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序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
81	Aerodynamic vehicle having a variable geometry, co-planar, joined wing	US10801750	2004-03-16	US07249734B2	2007-07-31	Rudolph N. Yurkovich
An aerodynamic vehicle is comprised of a pair of forward wing sections and a pair of rearward wing sections that are connected together by four pivot assemblies as a four-bar linkage. The four-bar linkage surrounds an opening provided between the forward wing sections and rearward wing sections. Movement of the wing sections varies the cumulative area of the wing sections, and adjusts the shape of the opening between the forward wing sections and rearward wing sections. Movement of the wing sections improves the aerodynamic performance of the vehicle and allows the wing sections to assume optimum configurations for operation of the vehicle at high speed and low speed.
82	Circular vertical take off and landing aircraft	US10084749	2002-02-26	US06698685B2	2004-03-02	Eric Ronald Walmsley
A circular VTOL aircraft with a central vertically mounted jet or rocket engine 7, (or engines) having below vertical thrust vents 14 at cardinal points, together with a jet/rocket engine 20 (or engines) horizontally mounted on turntable pod 16 which is steerable through 360 degrees and centrally situated below the vertical engine (s). Alternatively the horizontal engine can be replaced by central thrust vent 36 delivering thrust from the vertical engine to vectored thrust nozzle 37 attached to the turntable. Thrust from the four vertical thrust vents is controlled by valves 21 giving VTOL thrust control as well as pitch and bank control. The horizontal engine provides acceleration and retro-thrust for horizontal flight and directional control through 360 degrees. The passenger cabin is situated in the main body of the aircraft. Fuel tanks are installed around the central engines. The flight-deck is situated at the top-centre of the craft above the engines, which are detachable for maintenance.
83	Circular vertical take off & landing aircraft	US10084749	2002-02-26	US20030127559A1	2003-07-10	Eric Ronald Walmsley
A circular VTOL aircraft with a central vertically mounted jet or rocket engine 7, (or engines) having below vertical thrust vents 14 at cardinal points, together with a jet rocket engine 20 (or engines) horizontally mounted on turntable pod 16 which is steerable through 360 degrees and centrally situated below the vertical engine (s). Alternatively the horizontal engine can be replaced by central thrust vent 36 delivering thrust from the vertical engine to vectored thrust nozzle 37 attached to the turntable. Thrust from the four vertical thrust vents is controlled by valves 21 giving VTOL thrust control as well as pitch and bank control. The horizontal engine provides acceleration and retro-thrust for horizontal flight and directional control through 360 degrees. The passenger cabin is situated in the main body of the aircraft. Fuel tanks are installed around the central engines. The flight-deck is situated at the top-centre of the craft above the engines, which are detachable for maintenance.
84	Circular vertical take off & landing aircraft	US09967840	2001-10-01	US06581872B2	2003-06-24	Eric Ronald Walmsley
A circular VTOL aircraft with a central vertically mounted turboprop engine (14), driving contra-rotating co-axial propellers (24), above a central jet engine, or engines (12), horizontally mounted on a turntable pod (11) which is steerable through 360 degrees. The turboprop provides vertical thrust from contra-rotating propellers compressing air from an upper circular intake (5) downward through a funnel-shaped rotor-chamber (6) to a circular vent (10) at the base of the craft. The resulting column of compressed air supports the craft during take-off, hover and landing operations and provides a cushion of air in normal flight. The horizontally mounted jet turbine provides main thrust for horizontal flight and vectored thrust for VTOL. The passenger cabin (21) is circular and is situated in the main body of the disc-shaped craft. Fuel tanks are situated around the circumference of the craft to maximise fuel capacity. The flight-deck (2) is situated at the top center of the craft, above the engine unit (15), which is detachable.
85	Arial disk	US09834126	2001-04-12	US06398159B1	2002-06-04	Alfonso Di Stefano
An aircraft comprising a body and a plurality of disks rotatably coupled to the body. The disks may be configured to (i) rotate in the same or different directions, (ii) rotate at similar and/or different speeds, and (iii) provide lift and/or stability to flight of the aircraft.
86	Device for generating an aerodynamic force by rotational movement	US09509688	2000-06-16	US06318962B1	2001-11-20	Eduardo Bittencourt Sampaio
A generator of aerodynamic force by rotational movement, by means of a device which, starting from a rotational movement, induces a field of velocities in the surrounding fluid, which produces a difference in pressure on a surface, which in turn results in an aerodynamic force. The rotor element (1) is set in rotation at high speed by a motor (3). The rotational movement of the rotor element causes the fluid in which the device is immersed to assume a rotational movement, the velocity of the fluid layer that is in contact with the cylinder being equal to the velocity of a point at the surface of the cylinder. The planar element (2) separates the fluid into two regions. The fluid in the region below the surface is motionless, whereas the fluid above the surface is in motion. Since the higher the velocity of the fluid the lower its pressure, the fluid in the region below the surface exerts a higher pressure than that exerted by the fluid in the region below the surface. This difference in pressure results in a force that acts on the surface.
87	Aircraft	US68067	1998-04-28	US5996933A	1999-12-07	Johannes Schier
For an aircraft (1) having a balancing torque and including a motor-driven propeller (5) arranged on a central axis (3), and a useful load container (6), a solution should be provided which would insure that the aircraft is capable of carrying useful loads in a stable flying attitude and with simple control means.This is achieved by that the central propeller (5) driven by the drive motor (4), on one hand, and relative thereto, the motor (4) and/or torque-balancing means arranged thereon, on the other hand, are rotatable in opposite directions and together are supported for rotation relative to the useful load container.At that, the drawing figure to be published: FIG. 1.
88	Aircraft with a ducted fan in a circular wing	US9246	1993-01-26	US5303879A	1994-04-19	Franz Bucher
The aircraft comprises a rotor with a vertical axis arranged in a housing for generating a lift exceeding the weight of the aircraft. The housing is essentially shaped as a circular wing. A first way of guiding air is provided for controlling the air stream generated by the rotor, by means of which the position of the aircraft can be controlled in hovering flight. From hovering flight, the aircraft can be moved into a cruise flight, where the lift of the aircraft is generated aerodynamically by the circular wing of the housing and its forward thrust by a propeller. For the transition between hovering flight and cruise flight, a second way of guiding air is provided for controlling the pitch of the aircraft. The structure for the second way of guiding air is arranged outside a zone defined by the air stream of the rotor.
89	Method and means for generating a force	US520638	1990-05-08	US5155992A	1992-10-20	Robert E. Follensbee; Guy D. Riva
A method and means for generating a force. A flared body is enclosed in a shroud to form one or more ducts of axially diminishing cross-section for accelerating and directing the discharge of a fluid introduced into the ducts under pressure. A cambered vane is positioned at the exit of each duct, in the path of the accelerated fluid discharge. Fluid passing over and under each vane produces a force aligned axially with the body and in the direction of flow of the fluid in the associated duct. In a preferred embodiment a conically-shaped body and surrounding shroud form an annular duct for air delivered to the mouth of the duct by a compressor. The vane is an annular airfoil.
90	Circular airplane	US332489	1989-04-03	US5054713A	1991-10-08	Lawrence W. Langley; Hal L. Moses
The invention is a circular airplane with an oblately spheroidal body which derives lift from a wall or ribbon jet exhausting over its upper surface. The jet is produced by a mixed flow fan driven by an internal combustion or gas turbine engine within the body. A fixed guide van assembly removes the swirl from the outlet flow of the mixed flow fan. The jet exiting from the fixed guide vane assembly follows the curved surface of the body, exhausting downward, and produces lift. The magnitude of lift produced in each quadrant of the airplane may be reduced for thrust vectoring by flow control gates which partially block the flow of air from the fixed guide vane assembly. Rotation control vanes introduce a controlled swirl into the flow of air from the fixed guide vane assembly to effect rotation of the airplane. Actuators for flow control gates and rotation control vanes, and a flight control system, are provided.
91	Aircraft with counterrotating members	US956005	1978-10-30	US4273302A	1981-06-16	Heinz Jordan
A rotationally symmetrical supporting member provides lift in response to movement of air over its upper surface, and such air movement is produced by the impeller of a coaxially arranged drive unit, the base of which is connected to the supporting member so that counter torque from the drive unit imparts rotational movement to the supporting member. A carrier which may hold a load or supporting steering flaps is rotatably mounted in relation to the supporting means and to the driving unit.
92	Inverted cone aircraft	US947068	1978-09-29	US4215832A	1980-08-05	George L. Horn
An aircraft is disclosed which includes a body having the shape of an inverted cone with a downwardly extending rim formed about the edge thereof and a triangularly shaped tail section. The aircraft can be constructed as a glider or a powered device and several alternative tail sections are shown such as square, radii, circle and tangent.
93	Remotely piloted vehicle	US876576	1978-02-10	US4120468A	1978-10-17	Hans-Otto Fischer
The vehicle is constructed from a flat disc recessed in a slot in a thin, pencil-like fuselage having aft and front propulsion engines and mounted for rotating about the center of the disc and about an axis extending transversely to the disc and to the direction of extension of the fuselage.
94	Vertical take off and landing aircraft	US666467	1976-03-12	US4049218A	1977-09-20	Lian-Tong Wen
A method and apparatus to improve the performance of a Vertical Take Off and Landing (VTOL) aircraft having increased safety, efficiency and maneuverability is described. The utilization of an airbooster to achieve optimum air speed of jetted air, have made the increase in its efficiency feasible. A concealed rotor eliminates the great hazard of most VTOL.
95	Circular wing aircraft	US39419573	1973-09-04	US3871602A	1975-03-18	KISSINGER CURTIS D
An improved circular wing aircraft in which the main airfoil is of generally circular shape having a pair of vertical stabilizers running along chords of the circle and equally spaced from the longitudinal axis of the craft from points just ahead of the leading edge of the craft to points behind the trailing edge thereof in which a cut-out portion of the airfoil is displaced rearwardly and held in an elevated position by the vertical stabilizers so as to form a space in which a pushed prime mover is located. The central portion of the wing between the vertical stabilizers is provided with an undercamber.
96	Air-ground vehicle	US3489374D	1968-03-25	US3489374A	1970-01-13	MORCOM PAUL J

97	Circular wing structure	US51660465	1965-12-27	US3355124A	1967-11-28	KELSEY CADWALLADER W

98	Aircraft having wing with arcuate shaped trailing edge	US61795156	1956-10-24	US3129905A	1964-04-21	TAYLOR BRUCE G

99	Supersonic aircraft	US66936957	1957-07-01	US3066890A	1962-12-04	PRICE NATHAN C

100	Disc-type aircraft with peripheral jet control	US68880457	1957-10-01	US3022963A	1962-02-27	MEADOWS FROST JOHN CARVER; DESMOND EARL THOMAS

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