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Patent Searching and Data


Matches 601 - 650 out of 1,302

Document Document Title
JP4485630B2  
JP2010519456A
Conductive liquid metal or an ionic liquidIt is related with an electric field radiation type electric propulsion thruster, i. e., an electric field effect emitter for colloid thrusters, which has the first rotating parts (110) that form...  
JP2010519448A
RF antenna, an impression magnetic field, plasma, a plasma source that ionizes gas using a coaxial gas closed 込 pipe, and heats plasma, and art about especially as opposed to stationary state generation and heating of an antenna, magne...  
JP2010101300A
To develop a motive power principle needing no reaction of peripheral media, because conventional transport motive power adopting a motive power principle propelled through the reaction received from the peripheral media is based on cond...  
JP2010096186A
To provide a technology of floating by transforming atmospheric pressure into propulsion force.Ultrasonic waves of high intensity are propagated into the atmosphere, and a density structure thereof is regarded as a diffraction grating fl...  
JP3158488U
[Subject] A screw from which a powerful thrust is obtained is provided. [Means for Solution] It sees from the upper part on a large-sized flywheel, a circular U bend ring respectively attached at the U bottom on a large-sized flywheel by...  
JP2010071103A
To provide an ion engine testing device which is improved in vacuum evacuation speed without enlarging the device and responds to higher output of an ion engine or the like.In the ion engine testing device, targets 20-29 formed with inci...  
JP4431779B2  
JP2010053869A
To provide a technique for levitating by converting atmospheric heat to propulsion force with a reduced fine work.When oxygen and nitrogen (hereafter air molecular) composing air come into a system composed of a double slit and a screen,...  
JP4425838B2  
JP2010506095A
A plurality of heat exchangers stored in an inside of length type shell which has a section reduced towards the upper part and was insulated from the outside, By combining the conventional solar-heat equipment connected to these, it is e...  
JP4409846B2  
JP2009293609A
To develop a motive energy principle needing no reaction of peripheral media, because a conventional transport motive energy adopts the energy principle which is propelled by reaction receiving from the peripheral media on condition that...  
JP2009543980A
[Subject] An electric propulsion (EP) system is provided. [Means for Solution] The 1st output aperture (103) in which an electric propulsion system (100) has the 1st acceleration grid (104A) and screen grid (104B), It has a plasma chambe...  
JP4379296B2  
JP4377016B2  
JP2009541645A
An increase waveform in mass which is connected with a mass change thing and an accelerator so that it can operate in a mass change thing, and carries out that a time rate of change of power of an increase waveform in (1) mass is positiv...  
JP4347461B2  
JP2009197775A
To materialize an anti-gravity device generating floating force by biasing centrifugal force.When a mass point of mass m (kg) revolves at a constant angular speed (rad/s) along semi-circular orbit in such a shape combining two semicircle...  
JP4313697B2  
JP2009527693A
Gravity pulls this surfacing propulsive engine (LPU) by changing centrifugal force from a rotation wheel without an interaction with the outside environment into an internal upward thrust, and it opposes an effect. Centrifugal force by a...  
JP2009526943A
A promotion device using substance particle acceleration including a means for accelerating substance particles only mainly to one way. Power supply of the case is carried out from the energy source including a case in which the means st...  
JP2009162178A
To miniaturize an ion engine concerning an ion jet device, a propulsion device, and an artificial satellite.This ion jet device includes a vessel enclosing a plasma assembly containing positively charged particles and negatively charged ...  
JP4294867B2  
JP2009133294A
To realize and provide means for achieving saving of limited fuel resources and reduction in generation of carbon dioxide gas, and social contribution as well as environmental protection by applying thrust to a moving object and restrain...  
JP4279463B2  
JP4281600B2  
JP4272817B2  
JP2009115069A
To solve problems wherein since in many cases, a conventional electric propulsion system used in the aerospace is an ion jet type most of which have a structure for ionizing and injecting a propellant, the electric propulsion system has ...  
JP2009092057A
To provide a system capable of passing through a place other than a road for solving traffic congestion.Guiding cylinders 1, 2, 3 and 4 and rotary cylinders 5, 6, 7 and 8 are juxtaposed on a power shaft from an engine 21. Weights 9, 10, ...  
JP2009085206A
To provide a charged particle emission device with a high performance and a long life, capable of stably generating plasma.This charged particle emission device (4b) comprises a chamber (22) having a plasma generation space (22a) formed ...  
JP4253813B2  
JP2009515081A
Gas turbine engine 10 is provided with electric heaters 34 and 26 relevant to a gas path of at least one dynamos 30 and 32 and engine 10. In order that heaters 34 and 36 may apply heat to a gas turbine cycle alternatively, electric power...  
JP2009509075A
A thruster (1) has a main chamber (6) in a pipe (2). A longitudinal direction axis of this pipe defines an axis (4) of a thrust. An injector (8) injects ionizable gas at the end of a main chamber of this pipe. An ionizer (124) ionizes ga...  
JP4229328B2  
JP2009507170A
By introducing plasma environment into an asymmetrical capacitor, the present invention generates driving force and other power, and provides a method, a device, and a system to which power is made to increase remarkably using this. With...  
JP4223989B2
A high pulse repetition frequency (PRF) plasma gun is provided, which gun inlets (74) a selected propellant gas into a column (16) formed between a center electrode (12) and a coaxial outer electrode (14), utilizes a solid state high rep...  
JP4222527B2  
JP2009030528A
To provide a compact lithium vapor discharge device excellent in safety which is suitable for instantaneously and continuously vaporizing metal lithium from a solid state, can be used at a fixed position, has excellent resistance to vibr...  
JPWO2006126397A1
触媒を用いず着火燃焼を行うことができる二 液式液体推進薬、飛行体推進方法および推進 機を提供する。二液式液体推進薬は、酸化剤 にヒドロキシルアンモニウムナイトレー...  
JP2008309054A
To generate a propulsive power using centrifugal force and precession.When a small flywheel 2 is rotated 2,000 turns, revolved 200 turns along a U-shaped curved ring 3, and then rotated 100 turns by the overall rotation of a large flywhe...  
JP4158844B2  
JP2008223655A
To provide a Hall-type electric propulsion thruster which has overheating protection and stable operation for simultaneously solving a problem related to waste heat becoming severe in association with micronization and a problem related ...  
JP4130974B2  
JPWO2006093198A1
The Heat transfer thruster which can realize and have the optimal temperature distribution for heating a promotion agent, and can improve performance without complicating structure. While receiving heating from the thruster main part (10...  
JP2008180212A
To provide a motive power of a vehicle flying in the air except for an airplane and a helicopter.Electromagnets are arranged in a hexagon so that an N pole faces another N pole and an S pole faces another S pole. Voltage is applied to th...  
JP2008169779A
To provide a pulsed plasma thruster extending the service life by effectively using a propellant and by increasing a total generating impulse, and capable of enhancing propulsion efficiency with a simple structure.In a thruster unit 1, t...  
JP3143089U
[Subject] An asynchronous orbit type elevator which adopted doughnut shape wheel type structure as a space elevator is provided. [Means for Solution] Cable 13 is stretched mutually, a ring of two kinds of size is passed to it, and it is ...  
JP4104132B2  
JP4090503B2  

Matches 601 - 650 out of 1,302