the empennage is arranged to be a T-shaped empennage and comprises a high horizontal tail 3 and a vertical tail 4 which are arranged at the tail of the fuselage 1, and the turbofan engine 5 is installed above the integrally-fused intersection position of the wings 2 and the fuselage to form a high-lift-drag-ratio wing-body fused aerodynamic layout. High-wave-resistance double hulls 6 are symmetrically arranged on the two sides of the lower portion of the aircraft body 1, and the hydrodynamic layout of the low-wave motion response double hulls 6 of the water surface aircraft is formed. The water surface aircraft i |
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