| 摘要 |
The present invention relates to an airplane equipped with a wing booster. An airplane (1), which includes a fuselage (3) forming the body thereof and a main wing (5) coupled to intersect the central portion of the fuselage, is characterized by comprising: one or more intakes (11) formed in the main wing (5) and through which outside air flows into the main wing (5); one or more blower means (13) surrounded by a cladding (21) of the main wing (5) and disposed corresponding to the intake (11) to accelerate the outside air flowing in through the intake (11) along the length of the main wing (5) and to diffuse the air; a driving means (15) for driving the rotation of the blower means (13); an exhaust (17), open rearward along the leading edge of the top surface (23) of the main wing (5), for exhausting the outside air accelerated by the blower means (13) along the surface layer of the top surface (23) of the main wing (5); and a passage means (19), connecting the intake (11) and the exhaust (17), for compressing and diffusing the outside air accelerated by the blower means (13) disposed next to the intake (11) toward the exhaust (17). Thus, especially during takeoff, outside air which has flowed into the main wing through the intake is compressed and diffused at high speed by the blower means and is discharged through the exhaust and evenly diffused along the surface layer of the top surface of the main wing so as to significantly shorten takeoff time by increasing the lift at the main wing and to greatly improve the comfort of the flight for passengers. |
