CN202176456U - Three wind power mechanisms, aircrafts, aerological stations, wind power ships and high altitude water taking machines - Google Patents

Abstract

Three wind power mechanisms, aircrafts, aerological stations, wind power ships and high altitude water taking machines all adopt wing rings to serve as wind wheels. The wing rings abandons axle centers and low-efficiency section wings of ordinary wind wheels and adopts high-efficiency wing sections as the whole wing piece, the length of force arms which support the high-efficiency wing sections is shortened by several times, one force arm is increased into two force arms, and single-side supporting is changed into two-side supporting. Therefore, compared with common wind wheels, the largest radius can be expanded by more than ten times, and if the radiuses are identical, then effectively wing section area can be expanded by more than several times. Accordingly, compared with existing wind wheel generating mechanisms, three wing ring wind power mechanisms are enlarged by more than ten times in size, and adjacent wing rings of wing ring groups can mutually serve as rotors to perform reversing rotation, thereby enabling relative speed of the rotors to be doubled. Even if the body form, rotating speed and electromagnet load are all identical, generated energy can also be improved twice. Wingspans of a high altitude wing ring wind power mechanism, a wing ring aircraft and a wing ring aerological station can exceed kilometers, and bearing capacity can reach tens of thousands of tons. A wind power mechanism of a wing ring wind power ship can drive extra-large vessels, and a wing ring high attitude water taking machine can take water in large-scale high attitude air mode.

Description

Three kinds of wind-powered electricity generation mechanisms and aircraft, aerological station, wind electric power ship, high-altitude water intaking device

Affiliated technical field

High hollow wing ring wind-powered electricity generation mechanism relates to the wind generator set of a kind of generator in the high-altitude generating.

Wind tunnel type wing ring wind-powered electricity generation mechanism relates to the power facility of built-in wind wheel of a kind of pipeline or water wheels.

Tower wing ring wind-powered electricity generation mechanism relates to a kind of ground or low latitude wind wheel generation mechanism.

But wing ring aircraft relates to the rotor craft of the landing of a kind of original place, hovering.

Wing ring aerological station relates to a kind of aircraft that can forever hover or cruise in the high-altitude.

Wing ring wind electric power ship relates to a kind of boats and ships that drive with wind-force or wind-powered electricity generation.

It is the altitude air water intaking device of the energy with the high-altitude wind-powered electricity generation that wing ring high-altitude water intaking device relates to a kind of.

Background technique

At present; The wind generator set that directly generator is risen to the high-altitude mainly contains two kinds: a kind of is to combine wind wheel generator to form with balloon or kite; Also having a kind of is from the rotor wind wheel generator, from rotor rotates the drive generator for electricity generation in wind when, produces lift and makes the body lift-off and be suspended in the high-altitude.The former balloon, kite lift are limited, involve great expense and damaged easily; The latter lets wind wheel that lift is provided, and has saved many costs and has increased working life.Therefore the latter is more valuable, more promising.

At present, existing various wind wheels (rotor) generator mainly adopts the wind wheel in axle center, wind wheel and axle interlock, and axle drives rotor.

At present, go up and down in the original place, high-altitude hovering flight device mainly is with the common rotor that axle is arranged or the axle that has that can nature when rotating with the wind produces lift is installed on the top of common body or the middle part of annular body from rotor.

At present, permanent aloft work base station mainly is to form with the various communication Instruments of Piggybacking, Detecting device and filming instrument.

At present, the car and boat of wind-drive mainly are traditional sailing boat and sail driving RV that occurs in recent years and the boats and ships that draw with the umbrella shape kite.

Present air water intaking device need consume electric power or fossil energy, and can only get the airborne water molecule in ground to low latitude.

The model utility content

One, innovation purpose

The something in common of present wind wheel (rotor) generator and rotor craft is to adopt the wind wheel (rotor also is a kind of wind wheel) that axle is arranged, and has three deadly defects of a wind wheel to be:

(1) each fin from the axle center outward most of wing panel collection wind energy power little, and the closer to the wing panel in axle center gather wind energy render a service more little, until being zero; Real efficient collection wind wing panel is just more away from the wing panel in axle center, renders a service highly more more away from axle center collection wind, and the wing panel between therefore efficient wing panel to the axle center is should the abridged; But but can't omit; Because efficient wing panel must lean on this poor efficiency wing panel and invalid wing panel to maintain the interlock between itself and the axle center, this has just increased complete machine weight, has hindered the generator body further to enlarge; Increased harmful windage simultaneously, wind wheel (rotor) power has been reduced and mechanical vibration frequency and amplitude raising.

(2) efficient wing panel can only obtain one-sided and be that the axle center that is in far-end is supported, so rotor diameter is big more, the efficient wing panel of its fin just can only be done to such an extent that get over taper; Therefore it is low to collect wind efficient, can't promote more large-scale generator, though through increasing the means of fin quantity; Can increase the area of effective wing panel to a certain extent; Fin is just inevitable to increase poor efficiency, invalid wing panel simultaneously but increase, and correspondingly increases the weight of wind wheel and harmful wind load that wind wheel is born and the increase of these wing panels is inevitable, consequently makes wind wheel not only not reach the purpose of " synergy "; Also can become burden, make wind wheel " subtract effect " on the contrary;

(3) can only drive the rotation of internal layer iron core and winding (internal rotor) by axis, or can only drive outer iron core and winding (external rotor) rotation, and can not let the simultaneously relative counterrotating of rotor each other of inside and outside iron core winding by outer shaft.

Existing high tacho generator is in order to reduce the mechanical stress that produces because of centrifugal force and to reduce the wind abrasion; Root diameter is generally done smallerly, and length is bigger, promptly adopts elongated rotor; Particularly at the high-capacity and high-speed unit more than 3000 rev/mins; Because the relation of the strength of materials, root diameter receives strict restriction, generally can not be above 1.2 meters.And the length of rotor body receives the restriction of critical velocity.When body length reach diameter more than 6 times the time, second critical velocity of rotor will approach the running speed of motor, in service bigger vibration possibly take place, until breaking axis takes place.So the size of large high-speed generator amature receives strict restriction.Just because of this reason, existing technological limit aspect the increase generator bodily form, it is very big to develop more jumbo type difficulty.How to break through this technological limit? As if as if present technical measures can only be sought help from increases electromagnetic load, strengthen radiating and cooling, further improves but these measures are also difficult at present, so can only look for another way.If let original fixed iron core winding (being staor winding) also rotate to get up and sense of rotation opposite, the relative rotation speed that so original rotor just can obtain doubling just can reach the generate output of higher rotation speed with lower absolute rotating speed.

Present permanent aerological station mainly is on satellite, to settle various communications, detecting, filming instrument or the like; Its weakness is that cost superelevation, bearing capacity are too small, function very little; And it is far away excessively apart from ground; Transmission signal has delay and distortion inevitably, can not directly transmit to regular handset and individual Internet Access user.

Present wind-propelled watercraft; A kind of is with traditional sail traction; Also having a kind of is that the former can only utilize the wind-force in tens of meters low latitudes with the traction of umbrella shape kite, and the latter also can only utilize the wind-force below 300 meters; And the both can only use with the wind or under the skew wind state, and the storeship that can not generate electricity is used.

The weakness of several existing technologies more than the invention of this series will be directed against exactly solves following several technical barrier:

(1) only keeps the efficient wing panel of rotor generator or rotor craft fin and save invalid wing panel, poor efficiency wing panel and axle center, thereby reduce burden, weight reduction, saving material.

(2) under the prerequisite that does not enlarge rotor diameter, widen the size of the efficient wing panel of fin greatly, reduce waving and Oscillation Amplitude of fin simultaneously.

(3) let two adjacent annular core windings rotor counterrotating simultaneously each other; Their relative velocity is doubled; Thereby do not enlarging the generator bodily form, do not improving spinner velocity, do not increasing under the prerequisite of electromagnetic load generate output is significantly improved, even breaking through the bodily form limit and the capacity limitation of generation current machine.

(4) a kind of novel high altitude wind power generator structure that is flown and promoted by wing ring type rotor band is provided.

(5) a kind of novel wind tunnel type wind wheel generation mechanism that is promoted by wing ring type wind wheel and tower wind wheel generation mechanism are provided.

(6), provide that a kind of bodily form is huge, carrying capacity is huge, lifting force is huge and agile, rapid speed, can forever cruise or suspension and safe and reliable original place landing aircraft.

(7) provide that a kind of cost is extremely low, energy-autarchic and body and carrying capacity is huge, can forever cruise or suspend, the aloft work station.

(8) boats and ships that a kind of thousands of meters high altitude winds capable of using and even the above stratosphere wind-force of 2 myriametres are provided is main energy sources.

(9) provide a kind of and need not expend fossil energy, hang in the air year in year out, can from the abundant upper air circulation air of water vapour, obtain super sized type air water intaking device abundant, clean water source, realizes the extensive air water-intaking that limit no energy consumption, no region.

Two, technological scheme

(1) technological scheme of high hollow wing ring wind-powered electricity generation mechanism:

Place the rotor wind-powered electricity generation mechanism in high-altitude the same with existing generator; By rotor iron core winding and stator core winding relative movement generating; The iron core winding promotes rotation (wind wheel of high hollow wing ring wind-powered electricity generation mechanism is exactly a wing ring) by wind wheel, and frame provides the facility of tractive force to link to each other through tracting cable and below, and the circuit of power facility links to each other with the upper end of cable; The lower end of cable links to each other with below electricity consumption facility, it is characterized in that: equidistantly on annular support fin is set and forms wing ring; Fin adopts the cutting air can produce the fin of lift, and each fin all as the latter end of the fin of common wind wheel, forms angle between the circumferential surface of aerofoil and wing ring, i.e. angle down with the wind; Fin can stretch out outside ring or in the ring, also can stretch out to both sides simultaneously; The angle of facining the wind of all fins is identical on the same wing ring, and the angle of facining the wind of adjacent wing ring is opposite.

Fin on the wing ring can be in ring, to stretch or to the outer single-blade that stretches of ring, also can be from encircle same point in encircling, encircle outside the double-vane that stretches out of both sides.The inboard that single-blade on the existing wing ring can be arranged at ring fully becomes inner wing, or the outside that is arranged at ring fully becomes outer wing, also can fin be set by inner wing, mode that outer wing is alternate, the inside and outside wing no matter, and each fin span equates; The inner wing of the double-vane of same wing ring and outer wing can symmetry also can be asymmetric, but the specification of all wings of the same side, structure and the angle of attack angle of attack must be identical.

Above-mentioned wing ring can be shown in Fig. 2, Fig. 3 intuitively, and above-mentioned wing ring group can be shown in Fig. 1, Fig. 4, Fig. 5 intuitively, and the detailed description of each figure can be referring to the description of drawings of this paper.

Though wing ring is similar to a ring that is formed by single-blade aircraft or double-vane aircraft fuselage end-to-end, in fact it is a wind wheel, and be one can produce when rotating down with the wind lift from the rotor wind wheel; From rotor wind wheel again have differently from the rotor wind wheel with common though it is one, its fin can not link with the axle center; Even can omit the axle center fully, even keep the axle center, neither be in order to let axle drive fin or wing drive axle; But in order to be under too fast in wing ring rotational speed, that centrifugal force the is excessive situation, entad utilize through between ring body and axle center, setting up spoke that pulling force reaches the purpose of reinforcing ring body, in this case; If necessary; Can be wing with spoke design, make the effect of its existing spoke have again fin effect (as the spoke 4-2 of Figure 10 just can be designed as common wing or spin wing, if the wing 2-2 of ring linked to each other with the axle center in should figure; 2-2 both can be designed as wingly so, also can be designed as the entad shaft-like spoke of pulling force only is provided).

Form a wing ring group by two or three wing rings, each wing ring or be in same plane and the same center of circle is arranged, or each wing ring on the same group parallel surface and center of circle each other is on the same shaft axis; Can have only one group of wing ring in the complete machine; Two groups or more wing ring also can be arranged, and every group of wing ring can constitute a complete power facility, and (such as type shown in Figure 10 inside and outside two wing ring groups are just arranged, shown in Figure 12 then have two wing ring groups up and down; Each wing ring group in these two types all is complete a, power facility independently; Even disassemble wherein one group of wing ring, one group of remaining wing ring still can constitute complete power facility, comprises two groups or more wing ring group in the complete machine; Be not that Figure 10, two kinds of situation shown in Figure 12 are only arranged, in addition can be by the other forms of high hollow wing ring wind-powered electricity generation mechanism complete machine of forming by multiple wing ring group); Can join end to end through tracting cable and cable between the two or more high hollow wing ring wind-powered electricity generation mechanism complete machine; Promptly be in the complete machine of upper end or following public attention; Its lower end is connected through the upper end of tracting cable with another complete machine of below or last public attention; The circuit of each complete machine links to each other finally through cable and is connected (can referring to Figure 13) with ground electricity consumption facility through same cable; The benefit of this multimachine polyphone form is that multimachine can use same tracting cable and same cable, thereby reduces the load capacity of each complete machine and practice thrift a large amount of tracting cables and cable and the deadweight that alleviates each unit.It should be noted in the practical operation: one is the same with existing high-altitude rotor wind-powered electricity generation mechanism; High hollow wing ring wind-powered electricity generation mechanism must have tracting cable to be connected with ground installation; " draw " and it, guarantee that it can not rack, thereby form relative movement with wind; Rotor or wing ring are facingd the wind as windmill to be rotated; Because the fin that adopts has identical water droplet shape cross section with the wing of fixed wing aircraft, this fin high speed rotating cutting air certainly leads to the lift that makes progress, so high-altitude rotor mechanism or high hollow wing ring mechanism can aloft hover;

Two, in 11 Figure of description such as Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, Figure 11, Figure 12, Figure 13, Figure 21, Figure 22, Figure 24; Though all only have a tracting cable 5 between each high hollow wing ring wind power facility and the ground installation; But not representing between high hollow wing ring wind-powered electricity generation mechanism and the ground installation to have a tracting cable to link to each other; When the diameter of high hollow wing ring wind-powered electricity generation mechanism greatly when a tracting cable can't provide enough tractive force maybe can't make ring body keep balance; Just be necessary to increase the quantity of tracting cable; And when being provided with many tracting cables, the distribution of each tracting cable had better not close up or too near because suitable scattering is distributed with the flight attitude that is beneficial to control mechanism.

The pattern of generator is following:

First kind; Support with each wing ring in the same wing ring is that support is provided with stator iron core, winding and rotor iron core, the winding that is equivalent to common generator respectively; Form a huge generator that does not rely on axle to drive rotor by two or three such wing rings, in fact this generator does not exist stator core winding, because each iron core winding ring all rotates in the wind with fin; Adjacent wing ring sense of rotation is opposite, therefore can be as rotor.This kind generator, the ring support of wing ring has much, generator just has much, so its bodily form is big, especially its diameter is big, can ten times so hundred times to existing largest generator.(can referring to Fig. 4, Fig. 5)

Second kind; The equidistant generator that line shaft is installed on the support of wing ring; Let ring track coupling mutually on wheel and the adjacent arbitrary wing ring on the generator line shaft; Ring track is established around ring and is connected as a single entity with wing ring, and track must drive the generator motive power wheel rotation of phase coupling with it when rotating with wing ring.This kind pattern; Though it is the same with existing common generator with regard to single generator; But wing annular solid is huge, can arrange hundreds and thousands of generators, rotates (absolute synchronization) and these generators are inevitable synchronously with wing ring; Therefore can parallel connection or series connection become actual integrated big generator, its complete machine generated energy equally can ten times so that hundred times to existing largest generator.The advantage of this pattern is to utilize ready-made generator to reduce the workload and the cost of manufacture process; But every single generator all has end cap, axle and parts such as bearing and support; Especially end cap, axle and bearing are can't the position, abridged; The bearing of hundreds and thousands of units and end cap have increased the weight of complete machine, have in fact reduced the generating winding quantity that originally can reach.(can referring to Fig. 6, Fig. 7, Fig. 8)

Because the angle of facining the wind of adjacent wing ring is opposite on the same group; Therefore their sense of rotation is inevitable opposite; The result of two ring counterrotatings is that the relative velocity of two wing rings all is doubled; The relative rotational that is to say the iron core winding on the wing ring group doubles, and said here iron core winding comprises being the iron core winding of support and the iron core winding on the shaft type generator with wing ring directly.Therefore compare with existing common generator, if the diameter of rotor, length and rotating speed are identical, and electromagnetic load is identical, and generator capacity so of the present invention can increase considerably, even possibly double.

In the middle of above-mentioned second kind of structure, can be arranged at any place in the positions, three places such as edge, outer ring, inner ring edge or side edge of wing ring with the ring track of shaft type generator motive power wheel coupling; Generator motive power wheel and track can be imitateed train wheel and its track, but best mode is to adopt intermeshed gear and tooth-like track.In this kind structure; Minimum in two adjacent wing rings will have a wing ring that the shaft type generator is installed; And another wing ring is provided with the track of phase coupling with it, also can two the wing ring shaft type generator all is installed and be provided with another wing ring on the shaft type generator track of coupling mutually.

Except being used to drive the ring track of shaft type generator; Also has a kind of grooved track; It is a grooved with scooter coupling mutually, the cross section of this track, just in time matches coupling with scooter; Thereby the wing ring of two counterrotatings is coupled together, and Fig. 9 promptly is this kind grooved track and scooter coupling manner schematic representation.Complete machine and tracting cable upper end also can utilize this grooved track to couple together; The two ends that mode is passed the connecting rod 4 of wing ring axis are connected with scooter 3-3 respectively; Each bar connecting rod 4 intersects at same point wing ring axis; This crosspoint of connecting rod 4 links to each other with the upper end of tracting cable, and the lower end of tracting cable connects below electricity consumption facility.(concrete mode is please referring to embodiment one).

Need be noted that, more than two kinds of tracks all be continual closed ring, and the motive power wheel of scooter and shaft type generator all be interrupted, equidistantly distribute on track; Scooter on the track can not be less than three, and wing ring diameter is big more, and the scooter on the track just should be many more, and purpose is to make the both wings ring be neither too familiar nor too distant, keep constant spacing, does counterrotating smoothly.

Be in two adjacent wing ring groups in the same center of circle; Or two the different adjacent wing ring groups of radius that are on the same shaft axis can connect through spoke; These spokes also can be simultaneously as fin (referring to Figure 10); Spoke cutting air as fin must can produce lift, and promptly its cross section must be identical with the cross section of fixed wing aircraft wing; The sense of rotation of two adjacent wing rings is opposite, and the wing ring that turns clockwise on the same group equates with the wind energy total amount of the wing ring that is rotated counterclockwise in any same time period collection.The complete machine of forming by two groups or more wing ring; If wherein partly wing ring group because connector (scooter and connecting rod thereof) hinders or hangs the cabin has taken reason such as space and be not easy to arrange fin; Can complete machine be looked like a big wing ring group so; As long as all wing rings that turn clockwise of complete machine equate with the wind energy total amount that all wing rings that are rotated counterclockwise were gathered in any same time period; The moment of torsion that both direction is opposite just can reach balance, thereby makes complete machine in wind, keep steady running.

So; How does generator in the rotation link to each other with external circuits? Very simple in fact, no matter what electrodes generator is provided with, earlier the same joint that is parallel to of ability parallel connection; Then each joint is connected with corresponding brush track; The brush track is attached to the outer (between brush track and the wing loop orbit dielectric isolation layer will be set) of wing annular groove type track 3-1, and the brush track is touched with brush separately and is communicated with, and external circuits links to each other with brush; Brush then is fixed on the outer connective pole of scooter vehicle frame, and the brush track that rotates has so just formed continual circuit with brush and has been connected.

Also have, huge high hollow wing ring wind-powered electricity generation mechanism is soared high into the air? Most convenient mode efficiently is exactly to work as motor usefulness to generator, promptly imports electric energy through cable to power facility, makes the rotation of wing ring produce lift and ascends to heaven.As at no electricity or power leakage area, then use air bag device, just air bag is set in top or periphery, middle part even the bottom of annular body; Fill light gas in the air bag, let the air bag band high hollow wing ring wind-powered electricity generation mechanism and take off, treat that body rises to the enough height of wind-force; Wing ring will inevitably reach enough rotating speeds; Produce enough lift, be recyclable air bag or let air bag fly away this moment, letting air bag continuation reservation also not have certainly can not.Also have two ways to let high hollow wing environment-development electrical mechanisms fly away in the regional sky of not having electricity or few electricity; Method one is to let fly away in the sufficient area of electric power earlier; Again with the traction of boats and ships or heavy vehicle to not having electricity, power leakage area, certainly a method this more be applicable to the high hollow wing ring wind-powered electricity generation mechanism that the bodily form is not too big; Method is to drag several less high hollow wing ring wind-powered electricity generation mechanisms earlier from other places, is supplied power simultaneously by them, can let large-scale, huge high hollow wing ring wind-powered electricity generation mechanism fly away.

The high hollow wing ring wind-powered electricity generation mechanism that some purposes is special; If the equipment that loads is too much, body weight is excessive; The lift of fin is not enough to keep its suspension; Can permanent air bag be set at body upper or middle part, periphery even bottom so, perhaps at body upper permanent large-scale kite being set also is good method.

If can annular core winding of the present invention be done waterproof, anticreep processing and carry additionally the degree of depth of floating drum with the dive of control wing ring mechanism, also can place among the ocean current, tracting cable is anchored in the seabed.So ocean current will promote the rotation of wing ring as wind.

Consider that troposphere, high-altitude thunder and lightning is more, can conduction setting be done on the tracting cable surface, as at tracting cable surface coverage conductive fiber, or at tracting cable surface attachment or one or more lead of helical coiling, these conductive fibers or lead must ground connection; Conductive processing is made in wing periphery also can avoid the possible destruction of thunder and lightning.

Need explain a bit at last: so-called " shaft type generator " refers to the existing common generator that drives rotor or stator with axle.

(2) technological scheme of wind tunnel type wing ring wind-powered electricity generation mechanism:

Parallel surface and the center of circle are in the high hollow wing ring wind-powered electricity generation mechanism on the same shaft axis each other to select each wing ring for use; Be placed among the wind-tunnel; Give up original tracting cable; And remove the connecting rod 4 between tracting cable and the wing ring wind-powered electricity generation mechanism, and only keeping the track and the scooter thereof in the fin that stretches out in the guide vane ring and the wing ring outside, the vehicle frame of scooter links to each other with the wind-tunnel inwall; Wind-tunnel can be the level trend, also can be capwise.(like Figure 14, shown in Figure 15.)

The energized components of wind tunnel type wing ring wind-powered electricity generation mechanism makes also to go for after waterproof insulation is handled current generating becoming water wheel type power facility.

The setting of wind-tunnel: choosing has the mountain pass, valley (or the river that The turbulent river crashes its way through, submarine canyons) of wind throughout the year, with native stone filling, only stays a hole to make wind or current logical, and the stream power of the wind (or water) of this wind-tunnel (water hole) will be very considerable; Also wind tunnel type electricity generator can be set in the large-scale water transmission pipeline.

Also can build stone, the construction windbreak of laying bricks in the stable wilderness of wind direction, reserve the wall hole and settle wind tunnel type wing ring wind-powered electricity generation mechanism, the opening that answer at the two ends in wall hole should be wider than the diameter of generating wing ring, makes the two ends of wind-tunnel form two reverse horn mouths; If because of terrian condition can't be built wall not too high, also not too wide, so can be the direction of axis line elongation (promptly adding thick wall body) of wall as far as possible toward wind-tunnel, like this, wind-tunnel becomes a long tube, and the wing (shown in figure 15) of the side section shape of wind-tunnel wall such as aircraft.Because what flow through that the wind of wind-tunnel inwall walks is camber line, what flow through that the wind of wind-tunnel outer wall walks is straight line, two bursts of inevitable converging at the rear of wind-tunnel simultaneously of wind, so the wind in the wind-tunnel can obtain quickening.

(3) technological scheme of tower wing ring wind-powered electricity generation mechanism:

Select for use each wing ring to be in same plane and the high hollow wing ring wind-powered electricity generation mechanism in the same center of circle is arranged, remove the tracting cable between mechanism and the ground, and remove the connecting rod 4 between tracting cable and the wing ring wind-powered electricity generation mechanism; With the axial water intaking of wing ring mechanism square to; Then, perhaps inner wing is extended to the place, axle center, be connected with bearing outer wall; Bearing inner wall is connected with axle, and the two ends of axle are connected with the top of tower or strut; Perhaps the scooter connecting rod 3-3 with wing ring group front and back is connected with strut, wherein at both sides and the middle minimum strut (like Figure 16, shown in Figure 17) that respectively is provided with positive, the back side.

(4) technological scheme of wing ring aircraft:

High hollow wing ring wind-powered electricity generation mechanism with this series invention is the basis; On its original scooter vehicle frame as the connector between the wing ring body; Or (promptly be the vehicle frame that Fig. 5, Fig. 6, Fig. 7, Fig. 8, connecting rod 4 shown in Figure 12 are connected at its original scooter vehicle frame as the connector between wing ring body and the tracting cable; Comprise connecting rod 4 itself) on be fixedly connected or hang the cabin; The cabin can be annular, dish-shaped, cylindrical etc. (can certainly not establish bulkhead and only keep the cabin frame), the cabin can place in the ring of wing ring group, ring is outer or ring on, under the ring;

And; Perhaps with original be that the iron core and the winding of support setting removed directly with wing ring; And at the fin top of wing ring installation ramjet; Perhaps original shaft type motor is removed and explosive motor go up to be installed in position, perhaps keep original shaft type motor or annular core, winding and supply power from ground to them, or on its body, storage battery is set and supplies power to them through cable.No matter be ramjet, explosive motor to be installed or, all must reach and promote the purpose that these two wing rings are done opposite spin with original motor driving.The rotating speed of regulating wing ring just can make wing ring rise, descend or suspend;

On the position that cabin body or connector etc. do not rotate with wing ring, install or do not install the ramjet that the substantially horizontal Driving force is provided.Preferably four in this engine, all around each one, the pendulum across, the power that each is responsible for a direction just can advance promptly, retreat, brakes, brings to a halt, turns, takes a sudden turn even turn by the right angle track.If load onto steering equipment's (making puff prot can change direction) for these several ramjets, can also utilize them to increase the speed that rises, descends, advances, retreats, turns.Puff prot can quicken to descend up or on the deflection; Puff prot down or deflection down, can quicken to rise; Two or three puff prots towards or be partial to same direction, but then acceleration level moves, and increases speed and the brake of advancing, retreating, the agility of bringing to a halt, turn, taking a sudden turn, even might do right-angled bend.If to turn to, the agility and the speed of action such as brake do not have high request, can adopt the propeller cavitation engine yet.

Original tracting cable that is connected with the below of body and cable can be removed or keep, and also can only keep tracting cable and cable is changed to oil pipe, even with tracting cable with oil pipe unites two into one or with tracting cable, oil pipe, the cable three-in-one.

Figure 18, Figure 19 are an embodiment's of this aircraft plan view and sectional drawings.Shown in this instance, because both wings ring sense of rotation is opposite, rotating speed is identical, fin is identical, their torsion is cancelled out each other, so the cabin rotates with arbitrary wing ring in the flight or the Shi Buhui that hovers.

The fin fin of this aircraft can keep former high hollow wing ring wind-powered electricity generation mechanism fin from the rotor characteristic, promptly cut the characteristic that air can produce lift, also can not keep this characteristic and adopt the characteristic of the fin of common propeller cavitation.But; If adopt to have fin, can obtain two benefits from the rotor characteristic: the one, wing ring aircraft is during in level or near horizontal flight, as long as control the engine that is used to provide the power of moving horizontally well; Make wing ring aircraft produce suitable back rake angle; The rotation of can facining the wind of wing ring produces lift, so just can close to be used to order about the engine of wing ring rotation and to reduce energy consumption, and the 2nd, wing ring aircraft produces lift and makes the aircraft stable landing in the nature decline process wing centre section ring that the runs out of steam rotation of can facining the wind; If do not adopt from the rotor characteristic, aircraft just can only be by the accident of falling of the speed of freely falling body.

(5) technological scheme of wing ring aerological station:

High hollow wing ring wind-powered electricity generation mechanism or wing ring aircraft plug-in or be built-in with in following various device, the facility whole, partly or one of them: electronic equipment, communication apparatus, remote sensing equipment, the equipment of taking photo by plane, scientific experiment equipment, defensive weapon, astrovehicle emission and reclaim platform, crane gear, up-down cabin, recreational facilities, personnel working room.(like Figure 20, shown in Figure 21)

(6) technological scheme of wing ring wind electric power ship:

Lower end with the tracting cable of the high hollow wing ring wind-powered electricity generation mechanism of this series invention connects the towing point on the boats and ships, and its cable is connected as circuit with the storage battery or the motor of boats and ships.Here so-called " towing point " refers to let tracting cable firmly connect and pulls the object that boats and ships advance.(shown in figure 22)

The present technique scheme also is applicable to large-scale haulage vehicle, is particularly suitable for the metastable large-scale haulage vehicle of moving line, is not suitable for dilly.Because have only enough large-scale vehicle that the enough high hollow wing ring of tractive force " pulling " wind-powered electricity generation mechanisms just can be provided.

(7) high hollow wing ring water intaking device technological scheme:

High hollow wing ring water intaking device is made up of high hollow wing ring wind-powered electricity generation mechanism and device for fetching water from air, and the circuit of high hollow wing ring wind-powered electricity generation mechanism is connected with the circuit of device for fetching water from air; The water outlet of the water receiving disc of device for fetching water from air is connected with the water pipe upper end, and the water pipe lower end is connected with the below wet pit or with drainage facility; The vehicle frame of high hollow wing ring wind-powered electricity generation mechanism wing loop orbit scooter is connected with the support or the shell of air water-intaking mechanism through connecting rod; Or the tracting cable of high hollow wing ring wind-powered electricity generation mechanism passes from the center portion of air water-intaking mechanism; Air water-intaking mechanism hangs on the tracting cable, can hang one or more; Water pipe perhaps unites two into one with tracting cable, does not perhaps unite two into one with tracting cable.The compound mode of high hollow wing ring wind-powered electricity generation mechanism and air water-intaking mechanism has two kinds:

First kind, the vehicle frame connecting rod of the wing loop orbit scooter of high hollow wing ring wind-powered electricity generation mechanism is connected with the support or the shell of air water-intaking mechanism, and the gateway of the water receiving case of air water-intaking mechanism is connected with the water pipe upper end, and the water pipe lower end is connected with the below wet pit or with drainage facility.(shown in figure 23).

Second kind, the tracting cable of high hollow wing ring wind-powered electricity generation mechanism passes from the center portion of air water-intaking mechanism, and air water-intaking mechanism hangs on the tracting cable, can hang one, two or more (shown in figure 24).Use such high-altitude water intaking device; High hollow wing ring wind-powered electricity generation mechanism can go up the above stratosphere of myriametre; And water intaking device can hang on the troposphere, below, can utilize the powerful and stable wind-force of stratosphere to generate electricity like this, can utilize the abundant water vapour in troposphere to fetch water again; And can go here and there and hang more water intaking device, enlarge the water intaking work surface.

Water intaking mechanism is made up of air conditioner refrigerating device, condensation water-collecting machine, water receiving case, air conditioner heat radiator, fan etc.; Its principle is the same with working procedure with existing air conditioner; All be to suck warm-humid air, the ejection cold dry air, airborne moisture is condensed and separates; Different is that air water intaking device is not discarded with " air conditioner water ", but it is collected the principle that Here it is " air water-intaking ".

Owing to be in the high-altitude; Wind-force is powerful, thus the fan that air conditioner or common water intaking device must be equipped with to high hollow wing ring water intaking device just can in case, simultaneously establish horn mouth at the two ends of water obtaining device; What walk through the bell-mouthed wind in two ends is camber line; Must be faster than the distinguished and admirable speed that tube periphery takes the air line, therefore increase the wind-engaging of condensation water-collecting machine, thereby increased collecting water from runoff.In addition, can be placed on radiator public attention and be placed on down public attention to the condensation water-collecting machine, the heat that can utilize radiator to discharge be like this heated to air intake, makes wind when the condensation by contact water-collecting machine, receive the bigger temperature difference, thereby increases collecting water from runoff.

Three, beneficial effect

The beneficial effect of high hollow wing ring wind-powered electricity generation mechanism:

Common wind wheel is more little the closer to the wing panel collection wind energy power in axle center, and until being zero, and the wing panel collection wind energy power away from the axle center is big more more, and the former is poor efficiency wing panel and invalid wing panel, and the latter is efficient wing panel.In fact, the major function of common wind wheel poor efficiency wing panel is not a collection wind, but the efficient wing panel of support on the neck guarantees itself and axle interlock, and being referred to as " linkage lever " maybe be more suitable.This " lever " is owing to only obtain the one-sided support and the strong point far away from the axle center; If effectively wing panel is too wide, receive air quantity excessive; Serious vibration just will inevitably take place, rock even fracture, its actual effect is also less than the wing than taper, so the just efficient wing panel of the latter end of the fin of common wind wheel; Can not widen, can only taper.The wing of wing ring is most effective wing panel entirely, and it has abandoned collection wind function fully is zero and relatively poor wing panel, and changes and rely on fin near-end, that both sides are adjacent to provide support; Compare axle center original far-end, one-sided and support, the arm of force not only shortens, and also is increased to two from one; And two arm of forces supported on both sides that is placed in; Consequently: only from single fin, if the arm of force has shortened 10 times, support force is with regard to corresponding 11-fold increase so; The arm of force is increased to two from one, so the growth multiple of support force just becomes 20 times from 10 times; One-sided support becomes supported on both sides, and support force and stability are further enhanced again; From wing ring generally speaking, high-efficiency fin can be increased to tens of and even hundreds of, and the area of each fin can greatly be widened again, that is to say that the area of the efficient wing panel of wing ring can several times, tens of times and even hundreds of times are to the common wind wheel of same radius.Therefore can reach a conclusion: the wind resistance power of wing ring wind wheel should be the several times of the common wind wheel of same radius with the efficient that transforms wind energy, more than tens of times, and the lift (bearing capacity) of wing ring type rotor should be the several times of the common rotor of same radius, more than tens of times.

Because abandoned common wind wheel and axle center and efficient wing panel between " linkage lever ", therefore when efficient wing panel area is expanded on several times, tens of times of ground, also can reduce complete machine weight and save raw material.Existing rotor wind wheel, its high-efficiency fin can only have three segments, and the ten minutes taper, and the efficient wing panel of wing ring but can be increased to tens of still to hundreds of, and the wheel footpath is big more, differs big more.

The moment of torsion of existing common wind wheel or rotor is fully by an axle transmission; Therefore high to the technology and the requirement of strength of axle and bearing; Even but this root axle intensity is big more again; It also can not support diameter and reach hundreds of rice, thousands of meters wind wheel, and wing ring will be original be only shared array, tens of groups still to hundreds of groups of scooters by the heavy burden of a bearing load, therefore can build diameter easily and reach hundreds of rice and even thousands of rice.Certainly, build the giant swing ring mechanism, should not adopt the multiple wing ring structure on single-blade ring or individual layer plane, and should adopt a plurality of wing rings, stage construction, support mutually, mutual structure of reinforcing.

Also because wing loop technique makes efficient section expansion greatly of rotor; The support force that the efficient section of rotor is obtained increases greatly; And can be through the rotation of cable input power source driving wing ring, so the present invention can fly De Genggao than prior fuel oil helicopter, can go up stratosphere easily.

Existing fuel oil helicopter seldom has can reach the myriametre height, and trace it to its cause three: one, the area and the support force inadequate natural endowment of the efficient wing panel of rotor in the high-altitude of rarefaction of air, only can't provide enough lift with rated speed; Two, because carrying capacity is limited, the Low oil Fuel that carries; Three, fly highly more, air is thin more, and oxygen is few more, and the oil consumption of motor unit is bigger, power performance is poor more.And the invention solves the inadequate natural endowment of the area and the support force of the efficient wing panel of rotor, and be through cable power transmission, there is not the problem of energy deficiency; Though the cable weight that hangs down from the high-altitude is very big; But the motor of high hollow wing ring wind-powered electricity generation mechanism can be more powerful; And the present invention has enough large-area efficient wing panel and the wing ring that can when high speed rotating, keep balance; Therefore there is not the problem that is short of power, can rises to easily and rise to stratosphere and in the generating of forever hovering of 1-2 meters altitude.Stratosphere, highly approximately height above sea level 1-5.5 myriametre does not have thunder and lightning there; Do not have wind and rain, do not have ice and snow, (wind direction change half a year once to have only wind direction, the long-term stable strong wind of wind speed; Maximum wind speed can reach 50 meter per seconds, near 15 grades of violent typhoons, can easily the adult be thrown to sky).

Just because of high hollow wing ring wind-powered electricity generation mechanism can be in the high-altitude stratosphere and overtrades layer hover; And these two stratification of winds and surface wind is fluid different fully; The all very stable characteristics of wind direction, wind speed are arranged; Basically stable electric generation all the year round; Middle just influenced in the blink that annual wind direction changes, therefore can fundamentally change wind-power electricity generation could only be as the label of " the intermittently energy ", and therefore breaks through at one stroke and seriously restricted at present bottleneck---the blockade of electrical network that the Chinese feature electric industry develops in a healthy way!

At present wind-powered electricity generation industry in the world's is still little, the Chinese wind-powered electricity generation scale that also is far from being, but even so, still electrical network is forced to stop production or half stopping production because of not inserting in China many wind-powered electricity generations enterprise, and electrical network has been clutched the throat of Chinese wind-powered electricity generation! It is extra large excessively that the river need be crossed over mountain after mountain, striden to the electrical network enlarging, invest huge, easier said than done? Build the electrical network difficulty, yet in China, the transmission of electricity of being incorporated into the power networks is only really extremely difficult! So, how could Chinese wind-powered electricity generation break through the electrical network quagmire early?

Stratosphere wind-force is powerful and constant, does not have rain, snow, thunder, electricity again, is best wind energy turbine set.A small-sized high-altitude generating ring can satisfy a town or a big station service there; Large-scale high hollow wing ring wind-powered electricity generation mechanism then can satisfy the electricity consumption of big a, medium-sized city; In conjunction with the wing ring high-altitude water intaking device in the invention of this series; That just not only can be supplied power downwards, can also supply water downwards.No matter be that bustling urban is overhead, or the sky of alpine desert off-lying sea, can need not rely on length apart from electrical network at all, thereby make the Chinese feature electric industry break through the electrical network quagmire by high hollow wing ring wind-powered electricity generation mechanism's vertical supply or only through the short distance mains supply!

In addition, even do not consider the technological merit of adjacent foil ring of the present invention rotor counterrotating each other, high hollow wing ring wind-powered electricity generation mechanism compares with common upper wind turbine generator, and that generating capacity is eager to excel is much bigger, it is much easier to make, and cost is also much lower.

The present invention has the characteristics of adjacent foil ring rotor counterrotating each other; The relative velocity of each wing ring is doubled; Thereby do not enlarging the generator bodily form, do not improving spinner velocity, do not increasing under the prerequisite of electromagnetic load generate output is doubled; Therefore can break through the bodily form limit and the capacity limitation of generation current machine, develop with present technology huge wind-driven generator out of one's imagine.

The beneficial effect of wind tunnel type electricity generator and tower type aerogenerator:

Because fin advantage and the adjacent foil ring of having followed high hollow wing ring wind-powered electricity generation mechanism be the rotor advantage each other, thereby becomes ground and low latitude and the surface wind generator that a crane standing among chickens.

The beneficial effect of aircraft:

For large-scale wing ring, in fact just be equivalent to a frame older aircraft end-to-end and form a circle.In the time of the rotation of wing ring, the aircraft that just is equivalent to these end-to-ends runs on fixed track, so such seriously the rocking, vibrate of helicopter screw propeller can not take place for it; Each wing ring all has the wing ring of the counterrotating of matching with it; And equate to all wing rings of both direction rotation are gathered wind energy in any same time period total amount; Body all is under the twisting force of balance at any time; Whole deflection can not take place, whole rotation more can not take place or topple, so its flight attitude can both keep stable at any time.If the ramjet of four substantially horizontals all around has been installed; This aircraft just can be done stable and horizontal motion fast; And can quick accomplish advance, retreat, action such as turning, even accomplish brake, bring to a halt, exceedingly difficult movements that present all aircrafts such as zig zag, right-angle turning all can't be accomplished.

Utilize wing ring vehicle technology can manufacture and design that body is huge, carrying capacity is huge, lifting force is huge and agile, rapid speed, very safe novel original place landing aircraft.Utilize present technique can also manufacture and design inner wing formula original place landing aircraft; Promptly be that inner ring in annular is provided with the wing, the outer ring is not provided with the annular aircraft of the wing, and its outer ring can equidistantly be provided with four ramjets; Be used for advance and retreat and turning; Because the no wing of fuselage periphery is not afraid of scraping, collision, inner wing annular aircraft is particularly suitable for speedily carrying out rescue work, rescues and armoring the operation.The aircraft that wing ring vehicle technology is made; With existing jet-propelled comparing; Speed is slower, the carrying capacity of low consumption oil, the economic performance do not consume oil of suspending, super large, ultra wealthy freight house and upper platform, superpower Safety performance but it cruises, and present any aircraft all can't be reached.

Only need to keep tracting cable and power facility; Wing ring aircraft can also be used as the crane in places such as mine, harbour, goods yard, building site; This crane not only can self-supporting electric energy, and no matter the work activities face is big, and crane capacity all will be above other various hoists.As long as the connection of tracting cable is arranged; Wing ring aircraft just can kill engine; Can generate electricity at ordinary times provides ground installation electricity consumption or electric power storage; Rely on simultaneously from the facing the wind lift float in air of spinning of rotor, rely on self-supporting power that the lifting required drive is provided during work, and can break away from tracting cable, ato unit at any time when needing mobile position or long distance to convey goods.

Because the radius of wing ring aircraft can reach hundreds of rice still to km, therefore can research and develop fully becomes a kind of brand-new " space flight mother ship carrier ".This cheapness and practical " space flight mother ship carrier "; Have and do not consume oil fully at ordinary times and the high-altitude of hovering supplies power, supplies water downwards; The advantage of break off hawser, open up the engine wartime, initiatively cruising and launching an attack is on it even can resemble and carry opportunity of combat the marine airplane carrier and cruise and execute the task.Can rapidly China's military strength be risen to a new high degree.

The beneficial effect of aerological station:

Can permanent self-supporting power be suspended in hundreds of rice to tens thousand of meters sky, also can firing an engine initiatively cruises or pulled by large ship, vehicle cruises, and becomes real " Air fortress " that can never land.This " Air fortress " also can be carried enough electric power to argosy, warship even the airplane carrier at sea; Letting these large ships save fuel oil surpasses more than 50%; With the wind or beam wind voyage even can fuel-economizing 100%, can also greatly improve the attack and defense ability and the combat radius of aircraft carrier fleet simultaneously.Wing ring aerological station can existing self-sufficiency powerful electric power; The huge bodily form is arranged again; Therefore can various goods and materials and main equipment be lifted by crane on the base station; Make up scientific base that comprises the astrovehicle pad and the armament systems that comprise guided missile and laser weapon at low cost, keep watch on from the enemy's situation on space, sky and ground at any time and implement at any time and tackle and make an initiative sally.The weapon launch hole though do not draw in Figure 21 (wing ring aerological station sectional side view) side and bottom; But the wing ring aerological station as high-altitude battleship purposes could be provided with such launch hole and corresponding weaponry fully, well imagines for the commanding accurate strike power in vast zone, below!

Even only from communication function, the advantage that the present invention also has satellite or ground-based cellular systems not to compare.Compare with communication satellite; Cost of the present invention is not worth mentioning simply; And have signal round-trip delay short (the dialogue delay phenomenon such as making two places host in the television image is eliminated fully), the free space attenuation is few, helps realizing the miniaturization of communication terminal, the wireless access of broadband and symmetrical duplex; Compare with ground-based cellular systems, the decisive range of this aerological station is short, covering area is big, fading channel is little, thereby emissive power can significantly reduce.Not only greatly reduce the expense of building terrestrial information Infrastructure, and reduced the radiation pollution around the base station.

We can say; As long as hundreds of large-scale wing ring aerological stations of the overhead layout in soil that China is vast and vast coastal areas and territorial seas; Military capability of the country of China and civilian ability to communicate all will improve a level; Arrange tens of middle-size and small-size wing ring aerological stations as long as the South China Sea Islands is overhead, the several Southeast Asia micro state that occupies my oil of my islands and reefs, illegal mining will effectively be controlled, and existing air superiority of big countries such as the United States, Russia and sea superiority also will be done and dissolve!

This aerological station still one can never land from rotorcraft.Compare from rotorcraft with common; Except need not refueling and charge, it can also get into dynamic helicopter state from motorless from state of suspension when being necessary, during such as super-huge astrovehicle that surpasses unpowered bearing capacity in the needs carrying and emission control tower thereof; Can send to High Altitude Platform from ground conversely; Order about rotor and rotate sooner and produce enough lift, cut off power supply again after waiting the astrovehicle emission, recover unpowered, from state of suspension.

The high hollow wing ring wind-powered electricity generation mechanism of wing ring aerological station and front is the same; There is not power but can forever be suspended in the high-altitude; Why? Because the high wind in high-altitude can order about wing ring (rotor) high speed rotating; The fin cutting air of high speed rotating produces huge lift, as long as wind does not stop, tracting cable is continuous, this " aircraft " just falls down never.

Even something unexpected happened; This " Air fortress " can not resemble yet and fall as the sliding weight of steelyard that lands; It will be as from the slow safe falling of rotorcraft; Because whole decline process rotor all " is catching the wind " inevitably, so continue rotation, cutting air inevitably, the cutting air certainly leads to lift.

The beneficial effect of wind electric power ship:

Car, ship with traditional sail and the traction of umbrella shape kite; Can only utilize the low latitude wind-force below hundreds of rice, and can not electric power be provided, and the wind-powered electricity generation mechanism of this wind electric power ship can go up thousands of meters high-altitudes at any time in needs to car, ship; Utilize powerful high altitude wind; Even can be raised to the stratosphere of 2 myriametre height at any time, utilize constant and more powerful stratosphere wind-force, and in car, foot or the loading and unloading of berthing; Import powerful electric energy for the storage battery of car, ship; Therefore going up a slope or having enough powerful electric drive motor to implement independently to go under the situation against the wind yet,, even might not need fossil energy fully so the present invention can save more fossil energy than existing various boats and ships.

If replace high hollow wing ring wind-powered electricity generation mechanism with wing ring aerological station, replace common ship with capital ship, such just become to attach troops to a unit detecting station, high-altitude and the super battleship of high-altitude defence with attack base and power station, high-altitude are arranged.Electricity can replace partly or most fuel oil, and laser weapon or the ELECTROMAGNETIC WEAPON that also can directly supply with on the wing ring aerological station use.If connecting wing ring high-altitude water intaking device is technological again, the fresh water supply of warship and wing ring aerological station has also solved so.A cruiser like this will become common aircraft carrier jinx, and a such aircraft carrier will become the super aircraft carrier that surpasses any aircraft carrier.

The beneficial effect of wing ring high-altitude water obtaining device:

At present, in order to increase the supply of fresh water, except adopting conventional measure, outside diversion nearby or interbasin water diversion, a favourable approach is exactly to carry out the desalination of seawater or brackish water nearby.The method that seawater or brackish water are desalinated is a lot, but conventional method like the way of distillation, zeolite process, dialysis, reverse osmosis membrane and freezing etc., all will consume a large amount of fuel or electric power.It is reported that by nineteen ninety, the water-yielding capacity of the mounted sea water desalinating unit in the whole world is 13,000,000 meter/day.By 2000, this numeral was turned over one times, i.e. 2600 ten thousand steres.Increasing sharply of desalination water will produce a series of problem, and wherein the most outstanding is exactly the consumption problem of the energy.According to estimates,, produce the desalination water of 2600 ten thousand steres every day, need to consume 2.6 hundred million tons of crude oil every year with present technology.Even people are affordable the expense of this fuel, the greenhouse effect of the earth, atmospheric pollution etc. also must stop before going too far the caution people.Therefore, people generally believe at present, and the development desalination with Solar Energy is optimal selection.

But the solar seawater desalination cost is also very considerable, and coastal waters not, the place of many lacks of water, even the coastal waters, also can't utilize solar energy evening.Therefore, the human in recent years air water intaking device that can successfully fetch water of having developed, still existing device for fetching water from air is because energy consumption is too big; The cost that causes fetching water is too high; Mass production be can't implement, economic value, this external arid area (like the desert) that needs most air water-intaking also lacked with little type popularization; The air in its low latitude is equally extremely dry, and it is feasible hardly to carry out air water-intaking with existing technology.

Wing ring high-altitude water intaking device then reached fully no energy consumption, low cost, extensive and not round the clock branch, do not receive several highly difficult requirements such as region restriction.Since can be in the high-altitude self-supporting electric energy, do not have therefore that energy consumption is too big, the too high problem of water cost, can also supply power earthward simultaneously; Because water intaking device is suspended from the high-altitude; Especially be the high-altitude water intaking device of carrier with high hollow wing ring wind-powered electricity generation mechanism, can ascend to heaven to thousands of rice and even meters altitude by large-scale, the huge air water intaking device of load especially, even in the desert of arid; Equally there is cloud in its sky; Explain that its overhead water vapour is profuse, in fact water vapour be with the wind circulation in the whole world, the face of land, desert and low latitude drying too just; Moisture was cleared off already in air stream was crossed, even rainwater does not land as yet and just blotted by the air of arid.But this only is as far as ground and low latitude, to the air-flow in high-altitude less than influence.Therefore using the present invention to fetch water in the air is to receive the region restriction, even on the innerland, desert, also can equally with other places not have energy consumption, low cost, produces high-quality water on a large scale, incessantly.

No matter be samll cities and towns, a factory or a large-scale farm; No matter where be located in; As long as have one to be the high-altitude water intaking device of carrier, just can solve whole water, the electric demand of aspects such as industry, agricultural, pastoral farming, people's lives, public utilities fully with large-scale high hollow wing ring wind-powered electricity generation mechanism.And build a large-scale high hollow wing ring wind-powered electricity generation mechanism and be the high-altitude water intaking device of carrier with it, to compare with building traditional power plant, traditional water conservancy system or transporting water pipe-line system, cost that it is required and time only are a drop in the ocean!

Description of drawings

One, description of symbols

1: wing ring

1-1: outer wing ring

1-1-1: the outer wing ring in the outer wing ring group

1-1-2: the inner wing ring in the outer wing ring group

1-2: internal layer wing ring

1-2-1: the outer wing ring in the inner wing ring group

1-2-2: the inner wing ring in the inner wing ring group

1-3: upper strata wing ring

1-4: lower floor's wing ring

2: fin

2-1: to overhanging one-sided fin

2-1.3: the overhanging one-sided fin of upper strata wing hoop of the wing ring group of up-down structure

2-1.4: the overhanging one-sided fin of lower floor's wing hoop of the wing ring group of up-down structure

2-2: the one-sided fin of inwardly stretching

2-2.3: the one-sided fin of stretching in the upper strata wing hoop of the wing ring group of up-down structure

2-2.4: the one-sided fin of stretching in lower floor's wing hoop of the wing ring group of up-down structure

2-3: the double fins that stretches out to both sides

3: grooved track+scooter and assembly thereof

3-1: grooved track

3-2: the vehicle frame of scooter

3-3: the connecting rod between scooter and the scooter

3-3-3: scooter and extraneous connecting rod

3-4: pulley

3-4-3: among Fig. 9 its axially with other pulley spindles to vertical pulley

3-5: scooter

3-6: the connecting rod in scooter and cabin

3-7: the connecting rod of air duct wall and water intaking device

4: through the connecting rod of wing centre section ring medial axis

4-2: tab style spoke or connecting rod

4-3: the connecting rod of hollow (connecting rod and water pipe unification)

5: tracting cable (or tracting cable, cable two-in-one)

5-1: the hawser that connects high hollow wing ring wind-powered electricity generation mechanism of the superiors and the high hollow wing ring of second layer wind-powered electricity generation mechanism among Figure 13

5-2: the hawser that connects the second layer high hollow wing ring wind-powered electricity generation mechanism and the 3rd floor height hollow wing ring wind-powered electricity generation mechanism among Figure 13

5-4: the hawser that connects high hollow wing ring wind-powered electricity generation 19-1 of mechanism and water obtaining device 26-1

5-5: the hawser that connects wing ring high-altitude water intaking device 26-1 and wing ring water obtaining device 26-2

6: the shaft type generator

7: the generator motive power wheel

8: the track of shaft type generating wheel

10: the wind-tunnel inwall

10-1: the shell of water obtaining device (air duct)

11: the pylon strut

12: ground

13: ramjet

13-1: the ramjet of upper strata fin

13-2: the ramjet of lower floor's fin

13-3: the ramjet that is used to turn to

14: the cabin

15: the top layer platform

16: the space launch frame

17: defensive weapon

18: other facilities

19: high hollow wing ring wind-powered electricity generation mechanism or wing ring aircraft

19-1: the high hollow wing ring wind-powered electricity generation mechanism of the superiors among Figure 13

19-2: the high hollow wing ring wind-powered electricity generation mechanism of the second layer among Figure 13

19-3: the 3rd layer high hollow wing ring wind-powered electricity generation mechanism among Figure 13

20: ship

21: compressor

22: condenser

23: radiator

24: water receiving disc

25: water pipe type tracting cable (water pipe that the tracting cable function is arranged)

25-1: water pipe

26: water obtaining device

26-1: the upper strata water obtaining device among Figure 24

26-2: the lower floor's water obtaining device among Figure 24

Two, drawing explanation

Fig. 1: by being in same plane and by the same center of circle but the interior outer wing ring group plan view (left figure) that the different both wings ring of radius is formed, be in the last bottom wing ring group plan view (right figure) that the ring of both wings up and down of same shaft axis is formed by the center of circle;

Fig. 2: the independent plan view of each wing ring of outer wing ring group among Fig. 1;

Fig. 3: the independent plan view of each wing ring of going up bottom wing ring group among Fig. 1;

Fig. 4: with wing ring support is the high hollow wing ring wind-powered electricity generation mechanism sectional drawing that inside and outside two wing rings of iron core winding support constitute;

Fig. 5: with wing ring support is the high hollow wing ring wind-powered electricity generation mechanism sectional drawing that two wing rings up and down of iron core winding support constitute;

Fig. 6: with wing ring support is the high hollow wing ring wind-powered electricity generation mechanism sectional drawing that inside and outside two wing rings of common generator pit constitute;

Fig. 7: with wing ring support is the high hollow wing ring wind-powered electricity generation mechanism sectional drawing that two wing rings up and down of common generator pit constitute;

Fig. 8: with wing ring support is the high hollow wing ring wind-powered electricity generation mechanism sectional drawing that two wing rings up and down of common generator pit constitute;

Fig. 9: grooved track and scooter structural representation;

Figure 10: being by being in same plane and the same center of circle being arranged but high hollow wing ring wind-powered electricity generation mechanism plan view that two different wing ring groups of radius constitute, also is by being in different aspects but high hollow wing ring wind-powered electricity generation mechanism plan view that the center of circle is on the same shaft axis and radius is different two wing ring groups constitute;

Figure 11: be by being in same aspect but high hollow wing ring wind-powered electricity generation mechanism's plan view (last figure) that two different wing ring groups of radius constitute, and the sectional side view of corresponding position (figure below);

Figure 12: be by being in different aspects but the sectional side view of the high hollow wing ring wind-powered electricity generation mechanism that the center of circle is on the same shaft axis and radius is different two wing ring groups constitute

Figure 13: be a plurality of high hollow wing ring wind-powered electricity generation mechanism polyphone side view;

Figure 14: be wind tunnel type wing ring wind-powered electricity generation mechanism front view;

Figure 15: be wind tunnel type wing ring wind-powered electricity generation mechanism side cross section view;

Figure 16: be tower generator front view;

Figure 17: be tower generator lateral plan;

Figure 18: be wing ring aircraft plan view;

Figure 19: be wing ring aircraft sectional side view;

Figure 20: be wing ring aerological station plan view;

Figure 21: be wing ring aerological station sectional side view;

Figure 22: wing ring wind electric power ship side view;

Figure 23: wing ring high-altitude water intaking device sectional side view;

Figure 24: go here and there hanging wing ring high-altitude water intaking device side view.

Most preferred embodiment

Introduce several embodiments below in conjunction with accompanying drawing.

High hollow wing ring wind-powered electricity generation mechanism for implementing example one (as shown in Figure 4):

Support with wing ring 1-1, wing ring 1-2 is that support is provided with iron core, winding respectively, and these two wing rings are in same plane, the phase concentric is arranged but radius is different; The two ends up and down of wing ring 1-1, wing ring 1-2 connect ring track 3-1 respectively, and track 3-1 is around one week of wing ring, in fact with wing ring consubstantiality; The cross section of track 3-1 is a grooved, coupling scooter 3-5 (the little figure in lower right is grooved track and scooter compound mode schematic representation) in the grooved track; Scooter is formed (seeing for details in Fig. 9) by vehicle frame 3-2, connecting rod 3-3, pulley 3-4; Equidistant several (being no less than three) scooter 3-5 that is provided with on each track; Adjacent scooter 3-5 connects through connecting rod 3-3 in twos; Its effect is that the vehicle frame of two scooters on the different wing rings is connected and fixed, and two respectively coupling still can go slick in not co-orbital scooter, therefore though two wing rings rapidly rotate towards different direction separately; But keeping constant relative position forever, more can not be separated from each other or collide.

Article one, the scooter of relevant position is connected mutually through connecting rod 3-3 on the track of each scooter on the track and another wing ring; The two ends of connecting rod 4 are connected with a connecting rod 3-3 respectively; Each bar connecting rod 4 intersects on the shaft axis of wing ring; And be mutually permanently connected at intersection point; Except that intersection point is fixedly connected; Can also be between each connecting rod 4 that intersects the welding strut to form triangle moment structure, if be not enough to also guarantee that the relative position of each scooter does not change with the rotation of wing ring, that just should be the whole connecting rod 3-3 that connect the scooter on two tracks between the adjacent foil ring with connecting rod be linked in sequence (ring or the polygonal of a closure of formation).

In this embodiment, each fin of same wing ring, their area must be identical, but the sail area of different wing rings can be different.Because the efficient of interior ring fin collection wind energy is littler than outer shroud fin of the same area; Therefore the area of ring fin as for both scale, must be followed a principle greater than the outer shroud sail area in must letting; The efficient of the wing ring collection wind energy of two counter-rotatings is equated; Two rings torsion in the counter-rotating process of facining the wind is cancelled out each other, avoid complete machine, thereby guarantee that mechanism continues proper functioning and stop to twist the cable accident to take place with that bigger wing ring rotation of torsion.

As for the angle of attack of fin, if the angle of attack of outer wing ring fin is n, the angle of attack of inner wing ring fin is-n so, so both wings ring sense of rotation is inevitable opposite, the iron core winding on the both wings ring generates electricity with fin counter-rotating cutting magnetic line.

The circuit of power facility is through brush conjunction cable upper end, and the cable lower end is connected with ground electricity consumption facility.No matter what electrodes generator is provided with; Earlier the same joint that is parallel to of ability parallel connection; Then each joint is connected with corresponding brush track; The brush track is attached to the outer (between brush track and the wing loop orbit dielectric isolation layer will be set) of wing annular groove type track 3-1, and the brush track is touched with brush separately and is communicated with, and external circuits links to each other with brush; Brush then is fixed on the outer connective pole of scooter vehicle frame, and the brush track that rotates has so just formed continual circuit with brush and has been connected.

All pass wing ring axis at each bar connecting rod 4, their two ends are connected with separately scooter 3-3 respectively; Each bar connecting rod 4 intersects in same point and wing ring axis, and connecting rod 4 just connects the upper end of tracting cable on this crosspoint, and the lower end of tracting cable connects below electricity consumption facility.

Can implant tracting cable inside to cable, tracting cable and cable are united two into one.

High hollow wing ring wind-powered electricity generation mechanism for implementing example two (as shown in Figure 5):

Three wing rings 1 with the homophase diameter are arranged above and below by same shaft axis, up and down the wing ring 1 at two ends respectively have a track 3-1 around, middle wing ring 1 have two track 3-1 around; Equidistant several (being no less than three) scooter 3-5 that is provided with on each track; The pairing of the scooter of the scooter of upper limb ring and wing centre section ring upper edge, the scooter of wing centre section ring lower edge and the pairing of the scooter of bottom wing ring, per two scooters (last, down) are a pair of, every pair of scooter all passes through connecting rod 3-3 connection.

Support with three wing rings 1 is that support is provided with iron core, winding respectively; Middle wing ring is opposite with wing ring sense of rotation up and down; Therefore can cutting magnetic line and generate electricity, the fin angle of attack of the superiors and undermost two rings is identical, area is identical, thereby makes this two wing rings do rotation synchronously; The electric current of their winding generation or the magnetic line of force are the same like this, can not interfere with each other.

If the fin angle of attack of the superiors and two wing rings of orlop is n, the fin angle of attack of so middle wing ring is-n.The fin of same wing ring the same side (the promptly unified outside or the inboard of stretching to ring); Their area must be identical; But the area of the fin of homonymy can be not different for the fin of different wing rings or same wing ring; Do suitably adjustment to their area, the wind energy that all fins that turn clockwise and all fins that are rotated counterclockwise are gathered equates.

Each bar track 3-1 is all around its one week of wing ring, and in fact it dissolves with wing ring and is one; The cross section of track 3-1 is a grooved, coupling scooter (vehicle frame 3-2, connecting rod 3-3, pulley 3-4 by being contained within the grooved track 3-1 form, and see Fig. 9 for details) in the grooved.Because two adjacent scooter 3-2 connect through connecting rod 3-3, though therefore two wing rings can not be separated from each other or collide separately towards the different direction rotation.

As for connecting rod 3-3 and connecting rod 4 and tracting cable, cable, the setting of brush and the linkage structure between them, please with reference to embodiment one.

High hollow wing ring wind-powered electricity generation mechanism for implementing example three (as shown in Figure 6):

Inner wing ring 1-2 is in same plane with outer wing ring 1-1, the phase concentric is arranged but radius is different; On these two wing rings, press several shaft type generators 6 of equidistant installation respectively; Wing ring support is as the support of shaft type generator 6; The motive power wheel 7 of the generator on each wing ring all with another wing ring on ring track 8 coupling mutually, wheel is certainly imitateed train wheel and track for a train with the coupling manner of rail, but best mode is employing intermeshed gear and tooth-like track.

As for the setting of connecting rod 3-3 and connecting rod 4 and tracting cable, cable, brush and the linkage structure between them with reference to embodiment one.

High hollow wing ring wind-powered electricity generation mechanism for implementing example four (as shown in Figure 7):

Upper limb ring 1-3 is in same plane with bottom wing ring 1-4, the phase concentric is arranged but radius is different; On these two wing rings, press several shaft type generators 6 of equidistant installation respectively; Wing ring support is as the support of shaft type generator 6, the motive power wheel 7 of the generator on each wing ring all with another wing ring on ring track 8 coupling mutually.

As for the setting of connecting rod 3-3 and connecting rod 4 and tracting cable, cable, brush and the linkage structure between them with reference to embodiment one.

The structure at other each positions is such as embodiment two.

High hollow wing ring wind-powered electricity generation mechanism for implementing example five (as shown in Figure 8)

Except that generator axially from vertically becoming the level, its remove structure and embodiment four identical.

High hollow wing ring wind-powered electricity generation mechanism for implementing example six (like Figure 10, shown in Figure 11)

Inside and outside two wing ring groups are in same plane, the same center of circle is arranged but radius is different; Inner wing ring 1-1-2 in outer wing ring 1-2-1 in the inner wing ring group and the outer wing ring group is fixedly connected, rotates synchronously through tab style spoke 4-2; These spokes are spokes of flap-like; Therefore both played the effect of spoke, the function of fin had been arranged again.The Placement of middle on the same group both wings ring is identical with embodiment one, and the setting of the connecting rod 3-3 of inner wing ring group and connecting rod 4 and tracting cable, cable, brush and the linkage structure between them, also please with reference to embodiment one.

Connect as for the circuit of inside and outside both wings ring: each electrode in the outer wing ring group by the method among the embodiment one with separately accordingly brush be connected; And each brush is connected with separately electric wire respectively; These electric wires extend to inner wing ring group and parallelly connected with the circuit of the corresponding brush of this wing ring group through tab style spoke or connecting rod 4-2, and the brush of inner wing ring should be installed on the connecting rod 3-3 that connects two different wing ring top sheave cars.The connecting means of inner wing ring and external circuits is please with reference to embodiment one

High hollow wing ring wind-powered electricity generation mechanism for implementing example seven (like Figure 10, shown in 12)

Two radius differences but the center of circle is in the wing ring group on the same axis up and down; The Placement of upper limb ring 1-3 in bottom wing ring 1-4 in the upper limb ring group and the bottom wing ring group: the bottom wing ring in the upper limb ring group is fixedly connected with tab style connecting rod 4-2 with upper limb ring in the bottom wing ring group; The angle of attack of fin 2-1.4 in fin 2-1.4 in the upper limb ring group and the bottom wing ring group must be the same, and they facing the wind the direction of rotation must identical (can only be synchronized with the movement because of them).

The setting of the connecting rod 3-3 of bottom wing ring group and connecting rod 4 and tracting cable, cable, brush and the linkage structure between them are also please with reference to embodiment one.

Connect as for the circuit of both wings ring up and down: each electrode in the upper limb ring group by the method among the embodiment one with separately accordingly brush be connected; And each brush is connected with separately electric wire respectively; These electric wires extend to bottom wing ring group and parallelly connected with the circuit of the corresponding brush of this wing ring through tab style spoke or connecting rod 4-2; With regard to present embodiment, the brush of bottom wing ring should be installed on the connecting rod 3-3 of inboard two scooters up and down of wing ring.The connecting means of bottom wing ring and external circuits is please with reference to embodiment one.

High hollow wing ring wind-powered electricity generation mechanism for implementing example eight (shown in figure 13)

The upper end of the lower end connection cable 5-1 of the high hollow wing ring wind-powered electricity generation 19-1 of mechanism; The lower end of hawser 5-1 connects the upper end of the high hollow wing ring wind-powered electricity generation 19-2 of mechanism; The upper end of the lower end connection cable 5-2 of the high hollow wing ring wind-powered electricity generation 19-2 of mechanism; The lower end of hawser 5-2 connects the upper end of the high hollow wing ring wind-powered electricity generation 19-3 of mechanism, and the lower end of the high hollow wing ring wind-powered electricity generation 19-3 of mechanism connects the upper end of tracting cable 5, and the lower end of tracting cable 5-3 connects ground installation; The circuit of the high hollow wing ring wind-powered electricity generation 19-1 of mechanism, 19-2,19-3 is made parallel connection or polyphone, and converging is that a cable is connected with ground electricity consumption facility, and this cable can unite two into one with tracting cable 5-3.

Preferably the high hollow wing ring wind-powered electricity generation 19-1 of mechanism, 19-2,19-3 are let fly away in same airflow layer when adopting present embodiment, the voltage that makes each machine send is identical, makes things convenient for each machine to generate electricity by way of merging two or more grid systems and carries downwards with same cable 5-3.

Wind tunnel type wing ring wind-powered electricity generation mechanism for implementing example (like Figure 14, shown in Figure 15)

The wing ring group of the wind tunnel type wing ring wind-powered electricity generation mechanism of present embodiment is on the same shaft axis, parallel two wing ring 1-3 and wing ring 1-4 forms by the center of circle, and the angle of attack of the angle of attack of fin 2-2.3 and fin 2-2.3 is opposite.

The Placement of wing ring 1-3, wing ring 1-4 and wind-tunnel wall: grooved track 3-1 is around wing ring one week and be combined as a whole with it, three pulleys of scooter respectively with three face couplings of grooved track 3-1, the vehicle frame 3-2 and the wind-tunnel wall 10 of scooter are fixedly linked.

As for the circuit on the wing ring of two rotations and the connecting means of external circuits, can be with reference to embodiment one.

Tower wing ring wind-powered electricity generation mechanism for implementing example (like Figure 16, shown in 17)

Its wing ring wind-powered electricity generation mechanism by be in same plane, by the same center of circle but different two wing ring 1-1 and the wing ring 1-2 of radius form, the angle of attack of the angle of attack of outer wing ring fin 2-1 and inner wing ring fin 2-2 is opposite.

This wing ring wind-powered electricity generation mechanism provides support power by 6 pylon they sup-port 11-1,11-2,11-3,11-4,11-5,11-6; Wherein front-seat strut from left to right successively label be 11-1,11-2,11-3; Back row's strut from left to right successively label be 11-4,11-5,11-6; Middle strut 11-2 need only be connected with the connecting rod 3 of wing ring lower end with 11-4; Its height need only reach wing ring lower end, and the strut 11-1 of both sides, 11-3,11-4,11-6 are connected with the connecting rod 3 of wing ring both sides, and it highly need only reach the middle part of wing ring; The strut why Here it is sees from Figure 17 is " half "; Because strut 11-3, the 11-6 of Here it is both sides, the top of this two pole links to each other with the connecting rod 3-3 of (waist) rear and front end, wing ring wind-powered electricity generation mechanism middle part respectively and provides support power, and these two connecting rod 3-3 are in the outside side of drawing.

As for the circuit on the wing ring of two rotations and the connecting means of external circuits, can be with reference to embodiment one.

Wing ring aircraft embodiment (like Figure 18, shown in Figure 19)

On wing ring 1-3, the wing ring 1-4 grooved track 3-1 is arranged all, grooved track 3-1 coupling scooter 3-5, the vehicle frame of scooter links to each other with cabin 14 through connecting rod 3-6, and the top, cabin is cross four ramjet 13-3 that are used to turn to is installed, and puff prot is outwardly.

The end of each fin is installed the ramjet 13-1 that is used to promote wing ring, and the jet direction of the angle of attack of fin 2-1.3 and ramjet thereof and the fin 2-1.4 angle of attack and ramjet thereof are jet in the opposite direction.

Aerological station embodiment one (like Figure 20, shown in Figure 21)

On a last embodiment (wing ring aircraft embodiment) basis, remove all ramjets, and change the cabin into multilayer, it is the open platform at the middle and upper levels, and platform is provided with space launch frame 16, defensive weapon 17, other facilities 18.

On wing ring 1-3, wing ring 1-4, the iron core winding is set, concrete grammar is referring to high hollow wing ring wind-powered electricity generation mechanism for implementing example two, four, five.

Connect connecting rod 4 in cabin bottom, the rarest two and be on the medial axis that cross intersects at wing ring of connecting rod 4 connects the upper end of tracting cable 5 at this intersection point, and the lower end of tracting cable 5 connects ground installation.

Wing ring wind electric power ship embodiment (shown in figure 22)

The lower end of high hollow wing ring wind-powered electricity generation mechanism 19 connects the upper end of tracting cable 5, and the lower end of tracting cable 5 connects the deadman of ship; The circuit of high hollow wing ring wind-powered electricity generation mechanism 19 links to each other with cable, and cable links to each other with the storage battery of ship, and storage battery links to each other with motor circuit.

Wing ring high-altitude water intaking device embodiment (shown in figure 23)

High hollow wing ring wind-powered electricity generation mechanism and water obtaining device are combined, and the former circuit and the latter's circuit is connected, and:

The water intaking operation mechanism of water obtaining device is enclosed within the wing ring of high hollow wing ring wind-powered electricity generation mechanism, and the shell of water obtaining device is an air duct 10-1, and the air duct two ends are all the horn mouth shape.The outer wall of air duct 10-1 is connected with all scooter 3-5 of both wings ring up and down through connecting rod 3-6, scooter and grooved track 3-1 coupling, and each grooved track 3-1 is respectively around one week of wing ring separately, wing ring 1-3 connection fin 2-1.3, wing ring 1-4 connection fin 2-1.4.

The water intaking operation mechanism of water obtaining device is made up of air conditioner refrigerating device 21, condensation water-collecting machine 22, water receiving disc 24, air conditioner heat radiator 23, water pipe 25-1; Except that increase water receiving disc, reduce fan, radiator be placed on public attention, the condensation water-collecting machine be placed on down public attention and existing air conditioner basic identical.The operation mechanism of water obtaining device is connected and fixed on the inwall of air duct 10-1 through connecting rod 3-7, and its bottom links to each other with connecting rod 4.

The rarest two and be on the medial axis that cross intersects at wing ring of connecting rod 4 connects the tracting cable joint of water pipe type tracting cable 25 upper ends of hollow at this intersection point, and the water pipe of water pipe type tracting cable continues to extend and upwards is connected with the water outlet of water receiving disc; The lower end of water pipe type tracting cable 25, water pipe separates with tracting cable, and tracting cable connects ground installation, and water pipe links to each other with pond or aqueduct.

High-altitude water intaking device embodiment two (shown in figure 24)

The lower end of the lower end connection cable 5-4 of the high hollow wing ring wind-powered electricity generation 19-1 of mechanism; The lower end of hawser 5-4 connects the upper end of water obtaining device 26-1; The upper end of the lower end connection cable 5-5 of water obtaining device 26-1, the lower end of hawser 5-5 connects the upper end of water obtaining device 26-2, the joint of the tracting cable that water pipe type tracting cable 25 upper ends of the lower end connection hollow of water obtaining device 26-2 branch away; The lower end of water pipe type tracting cable 25 connects ground installation, and concrete grammar is referring to a last embodiment.

Equidistant 4 points of getting at horn mouth edge, the upper end of water obtaining device 26-1,26-2; Two ends with the identical hawser of two length are connected to 2 points on the same diameter, the tie point (shown in the partial enlarged drawing among Figure 24) of the tracting cable that the intersection point of this two cable hangs down as the top.

The high hollow wing ring wind-powered electricity generation 19-1 of mechanism is connected as circuit with two water obtaining device; The water receiving disc of two water obtaining device is connected with separately outlet pipe respectively, outlet pipe separately all with the water pipe type tracting cable 25 of hollow in the upper end of water pipe join.

Claims (9)

1. high hollow wing ring wind-powered electricity generation mechanism; By rotor iron core winding and stator core winding relative movement generating; The iron core winding is promoted by wind wheel, and frame provides the facility of tractive force to link to each other through tracting cable and below, and the circuit of power facility links to each other with the upper end of cable; The lower end of cable links to each other with below electricity consumption facility, it is characterized in that: equidistantly on annular support fin is set and forms wing ring; Its fin adopts the cutting air can produce the fin of lift, and each fin all as the latter end of the fin of common wind wheel, forms angle between the circumferential surface of aerofoil and wing ring, i.e. angle down with the wind; Fin can stretch out outside ring or in the ring, also can stretch out to both sides simultaneously; The angle of facining the wind of all fins is identical on the same wing ring, and the angle of facining the wind of adjacent wing ring is opposite; Form a wing ring group by two to three wing rings, each wing ring or be in same plane and the same center of circle is arranged, or each wing ring on the same group parallel surface and center of circle each other is on the same shaft axis; Can have only one group of wing ring in the complete machine, two groups or more wing ring also can be arranged, every group of wing ring can constitute a complete power facility; Can join end to end through tracting cable between two or more high-altitude generating ring complete machines; Promptly be in the complete machine of upper end or following public attention; Its lower end is connected through the upper end of another complete machine of tracting cable and below or last public attention, and the circuit of each complete machine finally is connected with ground electricity consumption facility through same cable through cable is continuous.

2. high hollow wing ring wind-powered electricity generation according to claim 1 mechanism, it is characterized in that: the support with each wing ring in the same wing ring group is that support is provided with stator iron core, winding or rotor iron core respectively, winding makes whole wing ring consist of a generator that does not rely on axle to drive rotor; The perhaps equidistant generator that line shaft is installed on the support of wing ring lets ring track coupling mutually on wheel and the adjacent arbitrary wing ring on the generator line shaft, and ring track is established around ring and is connected as a single entity with wing ring.

3. wind tunnel type wing ring wind-powered electricity generation mechanism; It is characterized in that: the described high hollow wing ring wind-powered electricity generation of claim 1 mechanism places among the wind-tunnel; Cored winding of institute and circuit are all made waterproof sealing; Give up the fin that original tracting cable and guide vane ring stretch out outward, and the track and the scooter thereof in the fin that stretches out in the reservation guide vane ring and the wing ring outside, the vehicle frame of scooter links to each other with the wind-tunnel inwall; Wind-tunnel or level trend, perhaps capwise.

4. tower wing ring wind-powered electricity generation mechanism is characterized in that: select for use each wing ring parallel surface and the center of circle to be in the high hollow wing ring wind-powered electricity generation mechanism of high hollow wing ring wind-powered electricity generation mechanism on the same shaft axis each other, remove the tracting cable between mechanism and the ground; And remove the connecting rod (4) that connects tracting cable and wing ring wind-powered electricity generation mechanism, with the axial water intaking of wing ring mechanism square to, then; Perhaps inner wing is extended to the place, axle center; Be connected with bearing outer wall, bearing inner wall is connected with axle, and the two ends of axle are connected with the top of support tower; Perhaps the scooter connecting rod (3-3) with wing ring group front and back is connected with strut, wherein at both sides and the middle minimum strut that respectively is provided with positive, the back side.

5. wing ring aircraft; Aircraft has the wing; The wing moves in air and produces lift; It is characterized in that: mechanism is the basis with the described high hollow wing ring wind-powered electricity generation of claim 1, is fixedly connected or hangs the cabin on the scooter vehicle frame of the connector between the connector between its original wing ring body or wing ring body and tracting cable; And; Perhaps with original be that the iron core and the winding of support setting removed directly with wing ring; And at the fin top of wing ring installation ramjet; Perhaps original shaft type motor is removed and explosive motor go up to be installed in position, perhaps keep original shaft type motor or annular core, winding and supply power from ground to them, or storage battery is set on its body supplies power to them through cable; On the position that cabin body or connector etc. can not rotate with wing ring, install or do not install the jet power of substantially horizontal Driving force engine is provided.

6. wing ring aircraft according to claim 5 is characterized in that: original tracting cable that is connected with the below of body and cable can be removed or keep, and also can only keep tracting cable and cable is changed to oil pipe, even tracting cable and oil pipe are united two into one; Fin can keep the characteristic that can produce lift from rotor cutting air, also can not keep this characteristic and adopts the characteristic of the fin of common propeller cavitation.

7. wing ring aerological station; High hollow wing ring wind-powered electricity generation mechanism according to claim 1 or the described wing ring of claim 5 aircraft is characterized in that: plug-in or be built-in with in following various device, the facility whole, partly or one of them: electronic equipment, communication apparatus, remote sensing equipment, the equipment of taking photo by plane, scientific experiment equipment, defensive weapon, astrovehicle emission and reclaim platform, crane gear, up-down cabin, recreational facilities, personnel working room.

8. wing ring wind electric power ship; Boats and ships bolt tracting cable lower end; The tracting cable upper end connects the aircraft that leans on wind-force to promote; It is characterized in that: the described high hollow wing ring wind-powered electricity generation of claim 1 mechanism, the lower end of its tracting cable connects the towing point on the boats and ships, and its cable is connected as circuit with the storage battery or the motor of boats and ships.

9. wing ring high-altitude water intaking device, device for fetching water from air is made up of air conditioner refrigerating device, condenser, water receiving disc, air conditioner heat radiator, fan etc., it is characterized in that: the circuit of the described high hollow wing ring wind-powered electricity generation of claim 1 mechanism is connected with the circuit of device for fetching water from air; The water outlet of the water receiving disc of device for fetching water from air is connected with the water pipe upper end, and the water pipe lower end is connected with the below wet pit or with drainage facility; The vehicle frame of high hollow wing ring wind-powered electricity generation mechanism wing loop orbit scooter is connected with the support or the shell of air water-intaking mechanism through connecting rod; Or the tracting cable of high hollow wing ring wind-powered electricity generation mechanism passes from the center portion of air water-intaking mechanism; Air water-intaking mechanism hangs on the tracting cable, can hang one or more; Water pipe perhaps unites two into one with tracting cable, does not perhaps unite two into one with tracting cable.

Images