|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/013; 244/055; 244/106|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 7|
An amphibious airplane having an engine assembly mounted at a top center location in the fuselage, and a tail assembly having a horizontal fin in an elevated position so as to be in the propeller air stream. A lift augmenting aerodynamic surface is positioned at the top middle portion of the aircraft fuselage, with the propeller being at the concavely curved rear end of the lift augmenting surface. A pair of platforms are positioned on opposite sides of the fuselage at lower locations adjacent to a passenger section of the aircraft. These platforms are a...
1. An airplane comprising:a) a fuselage having a longitudinal axis, a vertical axis, and a lateral axis, perpendicular to said longitudinal and vertical axes; b) a main wing mounted to the fuselage and extending generally laterally therefrom as right and left wing sections c) an engine assembly mounted above said fuselage and spaced upwardly therefrom and having a propeller which defines a propeller area through which the propeller rotates, said propeller creating a rearwardly traveling propeller flow stream; d) a tail section located at a rear portion o...