| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | Saucer shaped gyroscopically stabilized vertical take-off and landing aircraft | US12387770 | 2009-05-07 | US07971823B2 | 2011-07-05 | 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. | ||||||
| 142 | Integral powered wing aircraft | US12501971 | 2009-07-13 | US07950603B2 | 2011-05-31 | Waldemar F. Kissel, Jr. |
| Disclosed is a rotary winged aircraft. More specifically, this invention relates to an aircraft wherein lift is generated by two discs which rotate about a central axis. The discs generate equal and opposite forces such that the central axis remains fixed, thereby allowing it to be used for a crew compartment. In one embodiment, the two discs are concentrically located. | ||||||
| 143 | Homeostatic flying hovercraft | US11838040 | 2007-08-13 | US07931239B2 | 2011-04-26 | Brad Pedersen; Peter Spirov |
| A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control. | ||||||
| 144 | AIRCRAFT GENERATING A LIFT FROM AN INTERIOR THEREOF | US12699066 | 2010-02-03 | US20110001000A1 | 2011-01-06 | Xiaoyi Zhu |
| The invention discloses an aircraft generating a larger lift from its interior. The fluid channel inside the aircraft communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the aircraft. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the aircraft, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing aircraft. The unified big wing significantly improves the lift, the speed and the carrying capacity of the existing aircraft with lowered energy consumption. | ||||||
| 145 | RING WING-TYPE ACTINIC FLUID DRIVE | US12745744 | 2008-12-02 | US20100310357A1 | 2010-12-09 | Nikolaos Papageorgiou |
| Disclosed is an actinic (radial) fluid drive (AF) which can replace any propeller used, e.g. for fans, ventilators, pumps, hydraulic power plants and wind power plants (repeller), watercraft and aircraft (boats, helicopters, etc.) and can also reduce form drag (in tips of rockets, etc.) or wave-making resistance (in bulbous bows of ships, etc.). Said actinic (radial) fluid edge and trailing edge of which (corresponding to the drive (AF) is at least characterized by: a) a ring wing (11) (annular wing)—like a truncated cone—, the leading periphery of the top surface and base of a truncated cone) determine the chord of the ring wing (11) (rectilinear length of the side), said chord forming the angle of inclination (φ) of the ring wing along with the plane of the top surface; and b) an actinic main flow (15), the direction (plane) of which forms the angle of attack (θ) along with the chord on the leading edge of the ring wing (11), said angle of attack (θ) being greater than 0° and smaller than 90°, especially greater than 8°, and the actinic main flow (15) is inclined (thrust is generated) analogous to the angle of attack (θ) (as a result of the Coanda effect). | ||||||
| 146 | Plasma gun system utilizing an aerospace craft | US12661572 | 2010-03-19 | US20100243796A1 | 2010-09-30 | Gary Richard Gochnour |
| This invention relates to a plasma gun utilized in a plasma based aircraft maintained in a flight mode by rotating plasma vortices located above and beneath said aircraft. Plasma produced by aircraft is utilized by said plasma gun to facilitate initial take off of craft, and also to accelerate aircraft speed, or, within an emergency, as needed.Said aircraft can also eject plasma through aircraft central shaft or within any direction from sides of said craft, for escape, evasion or normal accelerated flight.Preferred embodiment for said plasma gun, is a coaxial plasma gun, utilizing the large capacitance potential of aircraft, the large supply of aircraft produced plasma off said capacitors, or from uninsulated conducting wires, and also utilizing the strong Lorentz force existing within craft.The plasma produced by ionization within craft strong magnetic field, will enable this craft to rapidly avoid impediments to flight, or oncoming dangers. | ||||||
| 147 | STABILIZING POWER SOURCE FOR A VEHICLE | US12688583 | 2010-01-15 | US20100116924A1 | 2010-05-13 | William Allen Bastian, II; Elizabeth Sobota |
| A power source for a vehicle includes at least one toroidal ring positioned in a housing. The toroidal ring includes magnetic material such as permanent magnets. The toroidal ring is magnetically levitated in the housing. A propulsion winding is coupled with the housing and energizable via a power signal to move the toroidal ring. Once moving, the magnetic material and the propulsion winding cooperate to produce electrical power and/or provide a stabilizing effect for the vehicle. In some applications, such as in an aircraft application, two or more toroidal rings may be used and rotated at counter directions so as to produce a predetermined net angular momentum. | ||||||
| 148 | Integral powered wing aircraft | US11521597 | 2006-09-14 | US07559506B2 | 2009-07-14 | Waldemar F. Kissel, Jr. |
| Disclosed is a rotary winged aircraft. More specifically, this invention relates to an aircraft wherein lift is generated by two discs which rotate about a central axis. The discs generate equal and opposite forces such that the central axis remains fixed, thereby allowing it to be used for a crew compartment. In one embodiment, the two discs are concentrically located. | ||||||
| 149 | INTEGRAL POWERED WING AIRCRAFT | US11521597 | 2006-09-14 | US20090145997A1 | 2009-06-11 | Waldemar F. Kissel, JR. |
| Disclosed is a rotary winged aircraft. More specifically, this invention relates to an aircraft wherein lift is generated by two discs which rotate about a central axis. The discs generate equal and opposite forces such that the central axis remains fixed, thereby allowing it to be used for a crew compartment. In one embodiment, the two discs are concentrically located. | ||||||
| 150 | Flying saucer | US11484553 | 2006-07-12 | US20080011898A1 | 2008-01-17 | Richard Wilton White |
| Multiple engines (with individual propellers), mounted upon a platform, with swivel mounts ganged together to a single control stick, to direct their propelled energy downward, giving said platform precise control. Said platform supported via three spring landing struts. | ||||||
| 151 | Hydrogen-fueled spacecraft | US11049150 | 2005-02-02 | US07108228B1 | 2006-09-19 | Manfred Marshall |
| A spacecraft having facilities for carrying astronauts and payloads into the earth satellite orbit and space having a composite fiber body with a Kevlar exterior skin. Said craft having a substantially round shape with a portion covered with solar cells. Said solar cells powering electrical motors and a plurality of rockets using a quantity of hydrogen fuel. | ||||||
| 152 | Craft with magnetically curved space | US10812018 | 2004-03-30 | US20050230525A1 | 2005-10-20 | Von Paterro |
| A craft can navigate through a magnetically curved space provided by an electromagnetically charged hull. The hull contains a plurality of sectionalized and independent electromagnetic plates forming portions of the hull exterior wall that can be adaptively energized to have a desired polarity. When combined together, these sectionalized plates can provide an ultra high frequency electromagnetic field of a strength that can magnetically curve the space around the craft. This enables the craft to expeditiously travel through air, space or water. A novel energy generating system using a combination of jet engines and high frequency oscillators is also provided. | ||||||
| 153 | Aerial vehicle controlled and propelled by oscillatory momentum generators and method of flying a vehicle | US10164416 | 2002-06-10 | US06751530B2 | 2004-06-15 | Avraham Seifert; David Greenblatt; Israel Wygnanski |
| A vehicle capable of flight including at least one wing including at least one oscillatory momentum generator mounted therein. A thrust force from the oscillatory momentum generator is directed outwards over the wing causing a lift-generating air flow over a wing surface. A method of flying a vehicle including providing at least one wing having at least one oscillatory momentum generator mounted therein and applying a thrust force from the generator which is directed outwards over the wing and directed to the trailing edge so that a lift generating air flow is created. | ||||||
| 154 | Power generation system | US10231703 | 2002-08-30 | US06672539B1 | 2004-01-06 | Stephen L. Schoeneck |
| A power generation system comprises an internal housing. The housing has a top portion, a bottom portion and a peripheral sidewall. An external housing is provided. The housing is coupled to and receives the internal housing. The housing has an upper lip, a lower lip and a smooth outer edge. The upper lip is spaced from the internal housing to allow the flow of air into the external housing. A rotary pump is comprised of an upper washer and a lower washer. Fins are provided between the washers. The washers form upper and lower surfaces. Fins are coupled to both the upper and lower washers. Each fin is curved such that when rotated the rotary pump draws air into the external housing from the upper lip and pushes it past the lower lip and out of the external housing to life the system. | ||||||
| 155 | Aerial vehicle controlled and propelled by oscillatory momentum generators and method of flying a vehicle | US10164416 | 2002-06-10 | US20030229428A1 | 2003-12-11 | Avraham Seifert; David Greenblatt; Israel Wygnanski |
| An aerial vehicle controlled and propelled by oscillatory momentum generators and method of flying a vehicle. A vehicle capable of flight is disclosed. The vehicle includes at least one wing including at least one oscillatory momentum generator mounted therein. A thrust force from the oscillatory momentum generator is directed outwards over the wing causing a lift-generating air flow over a surface of the at least one wing. Further disclosed is a method of flying a vehicle including providing at least one wing having at least one oscillatory momentum generator mounted therein and applying a thrust force from generator which is directed outwards over the wing so that a lift generating air flow is created. | ||||||
| 156 | Flying object with a rotational effect | US10354059 | 2003-01-29 | US20030155469A1 | 2003-08-21 | Srecko Ugrin |
| A flying object with a rotational effect including a base, eight wheels suitable for starting and landing the flying object, a platform, a cover, a bearing frame for shaft, an engine for rotation, a jet engine for starting, flying and landing the flying object, and an outlet of the jet engine. | ||||||
| 157 | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel | US10089908 | 2002-04-05 | US20020153449A1 | 2002-10-24 | Nikolaos C Hatzistelios |
| This invention called airwheel, concerns of a flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel. If we exercise a force from a fixed point on the edge of a turning wheel (fixed related to the main body of the vehicle) and the direction of the force is opposite to the direction of the linear speed of the edge, then we will simulate the friction force between the turning wheel of a car and the road which forces the rolling of the car wheel and not just the revolving of it. The airwheel uses to roll (fly) a wheel named in the invention rolling wheel (b) and it embraces the main body (a) of the airwheel as well as an other wheel (Angular Momentum Maintenance Wheel (c)) which turns the other way around to maintain the angular momentum. The airwheel uses nozzles (k) to manoeuvre. Airwheel ingests atmospheric air to fly and avoids/standsup against air pockets using gas saved in a cylindric tank in it which diverts gas under great pressure to the nozzles. For the interplanetary flight airwheel uses the magnetic fields of the magnetosphere, magnetotail and the magnetic fields of solar wind. It comprises T-shaped telescopic devices which on the upper side of the nullTnull contain couples of superconductor bobbins. | ||||||
| 158 | Flight vehicle having internal lift surfaces | US09781094 | 2001-02-12 | US20020109043A1 | 2002-08-15 | Tianfu Li |
| A vehicle capable of roadway travel and flight, both in an atmosphere and in a vacuum, includes a fluid passageway, a device for producing fluid flow in the passageway, and airfoil surfaces spaced mutually along the passageway and fixed to the structure of the vehicle, to which structure lift forces produced on the airfoils are transferred. The vehicle includes lift-producing wings extending from the body of the vehicle, the fluid passageway being located within the vehicle body or the external wings. Fluid flow within the passageway is produced by a fan, propeller, or exhaust from a jet engine. | ||||||
| 159 | Electrodynamic field generator | US09621152 | 2000-07-21 | US06404089B1 | 2002-06-11 | Mark R. Tomion |
| This device is a brushless high-voltage electrical generator, requiring suitable means of input rotary torque, for purposes of producing a very-high-energy external electrodynamic field or continuous quasi-coherent DC corona or arc discharge of uniform current density which completely encloses the machine's conductive housing. This housing is divided into distinct electrical sections and contains a flat conductive rotor which electrically links separate negative and positive housing sections and upon which a plurality of toroidal generating coils are rotatably mounted. Circular arrays of stationary permanent magnets are affixed within the housing which induce a constant DC voltage within said coils upon their rotation. The primary voltage so-generated is electrostatically impressed across the rotor such that great quantities of electronic charge may be transported between the opposite polarity sections of the housing, in such a manner that a much higher secondary voltage is caused to appear across interposed neutral sections thereof, and the resulting external breakdown current once initiated is independent of the generating coils' ampacity. Ancillary mechanical, electrical, an/or electronic features may be attached upon or within the housing to aid in harnessing and controlling the useful effects associated with the external dynamic electric field produced by the device. | ||||||
| 160 | High speed vertical take-off and land aircraft | US09655966 | 2000-09-06 | US06382560B1 | 2002-05-07 | Gordon Y. W. Ow |
| A high-speed vertical take-off and land (HSVTOL) aircraft includes a disk-shaped fuselage wit a rotatable fan having a nozzle ring driven by hot jet gasses and fan air from jet engines. Feed ducts and an annular plenum, have a composite duct-in-duct configuration to separate the hot gases from the relatively cool fan air. High efficiency air bearings serve to support the rotatable fan assembly on the fuselage in the vertical direction, and rollers around the perimeter provide horizontal support and stability. A bearing and seal interface hub and other components, are isolated from the hot gases. The combined exhaust is ejected downwardly at approximately 15° for maximum fan spin and provide direct reaction lift. The fan blades are angled at approximately 57° with moveable airfoil portions and stationary trailing flap portions to provide maximum lift and down wash. Various diverter valves and bypass doors are provided for hot gas/air control. Decoupler valves can interrupt all flow for engine out operation. Control of the pitch, roll and yaw is provided by aero flaps providing control surfaces in the path of the down wash. When twisted about a substantially horizontal control axis, the flaps generate lift, as well as being modulated for attitude control. Aerodynamic disk-shape of the fuselage provides high lift, low drag necessary to support the efficient high speed performance. A control circuit includes an on board CPU controller that operates and coordinates all functions through the various actuators, valves, transducers and other control components. | ||||||
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