CN101797980A - Ufo - Google Patents

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Publication number
CN101797980A
CN101797980A CN200910229309A CN200910229309A CN101797980A CN 101797980 A CN101797980 A CN 101797980A CN 200910229309 A CN200910229309 A CN 200910229309A CN 200910229309 A CN200910229309 A CN 200910229309A CN 101797980 A CN101797980 A CN 101797980A
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CN
China
Prior art keywords
flywheel
cabin body
cylinder
flying saucer
cabin
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CN200910229309A
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Chinese (zh)
Inventor
陈久斌
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Individual
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Individual
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Priority to CN200910229309A priority Critical patent/CN101797980A/en
Publication of CN101797980A publication Critical patent/CN101797980A/en
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Abstract

The invention relates to a UFO which comprises a cabin body, a control system, an electronic system, a cabin inboard facility, a fuel system, an ignition system and a starting system, wherein the cabin body is provided with a cabin body motion direction adjusting device and a cabin body stabilization adjusting device. A mass energy machine is arranged on the cabin body, and comprises a flywheel shaft, a flywheel and air cylinders, wherein the flywheel shaft is connected with the cabin body; the flywheel shaft is provided with the flywheel; a linear particle generating chamber is arranged on the flywheel, and the middle part of the linear particle generating chamber is provided with an air inlet hole; the air cylinders are arranged on the periphery of the flywheel; the end of the air cylinder near the flywheel shaft, is provided with an air inlet of the air cylinder; the air inlet of the air cylinder is communicated with the periphery of the linear particle generating chamber; an igniter is arranged on the air cylinder; the included angle between the air jet direction of the air cylinders and the radius of the flywheel is phi1; and the included angle between the air jet direction of the air cylinders and flywheel plane vertical to the flywheel shaft is phi2. The invention has the same characteristics with the legendary UFO and USO, can get rid of gravitation, can momentarily realize high speed, can use any element or dark matter as fuel, can submerge into sea and travel in galaxy, replace all of transportation tools, have excellent priority, and can become the final transportation tool.

Description

Flying saucer
Technical field
The present invention relates to aerospace flight vehicle, submersible, transport facility field, specifically is a kind of flying saucer.
Background technology
Existing aircraft mainly contains aircraft, autogyro, space shuttle, space station, space capsule, rocket etc., and there are a lot of defectives in aircraft, and landing is subjected to multiple condition restriction, and major part can't vertical takeoff and landing; Energy consumption is big; Influenced by special weather and can't fly etc.Space shuttle exists flying speed low, can't realize the galaxy navigation, and the landing difficulty enters defectives such as atmospheric envelope difficulty.These aircraft ubiquities are safeguarded problems such as use cost height, cost height.The existing aircraft sea of all can not diving, submarine more can not fly, and existing aircraft can't utilize nuclear power source substantially.
Summary of the invention
The invention provides a kind of flying saucer, it can realize vertical takeoff and landing (VTOL), and the mass-energy reaction that can use material to be converted into energy provides power, the flying speed height, and compact conformation is had a smooth flight.Its flying height do not limit, fly and control simple, airflight flexible movements, can arbitrarily pause, can utilize airborne various element to act as a fuel, can realize that fuel is free, can utilize hydrogen atom, dark matter in the space to act as a fuel aloft, it is safe, cost is low, be not subjected to weather effect, round-the-clock, vertical takeoff and landing, landing are not subjected to condition restriction, enter atmospheric envelope easily, safeguard that use cost is low.
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 fuel system in the cabin, igniting system and cranking system, cabin body sense of motion control apparatus and cabin body stabilizing adjusting device are installed on the body of cabin, on the body of cabin Mechanical-power-producing mechanism is installed, Mechanical-power-producing mechanism comprises flywheel shaft, flywheel and cylinder, flywheel shaft is connected with the cabin body, flywheel is installed on the flywheel shaft, linear particle generating chamber is set on the flywheel, linear particle generating chamber offers induction opening in the middle part, and the flywheel periphery is installed a plurality of cylinders, and cylinder is offered cylinder air inlet near the flywheel axle head, cylinder air inlet is communicated with linear particle generating chamber periphery, attachment point firearm on the cylinder, angle is Φ 1 between jet direction of cylinder and flywheel radius, the angle perpendicular to the plane of flywheel shaft at jet direction of cylinder and flywheel place is Φ 2.Cabin body sense of motion control apparatus comprises the installation direction plate and first pipe expansion joint on the direction plate and the first pipe expansion joint cabin body, and first expansion link is installed on first pipe expansion joint, and first expansion link, one end is connected with direction plate.Cabin body stabilizing adjusting device 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.The cylinder air inlet outer is parallel with the cylinder inner cavity tangent line, and the cylinder air inlet outer is concordant with line style particle generating chamber inwall.Catalyst chamber and nozzle chamber are set in the cylinder, and nozzle chamber's air inlet position cross-sectional area is less than catalyst chamber maximum cross section area, and nozzle chamber's inner chamber is expanded to flywheel edge opening.On the body of cabin Intaker controller is set, Intaker controller is corresponding with induction opening.On the body of cabin magnetic bearing is installed, flywheel shaft is installed on the magnetic bearing.Conical suface is set on the flywheel.Offer side-inlet on the flywheel.Mechanical-power-producing mechanism 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.
Mechanical-power-producing mechanism utilize one from the center to the periphery the vortex field that increases progressively of rotating speed supply with particle for Mechanical-power-producing mechanism, stablized particle simultaneously, it is linear that particle shape is become.Utilize another to cut linear particle from the periphery to the vortex field that the center rotating speed increases progressively, making linear particle be cut destruction at the eddy current center releases energy, utilize this eddy-current screen energy, cooling in realizing, realize a spiral spray air-flow that increases progressively to the center rotating speed from the periphery simultaneously, alleviate air-flow and casing wall friction, improved spray velocity and jet thrust.
The jet-stream wind that utilizes flywheel rotation that Mechanical-power-producing mechanism is produced forms the airflow field of a screw propulsion that increases progressively to the center rotating speed from the periphery below flywheel, below flywheel, form an air-flow spray less than cavity area, utilize the cavity area of flywheel below that the cabin body is installed, make flywheel shaft utilize the cabin body to be stablized, also make airflow field around cabin body screw propulsion below the body of cabin.Utilize airflow field to protect the cabin body, the torsion generating that the both direction that the airflow field of utilization rotation and the flywheel of rotation produce is opposite, stabilizing cabin body, change flying saucer sense of motion.
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, flying height can height can be low; Can realize vertical takeoff and landing; Control easily flight stability; The flight noise is very little, does not almost have noise; The Mechanical-power-producing mechanism high speed revolution can realize that multiple material is converted into the mass-energy reaction of energy, and flying saucer power significantly improves; The flying speed height; Speed can soon can be slow; Simple in structure; Break-in is flexible; Safe; The fuel cost free.
Its further advantage is: but its can be dived simultaneously the sea, can break away from gravitation moment and realize advantages such as high speed, it has impayable preceence, it will become ultimate vehicle.
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 plan structure scheme drawings of accompanying drawing 1; Accompanying drawing 5 is main TV structure scheme drawings of dual intensity drive machine 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, igniting system and cranking system, cabin body sense of motion control apparatus and cabin body spin stabilization control apparatus are installed on the cabin body 22, on the cabin body 22 Mechanical-power-producing mechanism is installed, Mechanical-power-producing mechanism comprises flywheel shaft 6, flywheel 5 and cylinder, flywheel shaft 6 is connected with cabin body 22, flywheel 5 is installed on the flywheel shaft 6, linear particle generating chamber 9 is set on the flywheel 5, linear particle generating chamber offers induction opening 21 in 9 middle parts, flywheel 5 peripheries are installed a plurality of cylinders 2, cylinder is offered cylinder air inlet near the flywheel axle head, and cylinder air inlet is communicated with attachment point firearm 30 on the cylinder 2 with linear particle generating chamber 9 peripheries, angle is Φ 1 between jet direction of cylinder and flywheel 5 radiuses, and the angle perpendicular to the plane of flywheel shaft 6 at jet direction of cylinder and flywheel 5 places is Φ 2.
The optimum value scope of Φ 1 is between 55.62 °-68.76 °, a part of centnifugal force can be helped to overcome,, high speed revolution can be realized in order to offset the huge centnifugal force that most of high speed revolution produces, 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 cylinder and flywheel 5 places is Φ 2, and Φ 2 is a non-zero angle, and angle too conference hinders the rotating speed of Mechanical-power-producing mechanism, and the optimum value scope of Φ 2 is at 10 °-34.38 °.Angle is more for a short time to enable the easy more raising of engine speed, and the screw propulsion that the suitable flying saucer of angle forms jet has higher rotating speed, can improve thrust and fltting speed.
Cabin body 22 diameters can be greater than 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 cylinder ejection, direction plate 26 can stop the cylinder ejection when launching gas for well with the gas spray of cylinder ejection less than the upper edge of cabin body 22, cabin body 22.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 the influence to jet-stream wind, reduce flight resistance.
Fuel Tank 27 is installed on the cabin body 22, cartridge 29 is set on the Fuel Tank 27, 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.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, makes 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.
Intaker controller 11 can be installed in the space between interior cabin 22 and the flywheel 5.Flywheel shaft 6 runs through whole interior cabin 22, and 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 the while sleeve pipe also plays the sealing function to cabin body 22.
Between flywheel shaft 6 and the cabin body 22 bearing is installed,, a plurality of bearings can be installed, can in sleeve pipe, inject the oil lubrication bearing in order to improve load-carrying capacity.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.
Cabin body 22 requires to select for use different materials according to different flight, common can use materials such as aluminum alloy, corrosion-resistant steel, iron plate, and keel, warm material are established in inside, and hatch door is also used it, add some seal approach and get final product, more senior slightly can be with the case material of present aircraft.The cabin body 22 that need carry out the flying saucer of space flight can be with 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 just can carrying 4-5 people.Can 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 2--3 rice gets final product, and 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, can replace 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.
Flywheel 5 materials 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.
During the flying saucer high-speed motion, Mechanical-power-producing mechanism is in the place ahead of cabin body, and flying saucer is at the endoatmosphere low-speed motion or hover over when aerial, and Mechanical-power-producing mechanism can be above the body of cabin.4 direction plates 26 can be installed on the cabin body 22, be evenly distributed in four orientation 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.
Direction plate 26 also can be made three, is evenly distributed on three orientation of cabin body 22, and method is basic with that 4 direction plates 26 are set is identical, 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 that cost is higher slightly.
Mechanical-power-producing mechanism is in case igniting, 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 stabilizing adjusting device is set on cabin body 22, cabin body stabilizing adjusting device 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 the manufacturing cost height.
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, makes the cabin body keep not changeing.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.
The flying saucer lifting can be controlled with adjusting the Mechanical-power-producing mechanism rotating speed, controls the flywheel 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 can be perfect more.
The radar emission receptor can be contained in the stringcourse zone of cabin body 22, can multiple facility be installed in the stringcourse zone of cabin body 22, comprises detector, feedway, illumination equipment etc.Some device can be arranged to stretch, and can reach during use out of my cabin beyond the cyclone, finishes better detection or emission, not in the body of time spent withdrawal cabin.
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.
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 that can stretch 19 can be installed on the flying saucer, when landing, flying saucer can play buffer action, and 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.
The structure of one of embodiment of the invention is: the structure of Mechanical-power-producing mechanism is: linear particle generating chamber 9 is set on the flywheel 5, and linear particle generating chamber offers induction opening 21 in 9 middle parts.What cylinder adopted is jet cylinder 2, in flywheel 5 peripheries a plurality of cylinders 2 are installed, are offered admission port 3 on the cylinder, cylinder air inlet 3 is communicated with linear particle generating chamber (9) periphery, cylinder air inlet 3 outers are parallel with the cylinder inner cavity tangent line, and the cylinder air inlet outer is concordant with line style particle generating chamber inwall.
Linear particle generating chamber 9 air inlet position diameters are less than the position diameter of giving vent to anger.Central axis and flywheel 5 central axis in-lines, the center of induction opening 21 and the flywheel 5 central axis in-lines of linear particle generating chamber 9.The center that linear particle generating 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 linear particle generating chamber 9 edges like this.
Linear particle generating 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 linear particle generating 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 linear particle generating chamber 9 in the lump together with gas.
Catalyst chamber 40 and nozzle chamber 41 are set in the cylinder 2, and nozzle chamber's 41 air inlet position cross-sectional areas are less than catalyst chamber 40 maximum cross section areas.Between catalyst 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.
Cylinder is provided with pedestal 48 in the dual-side edge about in the of 2.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 the screw thread that is the angle of inclination with cylinder 2 interior air-flow working direction on the inwall, depth of thread and width can be selected the 1-3 millimeter.The rotating speed that screw thread can aggravate eddy current cyclone periphery successively decreases, and can improve the relative rotation speed of eddy current center of cyclone, forms one deck gas shield layer simultaneously between casing wall and eddy current cyclone, can alleviate inner wall abrasion.
For better heat radiation, cylinder 2 outer walls can be provided with screw thread or radiating gill.Be the friction of avoiding air-flow velocity that high speed revolution causes too soon linear particle generating chamber 9 inwalls etc. to be located; the screw thread that is the angle of inclination with air flow line can be set on their inwalls; screw thread can produce one deck gas shield layer in inner wall surface, can alleviate friction greatly.
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 cylinder 2 outsides high-strength material such as coated metal or carbon fiber again.Also a tubbiness cover can be set outside cylinder 2, tubbiness is applied mechanically Materials with High Strength.
The axis of cylinder 2 inner chambers that the present invention uses always is a circular arc line, the outlet side of cylinder 2 and flywheel 5 and neat, and the radian of cylinder 2 lumen centers axis can be identical with the radian at flywheel 5 edges, and the radian of cylinder 2 lumen centers axis can be selected multiple radian.Only needing during installation with cylinder 2 top center axis is that the angle perpendicular to the plane of flywheel shaft that cylinder 2 can be adjusted jet direction and flywheel place is reversed in the axle center.Be easy to form eddy current in the cylinder 2, be easy to spray.
For well, the air nozzle area helps improving catalyst chamber 40 pressure less than the admission port area to catalyst chamber 40 air nozzle areas, can select the area ratio size of different air nozzles and admission port according to different needs for use less than the admission port area.The optimal proportion scope of admission port 3 areas and air nozzle area is 1: 0.618-1: 1.The optimal proportion of catalyst chamber admission port area and catalyst chamber air nozzle area is 1: 0.618.Catalyst chamber air nozzle diameter and catalyst chamber maximum cross section diameter proportion can be selected 0.382: 1, the length ratio of the length of catalyst chamber central axis and nozzle chamber's central axis can be selected 0.618: 0.382, and the air nozzle area helps improving chamber pressure less than the admission port area.
The jet end of cylinder 2 and flywheel 5 also are best together, the length of cylinder 2 lumen centers axis can be 0.618 times of flywheel radius, the diameter of cylinder 2 inner chamber cross-sectional planes can be 0.382 times of cylinder 2 lumen centers axial length, the length of nozzle chamber's lumen centers axis can be 0.382 times of cylinder 2 lumen centers axis, the cylinder 2 and the size of flywheel are coordinated, also made the rugosity and length ratio coordination of cylinder 2 self.
The cylinder inner cavity cross-sectional plane is rounded, cylinder is offered admission port 3 near the flywheel axle head, linear particle generating chamber 9 peripheries are communicated with cylinder air inlet 3, cylinder air inlet 3 outers are parallel with the cylinder inner cavity tangent line, cylinder air inlet 3 outers are concordant with linear particle generating chamber inwall, produce the air-flow concussion in the time of can avoiding the Mechanical-power-producing mechanism high speed revolution, can make gas under the effect of inertia that the flywheel rotation produces, in the quilt incision cylinder, in cylinder, form an eddy current cyclone that increases progressively to the center rotating speed from the periphery.High more helping more of flywheel rotating speed forms eddy current in the cylinder, can improve the rotative speed of eddy current in the cylinder more.
Admission port 3 cross-sectional planes of cylinder can be selected oblong or isosceles trapezoid for use, the height of rectangular long limit or isosceles trapezoid and cylinder axis parallel axes, their length can choice reaction chamber central axis 0.382 times, help forming in the cylinder eddy current.
In order to improve intensity, improve the centrifugal force resistant ability, binding 45 can be installed, its edge arrives cylinder 2 positions, covers above cylinder 2, and binding 45 and flywheel are linked together, form an integral body, cylinder is sandwiched between linear particle generating chamber and the flywheel, makes whole device more firm.
Attachment point firearm 30 in the catalyst chamber 40, firing unit 30 can adopt light-up plug.Firing unit 30 connects igniting system, and igniting system comprises power supply, switch, high-tension transformer, circuit etc., and power supply is provided with electrical generator, and electrical generator drives generating by Mechanical-power-producing mechanism and gives the charging of power supply storage battery.In order to simplify installation, avoid a series of problems such as high voltage circuit damage simultaneously, only need the position of close firing unit 30 below flywheel 5 that one or more electrodes 77 are installed, one circle high-field electrode 77 preferably is installed, electrode point of connection ignition circuit, the binding post that makes firing unit 30 during attachment point firearm 30 is near electrode, reserve certain interval, high-tension current can puncture the gap, realizes that 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.
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., Mechanical-power-producing mechanism need start by starter gear, obtains initial rotative speed, and starter gear can be directly installed on the flywheel shaft 6, starter gear drives flywheel shaft 6 rotations, thereby provides initial speed for Mechanical-power-producing mechanism.
In the present embodiment, at first start starter gear and make flywheel 5 rotations, along with after flywheel 5 rotation reaches certain speed, air and fuel is the linear particle of suction generating chamber 9 automatically, miscellaneous gas forms the eddy current cyclone that increases progressively of rotating speed from the center to the periphery automatically in linear particle generating chamber 9, the gaseous tension at linear particle generating chamber 9 edges is improved, make gas and fuel mix even, under centnifugal force and action of inertia, fuel mixture is rushed in the catalyst chamber 40 of cylinder 2, form an eddy current cyclone that increases progressively to the center rotating speed from the periphery, firing unit 30 igniting take fire the eddy current cyclone.Catalyst chamber 40 eddy current cyclones are in case form, can in catalyst 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 peripheral rotating speed increase progressively aggravation to the center, improved the relative rotation speed of eddy current center of cyclone greatly, made energy more concentrate on eddy current center of cyclone, catalyst 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 greatly.Mechanical-power-producing mechanism is realized self-high speed revolution in case igniting can be cancelled the external force boosting, and outputting power is closed starter gear and firing unit 30 simultaneously.
When flywheel 5 reaches certain rotating speed, can realize the mass-energy reaction in the cylinder 2, produce superelevation power.Mechanical-power-producing mechanism can use any element to act as a fuel, and directly burned air allows airborne element generation mass-energy react, and can allow protium generation mass-energy react, and can act as a fuel with the dark matter in the vacuum, and this point is very important in interstellar flight.
Principle of work: flywheel high speed revolution, make the interior eddy current cyclone of cylinder also along facade axle high speed revolution, flywheel 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 drives the cylinder rotation just makes the interior eddy current cyclone of cylinder 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 self has simultaneously, particle in the eddy current cyclone also is subjected to the rotary torsion that public affairs circle and circle certainly simultaneously as the moon, and these two kinds of power interaction partners particles can produce centrifugation.
When the flywheel rotating speed reaches certain rotating speed, the rotating speed and the flywheel synchronization of the vortex field that the rotating speed from the center to the periphery in the linear particle generating chamber increases progressively, make the rotating speed of vortex field very high, this eddy current centre rotational axis end can produce suction, throws away to the eddy current periphery fast after can making the automatic suction vortex of object center.All there is relative motion each other in each point in the vortex field, motion makes each point produce interaction force each other, the friction force that rotates and knead that there is a cutting in the vortex field, separates the object in the eddy current, this power improves synchronously with the raising of rotational speed of eddy current, can be separated into atom to gas molecule, atom is twisted into linear.Gas molecule, be flexible space, flexible, be easy to be deformed, separate, atom also is a flexible space, is easy to be deformed, all microcosmic particles all have similar characteristics.
When the Mechanical-power-producing mechanism rotating speed reaches certain speed, after particle enters the linear particle generating chamber of Mechanical-power-producing mechanism from induction opening, influenced by high-speed eddy, particle is in the motion process of eddy current periphery, be subjected to the influence of vortex field that the field of particle self is rotated by flat-out acceleration, can break the balance of particle self-field when the acceleration/accel of this flat-out acceleration acquires a certain degree, particle shape is changed.
In the eddy current kinematic velocity of particle from the flywheel axle center linear velocity far away more fast more, there is the friction force that rotates and knead in the eddy current center between the peripheral adjacent particle of eddy current, particle can be subjected to a rotation stranding from eddy current and hug friction force in the motion process of eddy current periphery, just as hugging dough with hand rubbing, make static particle be rubbed the linear particle that becomes rotation by fast speed, the major axis of linear particle remains parallel with flywheel shaft under the Mechanical-power-producing mechanism turning effort, the line style particle is S. A. high speed revolution, rotating speed and flywheel synchronization with the major axis.Linear particle generating chamber be an eddy current generating chamber also be a linear particle generator, its effect mainly is that particle shape is become is linear.
When linear particle enters in the cylinder eddy current center of cyclone district, can be cut by the eddy current cyclone, the eddy current cyclone is an eddy current cyclone that increases progressively to the center rotating speed from the periphery, the linear velocity difference of the circle of different radii, make and produce the phase mutual friction between the adjacent circle, intersecting angle of S. A. existence of the eddy current cyclone in the S. A. of this eddy current cyclone and the linear particle generating chamber simultaneously, the major axis of linear particle just in time intersects with eddy current S. A. near vertical, particle is cut by the eddy current cyclone, can make separate particles, the reaction of generation mass-energy makes material be converted into energy.
There is motion in the particle, there is moving littler material, when particle structure is destroyed, these moving littler materials, flip-flop sense of motion, collision has taken place in some moving littler material each other, causes moving littler material to be decelerated suddenly, causes giving off energy.The speed of the object of motion can release energy to the outside when reducing suddenly.
Minimum particle is the unit of the pulsation between existing and not existing, and it also is a space structure, and it is exactly the neat point that is commonly called as, and it is a unit minimum in the space.All visible particles all are condensed into various condensed state by unit, have been made of the fluid field of different structure unit.After particle structure was destroyed, fluid field had disappeared, and turned to the numerous unit to all directions motion, and these yuan have just constituted energy stream to certain direction motion, directly translate into power.
Can light the mass-energy reaction when flywheel reaches certain rotating speed, at first can realize the mass-energy reaction of high atomic weight material.In case light the mass-energy reaction, can close cranking system, the Mechanical-power-producing mechanism rotating speed can improve fast, and the rotating speed and the flywheel synchronization of the eddy current rotation in the Mechanical-power-producing mechanism cylinder improve, and the material that enters cylinder can be involved in the eddy current center automatically, just as the whirlpool of water.
Eddy current center of cyclone temperature, pressure can be higher in the cylinder, because the shielding action of eddy current, make energy be difficult to be delivered to the eddy current periphery, make the suffered temperature and pressure of casing wall not have much variations, along with the further raising of rotating speed, the mass-energy reaction can aggravate, and can make various materials that the mass-energy reaction can take place, quicken to realize the mass-energy reaction of hydrogen atom again, what Mechanical-power-producing mechanism sprayed at that time is exactly the energy stream that is made of littler particles such as neutrino, quark class, units.
High-pressure fluid sprays from nozzle chamber, forms thrust, promotes the flywheel rotation.The flywheel outer rim also forms an eddy current cyclone that increases progressively to the center rotating speed from the periphery, and this can reduce the jet noise of Mechanical-power-producing mechanism equally greatly.Whole Mechanical-power-producing mechanism works together does not have roar, and Mechanical-power-producing mechanism is not vibration, shake etc. also.
The whirlpool of tropical storm, typhoon, wind spout, current etc. all is an eddy current that increases progressively to the center rotating speed from the periphery, this eddy current all has three ring districts, from the eddy current center outwards is successively: the column meiobar in S. A. zone, cylinder shape higher-pressure region, cylinder shape meiobar.The column meiobar produces an outside repulsion, and the cylinder shape meiobar produces an inside gravitation, and gravitation and repulsion combined action have produced pressure, have produced the cylinder shape higher-pressure region.
The tricyclic structure of typhoon can say something, and the whirlpool of water is the most obvious, and is the most directly perceived, the easiest observing, the whirlpool center of water is a cavity zone, and this areal pressure is also minimum accordingly, and the water velocity around the cavity zone is the highest, this regional pressure is also the highest accordingly, the speed of the peripheral current of past more whirlpool is low more, and pressure is also low more accordingly, and the eddy current in the Mechanical-power-producing mechanism cylinder is just as the whirlpool of current, different is: this whirlpool rotating speed is higher, and Mechanical-power-producing mechanism has reached superfluidity when realizing the mass-energy reaction.
When linear particle enters the cylinder shape higher-pressure region at eddy current center in the cylinder, can be cut by eddy current: be an eddy current that increases progressively to the center rotating speed from the periphery in the cylinder, all there is relative motion each other in each point in the eddy current, motion makes each point produce interaction force each other, there is a cutting in eddy current to the object in the eddy current, the power of separating, this power improves synchronously with the raising of rotational speed of eddy current, the intersecting angle of a near vertical of S. A. existence of the vortex field in the S. A. of this eddy current and the linear particle generating chamber simultaneously, the major axis of linear particle just in time with cylinder in eddy current S. A. near vertical, linear particle is originally in high speed revolution, line style particle S. A. is parallel with flywheel shaft, S. A. is difficult for rolling, the gyro of rotation is difficult for rolling, make linear particle easier by eddy current cutting in the cylinder, be easy to make linear separate particles, make that linear particle structure is destroyed to be fallen, the mass-energy reaction takes place.
Mass-energy is reflected at eddy current center ring tubular higher-pressure region and takes place, eddy current maskable energy, and mass-energy reaction and cylinder wall be direct contact not, can not produce any influence to Mechanical-power-producing mechanism, just as the violent mass-energy on the sun instead would not have influence on the earth.
In case light the mass-energy reaction, the Mechanical-power-producing mechanism rotating speed can improve fast, the temperature, pressure of eddy current center ring tubular higher-pressure region can improve fast in the cylinder, concentration of energy breaks out in eddy current center ring tubular higher-pressure region, the column meiobar in eddy current centre rotational axis zone forms energy channel, energy is close to cylinder shape higher-pressure region inwall along this passage and is directly sprayed, energy channel has further avoided energy to the peripheral motion of eddy current, the contraction gradually of cylinder catalyst chamber air nozzle has more aggravated energy and has moved to cylinder shape higher-pressure region inwall, impel the column meiobar ejection of energy, avoided casing wall to be subjected to energy impact along eddy current centre rotational axis zone.
Points all in the peripheral cylinder shape meiobar of eddy current are all to the eddy current central motion, and the peripheral cylinder shape meiobar of eddy current can change the sense of motion to the energy of the peripheral motion of eddy current, can dissolve the energy to the peripheral motion of eddy current.Eddy current can play the shielding action to energy, makes energy be difficult to be delivered to the eddy current periphery, makes the suffered temperature and pressure of casing wall not have much variations.
Further raising along with the Mechanical-power-producing mechanism rotating speed, rotational speed of eddy current improves synchronously, eddy current improves synchronously to the screening ability of energy, eddy current center ring tubular higher-pressure region temperature, pressure improves synchronously, improve synchronously to the cutting power of linear particle eddy current center ring tubular higher-pressure region, the mass-energy reaction can aggravate, and can make various elements according to a.w. the mass-energy reaction can take place successively all from high to low.
Do not need very high flywheel rotating speed, atom is that the function influence that is rotated acceleration/accel becomes linear, the atom of a static state enter suddenly a rotating speed be several ten thousand rpms the field in, its suffered rotary acceleration is very large, will certainly change the balance of its field, the atom profile is changed, be twisted into linear.
Lighting of mass-energy reaction is slowly to light, and is not the moment detonation, needn't citing security concerns.The eddy-current screen energy that increases progressively to the center rotating speed from the periphery makes the suffered temperature and pressure of cylinder wall all the time can be too not high, adds the natural cooling of cylinder outer wall, and wall temperature is maintained in the stable scope all the time, makes the cylinder can be not destroyed.
The whirlwind periphery can be involved in object in the whirlwind, and cyclone is very similar with whirlwind in the cylinder, and the gas of being close to cylinder can be involved in the cyclone, makes the gaseous tension at cylinder inner wall place very low, when rotational speed of eddy current is very high in the cylinder, even forms negative pressure.Temperature and pressure is directly proportional, and when rotational speed of eddy current was very high in the cylinder, the temperature and pressure of cylinder inner wall was very low, gas temperature or even normal temperature.
Heat energy by radiation delivery behind cylinder inner wall, the gas that constantly is involved in eddy current is taken away, the cylinder inner wall temperature can not risen, the heat transfer direction of heat convection and air motion direction are in the same way, heat conducting heat transfer rate is well below air motion speed, take away so heat constantly is involved in the gas of eddy current, bring the eddy current center into, make casing wall keep relative low temperature.Outer cooling is generally all adopted in the tradition cooling, by to the outer wall of cylinder block cooling, transmits heat by cylinder body, realizes heat balance, has caused a large amount of losses of energy, has also caused the scaling loss of casing wall, makes cylinder temperature be subjected to materials limitations can't realize higher temperature.This Mechanical-power-producing mechanism has been realized the interior cooling of casing wall, has avoided the casing wall scaling loss, has solved the control difficult problem of hyperthermal environments, has solved cylinder block material and has held heat problem.
The opening expansion of cylinder nozzle chamber makes zone of negative pressure of the easier formation of cylinder nozzle chamber inwall, even forms a vacuum layer, can well isolate heat energy, so the temperature of nozzle chamber's inwall can be not high yet.The gaseous tension at cylinder air nozzle inwall place is not high yet, and is few with the difference of pressure at reaction chamber wall place.
When the present embodiment Mechanical-power-producing mechanism uses air to act as a fuel, in order to control Mechanical-power-producing mechanism, 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, on the Intaker controller 11 pipe expansion joint is set, and closing plate 10 is installed on the pipe expansion joint, pipe expansion joint is controlled by control system, keeps stable when pipe expansion joint will make closing plate 10 move up and down.Closing plate 10 can adopt and meet graphite material, improves surface lubrication, alleviates friction.
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; the Mechanical-power-producing mechanism suction quantity diminishes, and the mass-energy response intensity is reduced, and it is the rotating speed and the power of may command Mechanical-power-producing mechanism 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.
Because the rotating speed height of flywheel 6, especially when realizing the mass-energy reaction, rotating speed is very high, so needs setting can carry high-revolving bearing on the cabin body 22, can adopt the high-speed bearing or the multiple high speed transmission system of magnetic bearing 33 or other form.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 improve magnetic-field intensity, also the magnetic bearing internal magnets can be strengthened, flywheel shaft is installed in internal magnets one end, directly utilize internal magnets one section as flywheel shaft.The structure of magnetic bearing 33 has multiple, can adopt existing magnetic bearing.
Power generating system can externally be exported 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.
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.
In order to protect flywheel 5 to reduce the flying saucer resistance simultaneously; taper cambered surface 12 is set on the flywheel 5; taper cambered surface 12 can be made of one with flywheel 5; can improve the intensity of flywheel 5 greatly; the taper globoidal 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 screw thread be set on taper cambered surface 12 surfaces.The cambered surface central part of taper cambered surface 12 is made cylindrical-conical, and the vertebra point is wanted point, and the vertebra wedge angle can be selected 55.62 degree for use, and this helps reducing resistance.In order to launch signals such as receiving radar, radio, sonar better, can be installed in radar, radio transmission receptor on the awl point, radar, radio transmission receptor can be made into taper shape, can launch receiving radar, radio signal better, can find the obstacle that flies during high-speed flight, can utilize the radar emission receptor on the body stringcourse of cabin to determine flight obstacle orientation more accurately.Radar, radio transmission receptor can adopt large current, and induction brush 28 is set on flywheel shaft, utilize large current to realize the circuit communication of radar, radio transmission receptor.
Flywheel shaft passes flywheel, can be provided with fluid passage 42 in flywheel shaft, and the flywheel face is passed in the fluid passage, the flywheel central part of fluid passage above flywheel is provided with import 7, the fluid passage is provided with outlet 8 below flywheel, outlet 8 can be located on the sidewall of fluid passage, and a plurality of outlets 8 can be set.Outlet 8 penetrates hollow flywheel shaft, to exit expansion opening, can alleviate friction.Outlet 8 can be arranged to nozzle, is installed on the flywheel shaft, and the time has been grown, and changes during serious wear to get final product, and can avoid flywheel shaft impaired.
The fluid passage inner chamber is rounded, and the fluid passage is expanded to the exit end inner chamber gradually from entrance point, can guarantee that the fluid passage inner fluid is better to outlet 8 motions.For alleviating the abrasion of fluid convection body vias inner walls, can be the screw thread of a top rake angle in fluid passage inwall setting and liquid motion direction.
A fluid part acts as a fuel and supplies with Mechanical-power-producing mechanism work, and a fluid 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.Fall for cylinder and cabin body in order to increase the air admission amount, can offer side-inlet 1 on flywheel, side-inlet 1 passes flywheel, the interstitial area of side-inlet between adjacent cylinder, side-inlet will tilt to offer, and can make that fluid is easier to be entered by flywheel rotation.
In order to improve the flight stability of flying saucer, improve the flying saucer performance, at cabin body 22 Mechanical-power-producing mechanism is installed respectively up and down, form the flying saucer of dual intensity drive machine.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 Mechanical-power-producing mechanism 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 Mechanical-power-producing mechanisms simultaneously, their the ejection air-flow hand of rotation in the same way, the direction of propulsion of air-flow is opposite.
The flying saucer of dual intensity motivation can be realized reduction of speed better, and it is safer to fly, and dual intensity motivation itself is alternative engine each other just.The dual intensity motivation is when working simultaneously with equipower, and the air-flow of ejection meets at body stringcourse place, cabin, and expansion to the periphery forms a stringcourse ring of expanding to the periphery the body stringcourse of cabin outside.Improve Mechanical-power-producing mechanism power, can improve the rotating speed and the thickness of cyclone out of my cabin greatly, improve cyclone fgn tension force and screening ability.The flying saucer performance of dual intensity drive machine is more superior.The flying saucer of monoenergetic motivation can be used as the low speed flying saucer and uses, and advantage is that cost is low, but performance is compared with the flying saucer of dual intensity motivation and had a greatly reduced quality.
The injection direction of the cylinder of the Mechanical-power-producing mechanism of cabin body 22 bottoms also is towards cabin body 22, and just all to cabin body 22 directions, promptly direction is opposite for the injection direction of cabin body cylinder of two Mechanical-power-producing mechanisms about in the of 22, but the hand of rotation of the eddy current cyclone of their ejections in the same way.The two ends of cabin body 22 are provided with separately cabin body sense of motion control apparatus to two Mechanical-power-producing mechanisms respectively, start which platform Mechanical-power-producing mechanism 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 be used alternatingly Mechanical-power-producing mechanism according to the flight needs, can use a Mechanical-power-producing mechanism to advance, and uses another to retreat, and can realize better that flying saucer slows down.When working simultaneously, the dual intensity motivation can strengthen the power of motion forward directed Mechanical-power-producing mechanism.Another also can stop working when Mechanical-power-producing mechanism used one, and in the time of starting another, that Mechanical-power-producing mechanism that needs to start can direct-fire also at high speed revolution.
The further feature of flying saucer of the present invention is: it can be dived under water, and can enter benthos, and flying saucer can carry gas, supplies with biological breathing the in the body of cabin.Available water acted as a fuel when flying saucer was dived the sea, can will use after the water vapor, the mass-energy reaction sprayed after aqueous vapor entered cylinder, can form the outside cyclone of flying saucer, cyclone is a cyclone of the high speed revolution that successively decreases of rotating speed from the center to the periphery, this cyclone has one to the exterior tension force of flying saucer, and this tension force can be dissolved sea pressure.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 taper 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.
Cylindrical-conical awl point can be dissolved sea pressure equally also with the flywheel high speed revolution, and the pressure that awl point is subjected to is big relatively, but the area of awl point is very little, and the awl point of a high speed revolution can have the bigger pressure capability (pin can pierce through object) of dissolving.The eddy current body of the screw propulsion of flywheel shaft fluid passage inwall can alleviate fluid pressure greatly, and sea pressure can not forwarded on the inwall of fluid passage, and pressure turns to the fluid velocity to the screw propulsion of fluid passage outlet.
This flying saucer can dive arrive the innermost, seabed, and it also is a real USO, and latent the dwelling in the deep-sea that it can be long-term can utilize seawater electrolysis water to supply with oxygen, utilizes sea water desalination to supply with potable water, utilizes marine life to subsist.Can produce electric energy endlessly in the flying saucer, can utilize electric energy to produce light, regulate temperature, humidity in the flying saucer, even can plant plant in flying saucer, letting animals feed forms oneself and overlaps the ecosystem, and the mankind can utilize flying saucer life for a long time in the ocean.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 flying saucer that the dual intensity motivation is installed is better, can all put two Mechanical-power-producing mechanisms during entry and catch fire, and the takeoff output that makes can be realized entry easily less times greater than another takeoff output.In water, also can open two Mechanical-power-producing mechanisms simultaneously, can be implemented in the steady lifting in the water, can steadily be parked in the water.The kinematic velocity of flying saucer 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.
Utilize the ocean can take off more easily, land, during extraterrestrial over the ground talent scout's rope, better supply can be set up the base in the ocean, than safer on land, do not worry the influence or the injury of aerolite, earthquake, flood, storm, germ, virus etc.This flying saucer will become a perfect shelter in future, will replace present house, and people settle down safer in the ocean.
If the outman settles down at the earth, their first-selection is exactly in the ocean, their house is exactly a flying saucer, it is a house of can be voluntomotory, flowing, they live the life of flowing just as tellurian nomadic people in universe, live as migratory bird and to migrate life, in universe, freely migrate.Their value of life is exactly better to evolve oneself, and making oneself becomes more premium-quality life in the universe, becomes can be alive for evermore, omnipotent senior life, and flying saucer provides the most desirable safest evolution environment to them.Life is walked from the ocean landwards, finally returns the ocean again, and this is one and returns naturally.
This flying saucer can nap of the earth flight, cyclone 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.
Cyclone is exactly the fluid field of a high-speed motion, it is a field of the high speed revolution that successively decreases of rotating speed from the center to the periphery, high more the closer to cabin body air-flow rotative speed, current density is big more, and Mechanical-power-producing mechanism provides air-flow and power endlessly for cyclone, and cyclone externally has a tension force, swiftly flowing air-flow can be dissolved various energy impacts, the cyclone skin does not have tangible border, and cyclone is outer directly not to be contacted with extraneous air, so needn't consider windage.
Cyclone is made of medium of movement; this medium is made of multiple material; both molecule, atom; also quantum, neutrino, quark, unit etc. can form cyclone, and what lean on fully is motion; the jet thrust of Mechanical-power-producing mechanism makes various media move along unified direction; constituted energy stream, this energy stream can be dissolved various energy impacts, and cyclone also can be the protecting energy layer.With energy seawater is arranged, object is arranged, dissolve energy impact with energy with energy.Its field can self-protection oneself, can dissolve the impact of any energy to it.
Cyclone is just as Earth'S atmosphere, different is, and cyclone pasting the cabin body makes high speed rotary motion, it can change the direction perpendicular to the various power of cabin body that imposes on the cabin body, direction is changed into along the power of cabin body rotation, so cyclone can protect high-revolving particulate matter and aerolite perpendicular to the power of cabin body.Aerolite has size; too big aerolite; can detect during the flying saucer high-speed flight; can not knock; little particulate matter or aerolite can get up with cyclonic motion, and just as celestial body is caught satellite, little particulate matter or aerolite can be thrown away flying saucer by fast speed with cyclone;, can not bump against on the body of cabin fast away from the cabin body with cyclone.
Its high-speed flight is got up just as the bullet of rotation, and flywheel sees that from the side flying saucer is cylindrical or cigar shape forwardly, and is similar a bit with meteor.It needn't consider aerodynamic principle, the flywheel 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 very easily, and rotation simultaneously makes it have good stable as gyro.Can side fly during its low-speed operations,, see it is butterfly from the side, also have good stable just as flying disc.During its hovering, see it also is dish-shaped from the side, see it is circular from the bottom, a ring of light is arranged around the circle.During low-speed motion, also look sometimes to look like a ball-shaped in it, look from the side when side flies also to resemble cigar shape.It can do the flare maneuver of multiple complexity, can use multiple flight attitude, it has multiple outside flight characteristic complicated and changeable, and these all are that its outward appearance and flight characteristic etc. are just the same with legendary UFO, USO because the cyclone of its cabin external body causes.
The flywheel of its high speed revolution and peripheral eddy current cyclone have good protecting function to it; this point is flown particularly important in space; the radiation of cosmic rays and the harm of cosmic dust and aerolite etc. can be reduced greatly, the pressure that the cabin body bears can be reduced simultaneously.It can replace existing space shuttle, cost have only one of percentage of existing space shuttle less than.
Its peripheral cyclone is just as the resilient protection air cushion of a high speed revolution; 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; the air communication safety problem can be do not worried, the generation of traffic accident can be thoroughly stopped.
Its peripheral cyclone can absorb radar signal, also can change the reflection direction of radar signal behind the taper cambered surface high speed revolution of flywheel top, so radar does not detect it.It can make the external world observe it by the emission radar signal, can close radar transmitter when special requirement, realizes complete stealthy flight.
This flying saucer can thoroughly be broken away from outside gravitational field, the suffered gravitation of object is not the center of attraction from gravitational field, center of attraction only determines gravity direction, gravitation comes in the self-fields and tight each the adjacent point of object, this just looks like the object in current, the impulse force that it is subjected to is not the downstream from water, neither be from the source of water, but from object current at one's side.The gravitation that object in is subjected to is the power that a liquid motion produces.
The whirlpool of tropical storm, wind spout, current etc. all is a rotating speed rotating fluid field of successively decreasing from the center to the periphery, all has the condition that produces gravitation, and they all form a field, so they just are able to exist relatively for a long time.In the fluid field that they form, all have gravitation, beyond this, just do not have gravitation to the center, field.
Earth'S atmosphere is thin more more outward, and fluid density is thin more more outward, and rotating speed is low more more outward simultaneously, so the terrestrial gravitation that is subjected to more outward in the earth gravitational field is more little, the gravitational acceleration of diverse location is different in.The fluid field that the rotating speed from the center to the periphery of a screw motion of the external formation in flying saucer cabin successively decreases, particles all in this all move in the periphery to the field, all there is motion each other in particle, motion generation power, this power has just in time been dissolved gravitation, make gravitation can not transmit the center of showing up, this can make flying saucer cabin body and extraneous field isolate, and can break away from the effect of extraneous gravitational field to the cabin body.
Flying saucer cyclone out of my cabin is very similar with wind spout, and flying saucer just in time is in the central authorities of wind spout, is on public attention of wind spout.Wind spout can be rolled object, can make the object that enters the wind spout center break away from terrestrial gravitation, and object can be easy to air motion, and traditional view thinks that object is blown afloat by air-flow, is not right.Wind spout can pick up huge water column just can prove absolutely problem, if air-flow blows afloat water column come, water column has been dispelled by air-flow for a long time, has been blown to water smoke for a long time.Water column is up to high in the clouds, and height is considerably beyond down 13 meters of bar pressure effect, thus water column neither be merely because of the air pressure generation.Water column produces with breaking away under the gravitational combined action at air pressure, there is attractive interaction between the hydrone, makes hydrone agglomerated together, form huge water column with the air-flow rising, weightless water column only need apply slight power can make its voltuntary movement, can be with the through high in the clouds of air motion.
Gyro can change center of gravity, can be with Shift of Focus to the rotation axle head, the rotation axle head of gyro contacts at most with outside gravitational field, and other position of gyro is because gravitation has just in time been dissolved in the effect of rotary centrifugal force, the teetotum rotor shaft direction does not produce centnifugal force, can not dissolve gravitation.The closer to teetotum rotating shaft end, centnifugal force is more little, and the effect of the gravitational field that teetotum rotating shaft end regions is suffered is also just big more, and gravitation concentrates on teetotum rotating shaft end regions, makes teetotum rotating shaft end regions form the center of gravity of gyro.The upper extreme point of teetotum rotating shaft, the gravitation that is subjected to are joined with centnifugal force in gyro, have been changed direction by centnifugal force.The lower extreme point of teetotum rotating shaft, the gravitation that is subjected to is outside gyro, can not join with centnifugal force, centnifugal force can not change its direction, the lower extreme point of teetotum rotating shaft becomes the center of gravity of gyro, make gyro can be in certain S. A. angle of inclination be that fulcrum keeps rotation attitude with the S. A. lower extreme point.
The flywheel of flying saucer high speed revolution is exactly a gyro, huge centnifugal force with flywheel high speed revolution generation of globoidal structure all leans on less than on the flywheel surface any material, particle is thrown out of, the power that the particle that throws away produces in the impelling process has been dissolved gravitation, and flywheel face and outside gravitational field are better isolated.Flywheel below is in another of isolating with extraneous gravitational field, and flywheel more contacts with this by all multi-parts such as cylinder of flywheel shaft and below, and the suffered gravitation of flywheel is more from this.
Flywheel is between two fields, when the opposite graviational interaction of both direction during in same object, the field that object can be delivered to oneself bigger gravitation attracts, and break away from another influence, such as the aerolite between lunar gravity field and the earth gravitational field, aerolite can be attracted to fall into earth atmosphere by the earth.So the gravitation that flywheel is subjected to is from flying saucer cabin body region, flywheel can thoroughly be broken away from the influence of outside gravitational field to it thus, and this has just realized that flying saucer thoroughly breaks away from the influence of the outside gravitational field of flying saucer, breaks away from the motion restriction of outside gravitational field to it.
Break away from that its kinematic velocity is frame of reference with the external field no longer after the influence of external field, not influenced by any of external field, flying saucer becomes an object that is independent of outside the venue.It can act on the field that it is located, and the field but can not act on it, and field action has been dissolved, shielded by the field that flying saucer produces in the field effect of flying saucer, and flying saucer has not had motional inertia inside, can realize higher speed.
Flying saucer has formed oneself independently inner gravitational field, and this gravity direction points to the reversing sense of cabin body motion, and this is because the flying saucer effect of cyclone screw propulsion out of my cabin forms.Flying saucer cyclone out of my cabin forms the gravitation to the spiral air flow direction of propulsion, does not have weightless trouble in the flying saucer.
After this flying saucer is broken away from outside gravitational field, but the moment realization at a high speed, can just disappear at a wink as meteor.It oneself form own field, do not have too many transfer of energy with on every side field, a motion to it does not on every side have resistance substantially, so do not overcome resistance with regard to not needing to pay too many energy, does not have too many waste of power, what can fly is very fast.
The flying saucer of dual intensity drive machine can be become static moment by high-speed motion, but spot speed drops to 0, can realize the acute angle turning, can realize 0 degree turning, and promptly moment is realized 180 degree sense of motions changes, is become by the moment of advancing to retreat.The people does not have any sensation in flying saucer, the people less than acceleration/accel, does not have overweight and weightless trouble in the flying saucer enteroception.
Biological clock also can change, and can break away from the extraneous time, and the time in the theoretical derivation flying saucer with the extraneous time a lot of mysterious changes may take place.
Speed is relative notion, and speed is not absolute concepts.Object distance gravitational field center is far away more, the energy affect from gravitational field that object is subjected to is more little, the higher speed of the easy more realization of object, object can be realized higher speed after thoroughly breaking away from gravitational field, the kinematic velocity of object is determined according to selected object of reference.
The light velocity is constant to be meant that light kinematic velocity in relative space is constant relatively.What the propagation of light was leaned on is a transmission of interior moving medium, is the pulsation moment realization light velocity by unit.The kinematic velocity of the field of zones of different is different in the universe, the velocity of pulsation of the interior unit of zones of different also is different in the universe, so light propagation speed of zones of different in universe is different, propagation speed is different in different fields, light is different at water neutralization propagation speed in a vacuum to be exactly illustration, so the constant opinion of the light velocity is wrong.Different zones sees that the kinematic velocity of flying saucer is different in universe, and flying saucer some in universe regional kinematic velocitys sees to be exactly superlight speed on earth.
Can finish the galaxy navigation by the universe spaceflight, the outer space, universe is a sun upper area, the earth and solar other planet all are in sun below, can arrive the outer space, universe to the flight of sun top along an angle of 90 degrees perpendicular line direction of the line between the sun and the earth, the outer space, universe is a sun upper area, can be very fast with respect to the regional flying speed of the solar system in the universe spaceflight.Zone, outer space, universe can be called time tunnel, also is course line, best universe, and flight can the relieved bold higher flying speed of realization without any obstacle in this space, is exactly superlight speed in this zone flight with respect to earth zone.
The voyage of this flying saucer 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, can consider problem of energy saving never.The bigger mother space vehicle that can be used as that the present invention does, carry a plurality of small-sized flying saucers, flywheel diameter can accomplish hundreds of rice even more than the km, it both can be used as a space station and also can be used as a mother space vehicle, can be used as the artificial planet, can make human space life arbitrarily in universe.
It can replace existing all types of aerospace flight vehicle, 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.
It can reach more than 100,000 kilometers very easily in speed per hour in the atmospheric envelope, can arrive take up an official post what place of the earth in its half an hour, can really realize the global village, for example in U.S.'s working, can live in China, gets up to go to work morning and has arrived for a moment.Can thoroughly change human custom of living in concentrated communities in the city, people can arrive local arbitrarily the inhabitation, can 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.
This flying saucer can do that big it can replace train, steamer, automobile etc. a bit as the goods transport instrument, large cargo handling in the air, and bulk freight also can be contained in handling in the air in the container.Highway, railway, water route, airport, harbour etc. will recede into the background, even become utterly useless.It can bring traffic revolution completely, bring human society politics, economy, national boundaries, etc. a series of revolutions.It can thoroughly change human life, allows humanly real fly up, and allows the mankind enter times of flight, and that will be a unprecedented great change.
Use the course line, universe that proposes 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, and can find the celestial body of a lot of suitable human livings, the galaxy immigrant can be realized, each big galaxy can be to and from easily.Can find more new life, that will be a unprecedented species revolution, be human revolution truly, to thoroughly change human definition, the Earthian will become history, and new mankind will be born, 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, and 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, igniting system and cranking system, it is characterized in that: cabin body (22) is gone up cabin body sense of motion control apparatus and cabin body stabilizing adjusting device is installed, cabin body (22) is gone up Mechanical-power-producing mechanism is installed, Mechanical-power-producing mechanism comprises flywheel shaft (6), flywheel (5) and cylinder, flywheel shaft (6) is connected with cabin body (22), flywheel shaft (6) is gone up flywheel (5) is installed, linear particle generating chamber (9) is set on the flywheel (5), linear particle generating chamber (9) offers induction opening (21) in the middle part, flywheel (5) periphery is installed a plurality of cylinders (2), cylinder (2) is offered cylinder air inlet (3) near the flywheel axle head, cylinder air inlet (3) is communicated with linear particle generating chamber (9) periphery, cylinder (2) is gone up attachment point firearm (30), angle is Φ 1 between jet direction of cylinder and flywheel (5) radius, and the angle perpendicular to the plane of flywheel shaft (6) at jet direction of cylinder 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 stabilizing adjusting device 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 is characterized in that: cylinder air inlet (3) outer is parallel with the cylinder inner cavity tangent line, and cylinder air inlet (3) outer is concordant with line style particle generating chamber (9) inwall.
5. flying saucer according to claim 1, it is characterized in that: catalyst chamber (40) and nozzle chamber (41) are set in the cylinder (2), nozzle chamber (41) air inlet position cross-sectional area is less than catalyst chamber (40) maximum cross section area, and nozzle chamber (41) inner chamber is expanded to flywheel (5) edge opening.
6. flying saucer according to claim 1 is characterized in that: Intaker controller (11) is set on the cabin body (22), and Intaker controller (11) is corresponding with induction opening (21).
7. 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.
8. flying saucer according to claim 1 is characterized in that: taper cambered surface (12) is set on the flywheel (5).
9. flying saucer according to claim 1 is characterized in that: offer side-inlet (1) on the flywheel (5).
10. according to claim 1,2,3,4,5,6,7,8 or 9 each described flying saucers, it is characterized in that: Mechanical-power-producing mechanism 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.
CN200910229309A 2009-10-23 2009-10-23 Ufo Pending CN101797980A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104743118A (en) * 2015-04-13 2015-07-01 莫文油 Disk-type helicopter
CN112702484A (en) * 2020-12-23 2021-04-23 维沃移动通信有限公司 Camera module and electronic equipment

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104743118A (en) * 2015-04-13 2015-07-01 莫文油 Disk-type helicopter
CN112702484A (en) * 2020-12-23 2021-04-23 维沃移动通信有限公司 Camera module and electronic equipment
CN112702484B (en) * 2020-12-23 2022-02-08 维沃移动通信有限公司 Camera module and electronic equipment

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Application publication date: 20100811