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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-039/02 B64D-037/04 B64D-037/06 B64C-039/08|
|미국특허분류(USC)||244/135A ; 244/136 ; 244/45 ; R|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 12|
A refueling system mounted to an aircraft fuselage for transferring fuel from a tanker aircraft to a receiver aircraft. The refueling system including a pylon extending from the fuselage at a position aft of the main wing and having a refueling pod mounted thereto at an outboard location. A refueling hose is disposed within and extendable from the refueling pod and functions to transfer fuel from the refueling pod to the receiver aircraft. A means for transferring fuel from a fuel source, located within the aircraft, to the refueling hose is also provide...
A refueling system for an aircraft, the aircraft having a fuselage, a main wing extending from opposite sides of the fuselage, a stabilizer extending from opposite sides of the fuselage aft of the main wing, and a fuel source disposed within the aircraft, the refueling system comprising: at least one pylon extending from a side of the fuselage at a position aft of the main wing and forward of the stabilizer; said pylon having a refueling pod mounted thereon outboard of the fuselage; a refueling hose disposed within and extendable from the at least one po...