CN101219712A - Flying disk - Google Patents

Abstract

The invention discloses a flying saucer, belonging to an aircraft field; the invention comprises a cabin, an operation and control system, an electric system, a plurality of facilities inside cabin, a fuel system, a starting system and an ignition system; a device for regulating motion direction of the cabin and a device for regulating rotary stability of the cabin are arranged on the cabin; a fuel tank is arranged on the cabin and a fuel pipe is arranged on the fuel tank; a flywheel jet engine is arranged on the cabin and the flywheel jet engine includes a flywheel shaft, a flywheel and a jet device; the jet shaft is connected with the cabin; the flywheel is arranged on the flywheel shaft and a pluratliy of jet devices is arranged on the periphery of the flywheel. The flying saucer can realize vertical takeoff and landing; the invention is provided with the device for regulating the motion direction of the cabin and the device for regulating the rotary stability of the cabin; the flying saucer has simple operation, stable flight and convenient direction-changing; in the flight of the flying saucer, a spiral flow which surrounds the cabin, rotates around the cabin and at the same time spirally propels downwards the cabin is generated, thus greatly accelerating propelling speed of the flow downwards the cabin. The invention has the advantages of high flight speed, flexible direction-changing, high safety, and low fuel cost.

Description

Flying saucer

Technical field

The present invention relates to the aircraft field, specifically is a kind of flying saucer

Background technology

Existing aircraft mainly contains aircraft, autogyro, spacecraft, rocket, and there are a lot of defectives in aircraft, and for example: landing is subjected to multiple condition restriction, and major part can't vertical takeoff and landing; Flying speed is not high enough; Energy consumption is big; Complexity is controlled in airflight; Airflight is clumsy in one's movement; Influenced by special weather and can't fly etc.Defective such as can't fly that autogyro exists that flying speed is low, energy consumption is big, influenced by special weather; Spacecraft exists flying speed low; Can't realize the galaxy navigation; The landing difficulty; Enter defectives such as atmospheric envelope difficulty.These aircraft ubiquity poor stability are safeguarded problems such as use cost height.Existing aircraft all can not be dived under water, and submarine more can not fly.Most of aircraft can't utilize nuclear power source.

Summary of the invention

The invention provides a kind of flying saucer, it can realize vertical takeoff and landing (VTOL), it can be propulsion source with the nuclear reaction, the flying speed height, compact conformation, have a smooth flight, it has flying height and does not limit, it is handling strong to fly, control simple, the airflight flexible movements, can aloft arbitrarily pause, can use conventional fuel, also can utilize airborne various element as atomic fuel, can utilize the hydrogen atom in the space, quantum is as atomic fuel, can realize that fuel is free, it is safe, cost is low, be not subjected to weather effect, vertical takeoff and landing, landing is not subjected to condition restriction, it is easy to enter atmospheric envelope, safeguard that use cost is low, it can be dived under water simultaneously.

The present invention to achieve these goals, be achieved through the following technical solutions: flying saucer, comprise the cabin body, control and be, electric system, facility in the cabin, fuel system, cranking system and igniting system, cabin body sense of motion control apparatus and cabin body spin stabilization control apparatus are installed on the body of cabin, on the body of cabin Fuel Tank is installed, cartridge is set on the Fuel Tank, the flywheel jet engine is installed on the body of cabin, the flywheel jet engine comprises flywheel shaft, flywheel and air jet system, flywheel shaft is connected with the cabin body, flywheel is installed on the flywheel shaft, the flywheel periphery is installed a plurality of air jet systems, angle is Φ 1 between jet direction of air jet system and flywheel radius, and the angle perpendicular to the plane of flywheel shaft at jet direction of air jet system and flywheel place is Φ 2.Cabin body sense of motion control apparatus comprises the direction plate and first pipe expansion joint, and the installation direction plate and first pipe expansion joint on the body of cabin are installed first expansion link on first pipe expansion joint, and first expansion link, one end is connected with direction plate.Cabin body spin stabilization control apparatus comprises regulating plate, second pipe expansion joint and friction gear, the regulating plate and second pipe expansion joint are installed on the body of cabin, second expansion link is installed on second pipe expansion joint, second expansion link, one end is connected with regulating plate, friction gear comprises initiatively strigil, passive strigil and friction controller, and passive strigil is installed on the flywheel shaft, and the friction controller is installed on the body of cabin, initiatively strigil is installed on the friction controller, and initiatively strigil is corresponding with passive strigil.

Further aspect of the present invention is: the structure of flywheel jet engine is: gas mixer chamber is set on the flywheel, induction opening is offered at the gas mixer chamber middle part, cartridge is corresponding with induction opening, the flywheel periphery is installed a plurality of jet cylinders, the gas mixer chamber periphery sets out gas port, offer admission port on the jet cylinder, admission port is communicated with air extractor duct, attachment point firearm on the jet cylinder, be provided with free air diffuser in the admission port, free air diffuser one end opening is towards the hand of rotation of flywheel, the free air diffuser other end is towards jet cylinder inner cavity cross-sectional plane tangential direction, combustion chamber and nozzle chamber are set in the jet cylinder, and nozzle chamber's air inlet position cross-sectional area is less than combustion chamber maximum cross section area.The structure of flywheel jet engine is: the flywheel periphery is installed a plurality of turbojets.On the body of cabin magnetic bearing is installed, flywheel shaft is installed on the magnetic bearing.On the body of cabin Intaker controller is set, Intaker controller is corresponding with induction opening.Offer side-inlet on the flywheel.Cone-shaped hood is set on the flywheel.The flywheel jet engine is installed at body two ends, cabin respectively, and the cabin body is installed cabin body sense of motion control apparatus up and down respectively.

The invention has the advantages that: it has made full use of circular movement, and an effect that has utilized has utilized the stability of gyro, and the flywheel of rotation just plays the effect of gyro, flying height can height can be low; Engine installation is installed in the place ahead of aircraft, and the injection power that utilizes flywheel jet engine high speed revolution to produce advances or rises, and can realize vertical takeoff and landing; Be provided with cabin body sense of motion control apparatus and cabin body spin stabilization control apparatus, simple to operate, flight stability is convenient to break-in; Flying saucer when flight produce one be looped around around the body of cabin around the rotation of cabin body the time to the spiral air flow of cabin body below screw propulsion, spiral air flow can be dissolved noise, the flight noise is very little, almost there is not noise, simultaneously can be in the cabin one of the external formation air-flow of the screw propulsion that successively decreases of rotating speed from the center to the periphery, can improve the fltting speed of air-flow greatly to cabin body below; Flywheel jet engine high speed revolution, the pluralities of fuel that can burn can be realized nuclear reaction, flying saucer power significantly improves.The present invention has the flying speed height; Speed can soon can be slow; Have a smooth flight; Simple in structure; Simple to operate; Break-in is flexible; Safe; Fuel cost is low; Can realize advantages such as vertical takeoff and landing (VTOL).

Description of drawings

Accompanying drawing 1 is the main TV structure scheme drawing of one of embodiment of the invention; Accompanying drawing 2 be in the accompanying drawing 1 A-A to the sectional structure scheme drawing; Accompanying drawing 3 be in the accompanying drawing 2 B-B to analysing and observe the structure for amplifying scheme drawing; Accompanying drawing 4 is main TV structure scheme drawings of two of the embodiment of the invention; Accompanying drawing 5 is main TV structure scheme drawings of the double dynamical structure of the present invention; Accompanying drawing 6 is local enlarged diagrams of I portion in the accompanying drawing 5.

The specific embodiment

Agent structure of the present invention is: flying saucer, comprise cabin body 22, control and be, electric system, facility in the cabin, fuel system, cranking system and igniting system, cabin body sense of motion control apparatus and cabin body spin stabilization control apparatus are installed on the cabin body 22, Fuel Tank 27 is installed on the cabin body 22, cartridge 29 is set on the Fuel Tank 27, the flywheel jet engine is installed on the cabin body 22, the flywheel jet engine comprises flywheel shaft 6, flywheel 5 and air jet system, flywheel shaft 6 is connected with cabin body 22, flywheel 5 is installed on the flywheel shaft 6, flywheel 5 peripheries are installed a plurality of air jet systems, angle is Φ 1 between jet direction of air jet system and flywheel 5 radiuses, after deliberation, the optimum value scope of Φ 1 can help to overcome a part of centnifugal force between 55.62 °-68.76 °, in order to offset the huge centnifugal force that most of high speed revolution produces, can realize high speed revolution, needn't worry that flywheel 5 is separated by centnifugal force, can reduce the requirement to the flywheel material.The angle perpendicular to the plane of flywheel shaft 6 at jet direction of air jet system and flywheel 5 places is Φ 2, Φ 2 is a non-zero angle, and angle is the rotating speed of conference obstruction flying saucer too, the rotating speed that the little requirement of angle is higher, just can export more high thrust, the optimum value scope of Φ 2 is at 10 °-34.38 °.Angle is more for a short time to make the easy more raising of flying saucer rotating speed, and the screw propulsion of formation jet has higher rotating speed, can make its thrust bigger, fltting speed is higher.

Body 22 slightly larger in diameter in cabin are in flywheel 5 diameters, but not too big, are unfavorable for too greatly controlling.Body 22 diameter in cabin are close to the edge of the gas of air jet system ejection, direction plate 26 can stop the air jet system ejection when launching gas for well with the gas spray of air jet system ejection less than the upper edge of cabin body 22, cabin body 22.High speed flying saucer cabin body 22 diameters can be a little bit smaller slightly, and low speed flying saucer cabin body 22 diameters can be slightly bigger.The height of cabin body 22 is identical with the external diameter of cabin body 22.After deliberation, body 22 optimum structures in cabin are spherical, and spheroid is round more good more, and the outside is smooth more good more, can reduce aloft resistance like this.

Cabin 43 and hold 44 in the space can be divided in the cabin body 22, interior cabin 43 highly can be designed to 0.618 times of cabin body 22 diameters.Highly increase as required as far as possible in cabin 43 in the small-sized flying saucer, make full use of the space, makes its performance maximum effect.Large-scale flying saucer can be made multilayer to interior cabin 43, and interior cabin 43 can make many room units.The cabin body 22 of single room unit can be designed to rotate, and rotates according to the state of flight of flying saucer to make center of gravity constant, make take comfortable.Can Fuel Tank 27 be installed in the space between interior cabin 22 and the flywheel 5, Fuel Tank 27 is provided with cartridge 29.Intaker controller 11 also is installed in this zone.Clutch brush 28 also can be installed on this regional flywheel shaft 6, and flywheel shaft 6 runs through whole interior cabin 22.It is in the middle of cabin body 22, and its outside will put disrance sleeve 49, and its rotation just can not have influence in the cabin like this, and sleeve pipe also plays the sealing function to cabin body 22 simultaneously.Between flywheel shaft 6 and the cabin body 22 bearing is installed, in order to improve load-carrying capacity, a plurality of bearings can be installed, can inject the oil lubrication bearing in sleeve pipe, bearing also can be selected magnetic bearing 33 for use, can improve the flywheel rotating speed greatly, also can utilize the magnetic bearing external magnets to substitute disrance sleeve 49 when using magnetic bearing 33, can save the space, shortcoming is to isolate magnetic field, and high-intensity magnetic field can make in the cabin ironware be drawn onto to be difficult on the magnetic bearing take off.The height and the width of whole flying saucer are equal substantially, and one of the common formation of eddy current cyclone is positive spherical during its flight with out of my cabin, helps reducing resistance more, makes flight more steady.

Cabin body 22 requires to select different materials for use according to different flight, and common can use engineering plastics, or high-intensity foamed plastic one-shot forming, keel will be established in inside, hatch door is also used it, adds some seal approach and gets final product, more senior slightly can be with the case material of present aircraft.Need carry out the cabin body 22 of the flying saucer of space flight and can use carbon fibre material, also can use the canning material of present aerospacecraft.

Its cabin body 22 inner facilities simply can be similar with roadlice, and are premium-quality the same with aircraft, and the aerospacecraft standard of using of space flight gets final product.Two meters of cabin body 22 diameters can carrying 4-5 people.Need make full use of cabin body 22 upper areas and hold, the cabin height can make people's seat enter in making.The general cabin of common flying saucer body diameter gets final product for 2 to 3 meters, accomplishes the medium flying saucer that is more than ten meters, can replace existing all aircraft, and more than 100 meters is exactly large-scale flying saucer, can be used as mother space vehicle and replaces the space station.Cabin body diameter also can do less than one meter, cabin body diameter also can be done forr a short time, can be used for some other fields.

In order to reduce flying saucer weight, can make frame-type to flywheel 5, material can be with the material of high strength such as carbon fiber, and flywheel 5 diameters can be done very greatly like this.Common flying saucer gets final product with general material.The face of flywheel 5 tops will be made 111.24 degree cambered surfaces.This angle makes that flying saucer is no matter flat to fly or upright flying, and the suffered resistance of flywheel 5 is substantially all the same, and this helps having a smooth flight of flying saucer.

Cabin body sense of motion control apparatus is positioned at the top, the outside of cabin body 22, comprise the direction plate 26 and first pipe expansion joint 24, first expansion link, 25, the first expansion links, 25 1 ends are installed on installation direction plate 26 and first pipe expansion joint, 24, the first pipe expansion joints 24 on the cabin body 22 to be connected with direction plate 26.Cabin body 22 can be installed a plurality of direction plates 26,3 or 4 of operated by rotary motion just can, direction plate 26 will be evenly distributed on the cabin body 22, direction plate 26 is globoidal structures, direction plate 26 will be used temperature-resistant material, the upper edge of direction plate 26 is concordant with the top of cabin body 22, and direction plate 26 can keep flight stability when flying saucer flies, and can change the heading of flying saucer by the position of regulating all directions plate 26.First pipe expansion joint 24 is controlled the position of direction plate 26 by controlling stretching of first expansion link 25, thereby changes the heading of flying saucer, and first pipe expansion joint 24 is by the control system control of flying saucer.

4 direction plates 26 can be installed on the cabin body 22, be evenly distributed in four orientation, front, rear, left and right of cabin body.When not needing change of direction, direction plate 26 is close to cabin body 22, and cabin body 22 outer walls are spheres of a slyness when closing on the cabin body 22.Direction plate 26 upper limbs have axle to be connected with cabin body 22, and axle is vertical with flywheel shaft 6.The central control system of first pipe expansion joint, 24 usefulness is controlled, and can control with control lever, can send instruction by control lever with the circuit kit system, and first pipe expansion joint 24 is finished stretching to first expansion link 25 after receiving instruction.The folding angle of adjusting direction plate 26 can exert an influence to eddy current cyclone out of my cabin, will change the sense of motion of whole flying saucer.

When its high-speed flight, the flywheel 5 of flying saucer is top at flying saucer, at this moment the orientation title of direction plate 26 is exactly upper and lower, left and right, the perk of left direction plate, flying saucer will fly to left, the right perk will fly to right-hand, and following perk will fly downwards, and the top perk will fly upward.When it is parked in when aerial, the flywheel 5 of flying saucer is above flying saucer, and at this moment the orientation title of direction plate 26 is exactly front, rear, left and right, direction plate 26 perks in front, and flying saucer will fly obliquely upward, and back perk oblique upper backward flies.Left side perk oblique upper left flies.The right perk oblique upper to the right flies.When its low-speed operations, the flywheel 5 of flying saucer is at the oblique upper of flying saucer, at this moment the orientation title of direction plate 26 is front, rear, left and right equally, direction plate 26 perks in front, flying saucer will quicken to fly forward, the back perk will decelerating flight, and left side perk will be turned round left, and the right perk will be turned round to the right.

Direction plate 26 also can be made three, is evenly distributed on the preceding left of cabin body 22, preceding right-hand, three orientation, dead aft, and method is basic with that 4 direction plates 26 are set is identical, just controls more complicatedly, and advantage is to put down at flying saucer not influence sight line when flying.

For fear of the direction plate block vision, also direction plate 26 can be designed to parallel-moving type, direction plate 26 can be installed in cabin body 22 tops, above cabin body 22, make slideway, first pipe expansion joint, 24 controls, first expansion link 25 makes direction plate 26 slidably reciprocate along cabin body 22 cross-sectional plane radial directions and gets final product, and this programme shortcoming is the cost height.

The flywheel jet engine is in case start, will around cabin body 22, produce an eddy current cyclone, the hand of rotation of eddy current cyclone is just in time opposite with the hand of rotation of flywheel 5, the eddy current cyclone produces thrust to cabin body 22 belows, the eddy current cyclogenesis is in cabin body 22 simultaneously, make cabin body 22 produce one with the identical torsion of eddy current cyclone hand of rotation, this torsion direction is opposite with flywheel 5 rotary torsion directions, these two opposite torsion can drive the work of electrical generator, simultaneously can utilize it to regulate the stability of cabin body 22, cabin body 22 can not rotated.For these two torsion of better utilization, cabin body spin stabilization control apparatus is set on cabin body 22, cabin body spin stabilization control apparatus comprises regulating plate 23, second pipe expansion joint 46, the regulating plate 23 and second pipe expansion joint 46 are installed on the cabin body 22, second expansion link 38 is installed on second pipe expansion joint 46, second expansion link, 38 1 ends are connected with regulating plate 23, and second pipe expansion joint 46 is controlled the position of each regulating plate 23 by controlling stretching of second expansion link 38, thereby guarantee the balance of cabin body 22.Can a plurality of regulating plates 23 be installed outside cabin body 22, three or four regulating plates 23 can be installed, regulating plate 23 is evenly distributed in each orientation of cabin body 22.Each piece regulating plate 23 is just as Yishanmen, and it is in cabin body 22 middle parts, is distributed on the stringcourse of cabin body.Regulating plate 23 is globoidal structures, and the radian of regulating plate 23 is the same with cabin body 22 radians, and regulating plate 23 is wanted to be close to cabin body 22.It is spheroids of a slyness that regulating plate 23 is close to whole cabin, cabin body 22 backs body 22.Its height can be 0.382 times of interior cabin height, and width can be that 1/4th 0.382 multiple proportions of cabin body 22 circumferences is more better.Regulating plate 23 can open and, regulating plate opens, the eddy current cyclone to its outside produce one with the identical thrust of eddy current cyclone hand of rotation, make from the application force increasing of the torsion of eddy current cyclone cabin body 22; Regulating plate 23 closure function power diminish.The folding limit of regulating plate 23 connects second expansion link 38, second expansion link 38 connects second pipe expansion joint 46 again and controls second expansion link 38, can send instruction by control lever with the circuit kit system, second pipe expansion joint 46 is finished stretching to second expansion link 38 after receiving instruction.The rotating shaft limit connects has axle to be connected with cabin body 22 on 22, two angles of body, cabin.Direction from the rotating shaft limit to the folding limit is identical with eddy current cyclone hand of rotation.

Regulating plate 23 also can be made telescopic, the plane of telescopic regulating plate 23 is parallel with cabin body 22 cross-sectional plane radiuses with flywheel shaft 6, get final product with second pipe expansion joint, 46 the flexible of control and regulation plate 23, regulating plate 23 stretches out, what make that cabin body 22 is subjected to strengthens from the torsion of cyclone out of my cabin, shrinks torsion and diminishes.The structure of this telescopic regulating plate 23 takes up room greatly, and manufacturing cost is also high, and effect neither be very desirable, do not use substantially.

For better stabilizing cabin body 22, a friction gear is installed between flywheel shaft 6 and cabin body 22, friction gear comprises initiatively strigil 14, passive strigil 37 and friction controller 36, passive strigil 37 is installed on the flywheel shaft 6, friction controller 36 is installed on the cabin body 22, initiatively strigil 14 is installed on the friction controller 36, and initiatively strigil 14 is corresponding with passive strigil 37.Can adopt to be similar to braking automobile, as the folded structure of stopping, rousing brake apparatus.When cabin body 22 when eddy current cyclone hand of rotation rotates, with regard to the starting friction device, utilize the torsion of flywheel 5 to proofread and correct cabin body 22, when cabin body 22 during along eddy current cyclone rotation counter-rotation, just close friction gear, regulating plate 23 is opened, thereby increasing is from the torsion of eddy current cyclone, utilize the torsion of eddy current cyclone to proofread and correct cabin body 22, cabin body 22 is stopped operating.Regulating plate 23 has just been realized the stable of cabin body 22 with the alternating action of friction gear.General run of thins is the starting friction device seldom, with mediation board 23 is the stable of scalable cabin body 22, because friction gear can wear and tear, particularly high speed revolution is more serious to its wearing and tearing, electrical generator itself just plays the effect of a friction gear, mainly replace the work of most friction gear with it, friction gear is usefulness under special circumstances only, when significantly opening such as direction plate 26, when flying saucer quickens operation, when cabin body 22 is subjected to cyclone suddenly and influences etc.Under the weightlessness of space condition, can allow cabin body 22 by certain speed rotation, utilize centnifugal force to produce approximate gravity, thereby eliminate the weightless bad reaction that brings to the cosmonaut.

The flying saucer lifting can be controlled with adjusting flywheel jet engine rotating speed, controls flywheel air jet system rotating speed with throttle.Direction plate 26 is by control lever control, and control lever can all around arbitrarily be swung, and can make rod-type to control lever, controls with the right hand, and left hand control and regulation plate 23 and friction gear are put cabin body 22 left-handed turnings left, put cabin body 22 right-hand turnings to the right.If starting friction device cabin body 22 left-handed turnings, put so left with regard to the starting friction device, pendulum starts regulating plate 23 to the right, can be designed to direction wushu or steering wheel type control lever, rotation with steering handle or bearing circle comes control cabinet body spin stabilization control apparatus, comes control cabinet body sense of motion control apparatus with the swing of the rotating shaft of steering handle or bearing circle.Control throttle with pin, also can control them with some more advanced controlling equipments.Can drive from moving with computer system, can use aeronautical technologies such as radar, satellite positioning, flying saucer is perfection more, and radar transmitter is contained on the stringcourse of cabin body 22 and gets final product.Hatch door is installed in direction plate 26 belows or regulating plate 23 zones, can directly be installed in regulating plate 23 on the hatch door, porthole is installed in free area at cabin body 22, the operation bench of small-sized flying saucer can be watched situation out of my cabin with camera and radar system on screen, see through porthole and also can observe part situation out of my cabin, useful when landing, large-scale flying saucer porthole can be very big, can directly utilize porthole to observe more situation out of my cabin.

Further aspect of the present invention is: in order to guarantee flight safety, can safety air bag 18 be installed on hold 44 lower cabin bodies 22, gas can be selected helium or other safer gas for use in the safety air bag 18.The flying saucer safety air bag 18 that in a single day goes wrong can eject simultaneously inflation and forms balloon flying saucer is slowly landed, and avoids airplane crash to take place.The redundant space of hold 44 is as reserve tank.

Flying saucer landing for convenience, alighting gear pipe expansion joint 20 is installed on hold 44 lower cabin bodies 22, alighting gear 19 is installed on the alighting gear pipe expansion joint 20, and alighting gear pipe expansion joint 20 takes in alighting gear 19 in the cabin body 22 during flight, and alighting gear pipe expansion joint 20 stretches out alighting gear 19 outside the cabin body 22 during landing.In order to guarantee the steady landing of flying saucer, three alighting gears 19 are installed on the flying saucer, the flying saucer pulsation-free is risen and fallen.Also wheel and driving device can be installed on the alighting gear 19, flying saucer just can move on the ground like this, but cost can improve greatly, and this scheme is more suitable on large-scale flying saucer.

The structure of one of embodiment of the invention is: the structure of flywheel jet engine is: gas mixer chamber 9 is set on the flywheel 5, and induction opening 21 is offered at gas mixer chamber 9 middle parts, and cartridge 29 is corresponding with induction opening.What air jet system adopted is jet cylinder 2, in flywheel 5 peripheries a plurality of jet cylinders 2 are installed, the gas mixer chamber periphery sets out gas port 4, offer admission port 3 on the jet cylinder, admission port 3 is communicated with air extractor duct 4, attachment point firearm 30 on the jet cylinder 2, be provided with free air diffuser 39 in the admission port 3, free air diffuser 39 1 end openings are towards the hand of rotation of flywheel 5, free air diffuser 39 other ends tilt to expand opening to gas mixer chamber 9 simultaneously towards jet cylinder 2 inner chamber cross-sectional plane tangential directions, combustion chamber 40 and nozzle chamber 41 are set in the jet cylinder 2, and nozzle chamber's 41 air inlet position cross-sectional areas are less than combustion chamber 40 maximum cross section areas.

Gas mixer chamber 9 air inlet position diameters are less than the position diameter of giving vent to anger.The central axis of gas mixer chamber 9 and flywheel 5 central axis in-lines, the center of induction opening 21 and flywheel 5 central axis in-lines.The center that gas mixer chamber 9 inner chambers are done as far as possible is thicker, and the edge is done thinnerly as far as possible, can further improve the gaseous tension at gas mixer chamber 9 edges like this.Gas mixer chamber 9 can be made into one with flywheel 5, also can be made into split.Flywheel 5 can be designed to hollowly, utilize hollow part as gas mixer chamber 9.Cartridge 29 nozzles are located on induction opening 21 limits, establish several nozzles more, and they are located at around the induction opening 21, and quantity is more relatively good, can make fuel and air better mixing.Fuel can be sucked gas mixer chamber 9 in the lump together with gas.

Between combustion chamber 40 and the nozzle chamber 41 air nozzle that dwindles is arranged, nozzle chamber's 41 openings expansion, nozzle chamber's inner chamber strengthens gradually to jet direction internal diameter, and nozzle chamber's opening is expanded gradually and can better be improved jet velocity, improves capacity usage ratio.

Attachment point firearm 30 in the combustion chamber 40, firing unit 30 can adopt light-up plug, and jet cylinder is provided with pedestal 48 in the dual-side edge about in the of 2.Jet cylinder 2 inwalls will make that the lines flow smoothly, form streamline shape, particularly injection orifice place and want more that the lines flow smoothly, make air motion smooth and easy, alleviate wearing and tearing.Can offer hand of rotation and the opposite screw thread of jet cylinder 2 interior eddy current cyclone rotation working direction on the inwall, depth of thread and width can be determined according to the size size of jet cylinder 2, and be best when the screw advancement angle is 55.62 °.The rotating speed that reverse thread can aggravate eddy current cyclone periphery successively decreases; can improve the relative rotation speed of eddy current center of cyclone; between casing wall and eddy current cyclone, form one deck shock wave simultaneously; better energy and inwall from the eddy current cyclone are isolated; the effect of protection inwall can be played, inner wall abrasion can be alleviated simultaneously.If screw thread is cancelled, substantially do not influence jet cylinder 2 work yet, just increased the temperature of inwall, increased the scaling loss of inwall, increased inwall fgn energy simultaneously and scattered and disappeared, the rotating speed from the center to the periphery that has also reduced eddy current cyclone in the jet cylinder 2 simultaneously relatively successively decreases, the rotating speed of eddy current cyclone is reduced relatively, and then influencing jet velocity, influence realizes high speed revolution, influences the performance of whole flywheel jet engine.For better heat radiation, jet cylinder 2 outer walls can be provided with screw thread or radiating gill.For avoiding air-flow velocity that high speed revolution causes too high to the temperature that the friction of gas mixer chamber 9 inwalls and free air diffuser 39 inwalls causes too soon, the horizontal thread that is the angle of inclination with air flow line can be set on their inwalls, screw thread can produce one deck shock wave in inner wall surface, can alleviate greatly that friction generates heat.

Jet cylinder 2 can be used various materials, generally, uses general engine cylinder-body material to get final product, and cylinder body can adopt the foundry technique one-shot forming; Also can use the heat-resistant, high strength stupalith, can improve service life greatly, high to conditional request, intensity is strengthened in jet cylinder 2 outsides high-strength material such as coated metal or carbon fiber again.Also can a tubbiness cover be set outside jet cylinder 2, tubbiness is applied mechanically Materials with High Strength.

Jet cylinder 2 of the present invention can adopt various ways, the axis of jet cylinder 2 inner chambers commonly used is a circular arc line, the outlet side of jet cylinder 2 and flywheel 5 and neat words, the radian of jet cylinder 2 lumen centers axis can be identical with the radian at flywheel 5 edges, and the radian of jet cylinder 2 lumen centers axis can be selected multiple radian.Only needing during installation with jet cylinder 2 top center axis is that the angle perpendicular to the plane of flywheel shaft that jet cylinder 2 can be adjusted jet direction and flywheel place is reversed in the axle center.This scheme is a preferred plan, is easy to form eddy current in the jet cylinder 2, is easy to spray.

The axis of jet cylinder 2 inner chambers also can be selected wiggle for use, is the intersection point of angle with the air nozzle position of combustion chamber 40, constitutes lumen centers desired shape or cross-section line structure, makes jet cylinder 2 lumen centers axis begin bending from the air nozzle position of combustion chamber 40.Be as the criterion with nozzle chamber's 41 lumen centers axis during installation, make combustion chamber 40 lumen centers axis parallel, make nozzle chamber's 41 lumen centers axis and flywheel 5 radiuses be certain angle of inclination and get final product with flywheel 5 radiuses.Only needing during installation with jet cylinder 2 top center axis is that the angle perpendicular to the plane of flywheel shaft that jet cylinder 2 can be adjusted jet direction and flywheel 5 places is reversed in the axle center.The scheme of this wiggle structure also helps eddy current and forms.

The central axis of jet cylinder 2 inner chambers also can be selected straight line for use, and this structure manufacturing process is simple relatively, but result of use is least desirable, is unfavorable for forming eddy current, also is unfavorable for simplifying and installs.

Combustion chamber 40 air nozzle areas less than the admission port area for well, the air nozzle area helps improving combustion chamber 40 pressure less than the admission port area, but too smallly cause tempering easily, combustion chamber 40 and exterior difference of pressure have been improved simultaneously, capacity usage ratio is reduced, cause waste of power, can select the area ratio size of different air nozzles and admission port for use according to different needs.The air nozzle area causes ignition difficulties also to be unfavorable for keeping simultaneously burning greater than the admission port area easily, even does not just realize igniting at all.The air nozzle area equals the admission port area, also can light a fire and keep burning basically, and just in-cylinder pressure can be affected, and igniting is difficulty a little, should be slightly less than the admission port area with the air nozzle area.Air-flow in the jet cylinder 2 is an eddy airstream of doing the rotation ahead running, the residence time that can improve air-flow, better keeps burning.The optimal proportion scope of admission port area and air nozzle area is 1: 0.618-1: 1.The optimal proportion scope of admission port area and combustion chamber the maximum cross-section area is 0.382-0.618: 1.When combustion chamber 40 admission port areas during greater than combustion chamber 40 air nozzle areas, the firing tip of firing unit 30 is installed near combustion chamber 40 air nozzles, can be more prone to igniting, the tempering when better avoiding lighting a fire simultaneously, the conventional light-up plug of firing unit 30 usefulness gets final product.

The jet end of jet cylinder 2 and flywheel 5 also are best together, the length of jet cylinder 2 lumen centers axis can be 0.618 times of flywheel radius, the diameter of jet cylinder 2 inner chamber cross-sectional planes can be 0.382 times of jet cylinder 2 lumen centers axial length, the length of nozzle chamber's lumen centers axis can be 0.382 times of jet cylinder 2 lumen centers axis, the jet cylinder 2 and the size of flywheel are coordinated, also made the rugosity and length ratio coordination of jet cylinder 2 self.

In order to guarantee the formation of eddy current, admission port 3 is located on the jet cylinder 2 inner chamber cross-sectional plane tangential directions, free air diffuser 39 along jet cylinder 2 cross-sectional plane tangential direction openings at combustion chamber 40 tops, so that air is rushed in jet cylinder 2 with tangential direction.Admission port 3 cross-sectional planes can be selected different shape for use, circular, square, triangle, polygon, arc limit shape, irregular type etc. all can, best shape is an oblong, rectangular long limit is parallel with jet cylinder 2 central axis, helps forming eddy current like this.

Free air diffuser 39 is set in the admission port 3, flywheel 5 hand of rotation when free air diffuser 39 opening directions and 2 work of jet cylinder are best in the same way, help gas and enter jet cylinder 2 smoothly, this is because the rotation speed of advance of the gas in the gas mixer chamber 9 is lower than the speed of advance of gas mixer chamber wall 9, flywheel jet engine rotating speed is high more to embody this point more, can utilize this point that air inlet is better entered along jet cylinder 2 inner chamber cross-sectional plane tangential directions, the better utilization inertial impact force promotes eddy current to form, and can better improve the rotative speed of eddy current.Free air diffuser 39 angles of inclination are as far as possible little, make free air diffuser smooth and easy, form stream line pattern, can make air-flow enter jet cylinder 2 very smoothly.The expansion of free air diffuser 39 openings makes the easier free air diffuser that enters of air-flow, better improves intake pressure, can avoid tempering better simultaneously.

Firing unit 30 on the jet cylinder 2 connects igniting system, igniting system comprises power supply, switch, high-tension transformer, circuit etc., power supply is provided with electrical generator, electrical generator drives generating by the flywheel jet engine and gives the charging of power supply storage battery, igniting is that each parts are incorporated in the ignition device, can on flywheel shaft 6 ignition device be set, firing unit 30 is connected with ignition device, and firing circuit is connected by brush on the flywheel shaft 6 and external point ignition circuit.Establish insulation material layer between brush and flywheel shaft 6, the high tension cord that connects brush arrives flywheel 5 surfaces along flywheel shaft 6 and connects each firing unit 30 again.Another brush of high tension cord is arranged on the power-transfer clutch of electromagnet control, and two brushes constitute clutch brush 28 jointly, the outage of electromagnet and energising make two brushes from, close, clutch brush 28 can be avoided the wearing and tearing of high speed revolution to brush.Ignition device also can not adopt the clutch brush, power-transfer clutch is cancelled, make between two brushes and leave certain interval, constitute and separate brush, utilize high-tension current directly to puncture the brush interstitial area, the realization circuit is connected, and can avoid causing brush friction each other equally, can simplify the mounting structure of brush more.In order to simplify installation, avoid a series of problems such as high voltage circuit damage simultaneously, high voltage circuit and brush gear can be canceled, only need the position of close firing unit 30 below flywheel 5 that one or more electrodes are installed, one circle high-field electrode preferably is installed, electrode point of connection ignition circuit can be realized igniting better.The binding post that makes firing unit 30 during attachment point firearm 30 is reserved certain interval near electrode, and high-tension current can puncture the gap, the realization circuit connects, when one or more electrode is installed, along with flywheel 5 rotations, firing unit 30 can move to below the electrode, realizes that with high-tension current circuit is connected, and realizes igniting.

Lighting a fire is the ignition device that also can not adopt in the such scheme, is directly installed on each firing unit 30 side but make miniature ignition device, and this method and technology requires high, the cost height, and it is effective to be not so good as such scheme.

Adopt the flywheel jet engine of magnetic bearing 33 owing to there is not contact surface to be connected with cabin body 22, in order to realize that circuit connects, need add an earth electrode, can on flywheel shaft 6, establish one and separate brush, make the high-tension current negative pole realize being connected, make firing circuit form the loop with flywheel shaft 6.

Cranking system comprises power supply, switch, circuit, starter, driving device etc., the flywheel jet engine need start by starter gear, obtain initial rotative speed, starter gear can be directly installed on the flywheel shaft 6, starter gear drives flywheel shaft 6 rotations, thereby provides initial speed for the flywheel jet engine.

In the present embodiment, at first start starter gear and make flywheel 5 rotations, along with after flywheel 5 rotation reaches certain speed, air can suck induction opening 21 automatically, cartridge 29 beginnings are to induction opening 21 transfer the fuels, fuel and air are sucked gas mixer chamber 9 automatically, miscellaneous gas automatically forms the eddy current cyclone that increases progressively of rotating speed from the center to the periphery in gas mixer chamber 9, the gaseous tension at gas mixer chamber 9 edges is improved, make gas and fuel mix even, under action of centrifugal force, fuel mixture is through air extractor duct 4, admission port 3 enters the combustion chamber 40 of jet cylinder 2, form the eddy current cyclone that successively decreases of rotating speed from the center to the periphery, firing unit 30 igniting take fire the eddy current cyclone, the eddy current cyclone has prolonged the residence time of fuel at combustion chamber 40, makes fuel and air better mixing even, has better guaranteed the economic combustion of fuel.Combustion chamber 40 eddy current cyclones are in case form, can in combustion chamber 40, form a vortex, mixture gas can all enter eddy current center of cyclone from vortex, the continuous adding burning release heat of fuel has more been accelerated the rotating speed of eddy current center of cyclone, make the center to the aggravation of successively decreasing of peripheral rotating speed, improved the relative rotation speed of eddy current center of cyclone greatly, made energy more concentrate on eddy current center of cyclone, combustion chamber 40 centers can produce a high temperature and high pressure environment.

High pressure gas are discharged from nozzle chamber 41, form thrust, promote flywheel 5 rotations.Flywheel 5 outer rims also form the eddy current cyclone that successively decreases of rotating speed from the center to the periphery, and this can reduce noise equally greatly.The flywheel jet engine is realized self-high speed revolution, outputting power in case igniting can be cancelled the external force boosting.Close starter gear and firing unit 30 simultaneously.

In order to improve intensity, improve the centrifugal force resistant ability, binding 45 can be installed, binding 45 center drillings do not influence gas mixer chamber 9 air inlets, and its edge arrives jet cylinder 2 positions, cover above jet cylinder 2, the pedestal 48 of binding 45 and each jet cylinder 2 tightened together get final product, can improve intensity greatly, and the while does not influence heat radiation.Gas mixer chamber 9 can be increased during making, induction opening 21 edges and binding 45 tighten together, and help further improving intensity like this.Binding 45 edges add stay bearing plate again, can further improve intensity, and stay bearing plate and binding 45 can be made all-in-one-piece, and stay bearing plate and flywheel 5 are linked together to get final product, and so just forms an integral body, makes integral body more firm.

Present embodiment can be realized the flywheel high speed revolution, when flywheel 5 reaches certain rotating speed, can realize nuclear reaction in the jet cylinder 2, produces superelevation power.The flywheel jet engine promptly can use conventional fuel as driving engine powered by conventional energy, also can use any element as atomic fuel, direct burned air, allow airborne element generation nuclear reaction, can allow protium generation fission reaction, even can be with the quantum in the vacuum as atomic fuel, this point is very important in interstellar flight.

Principle of work: the eddy current center in the jet cylinder 2 produces the tubbiness pipe of a high pressure, eddy current center of cyclone successively decreases big more with respect to the rotating speed of periphery, the pressure that the eddy current center is subjected to is big more, simultaneously because the high speed revolution of flywheel 5, make the eddy current cyclone also along facade axle high speed revolution, flywheel 5 turns around, the eddy current cyclone also turns around along the facade axle, just look like that the moon is the same round earth rotation, moon public affairs turn around simultaneously also from turning around, flywheel 5 drives jet cylinder 2 rotations just makes jet cylinder 2 interior eddy current cyclones revolve round the sun round flywheel shaft, its public affairs circles and also circles certainly along the facade axle simultaneously, make the eddy current cyclone have plane rotary torsion and the facade rotary torsion that rotation produced that revolution causes that an eddy current cyclone itself has simultaneously, these two kinds of power interaction partners atoms can produce centrifugation.Atom in the eddy current cyclone also is subjected to public affairs as the moon and circles simultaneously from the rotary torsion that circles.

When flywheel 5 rotating speeds reach flank speed, the rotating speed and flywheel 5 synchronization of the facade rotation of the field of flywheel jet engine, make the rotating speed of the field that rotates from facade very high, in gas mixer chamber 9, form the eddy current that increases progressively of rotating speed from the center to the periphery, this eddy current can make fuel and air better mixing even, after atom enters gas mixer chamber 9 from induction opening 21, atom is subjected to the influence of field that the field of atom self is rotated by flat-out acceleration, the acceleration/accel of this flat-out acceleration is high, when acquiring a certain degree, can break the balance of atom self-field, atomic structure is changed, make atom become plasma.Gas mixer chamber 9 just plays the effect of composite fuel at the igniting initial stage, and when the flywheel jet engine reached certain rotating speed, the effect of gas mixer chamber 9 had just become one atom is converted into isoionic plasma generator.Can rotating speed have just determined and atom has been converted into plasma.

Eddy current center of cyclone produces a High Temperature High Pressure district in the jet cylinder 2, when rotating speed is very high, the temperature and pressure in eddy current center of cyclone district can be very high, when the atom of plasma state enters eddy current center of cyclone district, can be cut by the eddy current cyclone, the eddy current cyclone is the eddy current cyclone that successively decreases of rotating speed from the center to the periphery, the linear velocity difference of the circle of different radii, make and produce the phase mutual friction between the adjacent circle, there is an intersecting angle in the S. A. of the S. A. of this eddy current cyclone and the eddy current cyclone in the gas mixer chamber 9 simultaneously, the atom of plasma state is cut by the eddy current cyclone, the atom of plasma state is separated, nuclear reaction occurs, the mutual cutting of plane rotary torsion and facade rotary torsion influences atom makes atom generation nuclear reaction, and the nuclear fission reaction also can take place the enough high words hydrogen atoms of rotating speed.Complicated various nuclear reactions equally also can take place in other element.

This needs high rotating speed, can realize nuclear reaction when reaching certain rotating speed, at first can realize the nuclear reaction of high atomic weight atom, the easier realization nuclear reaction of gaseous atom.In case light nuclear reaction, rotating speed can be higher, eddy current center of cyclone temperature, pressure can be higher in the jet cylinder 2, the suffered temperature and pressure of jet cylinder 2 walls does not but have much variations, along with the further raising of rotating speed, nuclear reaction meeting aggravation can make various elements that nuclear reaction all takes place, quicken to realize the fission reaction of hydrogen atom again, the energy stream that constitutes by quantum, neutrino, quark class exactly of jet at that time cylinder 2 ejections.

Produce the rotating speed that the flywheel jet engine is depended in nuclear reaction, irrelevant with flywheel 5 sizes.Also concern not quite with the high-temperature and high-pressure conditions in the jet cylinder 2, do not need very high temperature and pressure, only require very high flywheel rotating speed.The eddy current cyclone that successively decreases of rotating speed makes the suffered temperature and pressure of jet cylinder 2 walls all the time can be too not high from the center to the periphery.Be used for space travel, band fuel seldom just can be finished space travel, can utilize the hydrogen atoms of a large amount of existence in the universe to come supplemental fuel simultaneously.Can be with any element as atomic fuel.

Can produce nuclear reaction under the present embodiment flywheel jet engine high speed revolution state, can use air as atomic fuel, when realizing nuclear reaction, in order to control the flywheel jet engine, Intaker controller 11 is set on cabin body 22, Intaker controller 11 is corresponding with induction opening 21, Intaker controller 11 generally is installed on the cabin body 22, also can be installed on the flywheel 5, influence flywheel 5 bulk strengths easily, generally not adopt but be installed on the flywheel 5, on the Intaker controller 11 pipe expansion joint is set, closing plate 10 is installed on the pipe expansion joint, and pipe expansion joint is controlled by control system, keeps stable when pipe expansion joint will make closing plate 10 move up and down.Between pipe expansion joint and the closing plate 10 magnetic bearing to be installed or other can bear the bearing arrangement of high rotating speed, make the closing plate 10 can high speed revolution.On closing plate 10, do a faulting of slab ends, magnetic bearing cover 33 gets final product on faulting of slab ends, just had no effect to the sealing of closing plate 10 in gap between the magnetic bearing like this, to be designed to inclined-plane or cambered surface or groove shape in the magnetic bearing 33 between the outer magnets, make it can bear power with magnetic bearing 33 rotating shaft parallels, guarantee that closing plate 10 can move up and down.When closing plate 10 to induction opening 21 near the time; flywheel jet engine suction quantity diminishes; nuclear reaction intensity is reduced; it is the rotating speed and the power of may command flywheel jet engine that the control sealing pulls 10; after closing plate 10 was all shut induction opening 21, closing plate 10 can be realized simultaneously ceasing fire along with flywheel 5 high speed revolutions.Closing plate 10 is enclosed within on the flywheel shaft 6, rotate synchronously with flywheel shaft 6, and can slide up and down along flywheel shaft 6, and can not be gapped between the flywheel shaft 6, make each other with Seal Oil and not only can slidably reciprocate but also can make each other clearance seal, refill magnetic bearing above the closing plate 10, magnetic bearing connects pipe expansion joint, pipe expansion joint will strengthen retraction force, make closing plate 10 in case with induction opening 21 sealings after can separate again because high speed revolution air inlet position can produce a very big suction, in case closing plate 10 with understand very difficult separating after induction opening 21 contact, can occur aerial flame-out, this thing happens in order to avoid, and closing plate 10 separated again, so will strengthen the retraction force of pipe expansion joint with induction opening 21, simultaneously induction opening 21 also will be reinforced, and makes the induction opening 21 can be with closing plate 10 activities.To separate in order realizing better, closing plate 10 can be designed to kicker magnet, adorn a circle kicker magnet around the induction opening 21 yet, they just can not lump together under the effect of magnetic field easily.In order to prevent that cartridge 29 from having influence on the use of Intaker controller 26, the structure of that cartridge 29 need be designed to stretch or swing, realize nuclear reaction after cartridge 29 leave induction opening 21, do not influence 10 work of movable sealing plate like this.Present embodiment flywheel jet engine does not need to install Intaker controller when using conventional fuel.

The advantage of present embodiment is: can adopt pluralities of fuel, can realize high speed revolution and produce nuclear reaction, the energy utilization rate height, speed is fast, and power is strong, can burned air, can realize the nuclear reaction of hydrogen atom in the space, be the preferred plan of space flight in space.

Two structure of the embodiment of the invention is: the structure of flywheel jet engine is, jet air jet system adopts turbojet 32, flywheel 5 peripheries are installed a plurality of turbojets 32, its profile geometry, dimension scale etc. can be identical with the jet cylinder among one of embodiment, installation method is also identical, flywheel 5 peripheries are installed a plurality of turbojets 32, and turbojet 32 is communicated with cartridge 29.In the present embodiment, the bottom that Fuel Tank 27 can be positioned at cabin body 22 also can be positioned at cabin body 22 tops, when Fuel Tank 27 is positioned at cabin body 22 tops, cartridge can 29 can arrive body 22 bottoms, cabin along cabin body 22 walls, rotation seat stand 34 is installed in cabin body 22 bottoms, on the rotation seat stand 34 feed pipe 35 is set, feed pipe 35 bottoms are communicated with cartridge 29, and feed pipe 35 tops are communicated with each turbojet 32.The start-up circuit of each turbojet connects the brush gear on the flywheel shaft 6, and brush gear is connected with external power supply.It starts can not need establish starter gear on flywheel shaft 6, directly directly start with each turbojet 32 to get final product.

In order to make fuel and air better mixing, also gas mixer chamber 9 can be set on flywheel 5, induction opening 21 is offered at gas mixer chamber 9 middle parts, corresponding induction opening 21 is provided with cartridge 29 and gets final product, fuel and air are fully mixed in gas mixer chamber 9, simplified the installation of cartridge 29 simultaneously, after flywheel jet engine rotating speed acquires a certain degree, mixture gas in the gas mixer chamber 9 can be rushed in turbojet by fast speed under action of centrifugal force, at this moment turbojet can become punching engine.This scheme is the preferred plan of flywheel jet engine.

The characteristics of present embodiment are: adopt conventional fuel, and complex structure, cost is too high, and energy consumption is too high, and rotating speed is lower, and performance is nothing like the structure among one of embodiment.

Because the rotating speed height of flywheel 6, especially when realizing nuclear reaction, rotating speed is very high, so needs setting can carry high-revolving bearing on the cabin body 22, can adopt magnetic bearing 33.Magnetic bearing 33 is set on cabin body 22, flywheel shaft 6 is installed on the magnetic bearing 33, two magnetic bearings 33 can be set on the flywheel shaft, also can increase a plurality of magnetic bearings 33 and improve load-carrying capacity.

In order to increase the stability of cabin body 22, carry higher rotating speed, can adopt a kind of special bearing mode.First external permanent magnets 31 is installed in cabin body 22, and the installation first inner permanent magnetic body 13, the first external permanent magnets 31 are corresponding with the first inner permanent magnetic body 13 on flywheel shaft 6, constitute a big magnetic bearing.In order to improve magnetic-field intensity, also magnetic bearing inner permanent magnetic body can be strengthened, flywheel shaft is installed in inner permanent magnetic body one end, directly utilize inner permanent magnetic body one section as flywheel shaft.

The structure of magnetic bearing 33 has multiple, can adopt existing magnetic bearing 33, also can adopt simple magnetic bearing 33, can constitute by inside and outside two permanent magnets, also can utilize permanent magnetism power and electromagnetic force combination, also can make electromagnetic force improve magnetic force with rotating speed increases synchronously, can establish the inner permanent magnetic body, electromagnet, the electromagnet cooling system, permanent magnet is established in the outside, electromagnet, the electromagnet cooling system, internal electrical magnet and cooling system are established power generating system, external electromagnets and cooling system are also established power generating system, and each electromagnet all has private circuit, rectifier is set in the circuit direction of current is remained unchanged, electromagnet magnetic field is remained unchanged, rotary magnet can use diode rectification, as long as will be switched on outage automatically after the stall.The magnetic field that cuts off the power supply between latter two permanent magnet can make the interior outer magnet of magnetic bearing can not contact, and avoids contact friction to cause mutual damage.Each electromagnet can be established a power coil and a cover cooling system, as long as rotate, will make the power coil generating, and electric current is worked electromagnet and their cooling system automatically.The high more electric current of rotating speed is big more, and the magnetic field of each electromagnet is strong more, and the power of cooling system is also big more.The cooling system of internal electrical magnet can be contained on the flywheel shaft 6, utilize the rotation natural cooling, the external cooling system can cool off with liquid helium, can improve the electric conductivity of electromagnet coils greatly, make electromagnet coils reach superconducting state, make the magnetic field of electromagnet stronger, can improve the rotating speed index of magnetic bearing 23 greatly.

The power coil system can externally export the electrical generator of electric energy simultaneously as starter also conduct, the tubbiness permanent magnet can be installed on flywheel shaft 6, with its peripheral magnetic field, can outside the tubbiness permanent magnet, install Materials with High Strength additional for improving the centrifugal force resistant ability as electrical generator, starter.Coil stationary is installed in tubbiness permanent magnet the inside.Two circuit of coil peripheral hardware are externally exported electric energy for one, and one as start-up circuit, the device of switching current direction is set in this circuit, can adopts the method for multiple change direction of current, can adopt frequency converter, inverter etc., make the electric current change of direction according to rotation, make starter work.A tubbiness permanent magnet is set to be fixed on the coil, the power coil of the electromagnet of a magnetic bearing 33 is set in the tubbiness permanent magnet on the coil, this power coil and flywheel 5 rotate synchronously, the electromagnet that makes magnetic bearing 33 forms magnetic field to flywheel 5 as long as moving coil just can generate electricity automatically, simultaneously cooling system is worked automatically.

Can also adopt a kind of simple magnetic bearing 33, it is made of in-to-in strong permanent magnetic body and exterior strong permanent magnetic body, only externally in the permanent magnet electromagnet is set, electromagnet has a private circuit that one cover cooling system is arranged simultaneously, also cooling system can be cancelled, flywheel 5 is the generation high-intensity magnetic field as long as rotary magnet will be switched on.It just can the electricity went off after flywheel 5 stalls.The magnetic field that cuts off the power supply between latter two strong permanent magnetic body can make the interior outer magnet of magnetic bearing 33 can not contact, and avoids contact friction to cause mutual damage.

In order to protect flywheel 5 to reduce the flying saucer resistance simultaneously; cone-shaped hood 12 is set on the flywheel 5; cone-shaped hood 12 can be made of one with flywheel 5; can improve the intensity of flywheel 5 greatly; cone structure can well utilize the centnifugal force of flywheel 5; make material can not utilize resistance to help flywheel 5 to dissolve the centnifugal force that a part of flywheel 5 rotations produce simultaneously near the flywheel surface.In order to reduce friction, can the rotation screw thread be set on cone-shaped hood 12 surfaces.Circuit installation and maintenance hole is reserved on cone-shaped hood 12 surfaces, with sheet material circuit installation and maintenance hole is shut usually, and the time spent opens.The cambered surface central part of cone-shaped hood 12 will be made cylindrical-conical, and the vertebra point must be sharp, sharp more good more, and the vertebra wedge angle can be selected 55.62 degree for use, and this helps reducing resistance.

Give air jet system and 22 coolings of cabin body in order to increase the air admission amount, offer side-inlet 1 on flywheel 5, side-inlet 1 passes flywheel 5, the interstitial area of side-inlet 1 between adjacent air jet system, side-inlet 1 will tilt to offer, and can make that air-flow is easier to be entered by flywheel 5 rotation.A gas part can be moved to cabin body 22 belows along cabin body 22 outer walls, can play the cooling protection effect to cabin body 22.

In order to increase air inlet, offer admission port 7 on the cone-shaped hood 12, gas channel 42 is set in the flywheel shaft 6, flywheel shaft 6 passes flywheel 5, sets out pore 8 on flywheel shaft 6 sidewalls, and flywheel shaft 6 is communicated with last admission port 7.Flywheel 5 high speed revolutions, gas enters flywheel shaft 6 through last admission port 7, throws away through air gate 8 again.Prevent simultaneously that in order to increase the suction quantity that enters flywheel shaft 6 foreign matter from entering, admission port 7 inclination net strip openings on the cone-shaped hood 12, beveled can make air-flow along with flywheel 5 rotations more enter flywheel shaft 6.

The lobate net bar of movable fan can be set on side-inlet 1 and the last admission port 7, and the lobate net bar of movable fan can be adjusted the angle of inclination, and it can be closed fully, also can tilt, and it does not influence air inlet in the time of can guaranteeing flywheel 5 high speed revolutions.When closing fully, it can avoid air-flow or water to enter.Every net bar is all by a minitype motor driving, and driven by motor net bar is opened in the time of need opening, and driven by motor net bar is closed fully when needing to close.Motor is controlled by a dedicated line, and link tester is crossed two clutch brushes 28 that are installed on the flywheel shaft 6 and is connected with power supply and gets final product.This scheme is useful when diving the sea, and the flying saucer in the sea of not diving does not need.The position of net bar surface and gas channel inwall first-class all and gas current friction all will be provided with the screw thread that is the angle of inclination with the air motion direction, can alleviate greatly that friction generates heat.

Starter gear and power generation assembly are set in the cabin body 22, its structure can have multiple, provide a kind of generating starter gear among the present invention: support 16 is set on the cabin body 22, power coil 15 is installed on the support 16, power coil 15 is connected with firing circuit with electric storage device, second external permanent magnets 17 is set on the flywheel shaft 6, and power coil 15 is positioned at second external permanent magnets 17.Support 16 can be installed in flywheel shaft 6 downsides, also can be installed on the cabin body 22 in flywheel shaft 6 outsides.Power coil 15 is maintained fixed motionless, and second external permanent magnets 17 is with flywheel shaft 6 high speed revolutions, and power coil 15 cutting magnetic lines produce electric current, and be power generation assembly this moment.When to power coil 15 energisings, power coil 15 produces magnetic field, drives 17 rotations of second external permanent magnets, thereby drives flywheel shaft 6 rotations, and be starter gear this moment.Clutch brush 28 is installed on the flywheel shaft 6, and clutch brush 28 is connected with firing circuit with firing unit 30 respectively.

Large-scale flying saucer is in order to realize in-flight ingition, avoids 22 rotations of cabin body, can a pair of air jet system be installed on the body stringcourse of cabin, utilizes jet power to make cabin body 22 keep stablizing, and makes the flying saucer can smooth starting.

In order to increase the flying speed of flying saucer, improve the flight stability of flying saucer, at cabin body 22 the flywheel jet engine is installed respectively up and down, body 22 sidewalls in cabin are installed 1 cover cabin body sense of motion control apparatus up and down respectively, and its structure is same as the previously described embodiments.When the described flywheel jet engine of startup is worked, produce one be looped around around the cabin body 22 around 22 rotations of cabin body the time to the spiral air flow of cabin body 22 other end screw propulsions, when starting two flywheel jet engines simultaneously, their the ejection air-flow hand of rotation in the same way, the direction of propulsion of air-flow is opposite.

As long as the hand of rotation of its eddy current cyclone and the hand of rotation of surround are in the same way, it can realize superlight speed flight, also can make the galaxy flying saucer thoroughly break away from gravitation, can fly more easily.It can utilize the field that self forms to dissolve the graviational interaction of surround to it, can break away from the time of surround, can change the biological rhythm of the biology in flying saucer, can prolong the biological life-span greatly.It can form simultaneously an own magnetic field, can utilize the magnetic field of self and the motion of the effect quickening self of surrounding magnetic field, just as the principle of magnetic suspension train, can realize superluminal motion more easily.Its superlight speed is not with respect to the field around it, but with respect to from its far field.Very slow in fact with respect to its kinematic velocity of field around it.

The bigger mother space vehicle that can be used as that the present invention does carries a plurality of small-sized flying saucers, and flywheel 5 diameters can be accomplished hundreds of rice even more than the km.Its Galaxy that can fly out easily in the short time can be flown at short notice in any one galaxy in the universe and go, it be a space station also be a mother space vehicle.Finishing the galaxy navigation must be by the universe spaceflight, and the outer space, universe is a sun upper area, and the earth and solar other planet all are in sun below, and the solar system is a pyramidal structure.Can be very fast in the universe spaceflight with respect to the regional flying speed of the solar system, definitely be superlight speed.

The injection direction of the air jet system of the flywheel jet engine of cabin body 22 bottoms also is towards cabin body 22, just the injection direction of cabin body air jet system of two flywheel jet engines about in the of 22 is all to cabin body 22 directions, be that direction is opposite, but the hand of rotation of the eddy current cyclone of their ejections but in the same way, sees above the flywheel jet engine out of my cabin that like this two flywheel jet engines just are one respectively and are left-hand revolution for clickwise, one.The two ends of cabin body 22 are provided with separately cabin body sense of motion control apparatus to two flywheel jet engines respectively, start which platform flywheel jet engine just with which cover cabin body sense of motion control apparatus.Their size is the same with single cover, installs just in time to be independent of each other.Alighting gear 19 can stretch to the two ends of cabin body 22 respectively at the different directions of rising and falling, and it can be installed on the stringcourse of cabin body 22.

Present embodiment can thoroughly be broken away from gravitation, can realize superlight speed flight by magnetic field, to be used alternatingly the flywheel jet engine according to the flight needs, just use a flywheel jet engine to advance during such as flight parallel with magnetic line of force, use another to retreat, when vertical with the magnetic line of force direction, just the miter angle along magnetic line of force flies, after arriving certain position, close the flywheel jet engine, start another flywheel jet engine, adjust angle again, revolve the reciprocal miter angle that turn 90 degrees to magnetic line of force and advance.So just can finish quick flight perpendicular to magnetic line of force.Another can stop working when the flywheel jet engine used one.Not flame-out when starting another in using this, could stop working after waiting that flywheel jet engine igniting.At this moment that flywheel jet engine that needs to start can direct-fire also at high speed revolution.

Flying saucer of the present invention can be dived under water, and can enter benthos, and the eddy current cyclone of the flywheel 5 of rotation and cabin body 22 peripheries can be dissolved the pressure at deep-sea.The eddy current cyclone is exactly the tight protective cover of one deck, and it is 22 tight the protecting of cabin body, and the external tension force of eddy current cyclone has just in time been dissolved the pressure of seawater.The globoidal structure of the top of flywheel 5 can well utilize the centnifugal force of flywheel 5, makes the material can not be near flywheel 5 surfaces, so flywheel 5 also can be dissolved sea pressure, it can dive to the innermost, seabed.Its kinematic velocity in seawater is exceedingly fast, and can reach several thousand nautical miles of speed per hours even up to ten thousand nautical miles, even taller.In case entering in the seawater will open the throttle wide, makes flywheel 5 high speed revolutions, its simultaneously also fast speed in seawater, move.It can stop in the shallow sea, strengthen it weight it can in the deep-sea, stop, also can roll the bottom fall into naturally down marine.It can finish human Science Explorations to the deep-sea, also can finish the exploration in a lot of planetary atmospheres.The latent extra large ability of galaxy flying saucer that round trip flight wheel jet engine is installed is better, can all put two flywheel jet engines during entry and catch fire, and the takeoff output that makes can be realized slowly entry easily less times greater than another takeoff output.In water, also can open two flywheel jet engines simultaneously, can be implemented in the steady lifting in the water, can steadily be parked in the water.

This flying saucer can paste ground and flying, air ring can well protect it make it not can with ground collision, it is just the same with an air cushion vehicle during nap of the earth flight.Its flying height is not limit, the discrepancy atmospheric envelope that it can be random, and friction generates heat to it not worry atmospheric envelope, needn't worry that more atmospheric envelope burns out it.It can be in the exoatmosphere reduction of speed very easily, can steadily must be parked in the exoatmosphere, can enter atmospheric envelope very easily.

Its high-speed flight is got up just as the bullet of rotation, high speed revolution can be dissolved windage, so its speed can be very high, small-sized flying saucer speed per hour in atmospheric envelope can reach more than 10,000 kilometers, rotation simultaneously makes it have good stable as gyro, its low-speed operations also has good stable just as flying disc.The flywheel of its high speed revolution and peripheral eddy current cyclone have good protecting function to it, and this point is flown particularly important in space.It can reduce the radiation of cosmic rays and the harm of cosmic dust and aerolite etc. greatly.It can reduce the pressure that the cabin body bears simultaneously.It can replace existing space shuttle, and cost also has only 1/tens of existing space shuttle.Its safety improves greatly, and it has the field can self-protection oneself, can exempt from the particle in the universe and the injury of aerolite.The attack of any energy to it can be dissolved in its field; its peripheral air ring is just as a resilient protection air cushion; can make it when flight, avoid bumping against; two flying saucers are flicked automatically mutually; can not produce collision; this point is flown very important under the air traffic congestion state of city, can not worry the air communication safety problem, can thoroughly stop the generation of traffic accident.What it can fly is exceedingly fast, it oneself form own field, with the too many transfer of energy that do not have on every side, field does not on every side have resistance substantially to its motion, so just not needing to pay too many energy overcomes resistance, does not have too many waste of power, very energy-conservation, what can fly is very fast.

Its voyage does not have the limit, it can fly down forever, it also can be steadily be parked in forever aerial, do not need to add any fuel, can be with it as real space station, and be omnibearing, can also can be in atmospheric envelope in space, and can be random get back on the ground, random being raised to is aerial.Can also will release track easily from the minor planet that generation threatens to the earth of space with it, avoid the destructiveness bump of minor planet the earth.It can use the free inexhaustible energy with existing various fuel, can consider problem of energy saving never.

This flying saucer can do that big it can replace train, steamer, automobile etc. a bit as the goods transport instrument, and their only are used for transporting the goods of some ultra-large types or low value in the future, and the effect of roadlice will become the effect of present bicycle.Highway, railway, water route, harbour etc. will recede into the background.It can bring traffic revolution completely.Bring a series of revolutions such as politics, economy, national boundaries of human society.It can thoroughly change human life, allows humanly real fly up.Allow the mankind enter times of flight.That will be a unprecedented great change.Mankind the Galaxy that can fly out easily in the short time can be flown at short notice in any one galaxy in the universe and go, and can find the celestial body of a lot of suitable human livings, can realize the galaxy immigrant.

It can reach more than 100,000 kilometers very easily in speed per hour in the atmospheric envelope.It can be with existing various fuel, energy consumption is low, safeguard that use cost is low, it replaces existing all types of aerospace flight vehicle simultaneously, comprise rocket, aircraft, airship, space station, can very easily satellite be taken in the space, also can very easily satellite be taken off from the sky, also can directly hang satellite, make satellite become the satellite that to be free to arrange motion with it.Highway, railway, bridge, water route, airport, harbour etc. will recede into the background, even become utterly useless.It can bring traffic revolution completely, brings a series of revolutions such as politics, economy, national boundaries of human society.It can thoroughly change human life, allows humanly real fly up, and allows the mankind thoroughly enter times of flight.Can arrive take up an official post what place of the earth in its half an hour, can thoroughly change human custom of living in concentrated communities in the city, thoroughly change human living environment, thoroughly solve the city environment problem, thoroughly solve the population problems and variety of issues such as the relevant energy that the population problem brings, traffic, resource, ecology, make humanly real to enter the space era.Use the space travel route propose previously, mankind the Galaxy that can fly out easily in the short time can be flown at short notice in any one galaxy in the universe and go.Can find the celestial body of a lot of suitable human livings, can realize the galaxy immigrant, can be to and from each big galaxy easily.Can find more new life.That will be a unprecedented species revolution, be human revolution truly, will thoroughly change human definition, and the Earthian will become history, and new mankind will be born, and human definition will become the extraterrestrial, and the definition of the earth really becomes human cradle.That will be a great changes biological evolution, species, human, life.

Technical scheme of the present invention is not restricted in the scope of embodiment of the present invention.The present invention not technology contents of detailed description is known technology.

Claims (10)

1. flying saucer, comprise cabin body (22), control and be, electric system, facility in the cabin, fuel system, cranking system and igniting system, it is characterized in that: cabin body (22) is gone up cabin body sense of motion control apparatus and cabin body spin stabilization control apparatus is installed, cabin body (22) is gone up Fuel Tank (27) is installed, cartridge (29) is set on the Fuel Tank (27), cabin body (22) is gone up the flywheel jet engine is installed, the flywheel jet engine comprises flywheel shaft (6), flywheel (5) and air jet system, flywheel shaft (6) is connected with cabin body (22), flywheel shaft (6) is gone up flywheel (5) is installed, flywheel (5) periphery is installed a plurality of air jet systems, angle is Φ 1 between jet direction of air jet system and flywheel (5) radius, and the angle perpendicular to the plane of flywheel shaft (6) at jet direction of air jet system and flywheel (5) place is Φ 2.

2. flying saucer according to claim 1, it is characterized in that: cabin body sense of motion control apparatus comprises direction plate (26) and first pipe expansion joint (24), cabin body (22) is gone up installation direction plate (26) and first pipe expansion joint (24), first pipe expansion joint (24) is gone up first expansion link (25) is installed, and first expansion link (25) one ends are connected with direction plate (26).

3. flying saucer according to claim 1, it is characterized in that: cabin body spin stabilization control apparatus comprises regulating plate (23), second pipe expansion joint (46) and friction gear, cabin body (22) is gone up regulating plate (23) and second pipe expansion joint (46) is installed, second pipe expansion joint (46) is gone up second expansion link (38) is installed, second expansion link (38) one ends are connected with regulating plate (23), friction gear comprises initiatively strigil (14), passive strigil (37) and friction controller (36), flywheel shaft (6) is gone up passive strigil (37) is installed, cabin body (22) is gone up friction controller (36) is installed, friction controller (36) is gone up initiatively strigil (14) is installed, and initiatively strigil (14) is corresponding with passive strigil (37).

4. flying saucer according to claim 1, it is characterized in that: the structure of flywheel jet engine:, gas mixer chamber (9) is set on the flywheel (5), induction opening (21) is offered at gas mixer chamber (9) middle part, cartridge (29) is corresponding with induction opening (21), flywheel (5) periphery is installed a plurality of jet cylinders (2), the gas mixer chamber periphery sets out gas port (4), offer admission port (3) on the jet cylinder (2), admission port (3) is communicated with air extractor duct (4), jet cylinder (2) is gone up attachment point firearm (30), be provided with free air diffuser (39) in the admission port (4), free air diffuser (39) one end openings are identical with the hand of rotation of flywheel (5), free air diffuser (39) other end opening is identical with jet cylinder (2) inner chamber cross-sectional plane tangential direction, combustion chamber (40) and nozzle chamber (41) are set in the jet cylinder (2), and nozzle chamber (41) air inlet position cross-sectional area is less than combustion chamber (40) maximum cross section area.

5. flying saucer according to claim 1 is characterized in that: the structure of flywheel jet engine is: flywheel (5) periphery is installed a plurality of turbojets (32).

6. flying saucer according to claim 1 is characterized in that: cabin body (22) is gone up magnetic bearing (33) is installed, and magnetic bearing (33) is gone up flywheel shaft (6) is installed.

7. flying saucer according to claim 4 is characterized in that: Intaker controller (11) is set on the cabin body (22), and Intaker controller (11) is corresponding with induction opening (21).

8. flying saucer according to claim 1 is characterized in that: offer side-inlet (1) on the flywheel (5).

9. flying saucer according to claim 1 is characterized in that: cone-shaped hood (12) is set on the flywheel (5).

10. according to claim 1,2,3,4,5,6,7 or 9 each described flying saucers, it is characterized in that: the flywheel jet engine is installed at cabin body (22) two ends respectively, and cabin body (22) is installed cabin body sense of motion control apparatus up and down respectively.

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