|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/34 B64D-037/04 B64D-037/28|
|미국특허분류(USC)||244/135R ; 137/263 ; 137/571 ; 60/734|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 31 인용 특허 : 1|
A high wing Canard aircraft mounts three strake fuel tanks within the top of the aircraft fuselage on the right and left sides thereof in a fore and aft array interconnected by horizontal interconnect lines at the bottoms of the strake tanks to provide an alternate fuel path in the event of tank-line contamination blockage and forming a secondary gravity feed system. A pair of wing tanks integrated to the high wing of the Canard aircraft, to the rear of the strake tanks, feed along with individual horizontal fuel lines from the strake tanks to a central ...
A gravity feed fuel system for a high wing Canard aircraft including: an elongated fuselage, a high, main wing mounted to the top of said fuselage and having right and left wing sections projecting outwardly thereof to opposite sides of said fuselage, said fuel system comprising: a plurality of fore and aft, spaced strake fuel tanks mounted within the top of said fuselage forward of said main wing at a common level, a wing tank within each main wing section at said common level, a common, central collector tank mounted between said wing tanks, in alignme...