| Entries |
| Document | Title | Date |
|---|
| 20090026309 | 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 aircraft, the fuselage of the aircraft having recesses for receiving the propulsion units which are arranged such that the first and the second propulsion unit are arranged above one another in the plane set by the longitudinal and vertical axis of the aircraft. The propulsion unit comprises an engine, a housing having an air inlet, devices for the releasable fastening of the propulsion unit to the fuselage of the aircraft as well as devices for establishing a releasable connection of electric supply and data lines as well as fuel lines between the propulsion unit and the fuselage of an aircraft. | 01-29-2009 |
| 20090127383 | 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 proton accelerator, plasma guns, diversion devices. Said craft will approach the speed of light. Said craft obtains fuel direct from an atmosphere or a radiation produced atmosphere in space, at no cost. This craft can travel to a g k star for only the cost of construction of craft. This invention is comparable to the discovery of fire insofar as man's future is concerned, particularly in view of our climate change, and a recent near impact from an asteroid—which would have put us within an ice age. The craft has three on-board escape craft. The craft is capable of producing plasma vortices within an electromagnetic field approaching the speed of light. Said field is an inhomogeneous, diamagnetic, orbiting plasma field with a magnetohydrodynamic electrically conducting plasma current. Said craft possesses approximately seven uninsulated tungsten bands encircling craft. Said bands are comprised of tungsten wire wrapped to form cables. | 05-21-2009 |
| 20090294582 | 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 vertical plane of symmetry of the lifting gas body and thus, the lifting gas body itself, are pivoted in an area of bending zones about angles a and β. An activated state exists when the actuator performs work for propelling the aircraft. Propulsion can be provided by deformation of the lifting gas body. Changes in direction can also be effected by asymmetrical sequences of movements. | 12-03-2009 |
| 20100059624 | 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 engine support pylon. At least one profiled bearing rod is positioned on each of the engine support pylons so as to generate a propulsive resultant force under action of an oblique air flow. | 03-11-2010 |
| 20100090057 | Conveyance - An apparatus which exhibits properties allowing it to levitate and travel utilizing magnetic energy. | 04-15-2010 |
| 20100147998 | 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 sun gear rotatable by a rotary input, a plurality of planet gears in meshed engagement with the sun gear, a carrier coupling the plurality of planet gears together, and a ring gear encircling and in meshed engagement with the plurality of planet gears. The exemplary apparatus also includes a first shaft member coupled to the carrier for transmitting motion in a first rotational direction. The exemplary apparatus also includes a second shaft member coupled to the ring gear for transmitting motion in a second rotational direction opposite the first rotational direction. The first shaft member at least partially encircles the second shaft member. | 06-17-2010 |
| 20100206982 | 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 unit which drives an inner blade row in counter rotational motion to the outer blade row. The counter rotation transmission unit exchanges power from the engine core with the shaft. An actuator engages the shaft for translation from a first retracted position to a second extended position. | 08-19-2010 |
| 20100243796 | 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 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. | 09-30-2010 |
| 20100294881 | 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. | 11-25-2010 |
| 20130020433 | REDUCED FLOW FIELD VELOCITY FOR A PROPULSOR - A system and methods for reducing flow field velocity into a propeller is disclosed. An aerodynamic structure is enhanced to provide a reduced velocity flow field region, and a propeller is positioned in the reduced velocity flow field region. | 01-24-2013 |
| 20140061376 | Reconfigurable battery-operated vehicle system - A quadrotor UAV including ruggedized, integral-battery, load-bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module, and skids configured as landing gear. The two arms are replaceable with arms having wheels for ground vehicle use, with arms having floats and props for water-surface use, and with arms having pitch-controlled props for underwater use. The control module is configured to operate as an unmanned aerial vehicle, an unmanned ground vehicle, an unmanned (water) surface vehicle, and an unmanned underwater vehicle, depending on the type of arms that are attached. | 03-06-2014 |
| 20140367510 | Aircraft with electric propulsion means - An aircraft with an electric propulsion arrangement which includes a fuselage, a wing system attached to the fuselage, and a tail unit attached to a rear part of the fuselage. The electric propulsion arrangement is arranged on each side of the fuselage, an electrical energy generator and electricity storage and supply devices are arranged substantially along a longitudinal axis of symmetry of the fuselage. The aircraft thus incorporates a hybrid motorization. | 12-18-2014 |
| 20150354672 | AIRCRAFT AND PLANETARY GEAR SYSTEMS - Planetary gear systems, transmissions, and apparatuses include a plurality of compound planet gears, each having three gear stages, a first non-fixed annular gear, a second non-fixed annular gear, a fixed annular gear, and a non-fixed sun gear. A rotational input to the non-fixed sun gear results in opposite rotational outputs of the first non-fixed annular gear and the second non-fixed annular gear. Compound planet gears and carriers for planetary gear systems are also disclosed. | 12-10-2015 |
| 20160121673 | UNMANNED AERIAL VEHICLE - Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles may have various configurations related to payload clamps. | 05-05-2016 |
