CN1349907A - Three similar kinds of flyer and their orbit facilities - Google Patents

Abstract

The present invention is aimed at providing three kinds of light flying vehicles capable of flying on low-level monorail track, one of them can be three kinds of flying vehicles, including track-riding type, magnetic suspension hanging type and six-wheel hanging type, as modern traffic tool, their external form is similar to aircraft, and power device is similar to that of trolley bus; second type can be used as simulation flying vehicle for aviation practise, physical culture, artistic perform, recreation and doing a movie, etc. and third type can be used for flying trapeze simulating bird, and for making air sports and air recreation, etc.

Description

Aircraft that three classes are similar and orbital facilities thereof

The invention belongs to the aircraft field.

The aircraft of prior art is of a great variety, as: various aircrafts, airship, dirigible, aerodone, gliding parachute, Aircraft etc. also have the control speed driving and the gravity of recreation to quicken driving etc. on the ground.The aircraft of prior art, particularly various aircrafts all do not have the flight track facility of respective fixation, fuselage is big from weight, its power plant or engine petrol or snail fan spray steam turbine, must load enough gasoline during flight, be equal to or greater than carrying or cargo-carrying weight, if the generation of contingency often brings fearful airplane crash calamity; The ground communications aspect along with Increase of population and expanding economy, has presented being on the rise that the crowded to capacity and exhaust pollution of vehicular communication brings to environment, also has a succession of traffic accident accident or the like, has become insoluble social concern.

The objective of the invention is provides three types of similar lightweight aircraft of all flying for the aircraft field on the track of low latitude single track: one, the rail formula of riding that can be used as the Modern Traffic transportation means, the floating suspension type and six of magnetic are taken turns three kinds of drivings of suspension type, their outer image aircraft, the type of engine installation such as electric car; Two, can be used as aviation coach, sports, artistic performance, recreation, shoot, the type of TV, the simulated flight device of taking a photo as a moment; Three, the existing simulation birds flying trapeze of circling in the air also has the picture type of aerial sports, artistic performance and the extraordinary aerial recreation of formula, frogman's formula and aerial dodgem formula by bike.

The present invention is achieved in that---the driving type of communications and transportation, its external form are as aircraft, and engine installation such as electric car are so be called " driving ".Driving is ridden the rail formula, and the floating suspension type and six of magnetic is taken turns three kind of suspension type, large, medium and small branch is all arranged, large-scale carrying 18-24 people, medium-sized carrying 8-12 people, small-sized carrying 4-6 people.This three kind of driving is on the single track of the low latitude that sets in advance (overhead) or suspension type flight (track comprises steel wire cable etc.).The driving of wherein riding the rail formula is fit to middle slower flight, and speed per hour is 30～40 kilometers/hour in the urban district, and speed per hour can reach 150～200 kilometers/hour in the open air.The floating underslung driving speed per hour of magnetic can reach or be 800～1200 kilometers/hour near velocity of sound.Six take turns suspension type driving speed per hour can reach 200～300 kilometers/hour.Because the power of driving is to realize flight at the direct supply on track both sides by the engine installation of direct current planar motor, its track can be formed overlapping up and down, crossed stereo layout in length and breadth, so it is little, light, fast that such driving can reach, no exhaust pollution, do not crowd, do not block up the purpose of flight safety.Because the power source of driving is a direct current (DC), so need not load fuel and can not improve load-carrying efficient, can dwindle 40～50% with the aircraft comparison volume of identical passenger capacity, cost can be reduced to 20～25%, that is to say, buy an airplane and can buy 4～5 drivings.The structure of driving has the compartment, and is similar to the fuselage of aircraft; Wing is arranged, similar to the wing of aircraft; Wind-force contend with rudder and wind power balance rudder are arranged, all be after computing, to make instruction according to the wind-force data that wind sensor and wind-force loadometer provide jointly by computer, by power element start-up control machinery, the angle that it is suitable that transmission wind-force contends with rudder kick reaches the purpose of contending with, these processes all are automatically controlleds, 0.05～0.1 second time lag of reaction.Uphill/downhill and about to turn also all be that the steering unit of operator's compartment is fairly simple by the computer automatically controlled, have only several knobs and brake-applying handle (not having traversing handwheel and lifting handle), all the other all are automatic.Seat on the driving is controlled by computer when uphill/downhill, all keeps horizontality, is provided with the air expansion bag around the seat, when the accident that meets accident can expand automatically, guarantees passenger safety.---it is the direct current planar motor of rotor that the engine installation of riding rail formula driving is made of with the wheel jointly the winding of the permanent magnet that 15～25 odd numbers are installed on the wheel that metal case contained and 12～24 even numbers on the direct current planar motor stator of both sides, permanent magnet one side on the wheel all is the N utmost point, another side all is the S utmost point, the interval of planar motor stator winding equates with the width of winding, and each at interval in diamagnetic material of embedding.The direction of current of winding is all identical on one side, and another side is all opposite.Rotating speed determines that by how many variations of quantity of stator winding electrifying the many more rotating speeds of the winding of energising are fast more, and the few more rotating speed of energising winding is slow more.The current field of winding produces a powerful electro-motive force (by the direction rotation trend of Faraday's right hand theorem indication) in the wheel permanent magnet field after energising, because stator is fixed, so force the direction phase despining of wheel, around this principle can design various brush DC stepless speed-change motors to right hand theorem indication.Its structure is to be embedded in permanent magnet by the groove that the rotor of aluminum alloy is cut 15～25 odd numbers, one end all is the N utmost point, the other end all is the S utmost point, stator is divided into former and later two identical windings that is embedded with 12～24 even numbers, the interval width of winding equates with the width of winding, and each at interval in diamagnetic material of embedding, the direction of current of a stator is all identical, another is all opposite.Form the brush DC stepless speed-change motor by shell, front and rear cover and cooling fan and outer cover.---the magnetic floated power device of the floating suspension type driving type of magnetic, be a softness and longer by 12～36 magnetic floated power partial installations, and have in the tube-like envelope of an elongated slot, it can adapt to uphill/downhill and about the variation of the various states of turning, the rate of curving is less, two adjacent split bendings are between 0.2～0.4 degree, this device is to be enclosed within the magnetic levitation track both sides of two-layer permanent magnet up and down, the two poles of the earth of C type magnet are corresponding with the two poles of the earth of track upper strata permanent magnet, polarity is identical, be in the state that repels each other, produce the floating effect of left and right sides magnetic, this device double swerve is suffered restraints, also identical with track lower floor permanent magnet polarity, produce the floating effect of magnetic upwards, can carry the static total weight of driving.The stator and the winding of a pair of DC linear electric motor are installed in the interval of two C type magnet.Each magnetic floated power split is provided with two to three pairs of stator winding, and one side direction of current of all windings is all identical, and another side is all opposite.After energising, produce an electro-motive force in the magnetic field of the current field of stator winding and the lower floor's permanent magnet on the track, press the direction straight line high-speed motion of right hand theorem indication, the speed of speed is to be decided by the quantity of control winding energising, multiple speed is fast more more for the quantity of energising, and few more speed is slow more.Prevent to lift on this device and set up at the permanent magnet that promptly is fixed on C type magnet belly under the magnetic levitation track.Be provided with two hanging axises in the bottom of magnetic floated power device, the distance account for this device length 3/5～2/3 between, this hanging axis is a weight of bearing the static or low-speed motion of the driving that plays.---because the driving volume is little, in light weight, wing is arranged, ride the track of rail formula driving during flight and only bear 20～30% weight, all the other weight are born by wing; The track of suspension type driving is only born the usefulness of navigation and supply power supply, the total weight of driving is born by wing, the construction cost of therefore riding rail formula track have only train railway construction cost 15～20% between, the construction cost of magnetic-suspension type track is equivalent between the construction cost 70～80% of train railway.The track of riding rail formula driving is provided with two parallel tracks up and down, 20～30% weight of last rail bearing load driving, following rail is to strengthen the load-carrying capacity of going up rail to establish with guaranteeing the driving smooth flight, ride general 8～12 meters of the column height of rail formula driving track, the highest should not be above 36 meters, minimumly should not be lower than 5 meters, spacing distance is 6 meters (if span increases the corresponding increases of construction cost).The floating underslung track of magnetic is to establish to come and go two tracks in the column frame of gantry frame type, generally highly be 10～15 meters, the highest should not be above 50 meters, spacing distance also is 6 meters (if span increases the also corresponding increase of construction cost), power supply on the driving track is provided by the segmentation of destination stop direction, distributes each current consumer to use through the cable connection switch box by computer the direct supply on both sides by wear-resisting carbon brush or rolling carbon brush or rolling metal wheel.Each column is provided with the light deflector of the safe signal flasher that is sent by destination stop in orbit, its principle is identical with the omniscope of Submarine, the parallel light deflector that inclines and expect 45 ° in the two sides is installed in a metal case, wherein one side receives the light signal for 45 ° with the light source relative tilt, another side the distance in parallel and 300～400m/m of being separated by reflects the light as safe signal, because repeatedly the reflected light signal weakens gradually, just the light signal should be amplified once through 8～10 secondary reflections, the structural principle of light signal amplifying apparatus is similar to light deflector, also be to carry out signal relatively for single board computer (SBC) (being computer) by one side and the light deflector reception light signal and the reflection of 45 ° of light source inclines, every frequency that meets is that the pointed pulse light signal of 50～60 He Zhi sends with regard to the instruction electroluminescent lamp and amplifies and identical light signal reflects as the safety light signal that amplifies by the another side light deflector and guarantees that the brightness of light does not subtract, chaufeur can be seen the safety light signal at any time, and noise alarms such as supersonic wave bird driving snake and lightening protection installation etc. also have been installed on column.A boosting roller is installed in front at driving, install one in the back and be pushed roller, after commonly used and two standby engine installations of certain driving all are out of order, can rush to repair,, can seek help from back one and push away continuation flight if can not repair in the short period of time, if when in the flight way, meeting with the strong wind attack, each wind sensor and all wind-force loadometers are made instruction with the wind-force data delivery to computer jointly, make the wind-force corresponding angle of rudder kick of contending with, and reach the purpose of contending with.If when meeting with the thunderstorm attack awing, lightening protection installation has been installed in advance all on each column.Discharging rod etc. also has been installed on driving, can have been turned danger into safety.The track in the place ahead meets with earthquake, mountain torrents, comes down, collapses or blast etc. when track is fractureed in flight way, because power supply provides from the destination stop direction, power supply also was cut off after track fractureed, safe signal flasher all extinguishes, the still surplus inertia of driving continues flight, at this moment chaufeur brakes, and can avoid wrecked.If driving runs into the somewhere of track just to promptly disconnected, when airplane crash can't be avoided, the air expansion bag can reduce personal casualty by the timely expansion of computer instruction at once.---its flying method of the type of simulated flight device and flight track facility are all same or similar with driving, also are on the track of the light-duty single track in low latitude (overhead) or the active flight device of suspension type flight (track comprises steel wire cable) or the driven flight instruments various simulated flight utensils below playing with steel wire (rope) that scribbles extinction and look coating or carbon fibre line are imitated flight.Its kind has various aircrafts, airship, dirigible, flying saucer and the device or the like that speeds across the sky.As simulated aircraft, its purposes can be used as aircrew's schoolaeroplane, and it is identical with genuine various schoolaeroplane that external form can be made, and inside is also identical, and difference is exactly that driving engine makes the brush DC stepless variable-speed motor into, and steering unit does not change.If student's misoperation or other faults take place can not sustain damage, can improve operation or rush to repair or fall ground maintenance after rise during training, training cost reduces relatively, and training quality improves relatively, can shorten the time limit of imparting knowledge to students; The simulated flight device can be used as and shoots, TV and the usefulness of taking a photo as a moment, and can reach the effect of mixing the spurious with the genuine; Also can be used as the event of sports, the sportsman steps on crank as pin by bike and drives hinge wheel and quicken chain by the first order and rotate little acceleration chain wheel and drive two hinge wheels in both sides and quicken the little acceleration chain wheel in the chain gear second stage by the second stage and drive power wheel high speed revolution in parallel, realizes the purpose of flying contest; Also has a kind of flight racing car of picture frogman formula, outer image aerodone, the player hand leg is also used, to pull the mode of motion transmission thrust paddle that leg is stepped on, promoting driven flight instruments plays with flight racing car, when drawing in simultaneously, athletic both hands and both legs all draw forward by stay cord or connecting rod transmission thrust paddle, because the effect of air resistance, all blades all close up automatically, when athletic both hands and both legs all stretch simultaneously, all draw backward by stay cord or connecting rod transmission thrust paddle, because the effect of air resistance, all blades all strut automatically, produce proal thrust, if the sportsman constantly with the hands draws, the motion that both legs are stepped on, flight racing car just constantly forward high-speed flight reach the purpose of match; Attempt taking advantage of the impression of an aircraft also can for some people that do not take advantage of aircraft as yet, can reach effect on the spot in person; Also can be used as the usefulness of artistic performance, can become the desirable stage property of artistic performance; Also can be used as the usefulness of recreation, can become hundred and play the toy of not minding.The structure of these its active flight devices of simulated flight device is similar to the engine installation of riding the rail formula, also being made up of with the wheel the direct current planar motor that embeds permanent magnet and both sides between the spoke of wheel is the direct current planar motor of rotor, difference is that its diameter is more much smaller than driving engine installation, be installed in the housing with two this small-sized engine installations, add a small-sized hoisting machine again and just form an active flight device.Driven flight instruments, external form is identical with the active flight device, and difference is a not embedding permanent magnet on the wheel, and both sides do not dispose direct current planar motor yet, and all the other are identical.The useful single line of simulated flight device plays, also useful two-wire plays, what two-wire played also is that a line is that the U font of ining succession is played in aircraft in fact, just in case any one of two of U font messenger wire fractures and equals two and all break, can not occur one disconnected one and constantly singly hang phenomenon, can guarantee that the simulated flight device is by the glide soft landing, in the aircraft and be provided with the air expansion bag, the weightless air valve that starts of loop wheel machine impels the air expansion bag to expand when messenger wire splits off, ground also can be filled up foamed materials or be drawn the safety net of a big type, guarantees personal security.---flying trapeze's type, promptly be on people's health, to wear the aircraft that has as the bird's wing wing, a loop wheel machine is installed on the light-duty driven flight instruments on the single track of low latitude (overhead), the play people that flies below and 95～98% weight of aircraft, still 2～5% the weight of surplusing is pounced on wing by the fleet-footed runner and just can be risen to the sky, and freely circles in the air.Wear the aircraft of bird's wing formula as people after, energized, just can feel be stand on aircraft, two legs still stand in ground, and that the load of leg has alleviated is many, when pulling down joystick or push away forward to produce, the fleet-footed runner pounces on the wing action, at this moment fleet-footed runner's weight saving 5～10% o'clock is because the action of the spring of loop wheel machine has promoted freight weight limit switch (being limit switch) starting relay, energized starts loop wheel machine drive cylinder slings the fleet-footed runner, and the speed of rising is 1～2 meter per second.At this moment the fleet-footed runner to feel to take off be fully by the result who oneself pounces on wing, do not know that really 95～98% weight is hung on by loop wheel machine.The time of pouncing on the wing expendable weight is very short, generally be no more than for 2 seconds and just recover original 100% weight, if in 2 seconds, pounce on wing for the second time again, can rise once more so again, just can constantly rise if constantly pounce on wing, when reaching capacity, limit Cheng Kaiguan just cuts off the electricity supply, and can not rise again.The state of flight is controlled by two legs, when rising to suitable height, as long as break into two legs into two with one's hands the A font, the fleet-footed runner just is in horizontality, if break off with the fingers and thumb into chevron shaped, the fleet-footed runner just dives downwards, if when needing turnon left, as long as just can make left wing downward-sloping left leg K/UP, right wing is inclined upwardly, because left leg K/UP has increased the air resistance on the left side, cause the condition of turning to reach the purpose of turning left, if need bend to right as long as right leg K/UP just can be reached the purpose that bends to right.Fleet-footed runner's loop wheel machine is exactly common small-sized hoisting machine, utilizes the freight weight limit spring loop wheel machine that plays, and just cuts off the electricity supply when the weight that surpasses 95～98%, and the weight less than 95～98% just starts loop wheel machine, so just can reach to be suitable for the desired purpose of fleet-footed runner's project.Loop wheel machine also can adopt clockwork spring by play fleet-footed runner's 95～98% weight of gear transmission winch, and it does not need the control system of power supply and spring and limit switch just can reach needed purpose.The track of fleet-footed runner's low latitude (overhead) single track can be designed to wall scroll or come and go two bars or many circuit, and this circuit can be made linear that also can make shaped form or ring-like, how ring-like or the like layout; Also can adopt large-scale overhead manipulator in the scopes of 360 degree, to create a trackless and flight space freely to the fleet-footed runner; A large-scale iron plate can also be installed on indoor ceiling, and the universal driven flight instruments back suction of adopting permanent magnet under iron plate is under iron plate, and the fleet-footed runner can freely fly arbitrarily under iron plate; Also can establish the universal driven flight instruments of a magnetic attraction on the large-scale plate of no magnetic paramagnetic material, establish a universal driven flight instruments linkage from top to bottom of the iron plate that is attracted relatively below large-scale plate, the fleet-footed runner can freely be circled in the air; Utilize this principle also can be designed to the dodgem of airflight, this car can be as by bike, utilize chain gear manpower flying device's wheel flight, utilize square frame handle controlling party to, settle rubber air tyre top off around this car, around athletic seat, also surround the fleet-footed runner and protect personal safety with air bag, dodgem can run foul of each other, make the people feel thrilling and interesting, the elasticated net of a big type is set in liftoff 1～2 meter eminence, if certain dodgem is hit to fall also and fatal accident can not taken place, high on one side the flowing to while the effect of hanging down the impulsive force that dodgem produced that will hit very soon and gravity of this net served collision again, proceeds amusement or game; The principle that fleet-footed runner's project also can be utilized lever is promptly: the theorem of power * arm of force=weight * weighing arm, in the rings seat of large-scale manipulator transverse arm outer end by the play fulcrum of lever of suspension ring hoist cable, heavily hanging down of weighing arm equals 95～98% weight of fleet-footed runner and aircraft, fleet-footed runner and aircraft so can not sling, when 2～5% the weight of still surplusing is pounced on wing and is alleviated 5～10% weight by the fleet-footed runner, at this moment because heavily the weight of hanging down is greater than the weight of fleet-footed runner and aircraft, fleet-footed runner and aircraft are sling; Also can the end of assembly pulley by messenger wire play fleet-footed runner and aircraft be installed on hand at big machinery, the other end directly play 95～98% heavily vertical, fleet-footed runner and the aircraft can not sling should hang down, when the fleet-footed runner pounces on wing and alleviates 5～10% weight, at this moment the weight of heavily hanging down is greater than the weight of fleet-footed runner and aircraft, and fleet-footed runner and aircraft are sling with regard to emptied.---the manufactured materials of above three types of similar aircraft and orbital facilities thereof: 1. the compartment of aircraft, wing, wind-force contend with rudder, wind power balance rudder, seat, case, support, connecting rod, hang bow, joint, roller, pulley, shackle etc. and can select material manufacture such as steel, aluminum alloy, glass-felt plastic, nylon, plastics, alloy glass for use; 2. the track of orbital facilities, column, crossbeam, reinforcing bar, cable wire etc. can select for use train rail, steel pipe, shaped steel, reinforcing bar to mix material manufacture such as earth and suspension bridge cable wire; 3. the floating permanent magnet of magnetic can be selected the second generation or the manufacturing of third generation permanent magnet for use.---the active flight device, the universal manufactured materials driven or manpower flying device and various loop wheel machines of driven flight instruments and sucked type can be selected steel, aluminum alloy, silicon steel plate, rubber, epoxy resin, the second generation or third generation permanent magnet, enamel wire, insulating material, diamagnetic material manufacturings such as (bismuth metals) for use.---the principle of the light deflector of safe signal flasher and the omniscope of light signal amplifying apparatus and Submarine is same or similar, be by the light deflector that the two sides opposing parallel is installed in the metal case, wherein one side reflects as the light signal for the another side light deflector with light signal inclination 45 ° of receptions light signals and reflection; Because repeatedly weaken gradually just should be with the amplification of light signal once to 10 secondary reflections through 8 times for the reflected light signal, the structural principle of light signal amplifying apparatus is similar to light deflector, also be to receive the light signal and reflection carries out signal relatively for single board computer (SBC) (computer) by the one side and the light deflector of 45 ° of light source inclines, every frequency that meets is that the pointed pulse light signal of 50 or 60 He Zhi sends with regard to the instruction electroluminescent lamp and amplifies and identical light signal reflects as the safety light signal that amplifies by the another side light deflector.---the direct supply on the track both sides of driving and simulated flight device is to distribute each current consumer to use through the cable connection switch box by computer by wear-resisting carbon brush or rolling carbon brush or rolling metal wheel.---power supply is by wear-resisting carbon brush the cable reel that the direct supply on track both sides flows in the simulated flight device to be tightened up through two copper rings with carbon brush output for switch box by computer distribution use by clockwork spring by active flight device or driven flight instruments by a paired cable that scribbles extinction and look coating in the various simulated flight devices.---the manufactured materials of fleet-footed runner's project flight wing: 1. the skeleton of wing can be selected: the reed pipe manufacturing of corrosion-resistant steel, aluminum alloy or brass; 2. the valve material of wing and outer wing can be selected manufacturings such as nylon, plastics, canvas, rubber, leather, artificial leather, chemical fabric for use in.---the manufactured materials of the big top ceiling of no magnetic paramagnetic can be selected manufacturings such as corrosion-resistant steel, aluminum alloy, brass plate, glass-felt plastic, epoxy plate, alloy glass for use.

The various aircrafts of prior art, they all have some shortcomings that are difficult to overcome: 1, the technical risk of making is big, 2, cost is very high, 3, power plant all is engine petrol or snail fan jet supersonic plane, complex structure technical requirements height, the kind of fault is many, 4, must adorn sufficient gasoline during flight, 100～150% load carrying ability accounts for, 5, because burns gasoline produces serious pollution to atmosphere, damage the ozone layer, increase the calorific effect of weather, 6, administrative services division is various, strict, 7, the airport that the bigger landing of taking off is arranged, 8, the complicated investment of navigational facility and instrument is huge, 9, navigating mate requires high training difficulty big, and 10, if driving engine or other equipment is out of order or suffer the birds bump or meet the generation that change in weather etc. all might cause air crash; Various vehicles on the ground, many shortcomings that are difficult to overcome are also arranged: 1, driving engine all is engine petrol or diesel engine, manufacture difficulty is big, cost is high, fault is many, 2, exhaust pollution is serious, 3, the traffic congestion crowding phenomenon often takes place, 4, traffic accident often has generation, and 5, traffic route landed property resource is growing on and on.---several lightweight aircraft beneficial effects of the present invention are as follows: 1, the manufacturing technology difficulty of three types of lightweight aircraft of the present invention is little, implements easily.2, driving compares with the aircraft of identical passenger capacity, and cost can be reduced to 20～25% of identical passenger capacity airplane, that is to say, buys an airplane and can buy 4～5 drivings.3, engine installation all utilizes power supply, does not have exhaust pollution, need not load fuel, and the energy reduced volume improves load-carrying efficient.4, do not need huge taking off and landing station.5, do not need more administrative services division.6, do not need complicated navigationsystem and complex instrument instrument.7, the navigating mate training is simple.8, single track moves the phenomenon that can not block up.9, driving orbit construction expense is low, as rides the rail formula and be equivalent to 20～25% of train railway construction cost, and the floating underslung track of magnetic is equivalent to the construction cost 70～80% of train railway.10, be provided with the contingency that multiple safety measure can avoid strong wind, thunderstorm, dense fog, birds bump etc. to cause.11, engine installation etc. is out of order, and can rush to repair, and can not repair in the short period of time, goes to a back driving for help and is pushing away and continue flight.12, the air activity of simulated flight device and fleet-footed runner's type and specific safety device can increase desire and the interest that people yearn for the sky activity.13, various simulated flight devices and fleet-footed runner's project have following multiple use: (1) can be made the schoolaeroplane of aircrew's training and use, external form is all identical with genuine schoolaeroplane with interior type, also can reequip with genuine schoolaeroplane, as long as make engine petrol into the brush DC stepless speed-change motor, student's misoperation or can the fatal crass when other faults take place when the coach.Can reduce the training funds in addition, can also improve the quality of teaching and teaching process, shorten the teaching time limit.(2) can shoot, TV and taking a photo as a moment, can reach the effect of mixing the spurious with the genuine.(3) can be used as the utensil of sports, the sportsman is as by bike or as frogman's match of aloft circling in the air.(4) can be used as the stage property of artistic performance, perform various highly difficult flare maneuvers and thrilling action and performance of other art or the like.(5) can be used as the simulated flight facility of recreation, child adult can participate in and play.

Drawing explanation of the present invention:

The large-scale front elevation of riding rail formula driving of Fig. 1 a.

The medium-sized left view of riding rail formula driving of Fig. 1 b.

The small-sized top view of riding rail formula driving of Fig. 1 c.

The top view of the floating suspension type driving of the small-sized magnetic of Fig. 1 d.

The front elevation of the floating suspension type driving of the large-scale magnetic of Fig. 1 e.

Fig. 2 a rides the track scheme drawing and the driving state of flight scheme drawing of rail formula driving.

Floating suspension type driving track scheme drawing of Fig. 2 b magnetic and driving state of flight scheme drawing.

Fig. 3 a rides rail formula driving Package power scheme drawing, and left side figure is positive multilayer cutaway view, and right figure is that the multilayer cutaway view is looked on a left side.

Fig. 3 b magnetic floats suspension type engine installation scheme drawing, and left side figure is local multilayer cutaway view, and right figure is that cross sectional drawing is looked on a left side.

Fig. 4 a the picture left above is the wind-force rudder front elevation that contends with, and lower-left figure is a top view, and right figure is left pseudosection.

Fig. 4 b is the wind-force loadometer, and left figure is that figure is partly cutd open in the front, and right figure is left pseudosection.

Fig. 4 c is the cross sectional drawing of the floating underslung wind-force loadometer of magnetic.

Fig. 5 is the external form figure of simulated flight device, wherein scheming a is the simulation autogyro, figure b is the simulation jetliner, figure c is the simulation land-effect plane, and figure d simulates the water surface airship that can not sink, and figure e is the simulation inflation airship, figure f is the simulated flight balloon, figure g is simulation two flying saucers up and down, and figure h is the first top of a simulation flying saucer, and figure I is that simulation is speeded across the sky.

Fig. 6 a is simulation autogyro state of flight scheme drawing and orbital facilities scheme drawing thereof.

Fig. 6 b is simulation jetliner state of flight scheme drawing and orbital facilities scheme drawing thereof.

Fig. 6 c is that cross sectional drawing is looked on the left side that the simulated flight device is ridden rail formula active flight device.

Fig. 6 d is that cross sectional drawing is looked on the left side that simulated flight device six is taken turns suspension type active flight device.

Fig. 7 a is flying trapeze's assembly scheme drawing and driven flight instruments and steel cable cable-track facility scheme drawing.

Fig. 7 b is fleet-footed runner's bird's wing physical construction scheme drawing and contract wing and spread the wings view and air flow condition scheme drawing.

The last figure of Fig. 8 a is the contract wing and the view of spreading the wings of top view.

Fig. 8 b figure below is the contract wing and the view of spreading the wings of forward sight.

Fig. 8 c hangs bow and spreads the wings partial elevation view, and upwards lift at the wing rear portion when expression is spread the wings, and the component of existing rising also has the component that advances when pouncing on wing.

Fig. 8 d hangs bow and contracts the wing partial elevation view, and the wing rear portion when wing is contracted in expression dips down, and has finished the constitution diagram of the overall process of the wing that contracts.

Fig. 9 a is the overhead large-scale manipulator fleet-footed runner's state of flight scheme drawing freely that plays.

The left figure of Fig. 9 b is the partial front scheme drawing that hangs bow and horizontality flight, and right figure is the left pseudosection of horizontality.

The left figure of Fig. 9 c takes off or plumbness scheme drawing when landing.

The right figure of Fig. 9 c is the scheme drawing that the fleet-footed runner is in dive status.

The left figure of Figure 10 a expression fleet-footed runner from eyes in figure during direction flight the left wing of left side leg K/UP dip down right wing to the turnon left view of updip, right figure is the scheme drawing that right leg K/UP bends to right.

Figure 10 b is fleet-footed runner's loop wheel machine (being small winch) scheme drawing, and left side figure is the tandem loop wheel machine, and middle figure is parallel loop wheel machine, and right figure is built-in loop wheel machine.

Figure 10 c is the loop wheel machine fundamental diagram.

Figure 11 a is a clockwork spring type loop wheel machine scheme drawing.

Figure 11 b is a formula flight racing car scheme drawing by bike.

Figure 11 c pulls foot to step on formula flight racing car scheme drawing.

Figure 12 a is the universal driven flight instruments scheme drawing of sucked type.

Figure 12 b goes up to inhale the universal driven flight instruments scheme drawing of eclipsed form.

Figure 12 c is the aerial dodgem scheme drawing of sucked type.

Figure 13 a is the 3rd better simply scheme drawing of realizing example of fleet-footed runner's project.

Figure 13 b is the 4th of fleet-footed runner's project scheme drawing of embodiment preferably.

The embodiment of the invention by the accompanying drawing order auspicious one by one state as follows:

1 of Fig. 1 a-vertical boosting roller, 2-operator's compartment, the 3-front upper part wind-force rudder that contends with, 4-front vehicle wheel case, 5-wing, the 6-bottom wind-force rudder that contends with, 7-compartment, the 8-upper back wind-force rudder that contends with, 9-rear wheel case, 10-level is pushed roller.Fig. 1 a is the large-scale rail formula driving of riding, both sides can carrying 18～24 people, its external form is as aircraft, engine installation such as electric car, front-wheel works independently on the track of level for engine installation commonly used, starts working with the purpose that guarantees that flying speed does not subtract under the instruction of trailing wheel stand-by power unit at computer when going up a slope.Wing 5 is provided in a side of the bottom in compartment 7, its carrying driving 70～80% weight in flight course are still surplused and 20～30% are born by the driving track, and wing can alleviate track load, can guarantee to produce on wheel and the track thrust of relative motion again, to reach required flying speed.The bottom that wing 5 is located at compartment 7 also has an effect, it can make the springboard of passenger getting on/off, the top boosting roller 1 of driving is after commonly used and standby two engine installations all are out of order at the driving in this driving the place ahead, in the time of can not repairing in the short period of time, this driving just helps preceding pushing away its continuation flight.The steering unit of driving front upper place operator's compartment 2 more simply has only several knobs and a brake-applying handle, does not have traversing handwheel and lifting handle, and all the other facilities all are the computer automatically controlleds.When in the process of flight, meeting with the strong wind attack, wind-force contends with and makes instruction after rudder 3,6,8 is given the computer computing by each wind sensor and wind-force loadometer with the data delivery that is measured simultaneously, starts the transmission facility to power element and impels each wind-force rudder that contends with to pass suitable angle partially and reach the purpose of contending with.Front and back wheel case the 4, the 9th can also reduce the effect of air resistance with the fleetline shell in the time of the safe handling of protection wheel.The first half of vehicle body is as the head of aircraft, and latter half is as the afterbody of car, the top view shape some as airplane tail group but do not have empennage and yaw rudder.It is that the back driving of can seeking help when commonly used and standby two engine installations all are out of order when this driving is pushing away and continues flight that afterbody is pushed roller 10.---Fig. 1 b is the medium-sized rail formula driving of riding, specified carrying 8～12 people, external form and interior type are all same or similar with Fig. 1 a, 1 is that wing is similar to Fig. 1 a5 among the figure, 4.5～4.8 meters of the spanes, space, both sides, 2 compartment is the corridor, seat is near track, and 3 operator'ies compartment are provided with simply, and all the other all are the computer automatically controlleds except that several knobs and brake-applying handle, the seat of 4 operator'ies compartment, can both keep horizontality by the computer automatic guidance when the driving uphill/downhill, 5 are the top wind-force rudder that contends with, principle of work and Fig. 1 a3,6,8 is identical, 6 wheels (explanation is arranged in addition), 7 direct current planar motors (explanation is arranged in addition), 8 passenger seats, uphill/downhill all keep horizontality, around seat, be provided with the air expansion bag if the contingency accident that meets accident is expanded by computer instruction, can reduce personal casualty, the 9th, following rail near wheel, it can guarantee that the driving smooth flight also can prevent the effect of lifting on the driving, the 10 bottom wind-force rudder that contends with is with Fig. 1 a3,6,8 is identical.---Fig. 1 c is the small-sized rail formula driving of riding, specified carrying 4～6 people, external form and interior type and Fig. 1 a, Fig. 1 b is similar, 1 operator's compartment and Fig. 1 a2 among the figure, Fig. 1 b3 is identical, wind power balance rudder before 2 wings, it can make instruction through the data that wind-force loadometer is up and down measured to vertically wind-force after computer is handled, the corresponding angle of deflection up or down reaches the purpose with wind power balance, and reacting when it is also to uphill/downhill in addition reaches suitable stabilized flight, and 3 wing sweepback, 15～20 degree spanes are similar to Fig. 1 b1, wind power balance rudder behind 4 wings, rudder is identical before function and the wing, 5 wind-force contend with rudder and Fig. 1 a3,6,8 is identical, and 6 vertical boosting rollers are identical with Fig. 1 a1,7 passengers pass in and out window, 8 compartments are similar to Fig. 1 a7, and 9 levels are pushed roller, and are identical with Fig. 1 a10.---Fig. 1 d is the floating suspension type driving of small-sized magnetic, specified carrying 4～6 people, and its external form and interior type be all as aircraft, 1 among the figure, 2,3,4,5,1,2,3,4,5 same or similar with Fig. 1 c, wing sweepback 40～45 degree, 3～3.5 meters of the spanes.Fig. 1 d 6,10 to Fig. 1 a 1,10, Fig. 1 c 6,9 similar.7 of Fig. 1 d is the floating underslung flight dynamic devices (auspicious stating arranged in addition) of magnetic, and the stream line pattern in 8 compartments is identical with the fuselage of aircraft, the 9 afterbody wind-force rudder that contends with, the also usefulness of double yaw rudder simultaneously.---Fig. 1 e is the floating suspension type driving of large-scale magnetic, specified carrying 18～24 people, its external form is all similar to aircraft with interior type, among the figure 1,9 and Fig. 1 a1,10 is similar, 2, operator's compartment is identical with Fig. 1 a2, wind-force contend with rudder and Fig. 1 a3,6,8 identical about in the of 3,6,4, wing is identical with Fig. 1 a5,5, the flight dynamic devices (auspicious stating arranged in addition) of the floating suspension type driving of magnetic, 7, the compartment is similar to Fig. 1 a7, and is identical with the fuselage of aircraft, and 8, the afterbody wind-force rudder that contends with is identical with Fig. 1 d9.---Fig. 2 a is the scheme drawing of riding rail formula driving and orbital facilities thereof, this track is low latitude (overhead) monorail design scheme, 5, being last rail, is the carrying driving in 20～30% weight in when flight, and this weight is that wheel produces the propulsion source that enough thrust is offset air resistance during to the track relative motion.6, being following rail, is to strengthen the rigid track of going up the rail bearing loading capability, plays the effect of driving smooth flight.2, be column, highly general 8～10 meters, the highlyest should not surpass 36 meters, minimumly should not be less than 5 meters, column be spaced apart 6 meters, greater than 6 meters corresponding raisings of cost, maximum span should not be greater than 1000 meters.The degree of depth that is embedded under ground portion is 1/4～1/6 of a length overall.4, being the diagonal brace reinforcing bar, is the load-carrying capacity that strengthens track.9, be the reinforcing diagonal brace reinforcing bar of large span.10,12 is the oblique rollering steel muscle, is the weight of holding the orbit centre part, the 13, the 14th, and middle holder support reinforcing bar.15, be that track connects the support shelves up and down.3, for riding the state of flight that rail formula driving is in climbing, 8, driving is in level flight condition, 11, the expression location that should not set up column, as: ditch, river, low ebb, drift sand, marsh, straits etc.1. being natural slope, 7. is flat-bottomed landes.---Fig. 2 b is the floating suspension type driving roundtrip trajectory design diagram of magnetic, this figure is the double track round arranged side by side of low latitude (overhead) single track gantry frame type, be the design plan of selecting by one section comprehensive distance of Plain, cross a river, climbing: this figure is general high 10～15 meters at the gantry pillar 1 of flat-bottomed land, the highest should not be above 50 meters, minimumly should not be less than 7 meters, be spaced apart 6 meters.If span is greater than more than 1000 meters, cost is greater than conventional 4～5 times.The length of crossbeam 2: small-sized driving track is 7～8 meters, and medium-sized is 9～10 meters, and large-scale is 11～12 meters.Suspention reinforcing bar 3 can be fixed on crossbeam and the rail with sieve bolt.Coming and going magnetic levitation track 4 (specific design has auspicious stating in addition), to increase column 5 be to determine the data of increasing according to the size of span, general desirable span 2～5% as the data of increasing.Additional column 6 height and crossbeam become the angles design of 6～8 degree quite or a little more than crossbeam by the extended line of crossbeam.Can calculate by 5～10% of span with the distance of gantry upright post.The horizontal cable wire 7 that draws of superiors is the stability that column is increased in protection, and the floating driving 8 of magnetic is the states that fly to the destination stop direction, and the floating driving 9 of magnetic is state of flights of being returned by the destination stop direction.Oblique rollering steel rope 10 is the stability that column is increased in protection.Ground oblique rollering steel rope the 11, the 12nd, the additional column tension effect of protection.Two cable wires 13 are by tiltedly hanging reinforcing bar 15 main beam transverse 14 that plays, play by suspention reinforcing bar 3 and come and go track 4, guaranteeing to come and go the stability that rail 4 keeps horizontalitys about the superiors.Haul two hyp cable wires 16 of level draws reinforcing bar 17 to strain at main beam transverse 14 to guarantee to come and go magnetic levitation track 4 and do not produce double swerve by horizontal on the top of 4 additional columns 6.Oblique rollering steel rope 18 is the tension force that guarantees two cable wires 13 about the superiors, and mountain valley 19 is that magnetic levitation track is by minimum part.Mountain top 20 is the barriers that should not set up magnetic levitation track.River 21 is the locations that should not set up portal frame.---engine installation Fig. 3 a of riding rail formula driving be the permanent magnet 5 that is embedded with 15～25 odd numbers on the wheel that is contained by a metal case 1 with wheel both sides stator 10 on be embedded with the winding 6 of 12～24 even numbers, be the engine installation of the direct current planar motor of rotor and form as driving with the wheel.2 of Fig. 3 a is wheel edges of wheel, and it is the barrier of not overstepping the limit when guaranteeing wheel and 12 relative motions of last track, and wheel rim 3 is to produce friction with last track 12 pushing away the propulsion source of driving flight.Spoke 4 be the space of embedding permanent magnet 5 at interval.The center internal diameter that ball bearing of main shaft 7 external diameters are fixed on stator 10 is with the axle core effect that center shaft 9 is realized wheel and stator 10 relative rotary motion.Wheel hub 8 outside with spoke 4 casts solid, interior and center shaft 9 close-fittings play the effect concentric with wheel rim 3.The copper strips 11 of direct supply is that to be embedded in the interior chamfered groove of T type track of rail 12 with track be non-conductive.Track is parallel about connecting support shelves 13 and track must keeping with sieve bolt is fixing up and down.Following rail 14 can also can weld with sieve bolt is fixing with column 15.N represents that arctic S represents the South Pole among the figure.Also can design various brush DC stepless speed-change motors according to the principle of riding rail formula engine installation, its structure is to be embedded in permanent magnet by the groove that the rotor of aluminum alloy is cut 15～25 odd numbers, one end all is that the N utmost point other end all is the S utmost point, stator is divided into former and later two identical windings that is embedded with 12～24 even numbers, the interval width of each winding equates with the winding width, and each at interval in diamagnetic material of embedding, the direction of current of a stator is all identical, and another is all opposite, by shell, front and rear cover and cooling fan and outer cover are formed the brush DC stepless speed-change motor.---engine installation Fig. 3 b of the floating suspension type driving of magnetic, be that 12～36 magnetic floated power splits are installed in the long and soft shell 7, establish 3～4 C type permanent magnets 1 in each split and be sleeved on the both sides of the upper strata permanent magnet 4 of magnetic levitation track 3, the identical state that repels each other that is in of polarity does not produce the friction phenomenon when guaranteeing both relative motions.Also identical the repelling each other of polarity of C type magnet 1 and lower floor's permanent magnet 5 of magnetic levitation track 3, the effect that produces come-up, the weight that can carry the static or low-speed motion of the floating driving of magnetic.It is corresponding with lower floor permanent magnet 5 to embed the stator of a pair of DC linear electric motor and winding 2 in the interval of two C type magnet 1.Establish 2～3 pairs of stator winding and permanent magnet 5 composition DC linear electric motor in the floating split of each magnetic, one side direction of current of this stator winding is all identical, and another side is all opposite.The current field after stator winding 2 energisings and the magnetic field of permanent magnet 5 produce an electro-motive force, and promptly the direction straight line high-speed motion by right hand theorem indication can reach the purpose that promotes the floating driving flight of magnetic.Permanent magnet 6 be fixed in the abdomen of C type magnet 1 be guarantee the magnetic floated power device can not on the effect of lifting.Hanging axis 8 is by the bearing 9 floating driving of static magnetic that plays, before and after this hanging axis totally two, account at interval the floating device length overall of magnetic 2/3～3/5 between, can left-right rotation a little angle.Direct supply copper strips 10 is installed in the both sides of magnetic levitation track bottom, with track be non-conductive.N represents that arctic S represents the South Pole among the figure.---Fig. 4 a is the wind-force rudder assembly scheme drawing that contends with: the picture left above is a front section view, and lower-left figure is a top view, and right figure is horizontal section left view.Its principle of work is: when windless condition, the handle of wind sensor and the wing are by the direction of driving flight hang behind as the crow flies.When wind-force, the wing of wind sensor and handle are pressed the corresponding angle of big primary deflector of wind-force.Suppose: the flying speed of driving is 200 kilometers/hour, and folding second speed is 55.6 meter per seconds, if laterally wind speed is 10 meter per seconds, and the angle a=10 meter per second of wind sensor deflection so: 10 ° 10 ' of 55.6 meter per second=tg α.When wind sensor deflection 10 is spent 10 fens, wind-force rudder and then deflection 10 degree 10 minutes in time that contend with, but can not reach the effect that contends with, in this rudder kick, difference of pressure has appearred in the loadometer on track both sides, computer is made the instruction that continues deflection according to the total data of sensor and loadometer after treatment.When reaching certain angle, when the loadometer difference of pressure on track both sides reverts to zero, just realize the purpose of contending with, computer is also just in time cancelled the instruction of continuation deflection.Among the figure 1 is the wind-force rudder fleetline shell that contends with, and the wing of wind sensor and handle 2 reflect the light that light source 12 is sent to photoelectricity nest of tubes 9 with lower end light deflector 11 by center shaft 4 along with wind-force deflection.Change the light signal into little electric current immediately and flow to computer after certain electro-optical tubes receives reflection source, computer is made instruction according to all data and is flowed to power element starter motor 13 transmission worm screws 8 and promote fan type worm gears 10 twisting hollow shafts 5 and reach the purpose of contending with by rudder hub 3 with the corresponding angle of rudder shell 1 deflection of contending with.Among the figure 6 is the contend with hollow support seat of rudder of wind-force, 7 plain bearings for the rudder that contends with.---Fig. 4 b is the scheme drawing of wind-force loadometer: left side figure is that figure is partly cutd open in the front, and right figure is left pseudosection.Its principle of work is according to the relation of the relative variation with pressure of aerodynamic gas flow rate and design-calculated, and gas flow rate is big more, and the pressure of gas is more little; Flow velocity is more little, and pressure is big more.Therefore this loadometer can be installed in each place relevant with gas flow rate, particularly be positioned on two sides of track and the side play of track and stay 1～2m/m, the flow velocity that reduces gas when the gap strengthens, and the gap increase flow velocity reduces, and the side pressure instrument on both sides will produce difference of pressure like this.Among the figure 1 is metal case, the 2nd, and the framework of pressure measurement film, the 3rd, pressure measurement film, the 4th, metal pressure transmission sheet, the 5th, piezoceramic, the 6th, base plate, the 7th, air pressure reacting hole.When driving awing the wind-force on certain limit driving is pressed to another side, the difference of gap length has appearred in the loadometer on these both sides, the pressure of one side loadometer that the gap is little reduces, the big one side pressure in gap increases, so produced difference of pressure, one side that pressure is big, pressure measurement film 3 increases by the pressure of 4 pairs of piezoceramics 5 of sheetmetal, little electric current just increases, and the little electric current in one side that pressure reduces just reduces, so computer is just made corresponding instruction according to the variation of the little electric current in both sides.---Fig. 4 c is the wind-force loadometer of the floating suspension type driving engine installation of magnetic, this wind-force loadometer is to be contained in the interval of two C type permanent magnets of this device, corresponding with the upper strata permanent magnet 2 of magnetic levitation track 1, the identical state that repels each other that is in of the permanent magnet 5 of loadometer with the polarity of permanent magnet 2, and give piezoceramic 4 with transmission of pressure, because piezoceramic 4 is to be fixed on the cushion block 3 to make a concession, piezoceramic 4 is pressurized all the time.Because the gap of the loadometer of magnet 2 the right and lefts equates, so little electric current of the piezoceramic on both sides equates that difference of pressure equals zero.Attack when certain runs into wind-force on one side, variation has taken place in the gap of the loadometer on both sides and permanent magnet 2, because the effect that repels each other of the permanent magnet 5 of both sides loadometer has produced difference of pressure, the variation of the little electric current of both sides piezoceramic makes computer make corresponding instruction.The pressure measurement effect does not take place in the lower floor's permanent magnet 6 and the loadometer of magnetic levitation track 1.N represents that arctic S represents the South Pole among the figure.---the simulated flight device is that the simulated flight device with various characteristics that plays with steel wire (rope) that scribbles extinction and look coating or carbon fibre line under light-duty active flight device of low latitude (overhead) single track or driven flight instruments is imitated flight.These simulated flight devices are as shown in Figure 5: a is the simulation autogyro among the figure, its external form and genuine autogyro do not have difference, its engine installation is not an engine petrol, but brush DC stepless variable-speed motor, and this power of electric motor is quite little, only as symbolic rotation, flight is main to drive flight by the active flight device on the track.If power of electric motor has own flight performance quite greatly, can adopt driven flight instruments on the track so.The active flight device is the same with driven flight instruments from external form.Difference is that driven flight instruments does not have direct current planar motor etc., but it also can be used as the flight instruments of traction flight formula, the mode of traction is the winch of end peace at track, pulley of other end peace just can come and go and draw, and also can drag train to fly as locomotive engine at many driven flight instrumentses in last active flight device traction back.The messenger wire of simulated flight generally all adopts the two-wire hanging otherwise the heading of the simulated flight device that quilt is hung is wanted entanglement.The two-wire hanging is a line in fact, and this line is the U font in aircraft, just in case this line is fractureed, equaling two lines has all fractureed, aircraft can fill up foamed materials or rubber air bag on ground in addition by the glide soft landing, or draws an elastic network(s) can guarantee personal security.Loop wheel machine can be with one or two, also can be on a loop wheel machine two ends respectively pacify a cylinder and sling simultaneously in two respectively.---Fig. 5 b is the simulation jetliner, and the external form of this machine is similar with genuine jetliner, and snail fan jet supersonic plane changes the brush DC stepless speed-change motor into, and all the other contents are identical with the simulation helicopter.---Fig. 5 c is the simulation land-effect plane, and the bottom of this machine is as the structure of ship, and top is similar to aircraft, and 8 jet engines of front portion and jet supersonic plane of tail vane are all used instead the brush DC stepless variable-speed motor, takes off and can aloft fly at the water surface.---Fig. 5 d is the mimetic surface airship, and it can be at water surface flying, but dried up is had only 300～500m/m.---Fig. 5 e, f are that the model configuration of dirigible and flight balloon also is to fly under track.---Fig. 5 g and h are the simulation flying saucers, play for children, edify science fiction.---Fig. 5 I is that simulation is speeded across the sky, and tool is rich in mythological flavor can take a photo as a moment for the lover, for the science fiction imagination of children, and artistic performance, the TV etc. of shooting.---the orbital facilities scheme of simulated flight device is shown in Fig. 6 a, b: Fig. 6 a is a T type track column, the roundtrip trajectory of simulated flight device is located at the two ends of T type crossbeam, by the active flight device, or driven flight instruments, the simulated flight device that plays following is imitated flight.The track column of Fig. 6 a1, T type, height are 10～12 meters, 2, crossbeam is long 5～6 meters, 3, the simulation autogyro, or other simulated flight devices, 4, active flight device or driven flight instruments, 5, go up track, 6, lower vehicle track, 7, the track that returns.---Fig. 6 b is the suspention track of gantry frame type, among the figure 1, be the column of portal frame, height is 10～12 meters, 2, crossbeam, and long 6～12 meters, 3, suspension type track, be inverted T shape, 4, the simulation jetliner, 5, active flight device or driven flight instruments, 6, scribble the messenger wire of extinction and look coating, 7, the track that returns.---Fig. 6 c is the cross sectional drawing of active flight device, and driven flight instruments is not established direct current planar motor, among the figure 1, the crossbeam of T type column, 2, be to go up track, 3, be C type shell, 4, be dynamic wheel, similar to the car wheel structure of Fig. 3 a, principle is identical, not embedding of driven wheel permanent magnet.5, direct current planar motor, similar to the planar motor of Fig. 3 a, principle is identical.6, prevent to lift roller, 7, messenger wire.---Fig. 6 d six takes turns suspension type active flight device, or six take turns the suspention driven flight instruments cross sectional drawing, this device is to be enclosed within on the track of Fig. 6 b inverted T shape, be provided with two wheels 2 in the both sides of inverted T shape track 4, the same permanent magnet that is embedded with of this wheel with Fig. 3 a, be provided with direct current planar motor 1 in the outside of wheel, identical with the planar motor of Fig. 3 a, below inverted T shape track 4, be provided with upper pressure wheel 5 and be the sporting flying that produces this engine installation of powered when the bottom that is pressed on track 4 can make wheel 2 runnings.3 is six to take turns suspension type active flight crust of the device, the 6th, messenger wire.---the flying trapeze is shown in Fig. 7 a: this project is to put on the aircraft that is equipped with as the bird's wing wing on people's health, light-duty driven flight instruments 2 on low latitude (overhead) single track 1, loop wheel machine 5 of last installation, by messenger wire 6 and rolling shackle 19, suspension ring 18 hang bow 7, hang play aircraft parking stand 20 and fleet-footed runner's 95～98% weight of bow fulcrum 17, but can not sling, 2～5% the weight of still surplusing is pounced on wing by the fleet-footed runner and just can be risen to the sky and aloft freely circle in the air up and down.The skyborne state of flight of fleet-footed runner is controlled by two legs, when the fleet-footed runner rise to aerial after as long as break into two legs off with the fingers and thumb the A font, control band 24 on leg, pulling stay cord (being the bicycle brake stay cord) makes aircraft parking stand 20 and hangs bow 7 and pulls into horizontality, if it is chevron shaped that two legs are broken off with the fingers and thumb into, stay cord pulls on and hangs bow and 7 make aircraft parking stand 20 pull into the state of downward underriding.If need only when wanting turnon left with left leg K/UP, the control band 25 pulling stay cords of a left side on the leg make rolling shackle 19 pull to the right and hang bow 7 places and make left wing 13 downward-sloping, right wing is inclined upwardly, because left leg K/UP has increased the air resistance on the left side, has therefore just realized the purpose of turnon left.If want right-hand corner to need only with right leg K/UP, opposite with the process of turnon left, just can realize the purpose of right-hand corner.The motion of the wing of aircraft is can make wing make the action of various flights by fleet-footed runner's the two-hand control control stalk 15 gimbal suspension 14 transmission the right and left connecting rods 9 and 10 by both sides, the fleet-footed runner is if push away control stalk to cephalad direction, two wings just draw in, if control stalk is pulled to belly, two wings just launch, if control stalk is pushed away human body, two wings are just pounced on wing downwards, if only one side is pushed away human body pounces on wing with regard to a wing, if control stalk is made various variation, wing is also just followed different motions.3 of Fig. 7 a is driven wheels; 4 lift wheel on anti-; 8 wing updips and the fulcrum that has a down dip; the control fulcrum that 11 wings draw in or launch; the back skeleton of 12 outer wings 13 and 11 is one, the commissure that 16 wings are fluttered up and down, the axle that 21 wings are fluttered up and down; the connecting band of 22 seat cushions and shoulder belt, 23 seat cushion bandages can make fleet-footed runner and flight support fuse.---Fig. 7 b is the structural representation of fleet-footed runner's wing: the wing on this figure left side is in rounding state, and the wing on the right is in deployed condition.Its principle of work is an one by control stalk 18,19 in fact, the 18th, be in the position that top folds its wings, the 19th, be in the position that the bottom stretches open wings, upwards shifting 18 position onto when control stalk is that wing 6 and outer wing 7 common skeleton upper joints 1 be the garden heart to control joint 5 by control joint 5 drivening rods 15 of gimbal suspension 3 by connecting rod 4 pulling companding wings with center fixation fulcrum 16 simultaneously are that the path of motion of a camber of radius work reaches the purpose that folds its wings in gimbal suspension 3 promotes by connecting rod 2; When control stalk is moved 19 position downwards to, be through gimbal suspension 22 by connecting rod 23 pullings in joint 24 on the common skeleton of wing 9 and outer wing 10, be the first heart by control joint 20 drivening rods 17 that connecting rod 21 promotes the companding wings with center fixation fulcrum 16 by gimbal suspension 22 simultaneously, is that the path of motion of a camber of radius work reaches the purpose that stretches open wings with control joint 20.In the A-A section-drawing of wing 9, the 14th, the kq air flows into fleet-footed runner's direction of bottom when pouncing on the wing from the top of valve, valve is closed and is produced the power that advances and rise when pouncing on down.The B-B section 11,12,13 of outer wing 10 is the same with A-A section-drawing principle, and valve is opened the kq air as 11 and flowed to fleet-footed runner's direction as 12 curve arrow when pouncing on the outer wing, and valve is closed as 13 and produced the power that advances and rise when pouncing under the outer wing.Valve 11,13 can play the feather effect with the birds wing, the 25th, valve schematic layout pattern.The 8th, the bed plate of fixed pivot 16.4 stains of---Fig. 8 ab is fleet-footed runner's wing structural representation: 1 of Fig. 8 a, b---curve indication are the expression-form of same outer wing outer skeleton in different conditions and different visual angles in fact, 2---4 stains of curve represent outer wing forward position skeleton.3---4 stains represent the back of outer wing along skeleton, 4---represent outer wing and the common skeleton of interior wing, the outer wing that these 4 skeletons are formed is the inclined ladder type form that can be out of shape, and Fig. 8 a represents spreading the wings of top view and receive the aliform attitude, and Fig. 8 b represents that forward sight spreads the wings and receive the aliform attitude.Because hind wing is to updip when spreading the wings, hind wing dips down when receiving wing, so the front elevation of Fig. 8 b is spread the wings behind the state along skeleton in the above, the forward position skeleton is received aliform attitude forward position bone in the above below, and the back along bone below, 5---the little garden circle of curve indication represent all Xiao Yuanquan be the joint of activity, 6---two lines of indication are the anchor shafts that wing is fluttered, 7---be the bearing that wing is fluttered, 8---be the central pivot point of wing fixed control of taking down the exhibits.9---4 stains of indication be about the two wings control link of taking down the exhibits, its motion is to be the garden heart with 8 central pivot point, is the camber path of motion of radius with the dotted line.10---be in the forward position skeleton of wing, 11---in the wing of lining along skeleton, 12---lining wing back along skeleton, 4---be in wing and the common skeleton of outer wing, the modification form that the parallel 4 limit types of 10,11,12 and 4 one of being formed of lining wing can draw in and launch.A-A represents it is the section schematic symbols of Fig. 8 C among the figure, B-B presentation graphs 8d section schematic symbols.---Fig. 8 C is the A-A cutaway view of Fig. 8 a, and this figure mainly expresses Fig. 8 a when spreading the wings, the acclivitous signal form of hind wing.Among the figure 1---hang bow,, flight instruments is rotated around fulcrum by lower fulcrum 3,4---shoulder belt is that the fleet-footed runner is tied up on support, 5---the flight instruments support, 6---connecting band is that shoulder belt and seat cushion are linked into an integrated entity securely, 7---fleet-footed runner's seat cushion is similar with bicycle saddle cushion, 8---the lining wing, 9---outer wing, lining wing 8 and outer wing 9 are to be the rotation that has a down dip on the center with fulcrum 2, this figure is the angle of updip maximum, is 15 degree.---Fig. 8 d is the B-B cutaway view of Fig. 8 b, the downward-sloping signal form of hind wing when this figure mainly expresses Fig. 8 b receipts wing, among the figure 1---the lining wing, 2---be in the central pivot point of wing and outer wing, 3---outer wing, in wing 1 and outer wing 3 be the rotation that has a down dip on the center with fulcrum 2, this figure is that the have a down dip angle of maximum is 15 to spend.---Fig. 9 a is second of flying trapeze's project embodiment preferably, and the wing of flight instruments and steering unit are all constant, just the light-duty orbital facilities in low latitude (overhead) is changed over the lifting facility of large-scale overhead manipulator.This facility circles in the air for fleet-footed runner's freedom in manipulator revolves the space of three-sixth turn up and down, and is more much bigger than the degree of freedom of orbital facilities.The flier device of orbital facilities is suitable for the event of sports is advisable, and the flier device of manipulator facility is suitable for artistic performance, multiple uses such as recreation and sports performance.Among the figure 1---balance is hung down, and is balancing machine hand and fleet-footed runner's weight, and 2---radial bearing, be to alleviate the friction that manipulator rotates, 3---radial thrust bearing, it is the resistance that alleviates rotation, also be the carrying manipulator, balance is hung down and is reached the thrust baring of fleet-footed runner's weight.4---column is high 30～40 meters.5---the lining manipulator, 6---radial thrust bearing, similar to 3,7---radial bearing, similar to 2,8---outer manipulator, 9---the fleet-footed runner is in dive status, and 10---loop wheel machine, (explanation is arranged in addition).---Fig. 9 b is fleet-footed runner's support and hangs bow, the functional schematic of suspension ring etc., among the figure 1---the roller shackle, go up and be connected securely with messenger wire, horizontal Xiao in bottom goes up roller 10 of peace, this take turns below suspension ring 11 can about roll, the suspension ring radian is to be the garden heart with center of gravity 9, suspension ring are radius, and the camber of being drawn by the R arrow is as the criterion, by fulcrum 2 with hang bow 3 and form one, hanging bow 3 bottom fulcrums 5 is supports 7 of supporting fleet-footed runner, this support is to be that the garden heart can be made suitable rotation, 4 on demand with supporting-point 5---be the supporting-point of wing, and can be by the effect wing of joystick in the rotations that make 15 degree that have a down dip on the supporting- point 4,6---be shoulder belt, 8---be seat cushion.---Fig. 9 C is the functional schematic of Fig. 9 b7 fleet-footed runner support, and when the fleet-footed runner takes off or lands, fleet-footed runner's support all is in the CZ plumbness.When the fleet-footed runner is liftoff soar after, as long as break into two legs off with the fingers and thumb the A font, fleet-footed runner's support just is in the horizontality of Fig. 9 b7, chevron shaped if the fleet-footed runner breaks into two legs off with the fingers and thumb, fleet-footed runner's support just becomes the dive status of fc, general downward-sloping 45 degree, maximum should not surpass 60 degree.The 3rd, hang bow, the 7th, support.---Figure 10 a is the functional schematic of Fig. 9 b fleet-footed runner suspension ring 11 and roller shackle 1 and 10, suspension ring 11 are to be that garden heart R is the garden camber of radius with center of gravity 9, when needing turnon left, the fleet-footed runner needs only left leg K/UP, effect by band and stay cord is hung bow 3 real turnon lefts with what roller shackle 1 roller 10 pulled to the right, if need only right leg K/UP when needing right-hand corner, by band and stay cord the bow 3 that hangs that roller shackle 1 roller 10 pulls to the left side is realized right-hand corner, generally between the 20-30 degree, maximum should not surpass 45 degree at the angle of inclination of turning about aircraft.---Figure 10 b is the loop wheel machine scheme drawing of fleet-footed runner's facility, and loop wheel machine 1 is serially connected, and it is the frame mode of directly being contacted by decelerator and loop wheel machine cylinder, and its feature is, and is simple in structure, bulky.Loop wheel machine 2 is parallel connection types, it be by reducing motor by gear or belt-driving loop wheel machine cylinder, complex structure some, contraction in length half.Loop wheel machine 3 is built-in, and it is to be installed in cylinder inside by reducing motor, structure more complicated, but one times of volume-diminished, and three kinds of loop wheel machines can be selected for use arbitrarily.---Figure 10 c is a loop wheel machine principle of work scheme drawing, and its principle of work is: after the fleet-footed runner puts on flight instruments, and energized, loop wheel machine is started working.Because the weight of fleet-footed runner and flight instruments 100% is played by messenger wire 10, loop wheel machine 4 is by base 3, commissure 2, horizontal Xiao 5, sieve bolt 6, spring perch 8, compression spring 7, because the compression of spring 7, impel freight weight limit switch 9 to cut off the electricity supply, 4 moments of loop wheel machine temporarily quit work, if the fleet-footed runner pounces on wing and alleviates 5～10% weight, the weight saving of messenger wire at this moment, spring 7 resets, by spring perch 8, sieve bolt 6, horizontal Xiao 5, commissure 2, footstock 3 is lifted to the freight weight limit position of work with loop wheel machine, and loop wheel machine is started working, and the fleet-footed runner is sling, the time that the fleet-footed runner pounces on the wing expendable weight is very short, generally can only continue for 1～2 second and will recover original 100% weight, the fleet-footed runner constantly pounces on wing and just can constantly rise if then pouncing on wing more for the second time in 1～2 second can then rise again, but when rising to upper limit (UL), limit Cheng Kaiguan cuts off the electricity supply and just can not raise again, if do not pounce on wing in 1～2 second, because weight goes back up to 100%, spring 7 is compressed, the freight weight limit switch cut off the electricity supply the fleet-footed runner just begin the landing.Figure 10 C1 is the base of driven flight instruments or the outer arm of manipulator.---Figure 11 a is second better implement example of flying trapeze's project loop wheel machine, this embodiment is that the loop wheel machine in fleet-footed runner's project utilizes clockwork spring (promptly and clock and watch, the clockwork spring of rolling door is similar) power that promotes as loop wheel machine, it neither needs power supply, there is not complicated control system yet, its principle of work is: in advance clockwork spring 5 is tightened, can play 95～98% weight of fleet-footed runner and flight instruments, but can not sling, treat that the fleet-footed runner pounces on after the wing, when having alleviated 5～10% weight, clockwork spring 5 begins to flick immediately, drive inner gear 8 (inner gear 8 is one with clockwork spring tube 4) transmission small planetary gear 11 by clockwork spring tube 4 and drive mafor planet gear 12 in parallel, reach the miniature gears 10 on the center shaft, because center shaft 6 is fixed, so central pinion 10 also is fixed, so planetary wheel 12 can only be around miniature gears 10 rotations, drive messenger wire cylinder 3 by planet circular system 9 and rotate, reach the fleet-footed runner's that slings purpose.The footstock of 1 among the figure---loop wheel machine, 2---the support of loop wheel machine, 7---the isolation bearings plate of clockwork spring tube.---Figure 11 b is the flight racing car of aerial sports, its external form is as aircraft, front wing 6 and rear wing 14 are arranged, sportsman 7 is as by bike, drive acceleration chain wheel 10 by sprocket wheel 8 chains 9, this acceleration chain wheel is in positive center, and both sides two hinge wheels 11 in parallel drive the purpose that wheels 2 in parallel high speed revolution on track 1 reaches racing car flight by the chain 12 transmissions acceleration chain wheel second time 5.Among the figure 3---be contact roller upwards, be to guarantee that track 1 top 4 wheels 2 are non-slip in the running, reach racing car 13 purpose of flight fast and can produce enough thrust, 4---be six to take turns suspension type manpower flying device's support, six power wheels of inner installation fuse with flight racing car 13 usefulness sieve bolts below.---Figure 11 c is paddle-type air flight racing car, this car adopts six to take turns the driven flight instruments 2 of suspension type, similar to Figure 11 b, be enclosed within above the inverted T shape track 1, the device of a similar aerodone of suspention below driven flight instruments 2, this device has front wing 18, rear wing 11, the upper limb 5 common buoyancy that circle in the air that produce.The bottom have framework 20 respectively with front wing 18, rear wing 11, suspension bracket 13 upper plates 6, upper limb 5 fuse, sportsman 22 crawls volt among cushion 7 up and down, ties up securely on upper plate 6 by bandage 12.Sportsman 22 both hands are to hold the joystick that is played by messenger wire 17, press the orbiting motion of camber dotted lines below the messenger wire 17, and both legs are played by band 10 by messenger wire 8, press the orbiting motion of messenger wire 8 following camber dotted lines, and both feet are to be through in the power shoe 9 that pin steps on.The flight theory of this racing car is by sportsman's 22 hand legs and uses; with the mode of motion that draws in or stretch this flight instruments is flown trippingly; when sportsman 22 both hands and both legs move in the mode of drawing in simultaneously; effect by stay cord or connecting rod makes thrust paddle 19; 21 and 23 all pull to the motion in the place ahead simultaneously; because the drag effect of air; push close up the two slit bamboo or chopped wood flaps up and down of all thrust paddles to state; as thrust paddle 19 and 16 represented states; when sportsman 22 both hands and both legs stretch simultaneously; effect by stay cord or connecting rod is with thrust paddle 19; 21 and 23 pull to the rear moves; because the drag effect of air two slit bamboo or chopped wood flaps is up and down pushed open as thrust paddle 21; state shown in 23 and 24; quick travel promotes air backward because thrust paddle launches backward; and produce a proal thrust; promoting this racing car flies forward; if the sportsman constantly steps on dynamicthrust oar 19 backward; 21 and 23; this flight racing car is constantly flight forward just; firmly big more; the speed of stepping on is fast more; the flying speed of racing car is also just fast more, then slow on the contrary.Among the figure 3---be 4 flower wheels in top of driven flight instruments, 4---be the flower wheel of bottom, 14---be the expression of athletic bimanual movements state, top wrist-watch shows the position of extended configuration, following wrist-watch shows the position of rounding state, 15---be the expression of athletic both legs state of kinematic motion, top sole represents it is the position of extended configuration, and following sole represents it is the position of rounding state.---Figure 12 a is the 3rd a better implement example of the indoor flight of flying trapeze's project: this embodiment installs below the large-scale iron plate 1 with permanent magnet 7 these iron plates of attraction on indoor high top ceiling more than 8 meters and is fixed on the universal driven flight instruments base plate 8, this universal driven flight instruments is by cardan wheel 2 and universal crab claw axle 3, radial thrust bearing 9 and 4 is formed on the cardan wheel assembly that can 360 degree the rotates chassis 8 that four are fixedly mounted in driven flight instruments totally, the fleet-footed runner is played and Fig. 7 a by loop wheel machine 6 messenger wires 5, Fig. 9 a, Figure 10 c is same or similar, and the degree of freedom that the fleet-footed runner flies below is bigger.N among the figure represents the arctic of permanent magnet, and S represents the South Pole.---Figure 12 b is another embodiment of the indoor flight of flying trapeze's project, principle and the function of this embodiment and Figure 12 a are same or similar, difference is that top ceiling 6 is not with iron plate and with other no magnetic paramagnetic material manufacturings, its feature is to establish take over a business 1 time that a universal driven flight instruments and mounting permanent magnet 2 are fixed on this device on top ceiling 6, attract below the top ceiling 6 a universal driven flight instruments take over a business iron plate 5, two universal driven flight instrumentses are by cardan wheel assembly 3 up and down, 4 realizations are universal driven, identical with the universal driven principle of Figure 12 a, among the figure 7-be loop wheel machine, 8-be messenger wire, N represents that arctic S represents the South Pole.---Figure 12 c is that the principle according to the universal driven flight instruments of fleet-footed runner's project implementation illustration 12a develops into universal human-powered flight's aerial dodgem, this car is by being fixed in permanent magnet 2 suction chambers on the chassis 5 the large-scale iron plate 1 of high top ceiling more than 8 meters, realizing universal movements by two driven steering wheels 3 and manpower driving wheel 4.Below chassis 5, be provided with four davits 8 compartment 14 that plays, in the compartment 14 around be provided with air tyre 17, sportsman 15 drives sprocket wheel 10 as stepping on crank with pin by bike, by quicken for the first time chain 11 transmissions just accelerating pulley 12 drive big gear wheel in parallel 13 engagement reversing gears, 9 transmissions hinge wheel in parallel drive quicken for the second time chain 7 transmissions for the second time acceleration chain wheel 6 drive the purpose that manpower driving wheels 4 high speed revolutions reach airflight, the dodgem travel direction realizes turning neatly effect by the directional lever 16 of sportsman 15 two-hand control block form through T profile shaft rotation direction wheel 3.Dodgem is through running foul of each other, the dodgem that has will be hit, just held between about 2～3 meters of the height that falls down from above by 19 pockets of the big net of following prior setting, since 18 1 on cylinder high one low, everyly fall dodgem at big net 19, at this moment be provided with big forklift or crane with the dodgem shovel or hang to deliver to once more and proceed collision after the top attracts with big iron plate 1 and play or compete at lower because the effect of gravity will flow to lower soon.---Figure 13 a is the easy embodiment of the 4th of fleet-footed runner's project: it is the principle design of power * arm of force=weight * weighing arm of utilizing lever, its structural principle is, the big transverse arm of Figure 13 a1 is to support overhead 10～15 meters height by rings seat 2 and suspension ring 3 usefulness hoist cables 10 95～98% weight that the fulcrum of lever plays fleet-footed runner and aircraft 13 on the arm of force top of lever 11 by messenger wire 12 of playing, 95～98% weight of equipped heavily hang down 9 energy balance fleet-footed runners and aircraft weight on the top of gravity arm of lever by column 8 up and down by what radial bearing 4 in the transverse arm hub 7 and bearing with cross roller bearing 5 tightly were enclosed within center shaft 6.

Figure 13 b is the 5th of fleet-footed runner's project embodiment preferably: it is to utilize large-scale manipulator similar to Fig. 9 a, difference is not adopt loop wheel machine but directly adopt weights formula 10 95～98% weight of playing fleet-footed runner and aircraft 21 by pulley and messenger wire of heavily hanging down, its structural principle is: outer arm 17 is by bearing with cross roller bearing 12, radial bearing 15 is sleeved on the two ends up and down of inner arm 9 fixation hollow axles 13, inner arm 9 up and down supports overhead 10～15 meters height by column 6 by what arm hub 4 radial bearings 2 bearing with cross roller bearings 5 tightly were enclosed within center shaft 3, and fleet-footed runner and aircraft 21 are by messenger wire 20,18,14,8,7, by pulley 19,16,11,1,10 95～98% the weight of playing fleet-footed runner and aircraft 21 of heavily hanging down with the weights formula.---the aircraft that above three kinds of type classes are similar and the manufactured materials of orbital facilities thereof: 1. the compartment of aircraft, wing, wind-force contend with rudder, wind power balance rudder, seat, case, support, connecting rod, hang bow, joint, roller, pulley, shackle and can select material manufacture such as steel, aluminum alloy, glass-felt plastic, nylon, plastics, alloy glass for use; 2. the track of orbital facilities, column, crossbeam, reinforcing bar, cable wire etc. can select for use train rail, steel pipe, shaped steel, reinforcing bar to mix material manufacture such as earth and suspension bridge cable wire; 3. the floating permanent magnet of magnetic can be selected the second generation or the manufacturing of third generation permanent magnet for use.---active flight device, the manufactured materials of the universal hunting gear of driven flight instruments and sucked type or manpower flying device and various loop wheel machines can be selected steel, aluminum alloy, silicon steel plate, rubber, epoxy resin, the second generation or third generation permanent magnet, enamel wire, insulating material, diamagnetic material manufacturings such as (bismuth metals) for use.---the principle of the light deflector of safe signal flasher and the omniscope of light signal amplifying apparatus and Submarine is same or similar, be by the light deflector that the two sides opposing parallel is installed in the metal case, wherein one side and light signal tilt 45 ° to receive light signals and reflection reflect as the light signal for the another side light deflector since repeatedly the reflected light signal weaken gradually just should be with the amplification of light signal once behind 8 to 10 secondary reflections, the structural principle of light signal amplifying apparatus is similar to light deflector, also be to receive the light signal and reflection carries out signal relatively for single board computer (SBC) (being computer) by the one side and the light deflector of 45 ° of light source inclines, every frequency that meets is that the pointed pulse light signal of 50 or 60 He Zhi sends with regard to the instruction electroluminescent lamp and amplifies and identical light signal reflects as the safety light signal that amplifies by the another side light deflector.---the direct supply on the track both sides of driving and simulated flight device is to distribute each current consumer to use through the cable connection switch box by computer by wear-resisting carbon brush or rolling carbon brush or rolling metal wheel.---power supply is by wear-resisting carbon brush the cable reel that the direct supply on track both sides flows in the simulated flight device to be tightened up through two copper rings with carbon brush output for switch box by computer distribution use by clockwork spring by active flight device or driven flight instruments by a paired cable that scribbles extinction and look coating in the various simulated flight devices.---the manufactured materials of fleet-footed runner's project flight wing: 1. the skeleton of wing can be selected the reed pipe manufacturing of corrosion-resistant steel, aluminum alloy or brass; 2. the valve material of wing and outer wing can be selected manufacturings such as nylon, plastics, canvas, rubber, leather, artificial leather, chemical fabric for use in.---the manufactured materials of the big top ceiling of no magnetic paramagnetic can be selected manufacturings such as corrosion-resistant steel, aluminum alloy, brass plate, glass-felt plastic, epoxy plate, alloy glass for use.

Claims (10)

1---three types are similar safe and reliable, cheap, no exhaust pollution, not crowded, the lightweight aircraft that does not block up, all (overhead) single track (comprising steel wire cable) is gone up flight in the low latitude,---the driving type of communications and transportation wherein: their feature is outer image aircraft, engine installation such as electric car, Fig. 1 a, b, c are that to ride rail formula driving big, in, little structural representation, Fig. 1 d, e is the floating suspension type driving scheme drawing of magnetic, Fig. 1 a1, c6, d6, e1 are vertical boosting rollers, assist pushing away it and continue flight when last driving engine installation is out of order, a2, b3, c1, d1, e2 is only several knobs and brake-applying handle of driving operator's compartment, and all the other are all by computer automatic guidance, a3,6,8, b5,10, c5, d5,9, e3,6, the 8th, the wind-force rudder that contends with, when meeting with the strong wind attack in the flight way, driving reaches the purpose of contending with, a4 by the corresponding angle of this rudder kick of computer instruction, the 9th, it not only protects the stream line pattern case of front and back wheel the wheel normal operation but also can alleviate air resistance, a5, b1, c3, d3, e4 be wing it the time bear 70～80% the weight of riding rail formula driving and load-carrying in flight, bear the weight of underslung driving 100%, a7, b2, c8, d8, e7 is the compartment, large-scale carrying 18～24 people, medium-sized carrying 8～12 people, small-sized carrying 4～6 people, a10, c9, d10, e9 is that level is pushed roller, when this driving engine installation be out of order can seek help after driving pushing away and continuing flight, b4, the 8th, seat, it is by computer control maintenance horizontality when the uphill/downhill, can reduce personal casualty, b6 at seat ambient air expanding bag by the computer instruction expansion just in case get into an accident, the 7th, wheel and engine installation, c2,4, d2, the 4th, the wind power balance rudder, when attacked by vertical wind-force, reach the purpose of smooth flight by the corresponding angle of computer instruction deflection, d7, e5 are the magnetic floated power devices,---Fig. 2 a is the orbital facilities scheme drawing of riding rail formula driving: it is characterized in that among the figure 5,6, be that two tracks connect support shelves keeping parallelism through 15 up and down, should not surpass 36 meters and minimumly be no less than 5 meters by liftoff 8～10 meters height of column 2 tracks is the highest, keep 6 meters spans to increase the corresponding increase of cost at interval, the 11st, the location span that column should not be set must increase, 10,12,13, the 14 oblique rollering steel muscle of setting up for large span support the weight that shelves are held the track middle part with holder, 3,8th, the state of flight of driving, commonly used work simultaneously with standby two engine installations keeps rapidly not subtracting during climbing, speed per hour is 30～40 kilometers/hour in the urban district, speed per hour is 150～200 kilometers/hour in the open air, and the maximum grade of track should not be greater than 25 °,---Fig. 2 b is the floating suspension type driving orbital facilities scheme drawing of magnetic: it is characterized in that 1 among the figure, 2, the 3rd, gantry pillar, crossbeam and suspention reinforcing bar, the height 10～15 meters the highest should not greater than 50 meters minimum should not be less than 7 meters, 7～12 meters of width are spaced apart 6 meters, and span increases the corresponding increase of cost, Fig. 2 b4 is the floating suspension type tracks of two round magnetic in portal frame, the scheme drawing in rivers is crossed in Fig. 2 b5～18 expression: the two ends tractive of two superiors's cable wires 13, hauls main beam transverse 14 and guarantees that tracks can double swerve, horizontal drawing and oblique rollering steel rope 7 in both sides simultaneously by the horizontal reinforcing bar 17 that draws on the top of four additional columns 6 through the horizontal arcing shaped steel of the right and left rope 16 two ends tractives in order to prevent the track double swerve by tiltedly hanging reinforcing bar 15 main beam transverses 14 suspention reinforcing bars 3 roundtrip trajectory 4 that plays on four tops of increasing column 5,10,11,12, the 18th, stable and superiors's cable wire and the horizontal intensity of drawing the tension tension force of cable wire that guarantee to increase column and additional column, Fig. 2 b8, the 9th, magnetic floats suspension type driving shuttle flight state, speed per hour can reach 800～1200 kilometers/hour, Fig. 2 a, the direct supply on b track both sides is provided by the segmentation of destination stop direction, and sends safe light signal by destination stop, on each column, be equipped with the light deflector of light signal, 8～10 columns of being separated by are established a light signal amplifying apparatus, also are equipped with the devices such as noise alarm of lightening protection installation and supersonic wave bird driving snake on each column,---Fig. 3 a rides rail formula driving engine installation: it is characterized in that the wheel 2 that contained by a metal case 1,3,4, it is the direct current planar motor of rotor that the permanent magnet 5 that 15～25 odd numbers are installed on 8 is formed with the wheel jointly with 12～24 the even number windings 6 on the both sides direct current planar motor stator 10, permanent magnet one side on the wheel all is the N utmost point, another side all is the S utmost point, the interval of each winding of planar motor stator equate with the width of winding and each at interval in diamagnetic material of embedding, on one side the whole identical another sides of direction of current of winding all opposite, rotating speed by the quantity of stator winding electrifying what variation and definite, the many more rotating speeds of energising winding are fast more, slow more more at least, and the current field of winding produces an electro-motive force in the magnetic field of wheel permanent magnet after energising, because stator is so that the fixed wheel that forces is to the despining of right hand theorem direction phase, around this principle can design various brush DC stepless speed-change motors,---Fig. 3 b magnetic floats suspension type driving engine installation: it is characterized in that by the floating partial installation of 12～36 magnetic one soft and long and have can adapt in the tube-like envelope 7 of elongated slot uphill/downhill and about the variation of turning, adjacent split bending is between 0.2 °～0.4 °, this device is the permanent magnet up and down 4 that is enclosed within magnetic levitation track 3, the two poles of the earth of the C type magnet 1 on 5 both sides are identical with the polarity at magnet 4 the two poles of the earth and repel each other this device double swerve is suffered restraints, also identical with magnet 5 polarity and repel each other and produce the static total weight of come-up interaction energy carrying driving, two C type magnet 1 at interval about the stator winding 2 of a pair of DC linear electric motor is installed, the whole identical another sides of one side direction of current that the floating split of each magnetic is provided with two to three pairs of stator winding 2 are all opposite, the magnetic field of the current field of stator winding and track 3 lower floor's magnet 5 produces an electro-motive force and presses right hand theorem direction straight line high-speed motion after energising, the speed of speed with the energising winding what and decide, the quantity of energising multiple speed more is fast more, and is slow more more at least, magnet 6 prevents to lift on this device and sets up, the distance that this bottom of device is provided with two hanging axises 8 account for this device length 3/5～2/3 between can bear the static weight of this driving,---Fig. 4 a is contend with rudder and a sensor scheme drawing of wind-force: it is characterized in that the top by fleetline metal case 1 is provided with the handle of a wind sensor and the wing 2 along with wind-force deflection, the light that with lower end light deflector 11 light source 12 is sent by center shaft 4 reflects and immediately the light signal is converted to little electric current to photoelectricity nest of tubes 9 after certain electro-optical tubes receives reflection source and flows to computer and make instruction and start brush DC stepless speed-change motor 13 transmission worm screws 8 and promote fan type worm gears 10 twisting hollow shafts 5 and drive the corresponding angle of rudder shell 1 deflection of contending with by rudder hub 3 and reach the purpose of contending with,---Fig. 4 b is the scheme drawing of wind-force loadometer: to be pressure measurement film 3 apply mobile pressure variation for piezoceramic 5 by metal sheeting 4 at the middle part that it is characterized in that a pressure measurement film framework 2 that is contained by metal case 1 is converted to little electric current and flows to computer as the computing foundation,---Fig. 4 c is the wind-force loadometer of the floating suspension type driving of magnetic: the pressure sensing that it is characterized in that this loadometer is 4 to produce the suffered pressure of pressure and the piezoceramic on the right and equate that the little electric current that produces is also equal by under permanent magnet 5 and the identical condition of repelling each other of track upper strata permanent magnet 2 corresponding polarity piezoelectricity being made pottery, on one side when certain is subjected to the attack of wind-force, the piezoelectricity pottery 4 on both sides difference of pressure occurred and has been converted to little electric current brain calculation process of powering;---the type of simulated flight device: their feature is that profile is identical with genuine various aircraft with the morphosis of interior shape, difference is that engine installation all adopts the brush DC stepless speed-change motor, the mode of flight is similar to driving also below the loop wheel machine by active flight device or driven flight instruments plays with steel wire (rope) that scribbles extinction and look coating or carbon fibre line on the single track of low latitude (overhead), and various simulated flight devices imitate flies, the existing schoolaeroplane of their purposes as aircrew's training, its can reduce instruction cost improve the quality of teaching shorten the teaching time limit if student's misoperation or had any fault can the fatal crass, flight racing car as sports is also arranged, also have as the artistic performance TV of shooting, the flight stage property of taking a photo as a moment can reach the effect of mixing the spurious with the genuine, the flight instruments of taking advantage of an aircraft as recreation and trial is arranged again,---a of Fig. 5, b, c, d is the simulation autogyro, jetliner, land-effect plane and the water surface airship that can not sink, all be to adopt U font two-wire to play, just in case certain single line fractures and equals two lines and all broken, can not occur one disconnected one and constantly singly hang phenomenon, the simulated flight device is by the glide soft landing, and ground all is provided with foamed materials or establishes the big net of elasticity and guarantee personal security.Fig. 5 e, f, g, h, i is an inflation airship, balloon and flying saucer, and the device that speeds across the sky, all be to be used for recreation to take a photo as a moment, or the project of artistic performance,---Fig. 6 a, b is the track design scheme drawing of two kinds of simulated flight devices: the feature of Fig. 6 a is at T type column and crossbeam 1,2 both sides are provided with two roundtrip trajectorys 5,6,7 simulation autogyros 3 are to play by active flight device or driven flight instruments 4 usefulness messenger wires to imitate flight, the feature of Fig. 6 b is that to be provided with two be through messenger wire 6 in the bottom of the column 1 of portal frame and crossbeam 2 by active flight device or driven flight instruments 5 toward anti-tracks 3 and 7 jetliners 4, play and imitate flight,---the sectional schematic diagram of Fig. 6 a4: 1 of Fig. 6 c, the 2nd, 2 of Fig. 6 a, 5 is characterized in that being provided with wheel 4 and 2 of Fig. 3 a by the top of c type shell 3,3,4,8 is similar, planar motor 5 and 6 of Fig. 3 a, 10 is similar, principle is identical, the bottom is provided with anti-rotate 6 active flight devices of composition or driven flight instruments is not established direct current planar motor,---Fig. 6 d six takes turns suspension type active flight device or driven flight instruments is the sectional schematic diagram of Fig. 6 b5: two wheels in both sides 2 and 2 of Fig. 3 a of it is characterized in that being enclosed within inverted T shape suspension type track 4,3,4,8 is similar, promptly the outside of two wheels 2 is provided with the stator winding 1 and 6 of Fig. 3 a of direct current planar motor in shell 3,10 is similar, principle is identical, be provided with in the bottom of inverted T shape track and skid when contact roller 5 upwards prevents the wheel running and establish, six take turns suspension type active flight device or driven flight instruments by what two Fig. 6 d formed, also can be used for six and take turns on the suspension type driving as the active flight device;---Fig. 7 a is flying trapeze's project principle schematic: it is characterized in that going up loop wheel machine 5 messenger wires 6 rolling shackles 19 suspension ring 18 by driven flight instruments at track 1 (or steel wire cable) hangs bow 7 and hang play aircraft 20 and fleet-footed runner's 95～98% weight of bow fulcrum 17; still 2～5% weight of surplusing are pounced on wing by the fleet-footed runner and just can be risen to the sky and aloft freely circle in the air; the state of flight is made support 20 and hangs bow 7 and pull into horizontality as long as break into both legs off with the fingers and thumb on the A font leg band 24 pulling stay cords (being the bicycle brake stay cord) by two legs control; if two legs are broken into chevron shaped stay cord off with the fingers and thumb and are pulled on and hang bow and 7 make support 20 pull into the state of downward underriding; if the band 25 pulling stay cords on the leg of a left leg K/UP left side being made when wanting turnon left roller shackle 19 pull to the right hangs and bends the purpose that air resistance that 7 places are inclined upwardly left wing 13 downward-sloping right wings to have increased the left side owing to left leg K/UP has been realized turnon left; if want right-hand corner to need only that process with right leg K/UP and turnon left is opposite just to realize right-hand corner; the motion of the wing of aircraft is that the fleet-footed runner handles the gimbal suspension 14 transmission the right and left connecting rods 9 and 10 of control stalk 15 by both sides and can make wing make various flare maneuvers; the fleet-footed runner just draws in if control stalk is pushed away two wings to cephalad direction; if control stalk is pulled to two wings of belly just to launch; if control stalk is pushed away human body; two wings are just pounced on downwards; if only one side being pushed away human body pounces on downwards with regard to a wing; if control stalk is made various different variations; wing is also just followed different motions; the back skeleton 12 of outer wing 13 is one with the conjunctura 11 of taking down the exhibits; motion by connecting rod 10 can make wing draw in or expansion;---Fig. 7 b is the principle schematic of fleet-footed runner's wing: the wing 6 that it is characterized in that the left side; 7 are in rounding state; the wing 9 on the right; 10 are in deployed condition; its principle of work is that control stalk 18 and 19 is one; control stalk 18 is in the state that folds its wings; control stalk 19 is in the state that stretches open wings; joint 1 on the common skeleton of the outer wing 7 of wing 6 in when control stalk is upwards shifted 18 position onto, promoting by connecting rod 2 by gimbal suspension 3; contract by connecting rod 4 pullings by gimbal suspension 3 simultaneously; control joint 5 drivening rods 15 of spreading the wings are the garden heart with control joint 5 with center fixation fulcrum 16 is that the path of motion that radius is made a camber reaches the state that folds its wings; when control stalk is moved 19 position downwards to through gimbal suspension 22 by connecting rod 23 pullings in joint 24 on the common skeleton of wing 9 and outer wing 10; simultaneously to be the garden heart close 20 with control to control joint 20 drivening rods 17 that promote the companding wings by connecting rod 21 by gimbal suspension 22 is that the path of motion that radius is made a camber reaches the state that stretches open wings with center fixation fulcrum 16; in A-A section Figure 14 of wing 9 be that valve was closed and produced the power that advances and rise when the Kq air was pounced under valve top flows into fleet-footed runner's direction of bottom when pouncing on the wing; the B-B of outer wing 10 analyses and observe Figure 11; 12; 13; valve is opened the Kq air and is flowed to fleet-footed runner's direction as 12 curve arrow as 11 when pouncing on the outer wing, and valve is closed as 13 and produced the power that advances and rise, valve 11 when pouncing under the outer wing; 13 can play the feather effect of birds wing; the 25th, the valve schematic layout pattern;---Fig. 8 a; b is fleet-footed runner's wing structural representation: it is characterized in that 4 stains on Fig. 8 ab1 indicative curve, is the same skeleton that outer wing outer skeleton is in different conditions and different visual angles, and 4 stains of 2 indicative curve are outer wing forward position skeletons; 4 stains of 3 are that the back is along skeleton; 6 stains of 4 be in the common skeleton of wing and outer wing, it all is that turning joint is similar to commissure that 5 all gardens of expression are enclosed, gimbal suspension is a bulb type or similar to cross universal-joint spindle; the 6th, the anchor shaft that wing is fluttered up and down; the 7th, the axle sleeve that wing is fluttered, the 8th, be fixed on the fixed pivot on the wing support, 4 stains of 9 are connecting rods that control is contracted wing and spread the wings; the 10th, the forward position skeleton of lining wing; the 11st, in the wing of lining along skeleton, the 12nd, lining wing back, the 4th, lining wing and the common skeleton of outer wing along skeleton;---Fig. 8 c is the spread the wings A-A cutaway view of state of Fig. 8 a: it is characterized in that when about two wings are in extended configuration; the rear portion of wing is inclined upwardly between 10～15 degree, and the lower fulcrum 3 that hangs bow 1 connects aircraft parking stand 5 and fused by connecting band 6 and seat cushion 7 by shoulder belt 4, and wing bevelled fulcrum 2 up and down links to each other with lining wing 8 outer wings 9;---Fig. 8 d is the contract B-B cutaway view of aliform attitude of Fig. 8 b: it is characterized in that between downward-sloping 10～15 degree in rear portion of wing when about two wings are in contraction state; wing 1 outer wing 3 is in downward-sloping state by fulcrum 2 among the figure,---Fig. 9 a is second of fleet-footed runner's project embodiment preferably: it is characterized in that the fleet-footed runner can freely circle in the air in the rotating range of large-scale manipulator 360 degree up and down, the column 4 of Fig. 9 a is the left rotation and right rotation freely of arm 5 in the garden heart support manipulator by bearing 2 with 3; outer side bearing 6 and 7 with lining arm 5 is that the garden heart supports outer arm freely to swing; freely fly by play fleet-footed runner and aircraft 9 of loop wheel machine 10 and messenger wire, 1 balancing machine hand and fleet-footed runner's the weight but balance is hung down,---Fig. 9 b is the Flight Vehicle Structure scheme drawing of fleet-footed runner's project: adorn a roller 10 suspension ring 11 that play on horizontal Xiao who it is characterized in that Fig. 9 b1 roller shackle 1 has and bend 3 lower fulcrum 5 connection aircraft parking stands 7 by connecting fulcrum 2 bow 3 that plays through hanging; suspension ring 11 are to be that garden heart R is the garden camber of radius with center of gravity 9;---Fig. 9 c be Fig. 9 b hang the bow 3 and the efficiency chart of aircraft parking stand 7: it is characterized in that when the fleet-footed runner when taking off or land, support 7 is in the CZ plumbness, needs only two legs and break into the horizontality that the A font just is in Fig. 9 b7 off with the fingers and thumb after soaring; when two legs are broken into the chevron shaped fc dive status that just is in off with the fingers and thumb; dive angle is generally in 45 °, and maximum should not surpass 60 degree,---Figure 10 a is Fig. 9 b suspension ring 11 and the functional schematic of roller shackle 1 and 10: it is characterized in that suspension ring 11 are is that garden heart R is the garden camber of radius with center of gravity 9; when needing turnon left, the fleet-footed runner needs only left leg K/UP; effect by band and stay cord realizes turnon left with the bow 3 that hangs that roller shackle 1 roller 10 pulls to the right, if need right-hand corner to need only right leg K/UP, by band and stay cord the bow 3 that hangs that roller shackle 1 roller 10 pulls to the left side is realized right-hand corner; the angle of inclination of turning about aircraft is generally between 20～30 degree; maximum should not surpass 45 degree,---Figure 10 b is three kinds of structural representations of fleet-footed runner's loop wheel machine: it is characterized in that Figure 10 b1 is the tandem loop wheel machine by the decelerator loop wheel machine cylinder of directly connecting, length simple in structure is big.Figure 10 b2 is that parallel loop wheel machine is in parallel with cylinder than one times of tandem contraction in length by reducing motor, Figure 10 b3 built-inly ensconces cylinder abdomen inner volume by reducing motor and dwindles cylinder outside one times of inner gear by cylinder and the epicyclic gear transmission,---Figure 10 c is the fundamental diagram of fleet-footed runner's project loop wheel machine: it is characterized in that when the fleet-footed runner put on aircraft energized loop wheel machine 4 start working by messenger wire 10 play aircraft and fleet-footed runner 95～98% weight but can not sling, because being loop wheel machines 4, freight weight limit spring 7 overweight compressed processes impel the handler displacement of freight weight limit switch 9 (being limit switch) to realize momentary pause on overweight force compresses spring 7 by footstock 3 commissures 2 horizontal Xiao's 5 sieve bolts 6 spring perches 8, the load of messenger wire 10 alleviates spring 7 and resets and will lift on the loop wheel machine 4 by spring perch 8 sieve bolts 6 horizontal Xiao's 5 footstocks 3 commissures 2 and repeat 95～98% the weight that above working process remains play aircraft and fleet-footed runner again when loop wheel machine suspends,---Figure 11 a is another embodiment preferably of fleet-footed runner's project loop wheel machine: it is characterized in that utilizing the power of clockwork spring 5 (promptly similar to the clockwork spring of clock and watch and rolling door) as loop wheel machine, it neither needs power supply also not need complicated on-off control system, its structure and principle of work are: by footstock 1 support 2 anchor shafts 6 clockwork spring 5 clockwork spring tubes 4 dividing plates 7 inner geares 8 engagement small planetary gears 11 are installed for one and are driven major planets tooth 12 engages fixed miniature gearss 10 in parallel, because miniature gears 10 is fixed, therefore mafor planet gear only drives and then rotation of cylinder 3 around miniature gears 10,---Figure 11 b six takes turns the flight racing car of suspension type sports: it is characterized in that sportsman 7 quickens minor sprockets 10 and drives both sides hinge wheels 11 and realize sporting flyings by the power wheel 2 that chain 12 quickens minor sprockets 5 transmission both sides as stepping on crank drive hinge wheel 8 chains 9 by pin by bike,---Figure 11 c six takes turns suspension type paddle type sports racing car: it is characterized in that sportsman 22 steps on action that both hands draw by stay cord or connecting rod transmission thrust paddle 19 by both legs, 21,23, realize sporting flying, its principle is that sportsman's 22 both hands and both legs draw in simultaneously by stay cord or connecting rod transmission thrust paddle 19,21,23 draw forward simultaneously, because the effect blade of air resistance is in as 19,16 close up state, when the both hands both legs stretch simultaneously by stay cord or connecting rod transmission thrust paddle 19,21,23 draw simultaneously backward, because the effect blade of air resistance struts automatically as 21,23,24 softened state, produce the power of flight forward, fleet-footed runner's both hands fore and aft motion is the curvilinear path motion of pressing cycloid by the joystick of messenger wire 17 lower ends, the pin that both legs are played by messenger wire 8 is stepped on footwear 9 bands 10 and is pressed the cycloid back and forth movement, its structure is six to take turns driven flight instruments 2 and be enclosed within on the inverted T shape track 1 by fixing front wing 18 rear wings 11 upper limbs cushion 7 suspender belts 12 thrust paddles 19 about in the of 5 on flower wheel 3 upper pressure wheels 4 racing car top boards 6 suspension brackets 13 underframe 20,21,23 form paddle type sports racing car, 14 is former and later two exercise end positions that both hands stretch and draw among the figure, the 15th, two final positions of both legs motion,---Figure 12 a is the 3rd of the driven flight instruments of fleet-footed runner's project embodiment preferably: the big iron plate 1 that it is characterized in that installing on indoor high 7～10 meters top ceiling above fixing permanent magnet 7 attracts on the driven flight instruments base 8 of universal sucker below the big iron plate 1 is passed through four universal flower wheel 2 universal crab claw axle 3 bearing with cross roller bearings 4,9 loop wheel machines, 6 messenger wires 5 are formed the driven flight instruments of the universal suckers fleet-footed runner that plays and are freely circled in the air up and down indoor,---Figure 12 b is another driven flight instruments of fleet-footed runner's project embodiment preferably: it is characterized in that aloft 7～10 meters high top installs the upper and lower surface of a big plate 6 of no magnetic paramagnetic and respectively establish a universal driven flight instruments, above one by take over a business fixed permanent magnet 2 below 1 by four groups of cardan wheels 3 forms iron plate 5 that driven flight instruments attracts the big plate 6 following universal driven flight instrumentses of no magnetic paramagnetic form by four groups of universal flower wheel 4 loop wheel machines 7 messenger wires 8 about the universal driven flight instruments of magnetic force that moves of two All-China Federation of Taiwan Compatriots fleet-footed runner that plays freely circle in the air up and down indoor,---Figure 12 c is the aerial dodgem that moves according to the indoor sport that the principle of Figure 12 a is extended, it is characterized in that on indoor 5～6 meters high top ceilings installing on the chassis 5 of the universal Manpower driver below the big iron plate 1 fixed permanent magnet 2 and take turns the aerial dodgem of 3 manpower drive wheels 4 suspension brackets, 8 compartments 14 pneumatic tyres, 17 compositions by both direction, to be sportsman 15 step on crank drive hinge wheel 10 as pin by bike to its motion principle quickens minor sprockets 12 by chain 11 and drive two big gear wheels in both sides, 13 engagement reversing gears 9 and drive hinge wheel in parallel and drive by chain 7 and quicken minor sprockets 6 transmissions manpower drive wheel 4 in parallel and realize the high-speed crashs motion, as if being hit to fall to falling down by the other side fatal accident can not take place, but a kind of amusement of thrill is enjoyed, the elasticated net 19 that is provided with a big type safety in the dodgem range of movement is enclosed within on two cylinders 18 as load-transfer device, liftoff 0.5～1 meter of liftoff 1～2 meter another of this cylinder, when being hit, certain dodgem gets off on big net 19, because 18 1 on cylinder high one low, so the impulsive force that falls down and the effect of gravity cause this car to flow to lower from eminence, by forklift or crane this dodgem is served again and proceeded collision on the big iron plate 1,---Figure 13 a is the easy embodiment of the 4th of fleet-footed runner's project: it is characterized in that utilizing lever principle promptly: the theorem of power * arm of force=weight * weighing arm and design-calculated, its structural principle is by the play fulcrum of lever 11 of arm hub 7 radial bearings 4 bearing with cross roller bearings 5 center shafts 6 columns 8 transverse arm outer end rings seats 2 suspension ring 3 hoist cables 10 at the large-scale manipulator transverse arm, weighing arm and heavily hang down 9 the weight=arm of force and the weight of fleet-footed runner and aircraft 95～98%, therefore fleet-footed runner and aircraft 13 can not be sling, when 2～5% the weight of still surplusing is pounced on wing and is alleviated 5～10% weight by the fleet-footed runner, at this moment since 9 the weight of heavily hanging down greater than fleet-footed runner and aircraft weight, therefore fleet-footed runner and aircraft are sling,---Figure 13 b is the 5th of fleet-footed runner's project embodiment preferably: it is characterized in that the thrust that outer arms 17 are installed at large-scale manipulator column 6 center shafts 3 radial bearings 2 bearing with cross roller bearings 5 inner arm hubs 4 inner arms 9 outer end hollow shafts 13 forms large-scale manipulators to bearing 12 radial bearings 15, fleet-footed runner and aircraft 21 are by hoist cable 20,18,14,8,7 pulleys 19,16,11,1 directly and the heavily hanging of weights formula 95～98% weight of fleet-footed runner and aircraft, but fleet-footed runner and aircraft can not be sling, when 2～5% the weight of still surplusing is pounced on wing and is alleviated 5～10% weight by the fleet-footed runner at this moment since heavily the weight of hanging down sling greater than the weight of fleet-footed runner and aircraft.

2---the three types of similar lightweight aircraft of claim 1 and the manufactured materials of orbital facilities thereof: material manufacture such as it is characterized in that 1. that compartment, wing, the wind-force of aircraft contend with rudder, wind power balance rudder, seat and case etc. can the aluminium alloy, glass-felt plastic, nylon, plastics, alloy glass; 2. the track of orbital facilities, column, crossbeam, reinforcing bar, cable wire etc. can select for use train rail, steel pipe, shaped steel, reinforcing bar to mix manufacturings such as earth and suspension bridge cable wire; 3. the floating permanent magnet of magnetic can be selected the second generation or the manufacturing of third generation permanent magnet for use.

3---the universal driven or manpower flying device's of the active flight device of claim 1, driven flight instruments and sucked type manufactured materials: it is characterized in that steel, silicon steel plate, aluminum alloy, rubber, epoxy resin, the second generation or third generation permanent magnet, enamel wire, insulating material, diamagnetic material bismuth metal etc.

4---the brush DC stepless speed-change motor of claim 1: it is characterized in that principle is identical with direct current planar motor, its structure is that the groove that rotor is cut 15～25 odd numbers by aluminum alloy is embedded in permanent magnet, one end all is that the N utmost point other end all is the S utmost point, stator is divided into former and later two and identical is embedded with 12～24 windings, the interval width of winding equates with the width of winding, and each at interval in diamagnetic material of embedding, the direction of current of a stator is all identical, another is all opposite, passes through shell, front and rear cover and cooling fan and outer cover are formed the brush DC stepless speed-change motor.

5---the light deflector of the safe signal flasher of claim 1 is identical with the omniscope principle of Submarine: it is characterized in that by the parallel light deflector that 45 ° of two face tilts are installed in the metal case, wherein one side and 45 ° of light source relative tilts receive the light signal, the distance of the in parallel and 300～400m/m of being separated by of another side and reflect light as safe signal.

6---the light signal amplifying apparatus of claim 1: it is characterized in that structural principle is similar to omniscope, receive mirror by the light signal of 45 ° of face tilts and the light signal is reflected to single board computer (SBC) (computer) carry out signal relatively, every frequency that meets is that the pointed pulse light signal of 50 He Zhi or 60 He Zhi sends with regard to the instruction electroluminescent lamp and amplifies and identical light signal reflects as the safety light signal that amplifies by the another side light deflector.

7---the driving track of claim 1 and the track both sides direct-current power supply scheme of simulated flight device: it is characterized in that being connected switch box by wear-resisting carbon brush or roller carbon brush or rolling metal wheel distributes each current consumer to use by computer.

8---power supply plan in the various simulated flight devices of claim 1: it is characterized in that the cable reel that the direct supply on track both sides flows in the simulated flight device being tightened up by two copper rings with carbon brush output for switch box by computer distribution use by clockwork spring by carbon brush by active flight device or driven flight instruments by a paired cable that scribbles extinction and look coating.

9---the manufactured materials of fleet-footed runner's project flight wing of claim 1: it is characterized in that 1. the skeleton of wing can be selected corrosion-resistant steel, the reed pipe manufacturing of aluminum alloy or brass; 2. the valve of wing and outer wing can be selected manufacturings such as nylon, plastics, canvas, rubber, leather, artificial leather, chemical fabric for use in; 3. joint material can be selected nylon, plastics, aluminum alloy, alloy glass etc. for use.

10---Figure 12 b of claim 1 does not have the manufactured materials of the big plate 6 of magnetic paramagnetic can select manufacturings such as corrosion-resistant steel, aluminum alloy, brass plate, glass-felt plastic, epoxy plate, alloy glass for use.

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