| 摘要 |
PURPOSE: An airplane having a wing booster is provided to increase lifting force applied to main wings by increasing outdoor air velocity flowing on the top of the main wings and to improve convenience of passengers by reducing takeoff time of the airplane. CONSTITUTION: An airplane having a wing booster(1) comprises a dynamic body(3), main wings(5), air suction ports, blowing units(13), driving units(15), exhaust ports, and passage units(19). The dynamic body is formed as a main body. The main wings are transversely coupled at the middle of the dynamic body. The air suction ports are penetrated through a shell of an airplane so that outdoor air can flow into an airplane. The blowing units are surrounded by the shell of the main wings to cope with the air suction ports. The blowing units accelerate the outdoor air flowing into through the air suction ports in a longitudinal direction of the main wings to diffuse. The driving units rotate the blowing units.
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