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JP2006316786 |
To provide an epoch-making and conventionally unavailable magnetic propulsion flight device capable of, for example, realizing free magnetic propulsion flight by mutual action with uniform magnetic field B in a space in which the uniform...
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JP2006315647 |
To reduce noise and eliminate an exhaust gas and to realize energy-saving as a conventional light aircraft or a helicopter or further as an aircraft for air transportation not competing in speed, monitoring and service from the air above...
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JP2006273320 |
To provide a suspension for hanging a jet engine on a strut of an aircraft capable of reducing weight of the suspension and simplifying machining of the suspension.The suspension is provided with a beam 10 having a platform 11; a first l...
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JP2006205755 |
To provide a propulsion system for an aircraft capable of securing optimum thrust and thrust direction according to a flying state and an optimum engine cross-sectional area and having high environmental adaptability.A power generation p...
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JP2006205757 |
To provide a small and light thrust generator of a flying object capable of quickly generating required thrust under a low noise state.A high pressure gas injection nozzle 13 for injecting high pressure gas is provided on a center axis C...
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JP3820818 |
To provide a miniaturized piezoelectric actuator for driving a driving object and to control which requires a clock signal, to a controlled system, without separately requiring an oscillation circuit. A diaphragm 10 is vibrated by elonga...
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JP2006144769 |
To increase a hypothetical output and a hypothetical power generation quantity to 1,000 times an existing reciprocating engine by raising atmospheric gravity work ability to a water output 1,000 times the combustion gas, and converting t...
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JP2006132533 |
To provide a gas turbine engine for a FLADE type aircraft being not complicated, not heavy, not bulky or not expensive and being very effective for thrust deflection.This aft FLADE type gas turbine engine 1 includes a fan section 115 in ...
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JP2006116539 |
To provide a mixer which, even when obstacles exist, can realize thorough fluid mixing.A nacelle 14 surrounds an engine, and a mounting brace suspends the engine from a blade. The front or rear end of an exhaust gas duct 22 surrounds a f...
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JP2006056364 |
To suppress the generation of temperature distribution of a tip turbine fan in a vertical take-off/landing aircraft utilizing the tip turbine fan as a propulsion force source.In the vertical take-off/landing aircraft provided with the ti...
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JP2006029336 |
To provide a device and a method for increasing efficiency in air foil.This device increases an apparent speed and efficiency of the air foil such as a blade of a vehicle, and includes at least one ionizer, that is, emitters 16, 18 and 2...
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JP2006009764 |
To provide a detonation engine simplifying structure of whole engine and providing continuous output.This detonation engine 10 producing propulsion force by generating detonation wave is provided with a swirl generation means 13 generati...
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JP2005320971 |
To provide an aircraft engine for allowing a fail-safe system to continue accepting thrust force, when one of the members of a forward suspension is damaged.The engine for aircraft includes a suspension means to the structure of the airc...
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JP2005299661 |
To remove vibration resulting from the wind mill condition of a fan by using a system having effective and simple construction.A turbo machine comprises, at least, a first rotating assembly having a first shaft, a stator, and bearings fi...
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JP2005280690 |
To provide a load transmission and fail-safe assembly improving durability, reliability and especially visibility of working in the middle of inspection while simultaneously leaving an advantageous point of a characteristic consolidating...
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JP2005271907 |
To provide a fail-safe engine mounting system transmitting not only axial thrust load but also lateral and vertical load between an engine and an aircraft.A fail-safe lug (116) is supported by an engine frame member (42) and receives cle...
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JP2005153856 |
To provide a floating moving device capable of lightening an actuator and an energy supply system.The floating moving device 1 comprises left and right blade sections 401 and 402 for performing flapping, left and right actuators 2 and 6 ...
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JP2005147126 |
To provide a various energy conservation cycle combined engine capable of preventing increase of pollution and large scale loss of combustion gas mass output.Separation to superheated steam explosion force + minimum temperature combustio...
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JP2005147146 |
To provide a turbojet installed at an upper position of a body tail part of an aircraft.The turbojet is a turbojet constituted so as to be fixed to the upper part of the body tail part of the body 1 of the aircraft using at least one cou...
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JP2005080345 |
To solve the problem that a machine for generating a lift in vacuum normally injects a gas from a boat disposed at a bottom of a vehicle; desires for another method for generating the lift in vacuum; and further always obtains to discove...
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JP2005022641 |
To improve a conventional device in mechanical aspects and viewpoint of production cost.This mount comprises a bracket 12, a lever 15; 15' with its central part 150; 150' attached to the bracket by first connection means with a pivot pin...
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JP2004352233 |
To provide a device for mounting an engine to an aircraft structure where the risk of error during assembly is minimized.The present invention relates to an attachment device, in particular a front attachment device, for attaching a turb...
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JP2004352231 |
To provide a device for mounting an engine to an aircraft structure where the risk of error during assembly is minimized.This rear suspension device includes an upper brace 12 fitted with a pylon fastening means, three rocker bars transv...
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JP2004352232 |
To improve a conventional device in a mechanical aspect and a manufacturing cost aspect.The present invention relates to a suspension of a turbo fan engine to an air craft pylon. The suspension includes a fitting 12 arranged to be attach...
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JP2004332730 |
To provide a general connection assembly, and more specifically, a method and a device for connecting a thrust link to a mount lug.A connector assembly (100) includes a thrust link (102) and a clevis (120). The thrust link includes a fir...
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JP2004276900 |
To provide an integrated high-speed aircraft such as a high-speed transport aircraft, and an associated manufacturing method.In one embodiment, a high-speed transport aircraft includes a fuselage having a first fuselage portion and a sec...
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JP2004276901 |
To provide a separating system which is high in reliability, and in which static and dynamic stresses applied on a turbojet are taken into consideration.A separating system is a system for separating a fan 10. A turbojet includes a movab...
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JP2004270691 |
To provide a combined-cycle engine by a ramjet engine having a swirl generator at the combustion efficiency of about 90-99%.In the combined-cycle engine having one core engine and one ram jet engine, the ram jet engine utilizes a swirl g...
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JP2004270513 |
To improve the operability of a decompression operation unit and prevent to forget the operation.An unmanned helicopter 1 includes a decompression unit 100 which opens a decompression valve at engine start and closes the valve after engi...
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JP2004249977 |
To provide a carrier structure that need not be removed completely for accessing engines in maintenance work and/or taking out the engines.The carrier structure comprises an upper section 20 having a front arch 22, a rear arch 24, and a ...
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JP2004108374 |
To prevent a tragedy that human beings have a dream of a vehicle canceling gravity and floating in the air and invented a rocket injecting a huge pillar of fire and flying by reaction thereof, and spend trillions yens to burn and kill do...
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JP2004052762 |
To provide an aircraft engine mount that can provide the fail-safe protection of a thrust load path without using two thrust links.First and second flanges 48, 50 of the mount 20 have bolt holes 70 formed therein. A single thrust link 56...
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JP2004034978 |
To provide an isolator assembly absorbing major noise tones generated by an engine of an aircraft or the like.The assembly is equipped with at least one fluid installed isolator 17, two dynamic absorbers 15a, 15b, at least one support po...
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JP2003254083 |
To provide an efficient and lightweight counter rotating aircraft gas turbine engine.The engine includes an inter-turbine frame 60 located between a high pressure turbine 24 and a low pressure turbine 26. The low pressure turbine 26 has ...
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JP2003194036 |
To provide an oil receiver for reducing fuel consumption, increasing durability and decreasing kinds of part to reduce a cost by reducing friction with a shaft body caused by introducing of an oil pressure into the oil receiver.In the oi...
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JP2003184653 |
To provide a system capable of supplying power and selectively supplying thrust as required to an aircraft system.This variable cycle boost propulsor system 10 has a core engine 14, a free turbine 30, a fan 34 connected to the free turbi...
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JP2003184733 |
To provide a repeated propulsion device capable of continuing the propulsion in a simple mechanism and to provide a light-weight and small-size airplane using the same.This repeated propulsion device is provided with an aluminum body 11 ...
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JP3410304 |
To simplify the supporting structure of an exhaust pipe and a silencer, and to reduce the cost and weight, by connecting the silencer with a downstream end of the exhaust pipe connected to an exhaust port of an engine, and arranging the ...
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JP2002173094 |
To provide a link part for an engine fixing system designed to have a resonant frequency not near to an excitation frequency of an engine for minimizing problems in weight and mounting of current links.This link used in the aircraft engi...
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JP2002127996 |
To apply a load on an elastic body mainly comprising vibration only by minimizing displacement between sleeves during operation.An engine side bracket 4 and a gear box side bracket 5 are rotatably connected to each other by a pin 6. A pi...
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JP2002104295 |
To provide a thrust mount constituted that vibration breakage and wear are minimized by coping with the flexibility of an equalizer lever.The thrust mount includes a platform capable of being mounted on an aircraft pylon, and an end clev...
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JP2001336520 |
To provide an aircraft engine mount having no problems of abrasion and thermal stresses while being relatively easy to assemble.The aircraft engine mount for supporting an engine on an aircraft includes a support frame fixedly connected ...
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JP2001334997 |
To improve the strength and the durability by employing a spring structure formed of only a metal.An engine side recessed bracket 4 and a gear box side projecting bracket 5 are turnably connected to each other by a pin 6. The diameter of...
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JP2001317406 |
To provide a new means using air liquefaction to supply a rocket oxidizer for placing a recyclable artificial satellite into a low earth orbit in relation to a field of aerospace crafts.High-pressure air is extracted from the central par...
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JP2001146200 |
To provide a propeller suspension for an aircraft airframe part that incorporates a safety device on its toggle joint part without an increase in mass and addition of complementary parts. The suspension includes a toggle joint 9 mounted ...
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JP2001100843 |
To provide a miniaturized piezoelectric actuator for driving a driving object and to control which requires a clock signal, to a controlled system, without separately requiring an oscillation circuit. A diaphragm 10 is vibrated by elonga...
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JP2000177697 |
To restrain a gear box from being adversely affected to the minimum even when a rotor is turned out to be in a very unstable condition.This mounting part 60 includes a cross member 62 both the ends of which are mounted on an engine case,...
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JP2000142591 |
To provide an engine mount having an excessive load path which is compact in shape and light in weight. A crevice pin 32 couples a thrust link 24 with support bodies 18, 26 in an engine thrust mount 10 of an aircraft. The pin includes a ...
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JP2000128088 |
To reduce the negative pressure peak above the main wing and delay the generation of impact waves and reduce wave resistance by providing a fluid control device such as an engine nacelle in a predetermined position on top of the main win...
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JP2000118500 |
To reduce wave drag by a method wherein a fluid element, such as an engine nacelle, is arranged in a given position on the upper surface of a main wing, an air flow generated by the fluid element is positively overlapped with an air flow...
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