|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||180/122 ; 180/117 ; 180/120 ; 180/129|
|발명자 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 8|
A craft for ground effect and aerodynamic flight has, in addition to the usual vertical and horizontal stabilizer(s), a primary, upper airfoil, a lower secondary airfoil and a pivotable flap. The upper surface of the primary airfoil forms the primary lifting surface for aerodynamic flight while the lower surface forms, at its anterior and, an air intake for the compressors powering the craft and, to the rear, the upper surface of a plenum for ground effect flight. The upper surface of the secondary airfoil forms the lower surface of the compressor air in...
A craft for hovercraft mode operation and aerodynamic flight including a control mechanism comprising, when the craft is in substantially the horizontal plane: at least one fuselage; vertical and horizontal stabilizer means; connected to each of the at least one fuselage for controlling the flight of the craft; at least one compressor means for providing propulsion and lift to the craft; at least one each of primary airfoil means, secondary airfoil means, air intake and anterior flap means; the at least one primary airfoil means, having an upper surface ...