|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-041/00 B64D-037/02 B64D-037/04 B64C-001/00 B64C-001/22|
|미국특허분류(USC)||244/058; 244/120; 244/119; 244/117R; 244/135R|
|우선권정보||FR-09 02941 (2009-06-17)|
|§371/§102 date||20111121 (20111121)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 6|
According to the invention, a rear portion of a fuselage of an aircraft contains a fuel cell system, and the aircraft further includes a rear cone which is removably mounted relative to the rear portion of the fuselage so as to form an extension thereof. The rear cone is shaped as a fuel tank for the fuel cell system contained in the rear portion of the fuselage. The rear cone includes at least one housing extending into the fuel tank and configured to receive at least one projecting slide extending from the rear portion of the fuselage.
1. An aircraft comprising: a fuselage with a rear portion containing a fuel cell system, the rear portion of the fuselage including a rear end side proximate to the fuel cell system, at least one projecting slide extending from the rear end side, and a first fluidic connection organ communicating with the fuel cell system and located at the rear end side; anda rear cone removably mounted relative to the rear portion of the fuselage so as to form an extension thereof, the rear cone shaped as a fuel tank defining a volume to be filled with fuel for the fue...