序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
61 Circular wing aircraft US3572613D 1969-02-17 US3572613A 1971-03-30 PORTER ARTHUR
A hollow, circular housing is open about its periphery and has a central opening in its top. Circumferentially spaced vanes extend between the central opening and the open periphery to direct air flow from the central opening radially outward through the open periphery and across the upper and lower surfaces of an annular airfoil wing secured to the housing. A pair of jet engines at the housing periphery operate to rotate the housing to effect said movement of air.
62 Vertical take-off aircraft with dual gyro guiding system US3531063D 1968-05-16 US3531063A 1970-09-29 PERSEGHETTI JACK A
63 Aircraft US3432120D 1966-05-20 US3432120A 1969-03-11 GUERRERO EFRAIN
64 Aircraft US54825666 1966-05-06 US3410507A 1968-11-12 MOLLER PAUL S
65 Vertical takeoff aircraft US53268166 1966-03-08 US3387801A 1968-06-11 KELSEY CADWALLADER W
66 Means and method of rotor augmented lift for airplanes US50071965 1965-10-22 US3372891A 1968-03-12 MALVESTUTO JR FRANK S
67 Lifting apparatus US36885264 1964-05-20 US3261162A 1966-07-19 HENRI COANDA
68 Circular airfoil aerodynmaic lift mechanism US34183764 1964-01-27 US3181811A 1965-05-04 MAKSIM JR JOHN
69 Disc shaped aircraft US54167455 1955-10-20 US2935275A 1960-05-03 GRAYSON LEONARD W
70 Convertible aircraft with disk shaped airfoil US30378852 1952-08-11 US2711295A 1955-06-21 PETERSON ADOLPHE C
71 Aeroplane US33088529 1929-01-07 US1755828A 1930-04-22 VON KORIES OTTO
72 Airplane US22967627 1927-10-29 US1735308A 1929-11-12 WORRELL PAOLA P
73 Airship US1303999D US1303999A 1919-05-20
74 Flying-machine. US1913750885 1913-02-26 US1076377A 1913-10-21 KITCHEN JOHN GEORGE AULSEBROOK
75 Aeroplane or the like or analogous machine or device. US1909478428 1909-02-17 US1023556A 1912-04-16 EDWARDS ARTHUR HENRY
76 VERTICAL TAKE OFF AND LANDING CLOSED WING AIRCRAFT US15593554 2017-05-12 US20180244381A1 2018-08-30 Carlos Alexander Fenny; Rohn Lee Olson; Andrew James Zahasky
An aircraft capable of vertical takeoff and landing, stationary flight and forward flight includes a closed wing that provides lift whenever the aircraft is in forward flight, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. One or more engines or motors are disposed within or attached to the closed wing, fuselage or spokes. Three or more propellers are proximate to a leading edge of the closed wing or the one or more spokes, distributed along the closed wing or the one or more spokes, and operably connected to the one or more engines or motors. The propellers provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight, and provide thrust whenever the aircraft is in forward flight.
77 FORWARD FOLDING ROTOR BLADES US15593521 2017-05-12 US20180186445A1 2018-07-05 Carlos Alexander Fenny; Rohn Lee Olson; Andrew James Zahasky
A rotor blade rotation system includes two or more rotor blades, each rotor blade in mechanical communication with a hub and pivotable about an axis of rotation, a bearing plate comprising a rotating portion and a non-rotating portion, a fold linkage coupled to the rotating portion of the bearing plate and in mechanical communication with the rotor blade, and an actuator coupled to the non-rotating portion of the bearing plate and operable to reposition the bearing plate from a first position to a second position such that the folding links pivot the rotor blades from a deployed position to a forward folded position.
78 CENTRIPETAL AERODYNAMIC PLATFORM SPACECRAFT US15394880 2016-12-30 US20170190446A1 2017-07-06 LAWRENCE ELLIS WILLIAMS, SR.
An aerodynamic platform or spacecraft including a habitable 1G centripetal force rotating gravity producing interior corridor within an aerodynamic shell and an aerodynamic drone booster launch system with reentry and reuse capability.
79 Disc-shaped turbo-jet aircraft US15166005 2016-05-26 US09550566B2 2017-01-24 John Francis Henning, Jr.
A disc-shaped aircraft including an airfoil having a convex upper surface and a planar lower surface with the edges of the surfaces meeting at the periphery of the disc and having a plurality of rotational mini turbine jets affixed sequentially at the edge of the circumference of the disc, the turbine jets effecting vertical, horizontal, and directional thrust under computer and pilot control. Stable flight is maintained by an internal gyroscopic counter-rotating rotor blade system, individual control of the turbine jets, and a series of retractable flaps.
80 Saucer shaped gyroscopically stabilized vertical take-off and landing aircraft US12387770 2009-05-07 US20100282918A1 2010-11-11 Herbert Martin
An aircraft that is housed within a gyroscope providing for improved flight stability that includes an inner hull which remains stationary within a rotating outer hull. A rotating sine-wave ring is used to activate and move a plurality of pistons which will intake air from above the upper surface of the inner hull configuration and create a negative pressure on the aircraft. The craft contains compression chambers which receive the air and which feed the various impeller thrusters which are rotational within three-fourths of a hemisphere.
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