|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/54 B64C-011/46 B64C-025/52 B64C-035/00|
|미국특허분류(USC)||244/101 ; 244/45 ; R ; 244/46 ; 244/218|
|발명자 / 주소|
|인용정보||피인용 횟수 : 30 인용 특허 : 0|
Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) with a belt drive system for turning wing-situated propellers; compound landing gear integrating ski, pontoon and wheel subcomponents; pivotal mounting armatures for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure featuring extendable wing panels that permit the wing span of the aircraft to be nearly doubled while in flight. A...
A multi-purpose aircraft comprising (a) a fuselage having a generally cylindrical structure defining a forward end to an aft end, the fuselage being closed at the forward end by a nose section and closed at the aft end by a tail section, said fuselage further having a hull-shaped underside having forward and aft landing gear openings, said fuselage further having a port lateral recess and a starboard lateral recess; (b) a compound aircraft wing attached to said fuselage comprising (1) a fixed wing section comprising a bilaterally symmetrical aircraft win...