|국가/구분||United States(US) Patent 등록|
|우선권정보||FR-07 54689 (2007-04-25)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 7|
A large-capacity airplane principally includes a fuselage which has no region of constant width between the front and the rear and a wing fixed to the fuselage. As a preference, the engines are fixed at the rear under a horizontal tail held above the fuselage by vertical stabilizers and maintenance wells are formed in the fuselage in vertical alignment with each engine to allow the engines to be fitted and removed. The width of the fuselage is determined, on the one hand, so that the airplane landing gear is fixed to the fuselage and in the up position i...
1. An airplane comprising a fuselage and at least one wing fixed to the fuselage between a forward end of said fuselage and a rear end of said fuselage, the fuselage comprising a longitudinal axis directed in a direction X and an exterior surface determining an envelope shape determining geometries of cross sections perpendicular to the longitudinal axis in successive positions offset along the longitudinal axis, each cross section having a maximum width l in a direction Y in a horizontal plane of an aircraft reference system and a maximum height h in a ...