|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/013; 244/055; 244/054|
|우선권정보||FR-09 51561 (2009-03-12)|
|§371/§102 date||20120207 (20120207)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 5|
An airplane, including a fuselage having an elongate shape along a longitudinal axis of the airplane, and at least one wing attached to the fuselage between front and back ends of the fuselage and a substantially cylindrical central portion and a rear scaleable portion on which a vertical tail assembly and a rear propulsion assembly are attached. Between a section for connecting the rear portion to the central portion of the fuselage and the back end: the maximum width of each fuselage section is constant or increases towards the rear up to a maximum fus...
1. An airplane comprising: a fuselage including at least one wing attached to the fuselage between a front end and a rear end of the fuselage, the fuselage having a substantially cylindrical central part and a tapered rear part joined to the central part at a connecting section, onto which a vertical tail assembly is attached and onto which a rear propulsive assembly is attached substantially at a vertical symmetry plane of the fuselage,wherein, in the tapered rear part:a maximum height of each section of the fuselage decreases toward a rear of the airpl...