CN102384042A

CN102384042A - Wing ring, four wing ring mechanisms, two wing ring airplanes and wing ring counter-pulling wind power mechanism

Info

Publication number: CN102384042A
Application number: CN2011102796483A
Authority: CN
Inventors: 罗琮贵
Original assignee: 罗琮贵
Current assignee: Beihai wing ring Aviation Equipment Co.,Ltd.
Priority date: 2011-09-20
Filing date: 2011-09-20
Publication date: 2012-03-21
Anticipated expiration: 2031-09-20
Also published as: CN102384042B

Abstract

A wing ring, four wing ring mechanisms, two wing ring airplanes and a wing ring counter-pulling wind power mechanism adopt wing ring mechanisms. In the wing ring, an axle center of a common wind wheel and a low-efficiency wing are removed, and a whole wing is a high-efficiency wing, so that an actuating arm for supporting the wing is not only shortened by several times, but also the number of the actuating arm is increased to two from 1, and single-side supporting is changed into double-side supporting. A blended wing ring group mechanism utilizes mutual supporting of multiple wing rings and multilayer to obtain sufficient mechanical strength and wind resistance, so that common steel products and aluminum products can be applied to building the wing ring airplanes with the diameter being hundreds of meters and even thousands of meters. Lifting force is provided for the wing ring mechanism with a fixed wing and a wing ring type in-situ takeoff and landing airplane by the fixed ring, so that the wing ring faces the wind on the front, further, maximum flying power or power generation effect are achieved, and the maximum net bearing capacity can reach thousands of tons and even tens of thousands of tons. The wing ring counter-pulling airplanes and the wing ring counter-pulling wind power mechanism obtain stable lifting force through reversed tension of reverse advection wind at the upper layer and the lower layer of an advection layer or a trade wind area, so that permanent self-suspension, universal autonomous cruise and continuous power generation all the year round are realized.

Description

Wing ring, four kinds of wing ring mechanisms, two kinds of wing ring aircrafts and wing ring are to drawing wind-powered electricity generation mechanism

Technical field

Wing ring relates to a kind of wind wheel or water wheels, fin rotation around the center of circle, and each fin top equates that with the distance in the center of circle distance between each fin equates.

Wing ring mechanism relates to wing ring and a kind of wind wheel organization or wheel mechanism.

Wing ring group mechanism; Relate to a kind of by two or more rotary wing type wind wheels or water wheels and same support or same rotor combination that is connected and forms; Especially the existing rotor that turns clockwise of wing ring in this rotor combination; The rotor that is rotated counterclockwise is also arranged, and the whole rotors that are rotated counterclockwise and whole rotors of turning clockwise gather in the section at one time wind energy or current can a total amount equate.

Mix wing ring group mechanism, connect to form by a plurality of wing ring group mechanisms and same support.

The wing ring mechanism of band fixed-wing relates to a kind of rotor mechanism and fixed-wing aircraft.

Wing ring type original place landing aircraft, relating to a kind of is angle of rake fixed wing aircraft and gyrodyne with propeller cavitation.

A kind of energy-autarchic, the wing ring that freely cruises be to drawing aircraft, relates to a kind of buoyant means that places wind or water that links together through tracting cable or connecting rod and ground or water-bed immovable point.

Wing ring relates to a kind of linking together mutually through tracting cable or connecting rod and places the buoyant means of wind or water drawing wind-powered electricity generation mechanism.

Background technique

At present all rotor mechanisms or wind wheel, wheel mechanism all have axle and link with axle; This is severely limited rotor mechanism or wind wheel, the diameter of wheel mechanism and the area of effective wing panel; Be difficult to further to expand, more can't realize rotor mechanism or wind wheel, the wheel mechanism of hundreds of rice and even thousands of rice diameters.

All large aircrafts all can not utilize natural energy resources especially can not utilize the wind energy that is easy to obtain most to originate as flying power at present.

The constraint of tracting cable all can not be broken away from all upper wind electrical mechanisms or aloft work stations (comprising the makings balloon) at present, or says so and have to rely on the contrary wind component that tracting cable provides, otherwise will fall with the wind or fly away.

Summary of the invention

One, innovation order (rotor)

Present wind wheel (rotor) generator, hydraulic turbine generator and rotor craft, the angle of rake something in common of propeller for vessels are to adopt the fin that links with axle, and this kind fin has three deadly defects of axle:

(1) each fin from the axle center outward most of wing panel collection wind or to pull out outlet capacity little, and the closer to the wing panel in axle center gather wind, pull out water can render a service more little, until being zero; Real efficient collection wind pulls out the hydrofoil section just more away from the wing panel in axle center, renders a service highly more more away from the axle center, 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 weight, has hindered mechanism's body further to enlarge; Increased detrimental resistance simultaneously, 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.

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 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), provide a kind of bodily form huge, diameter can reach thousands of meters aviation mechanism or wind wheel, water wheels, rotor mechanism.

(4) provide that a kind of bodily form is huge, carrying capacity is huge and also agile, at the fuselage datum line original place landing aircraft of flight fast that is the level of state down.

(5) provide that a kind of cost is extremely low, energy-autarchic and body and carrying capacity is huge, can be to aircraft or the permanent aloft work station that any substantially horizontal is freely cruised.

(6) provide huge, the single cover of a kind of bodily form mechanism generated energy can surpass a nuclear power station, need not tracting cable and naturally permanent suspension, the upper wind electrical mechanisms.

Two, technological scheme

Wing loop technique scheme:

The equidistant fin that is provided with on annular support, each fin links to each other with annular support and does not link to each other with the axle center; Form angle between the circumferential surface of each fin aerofoil and annular support, the angle promptly facings the wind; Fin perhaps stretches out outside ring, perhaps in ring, stretches out, and perhaps stretches out (respectively shown in three little figure among Fig. 1) to the inside and outside both sides of ring simultaneously; Fin on the same annular support or the common fin of unified employing, or the unified fin that adopts the cutting air can produce lift; Fin on the same annular support, thereby or unified directly linking to each other form the changeless angle that facings the wind with annular support, thereby or unifiedly can change the fin at the angle that facings the wind through the formation that links to each other with annular support of blade deflection mechanism.

In fact wing ring can be regarded as the closed ring of the fixed-wing aircraft end-to-end formation of double-vane or single-blade.The use of wing ring is to replace existing wind wheel, water wheels or rotor and applies to fields such as wind-driven generator, hydraulic turbine generator, marine propeller, aircraft engine.

Wing ring is actually a special rotor wind wheel, and is different with common rotor wind wheel, and its fin does not link with the axle center; 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; Utilize pulling force entad to reach the purpose of reinforcing ring body through between ring body and axle center, setting up spoke, in this case, if necessary; Can be wing with spoke design, make the effect of its existing spoke that the effect of fin arranged again.

Wing ring mechanism technological scheme:

Form by wing ring, scooter track, scooter; Wherein the scooter track is connected with the scooter coupling; And the annular support of wing ring; Perhaps be connected and each scooter vehicle frame is connected with the ring support of another wing ring or scooter support or other rigid objects with solid shape of another wing ring mechanism, perhaps be connected and the scooter track is connected with ring support or other figurate rigid objects of another wing ring with the vehicle frame of scooter with the scooter track; The joint of scooter track or scooter vehicle frame and wing ring ring support; Be arranged in two sides of wing ring annular support or a place of four positions such as inner ring circumference side, outer ring circumference side; And connection part forms annular trace or tie point and becomes equidistant points on the annular trace (center of circle of the center of circle of this annular trace and wing ring ring support is overlapping or be on the same shaft axis), these positions with wing ring annular support or directly link to each other perhaps pass through connecting rod, support is continuous; The scooter track or with annular support have the same center of circle or and be close together with ring support, perhaps the center of circle of its center of circle and annular support is on the same shaft axis and is parastate with ring support; A wing ring mechanism has the scooter track that is no less than, and the scooter of every scooter track coupling is no less than three, and the scooter spacing on the same scooter track equates; The scooter track is a ring, and its center of circle and wing ring support are overlapping or be on the same shaft axis.

Wing ring mechanism or be connected with another wing ring or wing ring mechanism and constitute wing ring group mechanism; Perhaps be connected and become the some of wing ring mixed organization with the support of wing ring mixed organization or connecting rod; Perhaps with platform, pylon be formed by connecting for ground windmill or the power that becomes the surface wind electrical mechanisms partly, perhaps being formed by connecting with aircraft fuselage is the special propeller cavitation or the rotor of aircraft.

The coupling manner of scooter and its track must make scooter move along the circumferential direction that track stretches, and can not move along any direction on the cross section of track.If the cross section of scooter track is a grooved; The mode of scooter track and scooter coupling so; Perhaps as scooter track in Fig. 4 and scooter zygosome 3; The rarest 3 pulleys of scooter are three walls that the track the inside of flute profile is withstood track outward from cross section, and perhaps as the scooter track in Fig. 6 and scooter zygosome 3, the rarest 5 pulleys of scooter are the wall that withstands four different direction of track inside the track of flute profile outward from cross section; If the cross section of scooter track is a T shape; Scooter track and scooter coupling then should be adopted dual mode shown in Figure 2 so; A kind of be three pulleys from three directions by outside clamp T shape track inward, a kind of be five pulleys from four direction by outside clamp T shape track inward.

Wing ring mechanism is the basic important document that constitutes wing ring group mechanism, mixes wing ring group mechanism, also can be directly as the wind wheel of ground or upper wind electrical mechanisms, or direct propeller cavitation as aircraft or engine for boat.

The compound mode of wing ring mechanism and generator or motor: equidistant generator or the motor that line shaft is installed on the ring support of wing ring; And on ring support next door the ring track of relative set and generator or the coupling of generator motive power wheel; This ring track and wing ring ring support have the same center of circle or its center of circle and the wing ring center of circle to be on the same shaft axis; Track or be arranged in the same wing ring group mechanism adjacent foil ring that provides support another counter-rotating of power for this wing ring; Perhaps be arranged on support, platform, pylon, the aircraft fuselage; Also can be conversely, generator is arranged on adjacent foil ring or support, platform, pylon, hull, aircraft fuselage etc., and the track of the motive power wheel institute coupling of generator, motor is arranged on the support of wing ring.

If wing ring mechanism is as the surface wind electrical mechanisms; Can be only with single wing ring mechanism; If rotor as aircraft propeller or upper wind electrical mechanisms; Just must wherein also must be provided with the wing ring mechanism that turns clockwise and be rotated counterclockwise simultaneously, and the whole wing rings that turn clockwise must equate with the torsion of the wing ring that is rotated counterclockwise with two or more single wing ring mechanisms.

The Placement of wing ring mechanism and aircraft; Perhaps fuselage is enclosed within the wing ring; Perhaps wing ring is placed top or following (make the longitudinal axis of fuselage vertical) of fuselage or both wings with the medial axis of wing ring; Perhaps wing ring is placed the front (make the longitudinal axis of fuselage parallel with the medial axis of wing ring) of head front or both wings, the scooter vehicle frame with wing ring mechanism is connected with fuselage then, or through connecting rod or support scooter is connected with fuselage.Effective sail area of wing ring is much larger than the rotor of same diameter, and its power is also much larger than the rotor of same diameter, so its torsion can not offset through tail vane, the wing ring mechanism that therefore must offset with two or more torsion.(like Fig. 3 is exactly the wing ring mechanism rear view that is supported on the pylon, and Fig. 4, H then represent the Placement between the wing ring mechanism in the wing ring group).

Common wind wheel or water wheels the closer to the wing panel collection wind in axle center, to pull out outlet capacity more little, until being zero, and more away from the wing panel collection wind in axle center, to pull out outlet capacity big more, the former is poor efficiency wing panel and invalid wing panel, 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.

Wing ring group mechanism technological scheme:

Relate to a kind of by two or more rotary wing type wind wheels or water wheels and same support or same rotor combination that is connected and forms; Especially the existing rotor that turns clockwise of wing ring in this rotor combination; The rotor that is rotated counterclockwise is also arranged; And whole rotors that are rotated counterclockwise and the whole rotors that turn clockwise are the interior total amount equal (the moment of torsion absolute value that is both sides is equal and in the opposite direction) of gathering wind energy or current ability of section at one time; It is characterized in that: link together by two or more wing ring mechanisms and form, wherein each wing ring or be in same plane and the same center of circle arranged but radius is different separately (like Fig. 4, G, wherein please pay special attention to Fig. 5; Its wing ring 1-1-2 and wing ring 1-2-1 connect as one through spoke 4-2; So they are the different wing rings that belong to two wing ring mechanisms, be again the same wing ring that unites two into one, the wing ring that this unites two into one is the outer wing ring of inner wing ring group; Be again the inner wing ring of outer wing ring group), or be not in same plane but the residing separately plane of each wing ring is in (like Fig. 4, Fig. 6) on the same shaft axis in the center of circle of parallel surface and each wing ring each other; Adjacent wing ring mechanism sense of rotation is opposite, and the total torque of the total torque of the whole wing ring mechanisms that are rotated counterclockwise and whole wing ring mechanisms of turning clockwise equate will (that is to say gather in the section at one time wind energy or current can a total amount equate);

The Placement of forming wing ring group mechanism between the wing ring mechanism or between wing ring mechanism and the wing ring: perhaps two adjacent wing ring mechanism (said here neighbouring relations; Both comprised the both wings ring that is in same plane and the same center of circle is arranged; Big wing ring surrounds the same aspect neighbouring relations than the winglet ring; Comprise that also the center of circle is in the neighbouring relations that both wings ring on the same shaft axis is in different aspects respectively); Scooter quantity equates; And scooter on wing ring mechanism and the scooter on another wing ring mechanism are become a partner one to one; Two scooter vehicle frames of becoming a partner directly are connected or are connected through connecting rod; Perhaps the scooter track of a wing ring mechanism or scooter vehicle frame are connected (scooter that is actually two shared one pair of scooter tracks of adjacent wing ring mechanism and coupling thereof) with the circular support of adjacent foil ring, and perhaps the vehicle frame of the scooter of each wing ring mechanism all links to each other with same other supports on (other supports that so-called here " other supports " refers to not be wing ring support), and are connected with same support that afterwards they have the same center of circle or their center of circle to be on the same shaft axis; Each is not to linking to each other between the connecting rod of scooter or mutually; Perhaps all intersect vertically with same circular support or same polygonal support and be connected at intersection point (; Can prevent effectively that like this each from changing equidistant state between any two to scooter, and increase the stability of scooter operation, and in wing ring group mechanism; Realize that through scooter the inevitable sense of rotation of two continuous wing rings of coupling is opposite; That is to say that the angle of facining the wind of all fins is identical on the same wing ring, angle is opposite but the fin of adjacent foil ring facings the wind).

Need note; The one, the scooter spacing on the same single-blade ring mechanism equates; The 2nd, in same wing ring group; For fear of last public attention wing ring following public attention wing ring is produced air-flow mutual interference mutually when blocking with both wings ring rotation up and down, also can the connecting rod between the adjacent foil ring mechanism scooter be extended, thereby the distance of both wings ring mechanism is suitably drawn back

Mix wing ring group mechanism technological scheme:

Two or more wing ring group mechanism links together through support or connecting rod; Or wing ring group mechanism and wing ring mechanism link together (because the wing ring that turns clockwise in the wing ring group mechanism is cancelled out each other with the wing ring torsion that is rotated counterclockwise through support or connecting rod; Therefore the single-blade ring mechanism that connects as one with wing ring group mechanism must be more than one; And the wing ring that turns clockwise of these single-blade ring mechanisms is cancelled out each other with the wing ring torsion that is rotated counterclockwise); Each all links to each other with this support to the connecting rod between the scooter in scooter on each wing ring mechanism or the wing ring group mechanism, and (connecting rod must place between the scooter of two wing ring mechanisms or wing ring group mechanism (as shown in Figure 7); Support then places (like Fig. 9) or ring peripheral (like Figure 10) within the ring of wing ring mechanism or wing ring group mechanism; Or the same support of formation is sandwiched in wherein (like Figure 11) with wing ring mechanism, wing ring group mechanism in the circle, outside the circle; Settle the principle of support: the one, connect fixing each scooter, the 2nd, the normal rotation of not overslaugh wing ring; The vehicle frame of scooter can directly link to each other with support, and can be connected together through connecting rod earlier between the paired scooter, links to each other with support again, also can distinguish directly to link to each other with support); All wing ring mechanisms or wing ring group mechanism or the center of circle are overlapping to be same point, and perhaps shaft axis is overlapping is the same line, and perhaps shaft axis becomes parallel lines each other; The size of each wing ring or wing ring group and mode of structure or identical, perhaps different; The total torque of the whole wing ring mechanisms that are rotated counterclockwise equates with the total torque of the whole wing ring mechanisms that turn clockwise.(that is to say; Can have concurrently simultaneously in the same mixing wing ring group mechanism each wing ring be in same plane and have the wing ring group mechanism in the same center of circle not to be in same plane with each wing ring but each other parallel surface and the center of circle be in the wing ring group mechanism on the same shaft axis, the diameter of each wing ring group, thickness etc. also can be different.)

The benefit of mixing wing ring group mechanism is to make diameter can utilize multiple wing ring, multi-level mutual support at hundreds of rice, thousands of meters super sized type wing ring wind-powered electricity generation mechanism or wing ring aircraft; And obtain enough big mechanical strength and enough big wind loading rating, use common iron, aluminium to build the fetch water purpose of factory of wing ring aircraft, wing ring aerological station and wing ring upper wind electric field, wing ring altitude air that diameter reaches hundreds of meters and even thousands of meters thereby reach.

The wing ring mechanism technological scheme of band fixed-wing:

(refer to wing aircraft, fixed wing aircraft, glider, paraglider, wherein wing aircraft entire body does not have fuselage to have only the wing, or says that the wing and fuselage have united two into one to relate to a kind of rotor mechanism and fixed-wing aircraft; The cross section of its wing is the same with the wing of fixed wing aircraft, shape such as water droplet section, and aerofoil air up and down separately arrives the rear end junction simultaneously from front end when streaking air; And the aerofoil upper edge is a camber line; Speed air flow on the aerofoil is faster than the air under the aerofoil, and barometric pressure diminished above this just made, below barometric pressure become big; Therefore produce climbing power); It is characterized in that: wing ring mechanism, wing ring group mechanism, mix in three kinds of wing ring mechanisms such as wing ring combined mechanism one or more, every kind of mechanism is neither to be limited to one, with in four kinds of fixed-wing aircraft such as wing aircraft, fixed wing aircraft, glider, paraglider one or more; Every kind of fixed-wing aircraft also is not limited to one; Connect as one Placement: perhaps the vehicle frame of the scooter of wing ring mechanism or scooter track directly are connected with the fixed-wing aircraft, or are connected with the fixed-wing aircraft through connecting rod or support; Perhaps directly be connected between two paired scooter vehicle frames of adjacent foil ring mechanism in the wing ring group mechanism, or be connected with the fixed-wing aircraft through other connecting rods or support with the fixed-wing aircraft; Perhaps the support of wing ring group mechanism directly is connected with the fixed-wing aircraft, or is connected (quantity of tie point and position, both are firm making, stable bond is as the criterion) with the fixed-wing aircraft through connecting rod or other supports; The wing ring mechanism that turns clockwise in the whole mechanism exists with the wing ring mechanism that is rotated counterclockwise simultaneously, and all wing ring mechanisms that turn clockwise cancel out each other with the torsion of all wing ring mechanisms that are rotated counterclockwise (or saying that the wind energy or the current of the interior collection of section can equate at one time).Here said wing ring mechanism, wing ring group mechanism or mixing wing ring group mechanism are connected with support or fixed-wing aircraft; Its mode: perhaps aircraft is placed within the wing ring; The axis of aircraft is overlapping or parallel with wing ring axis, and perhaps aircraft places outside the wing ring, the axis of aircraft or with wing ring axis equality; Or it is vertical with wing ring axis; But aircraft axis and the vertical person of wing ring axis, it must realize being connected with aircraft through steering equipment, and the effect of this steering equipment is after the lift-off of whole mechanism, to make wing ring mechanism, wing ring group mechanism or mix the realization of wing ring group mechanism to turn to; Make the axis of wing ring become parallel or overlapping with the axis of aircraft; Thereby the task of making each wing ring mechanism provides horizontal power (lift changes by fixed-wing to be provided) from providing lift to change into, if worry that transferring wing ring axis to level earlier can make the moment stall tenesmus of whole mechanism, can be earlier the axis of aircraft be transferred to vertically; Handle the up-down cabin of aircraft then, make whole mechanism gradually become horizontal flight awing.

The longitudinal central axis line of fixed-wing aircraft is perhaps overlapping, perhaps parallel with the medial axis of wing ring mechanism or each wing ring; When the quantity of fixed-wing aircraft greater than 1 the time, their arrangement mode or non-overlapping copies ground also are listed in same plane, or their vertical projection overlapped and they itself be in respectively on the different aspects of parallel surface each other; Also can interconnect between each fixed-wing aircraft and (thereby play the effect of mutual reinforcing through connecting rod or support; Simultaneously; When the fixed-wing aircraft two or more the time; Can all directly be connected with wing ring mechanism respectively by each fixed-wing aircraft; Be combined in a support and can whole fixed-wing aircraft be connected, be connected with wing ring mechanism by this support again, or other each fixed-wing aircraft are connected with a fixed-wing aircraft respectively and are connected with wing ring mechanism by this fixed-wing aircraft; When the quantity of fixed-wing aircraft greater than 1 the time, the combination of fixed-wing aircraft can also can be mixed by two or more and formed the fixed-wing aircraft by a kind of composition the in four kinds of wing aircraft, fixed wing aircraft, glider, the paragliders etc.); The fixed-wing aircraft is provided with can be with whole mechanism flight attitude from vertically changing into level or changing into vertical elevator from level; Also can be provided with or not be provided with can change of flight the rudder of direction (the operate lifting cabin makes the axis of mechanism change into level from plumbness arrive the advection stratification of wind of setting height in mechanism's lift-off after; Wing ring front facings the wind or is the positive state that facings the wind basically at this moment; Producing climbing power no longer is its task or no longer is its main task; Its whole tasks or main task are wind-power generation or the power that mechanism's horizontal flight is provided; And the task of keeping whole mechanism lift changes by the fixed-wing aircraft and takes on, and this moment, the longitudinal axis of fixed-wing aircraft was the same as with entire mechanism the vertical level that becomes)

The mode of wing ring mechanism and generator combination was introduced in the front; The wing ring mechanism of wing ring group mechanism, mixing wing ring group mechanism and band fixed-wing also can become the wind generator set in high-altitude stratosphere or the trade wind advection stratification of wind easily in fact; Method is: be that support is provided with stator iron core, winding or rotor iron core, winding respectively and each wing ring group is become respectively do not rely on axle to drive the big generator of rotor with the support of each wing ring perhaps; The perhaps equidistant generator that line shaft is installed on the support of wing ring; On wing ring, ring track is set; Ring track is established around wing ring and is connected as a single entity with wing ring, lets ring track coupling mutually on wheel and the adjacent arbitrary wing ring on the generator line shaft.The generating position of these upper wind electrical mechanisms with lead to the connecting means of the cable on ground, can be with reference to " high hollow wing ring wind-powered electricity generation mechanism " of I invent multi (be shown in application number be 201120077850.3 and 201110072980.2 patent specification)

The usefulness of this mechanism:

The one, but large-scale high altitude wind power generator structure VTOL, that wing ring front is facingd the wind at the advection stratification of wind of setting height built.The process on ground is fallen from ground lift-off or from high backlash by this mechanism, and wing ring mechanism axis normal relies on the rotation of wing ring group that lift is provided in horizontal line, realizes that the original place goes straight up to, lands vertically; After being raised to setting height, make the axis of wing ring mechanism from vertically becoming level, changing by fixed-wing lift is provided through controlling hydroplane, wing ring is positive to facing the wind and let, and the maximum collection of performance wind is renderd a service, thereby reaches the maximum generation effect.

The 2nd, the wing ring helicopter that construction VTOL, level are flown fast, clean bearing capacity reaches kiloton even ton.The rotor of common propeller driven airplane and pure helicopter, more little the closer to its actual generation lift of wing panel in axle center, until being zero, and the lift that produces away from the wing panel in axle center more is big 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 rotor poor efficiency wing panel is 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 oversize, too wide, receive air quantity excessive; Serious vibration all must take place, rock even fracture; Therefore the rotor fin size of propeller driven airplane and helicopter is restricted at present, and the lift that provides also can't have big expansion with the power that advances.

And the wing of wing ring is most effective wing panel entirely, and it has abandoned producing the lift 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 10 times of corresponding increases 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 lift (bearing capacity) and the Driving force of wing ring type rotor should be the several times of the common rotor of same diameter, more than tens of times.And the diameter of wing ring; Especially the diameter of the wing ring in the wing ring combined mechanism can extend to hundreds of rice easily and even surpass km; Therefore can infer: if the bearing of wing ring mechanism has enough intensity, maximum net bearing capacity of the present invention can reach thousands of tons of and even tens thousand of ton fully.

Does wing ring mechanism need how powerful axle just is enough to bear heavy burden like this so? Pure helicopter; Except receive the effective wing panel area of rotor little, can only obtain the long restriction of one-sided support and the arm of force; The strength of axle has also limited its bodily form and clean bearing capacity; Because its whole kinetic energy all will pass through an axle transmission; Whole weight all wants this same axis to bear again, so its requirements of making is high, and the largest in the world clean bearing capacity of helicopter does not reach 30 tons yet at present.And the science of wing ring mechanism, ingenious part; Not only be greatly to have increased efficient wing panel area, reduce the vibration of its operation, the possibility of stopping to fracture; Also be common rotor must be shared on tens of, hundreds of and even thousands of axles by the heavy burden of bearing load and go, thus wing ring mechanism not only to fin material and production technique require relatively low, and to shaft material the requirement with a production technique also can greatly reduce; Therefore the super sized type helicopter that adopts the present invention to build; Compare with pure helicopter, manufacture difficulty can't be greatly improved, and cost per unit can reduce a lot; Whole mechanism stress equalization degree, stable degree can improve a lot, and service life also can be much higher.

Wing ring type original place landing aircraft technology scheme:

Wing ring mechanism with the band fixed-wing is the basis, and electric engine perhaps is set, and ramjet perhaps is set;

Electric engine; Be that support is provided with stator iron core, winding or rotor iron core, winding respectively and each wing ring group is become respectively do not rely on axle to drive the big motor of rotor perhaps with the support of each wing ring in each wing ring group mechanism; Perhaps the place or in the upper side of the annular support of wing ring, downside, inner ring circumference, outer ring circumference sentences the equidistant motor that motive power wheel (wheel that promptly is used as power and is connected with the motor power axle) is installed of the circumference of the same radius in upper edge, and the motor wheel track of annular is set in the corresponding part of another wing ring annular support simultaneously; The motor wheel track directly links to each other with annular support or links to each other through connecting rod, thereby is close together with these positions or is parastate; Let the motor wheel track coupling mutually of motor power wheel with adjacent another wing ring mechanism of a wing ring mechanism; Fuel electric generator or nuclear energy generator are set in mechanism, the circuit of motor are linked to each other with generator circuit, or between motor and generator, storage battery is set, motor is connected as circuit through storage battery with generator;

Ramjet then is arranged at the top of wing ring fin, and the engine puff prot of same wing ring is towards unanimity, and the engine puff prot of adjacent both wings ring is towards on the contrary in the same wing ring group.

This " giant " helicopter; All advantages of the wing ring mechanism of band fixed-wing have been followed; The bodily form huge as the samll cities and towns and the clean bearing capacity of ton can be arranged; Therefore can transport or lift by crane super large, the Heavy lift boats and ships, submarine, oil drilling platform etc. of port maintenance (as return), can also be directly as the Air fortress of super sized type near-earth low spatial station or military attacking and defending, patrol the aircraft carrier warship.When need not to navigate by water, this Air fortress can rely on a hawser to keep that nature suspends and generating is simultaneously used when being stored in storage battery in order to navigation.Because electric power is sufficient, therefore the large-scale air water intaking device can be set, solve personnel's in the mechanism domestic water.

If place up and down two to flow in the opposite stratification of wind respectively in two this " giant " aircrafts; Be connected to become drawing aircraft through hawser or connecting rod, just can become terrestrial space station power self-support, that need not the ground tracting cable, never landing or patrol the aircraft carrier warship.

A kind of energy-autarchic, the wing ring that freely cruises are to drawing the aircraft technology scheme:

Select for use wing ring type original place landing aircraft, band fixed-wing wing ring mechanism, mix wing ring group mechanism, wing ring group mechanism in one or more as unidirectional aviation mechanism; Two unidirectional aviation mechanisms or two groups of unidirectional aviation mechanism (so-called here groups; Be the array that two or more individualities are interconnected to any form) in the opposite air-flow of the up and down two-layer flow direction of the same area that is placed in or the current and mechanism facing the wind towards opposite that (two mechanisms all facing the wind or the flight that meets water; Two mechanism's flight directions are opposite); Or both are through the hawser connection, and both connect through hard connecting rod or support; Connecting on their hawser, connecting rod or the support certain a bit can be provided with or not be provided with gondola and (mix wing ring group mechanism or wing ring group mechanism if unidirectional aviation mechanism is selected for use; So just gondola must be set, the function of gondola is not only extraly a working space to be provided or to carry the cabin, priorly provides a bearing down; Make the axis tilt of wing ring downward; Thereby guarantee that wing ring is oblique down with the wind, produce two component during rotation, one is contrary wind tractive force; One is lift upwards; Therefore apply to wing ring to drawing the wing ring of aircraft, the cross section of its fin must the same shape with the cross section of aircraft fixed-wing such as half of drops, can produce lift when that is to say the rotation of wing ring; If unidirectional aviation mechanism is selected the wing ring mechanism of wing ring type original place landing aircraft or band fixed-wing for use; Gondola is just not essential so; Because this both can produce the fixed-wing of lift; Wing ring mechanism and wing ring group mechanism can positive facing the wind to bring into play maximum generating energy supply effect), gondola or be suspended to hawser or the below of connecting rod, support, perhaps directly and hawser or connecting rod, support be connected as a single entity; Gondola perhaps is in both belows; Perhaps be between the two; The buoyancy that produces of the gross weight of two or two groups of wing ring type original place landing aircrafts, gondola and hawsers or connecting rod, support and two or two groups of wing ring type original place landing aircrafts must reach balance up and down; Make both can keep suitable height, be unlikely to excessive come-up or sink and the equilibrium of leaving two strands of air-flows or current to drawing active force; Consider two unidirectional aviation mechanisms to pulling force the time, must consider the wind that gondola receives or the power of current, and with this power be included into receive with it that identical unidirectional aviation mechanism of force direction in the pulling force, finally make opposite equal of both direction to pulling force; All can be provided with on unidirectional aviation mechanism or the gondola or mobile mechanism is not set (two unidirectional aviation mechanisms should be symmetrical set; Be provided with and the opposing party is not provided with like a side; The just easy disequilibrium of whole mechanism); Mobile mechanism or can change baffle plate, curtain or the auxiliary kite of the area of positive opposing wind or current (area becomes a big side can receive bigger power; Thereby break balance to the pulling force amount, thus cause with to identical the vertically moving of direction of pull), or can be to propeller cavitation engine, wing ring engine, steam jet engine, ionization injection engine or the rudder of any direction deflection; (such as; Be in the stratification of wind of opposite course or two unidirectional aviation mechanisms in the water layer respectively and all be provided with rudder or auxiliary kite; When this both direction rudder or zither body to the synchronous deflection in the same side, wind or current will to entire mechanism produce with to the vertical lateral dynamics of pulling force (as shown in the figure); Again such as, two the propeller cavitation engines, wing ring engine, steam jet engine or the ionization injection engine that place opposite course stratification of wind or water layer respectively and can be synchronously change to any lateral deviation, they can promote two mechanisms and do laterally that (vertical with wind direction) moves; Again such as, place gondola and can be to propeller cavitation engine, wing ring engine, steam jet engine, the ionization injection engine or the rudder of both sides deflection, can change the auxiliary kite of zither face and wind or current angle, they also can promote entire mechanism and move laterally; Here mention " Steam engine "; Be meant with electric boiler with water be heated to be steam and with the ejection steam as power; Fly outstanding machine wind generator set can be installed easily drawing, thereby provide sufficient and powerful electric power is supplied with super sized type air water intaking device and electric heating steam boiler use; The water that air water intaking device is obtained is not only enough supplied with electric heating steam boiler, can also supply with the usefulness that resides permanently personnel's life on the pull mechanism.) or fin and axle or wing ring ring support between through deflection mechanism link to each other and deflection mechanism can change fin facing the wind angle from rotor mechanism or wing ring mechanism (as long as deflection mechanism changes the angle of facining the wind of fin; Will make two sides to the pulling force disequilibrium, vertically move thereby make mechanism that integral body take place);

Is there the stratification of wind of reverse advection up and down the sky?

Have! A kind ofly be in stratosphere bottom and the stratosphere, the wind of the reverse flow on upper strata, a kind of is the trade wind of trade wind district lower floor and the counter trades on upper strata.These two groups reverse advection wind are that the God gives human huge energy treasure-house, and this treasure-house is inexhaustible, and with regard to large-scale development, its difficulty and cost all can be lower than other energy (comprising oil).

Wing ring mechanism or the wing ring type original place landing aircraft of band fixed-wing that so how just can make two " giant " formulas in the high-altitude to drawing, generating electricity?

Except that wing ring type original place landing aircraft; Must wing ring mechanism or wing ring group mechanism be set to wing ring wind-powered electricity generation mechanism; And use the afterbody that the two ends of drawing hawser or connecting rod, support are connected the head of two " giants " respectively or connect two " giants " respectively (if adopt hawser; Preferably connect afterbody, in order to avoid arc weighs down the hawser overslaugh wing ring rotation of hanging); After ready; To this two " giant " transmission of electricity they are taken off through cable; And wherein one is taken off earlier, and another takes off after drawing back suitable height again, together flies to control elevator after the setting height but wing ring type original place landing aircraft becomes horizontal attitude from perpendicular attitude; Let cable take off then and collude, perhaps keep cable.The fixed-wing of aircraft begins to produce lift after the horizontal attitude owing to become, and therefore whole mechanism can form balance to tension state under reverse advection wind action.

I had once proposed wing ring aircraft in CN201120077850.3 and CN201110072980.2; This aircraft also can energy-autarchic; But the pulling force that must rely on the ground tracting cable to provide can be suspended in and do the wind-force generating in the air; This aircraft also can freely cruise, but just must regain tracting cable when cruising, interrupts generating.And the present invention need not the ground tracting cable at all, therefore can be at any time to any direction autokinetic movement, and movement process also needn't interrupt generating.

Therefore the present invention should be first huge aircraft of can energy-autarchic, freely cruising on the human history.Wing ring is to drawing wind-powered electricity generation mechanism; Wing ring all can be provided with or not be provided with on to the unidirectional aviation mechanism, gondola and the hawser that draw aircraft or connecting rod, support air water intaking device (all can be provided with or not be provided with power facility on supplying with unidirectional aviation mechanism, gondola and hawser on the pull mechanism or connecting rod, support, power facility be comprise common wind wheel generation mechanism, from all power facilities of rotor power facility, wing environment-development electrical mechanisms, kite or water zither power facility (by the power facility of reciprocating kite or water zither pushing generator), solar generating mechanism.

Wherein feasible is; Wing ring is docked with generator wing ring mechanism, wing ring group mechanism or the mixing wing ring group mechanism of drawing aircraft; Making it to become one utilizes wing ring mechanism or wing ring group mechanism as the high-rating generator structure of power mechanism with generating position carrier; This power facility can be provided with hundred thousands of medium and small generators, and these generator parallel connections or polyphone are one, and its whole generated energy can surpass the water power plant that nuclear power station is medium-sized or medium-sized or above.

Wing ring is to drawing the technological scheme of wind-powered electricity generation mechanism:

Power facility is set at wing ring on to the unidirectional aviation mechanism, gondola and the hawser that draw aircraft or connecting rod, support, power facility be comprise common wind wheel generation mechanism, from all power facilities of rotor power facility, wing environment-development electrical mechanisms, kite or water zither power facility, solar generating mechanism.

In wing ring group mechanism; Be that support is provided with corresponding stator core winding or rotor iron core winding respectively and each wing ring group is become respectively do not rely on axle to drive the huge generator of rotor perhaps with the support of each wing ring in each wing ring group mechanism; Perhaps the place or in the upper side of the circular support of wing ring mechanism, downside, inner ring circumference, outer ring circumference sentences the equidistant generator (promptly existing generator) that motive power wheel (wheel that promptly is used as power and is connected with the generator line shaft) is installed of the circumference of the same radius in upper edge; The generator motive power wheel track of ring is set in the corresponding part of the circular support of another wing ring simultaneously; Generator motive power wheel track directly links to each other with the circular support of wing ring or links to each other through connecting rod, thereby is close together with these positions or is parastate;

At single wing ring mechanism; Let generator motive power wheel and wing ring on the wing ring mechanism to drawing the generator motive power wheel track coupling mutually on the aircraft rack; Or conversely generator is arranged at wing ring on the support that draws aircraft, and the track of the motive power wheel institute coupling of generator is arranged on the support of this wing ring.

How is the circuit of the Power Generation Section in rotating so connected with the circuit on the fixed support? Very simple in fact; No matter what electrodes generator is provided with; Elder generation is the parallelly connected of ability parallel connection or polyphone or be connected in series to same joint, then each joint and corresponding brush track is connected, and 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; The brush track is touched with brush separately and is communicated with; External circuits links to each other with brush, and 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.

As for the be connected connecting means of circuitry with ground electricity consumption facility, the cable that directly hangs down on the slave, the two ends of cable are connected with electricity consumption facility circuit with generator circuit respectively and get final product.

Wing ring to draw wind-powered electricity generation mechanism generate electricity can, little part is supplied with wing ring and is used drawing the various device on the aircraft, major part can will be transported to the ground electrical network or directly by the large ship traction and directly supply power to the boats and ships electric drive system through a common cable.Compare with common high-altitude power facility, wing ring has been broken away from the dependence to tracting cable to drawing wind-powered electricity generation mechanism, and the cable that hangs down in this root high-altitude need not to bear the task of tracting cable, therefore only needs to use common cable to get final product.With kite, rotor or wing ring serve as the lift-off mechanism the upper wind electrical mechanisms must have tracting cable to haul; Otherwise will as the kite of broken string, descend slowly and lightly; The little then tens of millimeter of the diameter of tracting cable, greatly then hundreds of millimeters, its tracting cable with material more than, weight is big is that ten minutes is surprising.Wing ring is to the omission of drawing wind-powered electricity generation mechanism tracting cable or dwindle greatly, uses material and weight to subtract greatly, and bigger generating functions are installed in the mechanism more than having improved economic performance and having made more, have strengthened mechanism's generate output.

After in the future practicality can being supplied, also can electric energy directly be transferred to factory building, mansion, car and boat, aircraft or other electricity consumption facilities with microwave or laser with the technology of microwave or the direct electric energy transmitting of laser.Microwave current carries power technology carrying out the practicability running test, must exhibit one's skill to the full on to the power delivery of drawing wind-powered electricity generation mechanism at wing ring in the near future.

Even at present under the technical specifications; Also can consider electricity is converted into laser or microwave, ground boiler is shone, heated to fixed point, with the steam pushing generator generating of boiler; Or follow the trail of the steamer of irradiation use steam engine, the boiler of train, directly be these car and boat energy supplies.Though this conversion regime energy loss under present technical specifications is very big; But consider the bodily form and the generated energy all extremely huge (a large-scale wing ring to the generated energy that draw wind-powered electricity generation mechanism can meet or exceed a nuclear power station) of wing ring type to drawing wind-powered electricity generation mechanism; Again can be year in year out, wind direction is constant and generating does not incessantly consume fossil energy yet, even therefore in the transmission course loss most; Also still be very to possess use value and economic benefit; If utilize wing ring to send the advantage of electrical method to drawing wind-powered electricity generation machine and laser, developing again with the steamer is the steamer and the train of power, and fossil energy consumption in the world's can reduce major part so!

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

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

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

3: the entire combination after scooter track and the scooter coupling

3-1: grooved track

3-2: the vehicle frame of scooter

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

3-4: pulley

3-5: scooter

3-8:T shape track

3-9: the connecting rod between scooter and the support

3-10:T shape track and wing ring or other have the connecting end of the rigid objects of solid shape

4: through the connecting rod of wing ring medial axis

4-2: tab style spoke or connecting rod

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

6: the shaft type generator

7: the generator motive power wheel

8: the track of shaft type generating wheel

11-1: the vertical support bar of forming pylon

11-2: the vertical support bar of forming pylon

11-3: the vertical support bar of forming pylon

11-4: the oblique strut of forming pylon

11-5: the oblique strut of forming pylon

11-6: the oblique strut of forming pylon

11-7: the oblique strut of forming pylon

27: wing ring mechanism or wing ring group mechanism are combined as the connecting rod that mixes wing ring group mechanism

27-1: wing ring mechanism or wing ring group mechanism are combined as the support that mixes wing ring group mechanism

28: wing ring is to drawing the unidirectional aviation mechanism of aircraft

29: two or two groups are to the unidirectional aviation mechanism that draws or to drawing tracting cable or connecting rod or the support between the wind-powered electricity generation mechanism

30: wing ring is to drawing the rudder of aircraft

31: wing ring is to drawing the gondola of aircraft

32: wing ring mechanism or wing ring group mechanism

33: the fixed-wing that can produce lift

34: elevator

35: rudder

36: fuselage

37: cockpit

38: wing ring steering equipment

39: the connecting rod between wing ring mechanism or wing ring group mechanism and wing ring steering equipment

40: wing ring is to drawing wind-powered electricity generation mechanism

41: the electricity consumption facility

Two, drawing explanation

Fig. 1 is the front view (front view of the wing ring that three little figure wing ring that to be respectively fin stretch out in ring to the outer wing ring that stretches out of ring, fin and fin stretch out to the inside and outside both sides of encircling simultaneously) of three kinds of wing rings

Fig. 2 is the cross-sectional view (three coupling manner that pulley is clamped T shape scooter track from outside to inside from three different direction of left figure expression, five coupling manner that scooter is clamped T shape track from outside to inside from four different direction of right figure expression) of T shape scooter track and two kinds of scooter couplings

Fig. 3 is the windmill rear view that a kind of wing ring mechanism and pylon are formed

Fig. 4 is a kind of wing ring group structural scheme of mechanism (last figure is the side cross section view, and figure below is a front view)

Fig. 5 is an a kind of wing ring group mechanism front view

Fig. 6 is a kind of wing ring group structural scheme of mechanism (last figure is the side cross section view, and figure below is a front view)

Fig. 7 is a kind of mixing wing ring group structural scheme of mechanism (last figure is half in the symmetrical two halves of the front view of each level wing ring group, and figure below is the sectional side view of corresponding position)

Fig. 8 is a kind of mixing wing ring group structural scheme of mechanism (is in upper left be the side cross section view, to be in bottom-right be front view)

Fig. 9 is a kind of mixing wing ring group structural scheme of mechanism (left figure is a front view, and top right plot is half in the symmetrical two halves of front view, and bottom-right graph is the sectional side view of corresponding position)

Figure 10 is a kind of mixing wing ring group structural scheme of mechanism (left figure is a front view, and top right plot is half in the symmetrical two halves of front view, and bottom-right graph is the sectional side view of corresponding position)

Figure 11 is that (the picture left above is a front view to a kind of mixing wing ring group structural scheme of mechanism, and left figure below is the sectional side view of its corresponding position; Top right plot is the front view of the support of complete machine, and bottom-right graph is the sectional side view of its corresponding position)

Figure 12 is a kind of wing ring mechanism schematic representation with fixed-wing (last figure is a front view, and figure below is the sectional side view of corresponding position)

Figure 13 is a kind of wing ring mechanism schematic representation with fixed-wing (left figure is a front view, and right figure is the sectional side view of corresponding position)

Figure 14 is a kind of wing ring type VTOL aircraft schematic representation (left figure is a front view, and right figure is a side view)

Figure 15 is a kind of wing ring type VTOL aircraft schematic representation (axis of the front view when left figure is VTOL---wing ring is vertical with wing, the front view when right figure is horizontal flight---the axis of wing ring is parallel with wing or be in same plane)

Figure 16 is with the wing ring of gondola to drawing the aircraft side view

Figure 17 be a kind of not with the wing ring of gondola to drawing the aircraft side view

Figure 18 is that wing ring is to drawing wind-powered electricity generation mechanism side view

Figure 19 is a kind of bottom wing ring group and power facility combination schematic representation thereof gone up

Figure 20 is a kind of interior outer wing ring group and power facility combination schematic representation thereof

Figure 21 is another kind of bottom wing ring group and the power facility combination schematic representation thereof gone up.

Claims

1. wing ring relates to a kind of wind wheel or water wheels, fin rotation around the center of circle; Each fin top equates with the distance in the center of circle; Distance between each fin equates, is characterized in: the equidistant fin that is provided with on circular support, and each fin links to each other with annular support and does not link to each other with the axle center; Form angle between the circumferential surface of each fin aerofoil and annular support, the angle promptly facings the wind; Fin perhaps stretches out outside ring, perhaps in ring, stretches out, and perhaps stretches out to the inside and outside both sides of ring simultaneously; Fin on the same circular support or the common fin of unified employing, or the unified fin that adopts the cutting air can produce lift; Fin on the same circular support, thereby or unified directly linking to each other form the changeless angle that facings the wind with circular support, thereby or unifiedly can change the fin at the angle that facings the wind through the formation that links to each other with circular support of blade deflection mechanism.

2. wing ring mechanism; Relate to wing ring and a kind of wind wheel organization or wheel mechanism; It is characterized in that: form by wing ring, scooter track, scooter; Wherein the scooter track is connected with the scooter coupling; And the circular support of wing ring perhaps is connected with the scooter track and each scooter vehicle frame is connected with the ring support of another wing ring or scooter support or other rigid objects with solid shape of another wing ring mechanism, perhaps is connected with the vehicle frame of scooter and the scooter track is connected with ring support or other figurate rigid objects of another wing ring; The joint of scooter track or scooter vehicle frame and wing ring ring support; Be arranged in two sides of the circular support of wing ring or a place of four positions such as inner ring circumference side, outer ring circumference side; And connection part forms annular trace or tie point becomes the equidistant points on the annular trace, and these positions perhaps directly link to each other with the circular support of wing ring or link to each other through connecting rod, support; Scooter track or with circular support the same center of circle is arranged and person and circular support are close together, perhaps the center of circle of its center of circle and shape annular support is on the same shaft axis and is parastate with ring support; A wing ring mechanism has the scooter track that is no less than, and the scooter of every scooter track coupling is no less than three, and the scooter spacing on the same scooter track equates; The scooter track is a ring, and its center of circle and wing ring support are overlapping or be on the same shaft axis.

3. wing ring group mechanism; Relate to a kind of by two or more rotary wing type wind wheels or water wheels and same support or same rotor combination that is connected and forms; Especially the existing rotor that turns clockwise of wing ring in this rotor combination; The rotor that is rotated counterclockwise is also arranged; And the whole rotors that are rotated counterclockwise and the whole rotors that turn clockwise gather in the section at one time wind energy or current can a total amount equate; It is characterized in that: link together by two or more wing ring mechanisms and form, each wing ring or be in same plane and the same center of circle arranged but radius is different separately wherein, or be not in same plane but the residing separately plane of each wing ring is on the same shaft axis in the center of circle of parallel surface and each wing ring each other; Adjacent wing ring mechanism sense of rotation is opposite, and the total torque of the total torque of the whole wing ring mechanisms that are rotated counterclockwise and the whole wing ring mechanisms that turn clockwise equates to want;

4. according to claim 3; It is characterized in that: perhaps two adjacent wing ring mechanisms; Scooter quantity equates; And scooter on wing ring mechanism and the scooter on another wing ring mechanism are become a partner one to one, and two scooter vehicle frames of becoming a partner directly are connected or are connected through connecting rod, and perhaps the scooter track of a wing ring mechanism or scooter vehicle frame are connected with the circular support of adjacent foil ring; Perhaps the vehicle frame of the scooter of each wing ring mechanism all links to each other with same other supports, and they have the same center of circle or their center of circle to be on the same shaft axis to be connected the back with same support; Each is to linking to each other between the connecting rod of scooter or mutually, perhaps all intersects vertically with same circular support or same polygonal support and is connected at intersection point.

5. mix wing ring group mechanism; According to claim 2 or 3; It is characterized in that: two or more wing ring group mechanism links together through support or connecting rod; Or wing ring group mechanism and wing ring mechanism link together through support or connecting rod, and each all links to each other with this support to the connecting rod between the scooter in scooter on each wing ring mechanism or the wing ring group mechanism; All wing ring mechanisms or wing ring group mechanism or the center of circle are overlapping to be same point, and perhaps shaft axis is overlapping is the same line, and perhaps shaft axis becomes parallel lines each other; The size of each wing ring or wing ring group and mode of structure or identical, perhaps different; The total torque of the whole wing ring mechanisms that are rotated counterclockwise equates with the total torque of the whole wing ring mechanisms that turn clockwise.

6. be with the wing ring mechanism of fixed-wing; Relate to a kind of rotor mechanism and fixed-wing aircraft; It is characterized in that: wing ring mechanism, wing ring group mechanism, mix in three kinds of wing ring mechanisms such as wing ring combined mechanism one or more, every kind of mechanism is neither to be limited to one, with in four kinds of fixed-wing aircraft such as wing aircraft, fixed wing aircraft, glider, paraglider one or more; Every kind of fixed-wing aircraft also is not limited to one; Connect as one Placement: perhaps the vehicle frame of the scooter of wing ring mechanism or scooter track directly are connected with the fixed-wing aircraft, or are connected with the fixed-wing aircraft through connecting rod or support; Perhaps directly be connected between two paired scooter vehicle frames of adjacent foil ring mechanism in the wing ring group mechanism, or be connected with the fixed-wing aircraft through other connecting rods or support with the fixed-wing aircraft; Perhaps the support of wing ring group mechanism directly is connected with the fixed-wing aircraft, or is connected with the fixed-wing aircraft through connecting rod or other supports; The wing ring mechanism that turns clockwise in the whole mechanism exists with the wing ring mechanism that is rotated counterclockwise simultaneously, and the torsion of all wing ring mechanisms that turn clockwise and the wing ring mechanism that all are rotated counterclockwise is cancelled out each other.

7. according to claim 5, it is characterized in that: the longitudinal central axis line of fixed-wing aircraft is perhaps overlapping, perhaps parallel with the medial axis of wing ring mechanism or each wing ring; When the quantity of fixed-wing aircraft greater than 1 the time, their arrangement mode or non-overlapping copies ground also are listed in same plane, or their vertical projection overlapped and they itself be in respectively on the different aspects of parallel surface each other; Also can interconnect between each fixed-wing aircraft through connecting rod or support; The fixed-wing aircraft is provided with and can also can be provided with or be provided with the rudder of ability change of flight direction with whole mechanism flight attitude from vertically changing into level or changing into vertical elevator from level.

8. wing ring type original place landing aircraft; Relating to a kind of is angle of rake fixed wing aircraft and gyrodyne with propeller cavitation; It is characterized in that: the wing ring mechanism with the described band fixed-wing of claim 6 is the basis, and electric engine perhaps is set, and ramjet perhaps is set;

Electric engine; Be that support is provided with stator core winding or rotor iron core winding respectively and each wing ring group is become respectively do not rely on axle to drive the big motor of rotor perhaps with the support of each wing ring in each wing ring group mechanism; Perhaps the place or in the upper side of the circular support of wing ring, downside, inner ring circumference, outer ring circumference sentences the equidistant motor that motive power wheel is installed of circumference of the same radius in upper edge, and the motor wheel track of ring is set in the corresponding part of the circular support of another wing ring simultaneously; The motor wheel track directly links to each other with circular support or links to each other through connecting rod, thereby is close together with these positions or is parastate; Let the motor wheel track coupling mutually of motor power wheel with adjacent another wing ring mechanism of a wing ring mechanism; Fuel electric generator or nuclear energy generator are set in mechanism, the circuit of motor are linked to each other with generator circuit, or between motor and generator, storage battery is set, motor is connected as circuit through storage battery with generator;

9. an energy-autarchic, the wing ring that freely cruises are to drawing aircraft; Relate to a kind of buoyant means that places wind or water that links together through tracting cable or connecting rod and ground or water-bed immovable point, it is characterized in that: select for use the described mixing wing of wing ring mechanism, the claim 4 ring group mechanism of the described wing ring type of claim 7 original place landing aircraft, the described band fixed-wing of claim 5, in the described wing ring of the claim 3 group mechanism one or more as unidirectional aviation mechanism; Two unidirectional aviation mechanisms or two groups of unidirectional aviation mechanisms are placed in the air-flow that the two-layer flow direction is opposite up and down or the current of the same area and mechanism facings the wind towards on the contrary, both or connect through hawser, both connect through hard connecting rod or support; Certain that connects on their hawser, connecting rod or the support a bit can be provided with or not be provided with gondola, gondola or be suspended to hawser or the below of connecting rod, support, perhaps directly and hawser or connecting rod, support be connected as a single entity; Gondola perhaps is in both belows, perhaps is between the two; All can be provided with or not be provided with mobile mechanism on unidirectional aviation mechanism or the gondola; Mobile mechanism or can change baffle plate, curtain or the auxiliary kite of the area of positive opposing wind or current, or can be to propeller cavitation engine, wing ring engine, steam jet engine, ionization injection engine or the rudder of any direction deflection; Or link to each other through deflection mechanism between fin and axle or the wing ring ring support and deflection mechanism can change fin facing the wind angle from rotor mechanism or wing ring mechanism.

10. according to claim 9, it is characterized in that: all can be provided with or not be provided with air water intaking device on unidirectional aviation mechanism, gondola and hawser or connecting rod, the support.

11. wing ring is to drawing wind-powered electricity generation mechanism; Relate to a kind of linking together mutually and place the buoyant means of wind or water through tracting cable or connecting rod; And according to claim 9; It is characterized in that: power facility is set at wing ring on to the unidirectional aviation mechanism, gondola and the hawser that draw aircraft or connecting rod, support, power facility be comprise common wind wheel generation mechanism, from all power facilities of rotor power facility, wing environment-development electrical mechanisms, kite or water zither power facility, solar generating mechanism.

12. based on claim 11; It is characterized in that: in wing ring group mechanism; Be that support is provided with corresponding stator core winding or rotor core winding respectively and each wing ring group is become respectively do not rely on axle to drive the huge generator of rotor perhaps with the support of each wing ring in each wing ring group mechanism; Perhaps the place or in the upper side of the circular support of wing ring mechanism, downside, inner ring circumference, outer ring circumference sentences the equidistant generator that power wheel is installed of circumference of the same radius in upper edge; The generator power wheel track of annular is set in the corresponding part of the circular support of another wing ring simultaneously; Generator power wheel track directly links to each other with the circular support of wing ring or links to each other through connecting rod, thereby is close together with these positions or is parastate;