|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/119; 244/102R; 244/118.1|
|우선권정보||FR-08 54459 (2008-07-01)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 5|
An aircraft fuselage with a shape elongated along a longitudinal axis X along a longitudinal axis of the aircraft that determines a direction toward the front along a direction of motion of the aircraft in flight. A front section with straight cross sections widening relative to the X axis, located at the front of the fuselage and ending in the front of the fuselage in a fuselage nose, and delimited at the rear by a cross section for joining to a rear part of the fuselage behind the front section. The front section includes a cockpit located above a floo...
1. An aircraft fuselage elongated along a longitudinal axis of an aircraft that determines a direction toward a front of the aircraft along a direction of motion of the aircraft in flight, comprising: a front part with straight cross sections widening relative to the longitudinal axis,said front part ending in front with a fuselage nose and being delimited at a rear by a joining cross section similar to a cross section of a rear part, essentially cylindrical of the fuselage,said front part comprising a cockpit located above a floorboard between a cockpit...