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US20100294881 |
Electrolysis system
The invention relates to an electrolysis system. Said system can be utilized in a nuclear fusion process, on roof of a ferromagnetic aircraft in preferred embodiment. Said electrolysis system will...
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US20120018571 |
SYSTEM AND METHOD FOR SOLAR-POWERED AIRSHIP
A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The...
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US20060108471 |
Method and system for maintenance, in particular disassembly, of gas turbines
A system and method for maintenance, in particular disassembly, of gas turbines, in particular aircraft engines, wherein a gas turbine is introduced, before being disassembled, into a first...
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US20060071122 |
Full body teleportation system
A pulsed gravitational wave wormhole generator system that teleports a human being through hyperspace from one location to another.
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US20070102572 |
Method for making gas turbine elements and corresponding element
A vane segment and a method is provided for manufacturing elements, namely gas turbine vane segments, in particular for an aircraft power train. Each vane segment comprises at least two vanes, one...
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US20100090057 |
Conveyance
An apparatus which exhibits properties allowing it to levitate and travel utilizing magnetic energy.
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US20090294582 |
Propulsion Unit for Lighter-Than-Air Aircraft
A lighter-than-air aircraft is propelled via a bending-rotating tail whip. Two actuating areas located on opposite sides in a rear area of a lifting gas body are shortened by activated actuators. A...
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US20060144994 |
Homeostatic flying hovercraft
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...
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US20090127383 |
Tubular shaped interstellar space craft
The invention relates to a plasma based aircraft possessing a magnetic field, and, a huge plasma vortex. Said craft is tubular in shape. Said craft has a vast array of capacitors. The craft has a...
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US20070181743 |
Method for streamline traced external compression inlet
Embodiments of the present invention provide a Streamline Traced External Compression Inlet (STECI) that represents a new solution to external compression inlet integration issues. STECI utilizes a...
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US20090072084 |
LIGHTER-THAN-AIR VEHICLES
The present invention describes lighter-than-air vehicles. An exemplary embodiment of the present invention provides a lighter-than-air vehicle having a payload module, the payload module including...
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US20050077425 |
Thruster for propelling and directing a vehicle without interacting with environment and method for making the same
A thruster for propelling and directing a vehicle without interacting with its environment without using propellant and particularly adapted for use in space, comprising rotating means having a...
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US20100001143 |
Discoidal flying craft
A flying craft has an aerodynamic aircraft fuselage structure preferably disc shaped. A pair of coaxial electrokinetic motor-generators are mounted concentrically, and preferably centered within...
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US20100176248 |
SPACECRAFT PROPULSION SYSTEM WITH GYROSCOPIC MECHANISM
A propulsion method employing gyroscopes (1,2) with electric motors (4) which are being moved along a closed path in the spacecraft. Rotation axis of the gyroscopes are rotated periodically...
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US20050017127 |
Mobile object with force generators
A mobile object being a vehicle of any type includes a plurality of force generators, enclosed in a hermetically sealed generator chamber filled with a pressurized gas, and a plurality of engines....
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US20100243796 |
Plasma gun system utilizing an aerospace craft
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...
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US20100206982 |
COUNTER ROTATING FAN DESIGN AND VARIABLE BLADE ROW SPACING OPTIMIZATION FOR LOW ENVIRONMENTAL IMPACT
An air vehicle propulsion system incorporates an engine core with a power shaft to drive an outer blade row. The power shaft is extends through and is supported by a counter rotation transmission...
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US20070114330 |
Method for converting low-grade energy and a fuelless jet engine for its implementation
The invention can be used for converting atmospheric energy and low-grade heat of environmental thermal energy sources, for example water of natural water reservoirs into mechanical work,...
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US20100059624 |
AIRCRAFT COMPRISING A DEVICE FOR REDUCING THE INDUCED DRAG
An aircraft including a longitudinal fuselage, at least two lateral wings connected symmetrically one on each side of the fuselage and at least one engine pod fixed to each lateral wing via an...
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US20090026309 |
Aircraft
The invention relates to an aircraft having a first propulsion unit with an air inlet above the fuselage of the aircraft and a second propulsion unit with an air inlet below the fuselage of the...
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US20100051755 |
TAIL-LESS BOXED BIPLANE AIR VEHICLE
An exemplary embodiment of the present invention sets forth an exemplary bi-plane air vehicle. The air vehicle may include, a plurality of wings coupled to one another in substantially a box...
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US20070295010 |
Method and apparatus to generate thrust by inertial mass variance
A device for producing a net force against a base comprising a mass change object, an accelerator, a power source operatively connected to the mass change object and configured to selectively apply...
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US20050211829 |
Magnetic Motive System
The invention is directed to a motive structure that, in one embodiment, is comprised of a body, a first magnetic field generator, a second magnetic field generator, and a controller for...
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US20100116927 |
Solar cell module
The present invention pertains to a solar cell module comprising at least one photovoltaic element encapsulated between a front layer on its light receiving surface side and a back layer, said...
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US20100147998 |
APPARATUS AND METHOD FOR TRANSMITTING A ROTARY INPUT INTO COUNTER-ROTATING OUTPUTS
An apparatus and method for transmitting a rotary input into counter-rotating outputs is disclosed herein. An exemplary apparatus for performing the method includes a planetary gear set having a...
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