CN102384042B - Wing ring mechanism and wing ring aircraft - Google Patents
Wing ring mechanism and wing ring aircraft Download PDFInfo
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- CN102384042B CN102384042B CN201110279648.3A CN201110279648A CN102384042B CN 102384042 B CN102384042 B CN 102384042B CN 201110279648 A CN201110279648 A CN 201110279648A CN 102384042 B CN102384042 B CN 102384042B
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/30—Wind power
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
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Abstract
Wing ring, four kinds of wing ring mechanisms all use wing ring.Wing ring give up common wind wheel axle center and the poorly efficient section of wing, whole fin is all efficient wing panel, the arm of force of support flap is shortened several times, and increases to two from one, and supported on both sides is become from one side support, therefore wing ring mechanism, the wing ring group mechanism collection wind are more, intensity is bigger.Wing ring group mechanism is mixed with multiple wing ring, multi-level mutually support enhancing mechanical strength and wind resistance power, common iron, aluminium is suitable to build diameter up to hundreds of meters or even thousands of meters of wing ring aircraft.Wing ring mechanism with fixed-wing and wing ring type original place landing aircraft provide lift by fixed-wing and allow wing ring front windward, so as to reach maximum landing and flying power, maximum net carrying capacity is up to tens thousand of tons.
Description
Technical field
Wing ring, is related to a kind of wind wheel or water wheels, and fin rotates around the center of circle, and each flap apex is equal with the distance in the center of circle,
The distance between each fin is equal.
Wing ring mechanism, is related to wing ring and a kind of wind wheel organization or wheel mechanism.
Wing ring group mechanism, is related to one kind by two or more rotary wind type wind wheels or water wheels and same support or same
Rotor combination formed by axle connection, the existing rotor turned clockwise of wing ring in especially this rotor combination, also has inverse
The rotor of hour hands rotation, and whole rotors of rotate counterclockwise and whole rotors for turning clockwise adopt within the same period
The total amount for collecting wind energy or current energy is equal.
Wing ring group mechanism is mixed, is connected and constituted with same support by multiple wing ring group mechanisms.
Wing ring mechanism with fixed-wing, is related to a kind of rotor mechanism and Fixed Wing AirVehicle.
Wing ring type original place landing aircraft, be related to a kind of fixed wing aircraft using propeller as propeller and rotary wind type go straight up to it is winged
Machine.
Background technology
All rotor mechanism or wind wheel, wheel mechanism all have axle and linked with axle at present, this make rotor mechanism or
The area of wind wheel, the diameter of wheel mechanism and effective wing panel is severely limited, it is difficult to further expand, can not more realize hundreds of
The rotor mechanism or wind wheel, wheel mechanism of the thousands of rice diameters of meter Nai Zhi.
Large aircrafts all at present all can not can not especially be made using natural energy resources using the wind energy for being easiest to obtain
Originated for flying power.
All at present high-altitude wind power mechanisms or aloft work station (including makings balloon) can not all break away from the beam of tracting cable
Tie up, or the contrary wind component that must not be and provided independent of tracting cable is provided, otherwise will fall or fly away with the wind.
The content of the invention
First, mesh (rotor) is innovated
Current wind wheel (rotor) generator, hydrogenerator and rotor craft, propeller for vessels propeller it is common
Part, is to use the fin linked with axle, such a fin has three deadly defects of axle：
(1) each fin is from axle center most of wing panel collection wind outward or pulls out outlet capacity less, and closer to axle center
Wing panel collection wind, to pull out water energy effect smaller, until being zero, real efficiently collection wind pulls out hydrofoil section simply further away from the wing panel in axle center,
Further away from axle center, effect is higher, therefore efficiently wing panel to the wing panel between axle center should be omitted, but can not omit, because
It must lean on this poorly efficient wing panel and invalid wing panel to maintain its linkage between axle center for efficient wing panel, this adds increased weight,
Hamper mechanism body further to expand, while adding detrimental resistance, make power reduction and mechanical oscillation frequencies and amplitude are carried
It is high.
(2) efficiently wing panel can only obtain one side and also be that the axle center in distal end is supported, so rotor diameter is bigger,
The efficient wing panel of its fin can only just be made more tapering, therefore collection wind efficiency is low, it is impossible to promote larger generator, although logical
Cross the means of increase fin quantity, can increase the area of effective wing panel to a certain extent, but increase fin just it is inevitable simultaneously
Poorly efficient, the invalid wing panel of increase, and that the weight and wind wheel of the inevitable correspondingly increase wind wheel of the increase of these wing panels are born is harmful
Wind load, the result is that so that wind wheel does not reach the purpose of " synergy " not only, will also become burden, wind wheel " decreasing effect " is made on the contrary；
(3) internal layer iron core and winding (internal rotor) can only be driven to rotate by axis, or outer layer iron core can only be driven by outer shaft
With winding (outer rotor) rotation, and it can not allow inside and outside iron core winding rotor is simultaneously relative each other and reversely rotate.
Large aircrafts all at present all can not can not especially be made using natural energy resources using the wind energy for being easiest to obtain
Originated for flying power.
All at present high-altitude wind power mechanisms or aloft work station (including makings balloon) can not all break away from the beam of tracting cable
Tie up, or the contrary wind component that must not be and provided independent of tracting cable is provided, otherwise will fall or fly away with the wind.
The invention of this series seeks to the weakness of several prior arts for more than, solves following several technical barriers：
(1) only retain the efficient wing panel of rotor fin and save invalid wing panel, poorly efficient wing panel and axle center, so as to reduce tired
Superfluous, mitigation weight, saving material.
(2) on the premise of rotor diameter is not expanded, the size of the efficient wing panel of fin is widened significantly, while reducing fin
Wave and Oscillation Amplitude.
(3), provide that a kind of bodily form is huge, diameter is up to thousands of meters of aviation mechanism or wind wheel, water wheels, rotor mechanism.
(4) a kind of bodily form of offer is huge, loading capacity is huge and agile, in the case where fuselage datum line is horizontal
The original place landing aircraft of rapid flight.
2nd, technical scheme
Wing loop technique scheme：
Fin is equidistantly positioned on annular support, each fin is connected with annular support and is not attached to axle center；Each fin
Angle is formed between aerofoil and the periphery of annular support, i.e. angle windward；Fin either overhangs to ring or stretched into ring
Go out, or simultaneously to stretching inside and outside ring (respectively as shown in three small figures in Fig. 1)；Fin on same annular support
Or it is used uniformly common fin, or be used uniformly cutting air and can produce the fin of lift；Fin on same annular support, or
It is unified to be directly connected to form changeless angle windward with annular support, or uniformly pass through blade deflection mechanism and ring-type branch
Frame is connected can change the fin at angle windward so as to be formed.
Wing ring can essentially regard the close ring of the end to end formation of the Fixed Wing AirVehicle of double-vane or single-blade as.Wing ring
Be useful in that the existing wind wheel of substitution, water wheels or rotor and apply to wind-driven generator, hydrogenerator, marine propeller,
The fields such as aircraft engine.
Wing ring is actually a special rotor wind wheel, different from common rotor wind wheel, its fin not with axle center
Linkage, completely omits axle center, even if retaining axle center, nor in order to allow axle to drive fin or the wing with moving axis, but in order to
Wing ring rotary speed is too fast, centrifugal force it is excessive in the case of, drawn by setting up spoke between ring body and axle center using centripetal
Power reaches the purpose for reinforcing ring body, in this case, if it is necessary, can be wing by spoke design, makes the work of its existing spoke
With again play the role of fin.
Wing ring mechanism technical scheme：
It is made up of wing ring, scooter track, scooter, wherein scooter track is of coupled connections with scooter, and wing ring
Annular support, or be connected and the annular support or another wing ring mechanism of each pulley vehicle carriage and another wing ring with scooter track
Pulley kickstand or other have the connection of figurate rigid objects, or be connected and pulley track with the vehicle frame of scooter
Road is connected with the annular support or other figurate rigid objects of another wing ring；Scooter track or pulley vehicle carriage with
The connecting portion of wing ring annular support, positioned at two sides or inner ring circumference side of wing ring annular support, outer ring circumference side etc.
In four positions one at, and connecting portion formation annular trace or tie point turn into annular trace on equidistant points (this
The center of circle of annular trace is overlapping with the center of circle of wing ring annular support or on same axial line), these positions and wing ring ring-type
Support is joined directly together or is connected by connecting rod, support；Scooter track or have the same center of circle with annular support and with
Annular support is close together, or its center of circle and the center of circle of annular support are on same axial line and with annular support in flat
Row state；One wing ring mechanism has the scooter track no less than one, and the scooter of every scooter orbit coupling is no less than
Three, the pulley following distance on same scooter track is equal；Scooter track is the circle of annular, its center of circle and annular support
The heart is overlapping or on same axial line.
Wing ring mechanism be either connected with another wing ring or wing ring mechanism and constitute wing ring group mechanism or with wing ring mixer
The support or connecting rod of structure are connected and some as wing ring mixed organization, or are formed by connecting with platform, pylon as ground
Windmill or the power part as ground wind power mechanism, or be formed by connecting with aircraft fuselage as the special propeller of aircraft
Or rotor.
The coupled modes of scooter and its track must be such that scooter is moved along the circumferential direction that track stretches, without
It can be moved along any direction on the cross section of track.If the cross section of scooter track is groove profile, then scooter track
The mode coupled with scooter, or such as the scooter track in Fig. 4 and scooter coupling body 3, a minimum of 3 cunnings of scooter
Take turns from cross section to withstand three walls of track inside the track of flute profile outward, or as the scooter track in Fig. 6 with
Scooter zygosome 3, a minimum of 5 pulleys of scooter are from cross section to withstand four of track outward not inside the track of flute profile
Equidirectional wall；If the cross section of scooter track is T-shaped, then scooter track is coupled with scooter then should be using figure
Two ways shown in 2, one kind is three pulleys from three directions by clamping T track inward outside, one kind be five pulleys from
Four direction by clamping T track inward outside.
Wing ring mechanism is to constitute wing ring group mechanism, the basic important document of mixing wing ring group mechanism, can also be directly as ground
Or the wind wheel of high-altitude wind power mechanism, or directly as aircraft or the propeller of engine for boat.
The combination of wing ring mechanism and generator or engine：It is equidistant on the annular support of wing ring that power is installed
The generator or engine of axle, and the circular rails that relative set is coupled with generator or generator power wheel beside annular support
Road, the circular orbit has the same center of circle or its center of circle to be in wing ring center on same axial line with wing ring annular support, track
Either it is arranged in same wing ring group mechanism and provides the adjacent foil ring of another counter-rotating of support force for the wing ring or set
On support, platform, pylon, aircraft fuselage, can also in turn, by generator be arranged at adjacent foil ring or support,
On platform, pylon, hull, aircraft fuselage etc., and the track that the power wheel of generator, engine is coupled is arranged at wing ring
Support on.
Wing ring mechanism, can be only with single wing ring mechanism, used as vehicle spin used as ground wind power mechanism
The rotor of oar or high-altitude wind power mechanism, just must be with two or more single wing ring mechanisms, wherein must also set simultaneously
It is equipped with the wing ring mechanism turned clockwise with rotate counterclockwise, and the whole wing rings and the wing of rotate counterclockwise turned clockwise
The torsion of ring must be equal.
The connected mode of wing ring mechanism and aircraft, is either placed in fuselage or two by body sleeve in wing ring or by wing ring
Above the wing or below (making the longitudinal axis of fuselage vertical with the axis of wing ring), or wing ring is placed in before head or both wings
Before (make the longitudinal axis of fuselage and the axis parallel of wing ring), then the pulley vehicle carriage of wing ring mechanism and fuselage are connected
Connect, or scooter is connected with fuselage by connecting rod or support.Effective sail area of wing ring is much larger than the rotor of same diameter,
Its power is also much larger than the rotor of same diameter, therefore its torsion can not possibly be offset by tail vane, it is therefore necessary to two or two
The wing ring mechanism that individual above torsion is offseted.(such as Fig. 3 is exactly to be supported in the wing ring mechanism rear view on pylon, Fig. 4 then tables
Show the connected mode between the wing ring mechanism in wing ring group).
Common wind wheel or water wheels are smaller closer to the wing panel collection wind in axle center, drying ability, until be zero, and further away from axle center
Wing panel collection wind, pull out that outlet capacity is bigger, the former is poorly efficient wing panel and invalid wing panel, and the latter is efficient wing panel.In fact, common wind
The major function for taking turns poorly efficient wing panel is not collection wind, but the efficient wing panel of support on the neck, it is ensured that it links with axle, is referred to as " linkage
Lever " is likely more properly.This " lever " is due to only obtaining unilateral support and the strong point far away from axle center, if effectively wing panel
It is too wide, excessive by air quantity, will necessarily just occur high vibration, rock or even fracture, its actual effect is also less than more tapering
The wing, i.e. so the efficient wing panel of latter end of the fin of common wind wheel, it is impossible to widen, can only be tapering.The wing of wing ring is efficiency entirely
Highest wing panel, it abandon completely collection wind function be zero and poor wing panel, and change and by near-end, both sides it is adjacent
Fin provides support, compared to original distal end, unilateral axle center support, and the arm of force not only shortens, and also increases to two from one, and
And two arm of forces are placed in supported on both sides, the result is that：Only for single fin, if the arm of force shortens 10 times, then branch
Support force is with regard to corresponding 11-fold increase, and the arm of force increases to two from one, therefore the increased times of support force are just changed into 20 times from 10 times；
One side support is changed into supported on both sides, and support force and stability are further improved；From wing ring generally speaking, high-efficiency fin can
To increase to tens of or even hundreds of, the area of each fin can be widened greatly again, that is to say, that the efficient wing of wing ring
The area of section can be with the common wind wheel of several times, decades of times or even hundreds of times of same radius.Therefore it is concluded that：Wing ring wind
The efficiency of the wind resistance power of wheel and conversion wind energy should be the several times of the common wind wheel of same radius, more than decades of times, the rotation of wing ring type
The lift (bearing capacity) of the wing should be the several times of the common rotor of same radius, more than decades of times.
Wing ring group mechanism technology scheme：
It is related to one kind to be connected and shape with same support or same axle by two or more rotary wind type wind wheels or water wheels
Into rotor combination, the especially existing rotor turned clockwise of wing ring in the combination of this rotor also has rotate counterclockwise
Rotor, and whole rotors of rotate counterclockwise gather wind energy or water with the whole rotors turned clockwise within the same period
The total amount for flowing energy is equal (i.e. the torque absolute value of both sides is equal and in opposite direction), it is characterized in that：By two or more wings
Ring mechanism links together composition, wherein each wing ring or is in same plane and has the same center of circle but respective radius is different (such as
Fig. 4, Fig. 5, wherein particularly noting that Fig. 5, its wing ring 1-1-2 and wing ring 1-2-1 are connected as one by spoke 4-2, so it
Be both the different wing rings for belonging to two wing ring mechanisms, be the same wing ring united two into one, this wing united two into one again
Ring is both the outer wing ring of inner wing ring group, is the inner wing ring of outer wing ring group again), or it is not at same plane but each wing ring is each residing
Plane each other parallel surface and each wing ring the center of circle be in same axial line on (such as Fig. 4, Fig. 6)；Adjacent wing ring mechanism rotation
In the opposite direction, and the total torque of whole wing ring mechanisms of rotate counterclockwise and the total torque of whole wing ring mechanisms that turns clockwise
Equal (total amount that wind energy or current energy are that is gathered within the same period is equal)；
The connected mode of wing ring group mechanism is constituted between wing ring mechanism or between wing ring mechanism and wing ring：Or two adjacent
Wing ring mechanism (neighbouring relations mentioned here, both including in same plane and having a both wings ring in the same center of circle, larger wing ring
The same aspect neighbouring relations compared with winglet ring are surrounded, the both wings ring being also in including the center of circle on same axial line is respectively at different layers
The neighbouring relations in face), scooter quantity is equal, and the scooter on a wing ring mechanism and the pulley on another wing ring mechanism
Car is peering one to one, and two peering pulley vehicle carriages, which are joined directly together, to be connect or be connected by connecting rod, or a wing ring machine
It (is actually two adjacent wing ring machines that the scooter track or pulley vehicle carriage of structure are connected with the circular support of adjacent foil ring
Structure shares the scooter of one pair of scooter track and its coupling), or each wing ring mechanism scooter vehicle frame all with it is same
Other supports be connected (so-called here " other supports " refer to be not annular support other supports), and after being connected with same support
They have the same center of circle or their center of circle to be on same axial line；Between the connecting rod of each pair of scooter or mutually it is not attached to,
Or all intersect with same circular support or same polygon support vertical and connect in intersection point (, so can effectively prevent each
Change equidistant state between any two to scooter, and increase the stability of scooter operation, and in wing ring group mechanism, lead to
Cross scooter and realize that the inevitable direction of rotation of two connected wing rings of coupling is opposite, that is to say, that all fins on same wing ring
Windward angle it is identical, but the fin Windward angle of adjacent foil ring is opposite).
It need note, one is that pulley following distance on same single-blade ring mechanism is equal, and two be in same wing ring group, to be
Avoid public attention wing ring from producing lower public attention wing ring to block and air-flow is interfered when both wings ring rotates up and down, can also be by phase
Connecting rod between adjacent wing ring mechanism scooter is lengthened, so that the distance of both wings ring mechanism is suitably pulled open.
Mix wing ring group mechanism technology scheme：
Two or more wing ring group mechanisms are linked together by support or connecting rod, or wing ring group mechanism and wing ring
Mechanism is linked together (due to the wing ring and the wing of rotate counterclockwise that are turned clockwise in wing ring group mechanism by support or connecting rod
Ring torsion is cancelled out each other, thus the single-blade ring mechanism connected as one with wing ring group mechanism must at more than one, and these
The wing ring turned clockwise of single-blade ring mechanism and the wing ring torsion of rotate counterclockwise are cancelled out each other), on each wing ring mechanism
Connecting rod on scooter or wing ring group mechanism between each pair of scooter is all connected with the support, and (connecting rod is necessarily placed in two wing ring machines
Between structure or the scooter of wing ring group mechanism (as shown in Figure 7), and support is then placed in the ring of wing ring mechanism or wing ring group mechanism
Within (such as Fig. 9) or ring it is peripheral (such as Figure 10), or in circle, circle is outer forms same support and press from both sides wing ring mechanism, wing ring group mechanism
In wherein (such as Figure 11), the principle of support is disposed：One is each scooter that is connected, and two be the normal rotation for not hindering wing ring；
The vehicle frame of scooter directly can be connected with support, and can first pass through connecting rod between paired scooter and be connected together, then
It is connected with support, directly can also be connected respectively with support)；All wing ring mechanisms or wing ring group mechanism or the center of circle it is overlapping be same
A bit, either axle center line overlap is that the same line or axial line become mutually parallel lines；The size of each wing ring or wing ring group and
Frame mode or identical or difference；The total torque of whole wing ring mechanisms of rotate counterclockwise and the whole turned clockwise
The total torque of wing ring mechanism is equal (that is, can have each wing ring concurrently simultaneously in same in same mixing wing ring group mechanism
Plane and the wing ring group mechanism and each wing ring that have the same center of circle are not at same plane but each other parallel surface and the center of circle be in it is same
Wing ring group mechanism on axial line, diameter, the thickness of each wing ring group etc. can also be different).
The benefit for mixing wing ring group mechanism is the ultra-large type wing ring wind power mechanism or wing ring for making diameter at hundreds of meters, thousands of meters
Aircraft can be using multiple wing ring, multi-level mutual support, and obtains sufficiently large mechanical strength and sufficiently large wind resistance energy
Power, diameter is built up to hundreds of meters or even thousands of meters of wing ring aircraft, wing ring aerological station so as to reach using common iron, aluminium
With wing ring high-altitude wind power plant, the purpose of wing ring altitude air water intaking factory.
Wing ring mechanism technical scheme with fixed-wing：
Be related to a kind of rotor mechanism and Fixed Wing AirVehicle (refer to wing aircraft, fixed wing aircraft, aerodone, paraglider,
Wherein wing aircraft entire body does not have fuselage there was only the wing, or says that the wing and fuselage unite two into one, the cross section of its wing and fixed-wing
The wing of aircraft is the same, shape such as water droplet section, and air when streaking air above and below aerofoil separately reaches rear end from front end and merged simultaneously,
And along being camber line on aerofoil, the speed air flow on aerofoil is faster than the air under aerofoil, this allows for atmospheric pressure above and diminished,
Air buckling is big below, therefore produces climbing power), it is characterized in that：Wing ring mechanism, wing ring group mechanism, mixing wing ring combined mechanism
More than one or both of three kinds of wing ring mechanisms, every kind of mechanism is all not limited to one, flies with wing aircraft, fixed-wing
More than one or both of four kinds of Fixed Wing AirVehicles such as machine, aerodone, paraglider, every kind of Fixed Wing AirVehicle is also not limited to
One, connect as one, connected mode：Or the vehicle frame or scooter track of the scooter of wing ring mechanism directly fly with fixed-wing
Row device is connected, or is connected by connecting rod or support with Fixed Wing AirVehicle；Or in the wing ring group mechanism adjacent foil ring mechanism two
Directly it is connected, or is flown by other connecting rods or support with fixed-wing with Fixed Wing AirVehicle between individual paired pulley vehicle carriage
Device is connected；Or the support of wing ring group mechanism is directly connected with Fixed Wing AirVehicle, or pass through connecting rod or other supports and fixation
Rotor aircraft connection (quantity of tie point and position, so that both can be made firm, stable bond to be defined)；Up time in integrated model
The wing ring mechanism and the wing ring mechanism of rotate counterclockwise of pin rotation exist simultaneously, and all wing ring mechanisms turned clockwise and
The torsion of the wing ring mechanism of all rotate counterclockwises, which is cancelled out each other, (or says the wind energy collected within the same period or current energy phase
Deng).The connection of wing ring mechanism mentioned here, wing ring group mechanism or mixing wing ring group mechanism and support or Fixed Wing AirVehicle,
Its mode：Or aircraft is placed within wing ring, the axis of aircraft is put with wing annulate shaft line overlap or parallel, or aircraft
Outside Yu Yihuan, the axis of aircraft or with wing ring axis equality, it is or vertical with wing ring axis, but aircraft axis and wing annulate shaft
The vertical person of line, it must be realized by steering mechanism with aircraft and is connected, and the effect of the steering mechanism is in integrated model lift-off
Wing ring mechanism, wing ring group mechanism or mixing wing ring group mechanism is realized and is turned to afterwards, make the axis of wing ring and the axis of aircraft
It is changed into parallel or overlapping, (lift changes by solid so that the task of each wing ring mechanism is changed into offer horizontal power from offer lift
Wing offer is provided), can be first by aircraft if worrying that wing ring axis first are switched into level can make integrated model moment stall drop
Axis switch to vertically, then manipulate aircraft lifting cabin, integrated model is awing gradually become horizontal flight.
The axis or overlapping or parallel of the longitudinal central axis line of Fixed Wing AirVehicle and wing ring mechanism or each wing ring；
When the quantity of Fixed Wing AirVehicle is more than 1, their arrangement mode either without overlapping and is listed in same plane, or
Be they upright projection it is overlapped and themselves be in respectively in the different aspects of parallel surface each other；Each fixed-wing flies
Can also be connected with each other between row device by connecting rod or support (so that play a part of reinforcing mutually, meanwhile, when fixed-wing flight
Device is at two or more, it may not be necessary to which each Fixed Wing AirVehicle is directly connected to wing ring mechanism respectively, and can be with
The connection of whole Fixed Wing AirVehicles is combined in a support, then is connected by the support with wing ring mechanism, or other each fix
Rotor aircraft is connected with a Fixed Wing AirVehicle is connected again by this Fixed Wing AirVehicle with wing ring mechanism respectively；Work as fixed-wing
When the quantity of aircraft is more than 1, the combination of Fixed Wing AirVehicle can be by wing aircraft, fixed wing aircraft, aerodone, gliding
A kind of composition in four kinds of umbrella etc., can also constitute Fixed Wing AirVehicle by two or more mixing)；Fixed Wing AirVehicle
Being provided with can be by integrated model flight attitude from vertically changing into level or vertical elevator being changed into from level, can also
The rudder for setting or being not provided with energy change of flight direction (manipulates lifting after the advection stratification of wind for reaching setting height that gone up to the air in mechanism
Cabin makes the axis of mechanism change into horizontality from plumbness, and now wing ring front is windward or substantially in positive shape windward
State, generation climbing power is no longer its task or is no longer its main task, and its whole tasks or main task are collection wind
The power of mechanism horizontal flight is generated electricity or provided, and maintains the task of integrated model lift to change and is taken on by Fixed Wing AirVehicle, this
When Fixed Wing AirVehicle longitudinal axis as whole mechanism from being vertically changed into level).
The previously described mode for crossing wing ring mechanism and generator combination, in fact wing ring group mechanism, mixing wing ring group mechanism and
Wing ring mechanism with fixed-wing can also easily turn into the wind-driven generator in high-altitude stratosphere or trade wind advection stratification of wind
Structure, method is：Or set stator core, winding or rotor core, winding to make each respectively using the support of each wing ring as support
Wing ring group respectively becomes the big generator not against axle rotor driven, or equidistant on the support of wing ring is provided with line shaft
Generator, circular orbit is set on wing ring, and circular orbit sets around wing ring and is connected as a single entity with wing ring, generator power is allowed
Wheel on axle is coupled with the circular orbit on adjacent any wing ring.
The usefulness of mechanism：
One be build can VTOL, in the advection stratification of wind of setting height can make wing ring front large-scale upper-level winds windward
Power generator structure.Mechanism is gone up to the air from ground or the process on ground is dropped from high backlash, wing ring mechanism axis perpendicular to horizontal line, according to
Rotation by wing ring group provides lift, realizes that original place is gone straight up to, landed vertically；Make wing ring by manipulating hydroplane after setting height is raised to
The axis of mechanism changes from vertically level is changed into and provides lift by fixed-wing, and allows wing ring front windward, plays maximum collection wind effect
Power, so as to reach maximum generation effect.
Two be to build VTOL, horizontal rapid flight, net bearing capacity to reach that the wing ring of kiloton even ton is gone straight up to
Aircraft.The rotor of general propeller aircrafts and pure helicopter, closer to the wing panel in axle center, its actual generation lift is smaller, until
It is zero, and the lift that the wing panel further away from axle center is produced is bigger, the former is poorly efficient wing panel and invalid wing panel, and the latter is the efficient wing
Section.In fact, the major function of the poorly efficient wing panel of common rotor is the efficient wing panel of support on the neck, it is ensured that it links with axle, is referred to as
" linkage lever " is likely more properly.This " lever " due to only obtaining unilateral support and the strong point is far away from axle center, if
Imitate wing panel oversize, too wide, excessive by air quantity, all necessarily occur high vibration, rock or even fracture, therefore propeller aeroplane at present
With the rotor wing dimensions of helicopter be restricted there is provided lift and advance power can not also have big expansion.
And the wing of wing ring is efficiency highest wing panel entirely, it is zero the and poor wing that it abandons generation lift function completely
Section, and change and by near-end, the fin offer support that both sides are adjacent, supported compared to original distal end, unilateral axle center, the arm of force
Not only shorten, also increase to two from one, and two arm of forces are placed in supported on both sides, the result is that：Only from single fin
For, if the arm of force shortens 10 times, then support force just corresponding 10 times of increase, the arm of force increases to two, therefore branch from one
The increased times of support force are just changed into 20 times from 10 times；One side support is changed into supported on both sides, and support force and stability are further obtained
To raising；From wing ring generally speaking, high-efficiency fin can increase to tens of or even hundreds of, and the area of each fin again can
Greatly to widen, that is to say, that the area of the efficient wing panel of wing ring can be with several times, decades of times or even hundreds of times of same radius
Common wind wheel.Therefore it is concluded that：The lift (bearing capacity) and motive force of wing ring type rotor should be the general of same diameter
It is more than the several times of logical rotor, decades of times.And the diameter of the wing ring in the diameter of wing ring, especially wing ring combined mechanism can gently and
Extend to hundreds of meters or even more than km with easily lifting, it can therefore be concluded that：If the bearing of wing ring mechanism has enough intensity, this
The maximum net bearing capacity of invention is fully able to reach thousands of tons of or even tens thousand of tons.
So wing ring mechanism needs how powerful axle is just enough to undertake such heavy burdenPure helicopter, except by
The effective wing panel area of rotor is small, can only obtain outside unilateral support and the long limitation of the arm of force, and the endurance of axle also limit it
The bodily form and net bearing capacity because its whole kinetic energy will be transmitted by axle, whole weight again will be this same
Bearing is carried on a shoulder pole, so its making requires high, and the largest net bearing capacity of helicopter does not reach 30 tons yet in the world at present.
And the science of wing ring mechanism, ingenious part, not only it is to substantially increase the area of efficient wing panel, reduces shaking for its operation
Move, prevent the possibility that fractures, tens of, hundreds of must be shared by the heavy burden of a bearing load by common rotor and be by also residing in
Get on to thousands of axles, therefore requirement of the wing ring mechanism not only to fin material and production technique is relatively low, and to axial wood
The requirement of material and axle production technique can also be greatly lowered, therefore the ultra-large type helicopter built using the present invention, with ordinary straight
The machine of liter is compared, and manufacture difficulty can't be greatly improved, and unit cost can be reduced a lot, integrated model stress equalization degree,
Stable degree can be improved a lot, and service life also can be much higher.
Wing ring type original place landing aircraft technology scheme：
Based on the wing ring mechanism with fixed-wing, electric engine is either set or ramjet is set；
Electric engine, or the support of each wing ring sets stator core, winding as support respectively using in Ge Yi ring groups mechanism
Or rotor core, winding make each wing ring group respectively become the big motor not against axle rotor driven, or in the ring-type of wing ring
In the upper side of support, downside, inner ring circumference, outer ring circumference one at or two at more than it is equidistant along the circumference of same Radius
The motor of power wheel (be used as power the wheel being connected with motor power axle) is installed, while in the corresponding of another wing ring annular support
Part sets the motor wheel track of annular；Motor wheel track is joined directly together with annular support or is connected by connecting rod, so that and this
A little positions are close together or in parastate；Allow the motor power wheel and adjacent another wing ring mechanism of a wing ring mechanism
Motor wheel track is coupled；Fuel electric generator or nuclear energy generator are set in mechanism, by the circuit and generator circuit of motor
It is connected, or battery is set between motor and generator, motor and generator makees circuit connection by battery；
Ramjet is then arranged at the top of wing ring fin, and the engine puff prot direction of same wing ring is consistent, same wing ring
The engine puff prot of adjacent both wings ring is towards conversely in group.
This " giant " helicopter, has followed all advantages of the wing ring mechanism with fixed-wing, can have as samll cities and towns
The huge bodily form and the net bearing capacity of ton, thus can transport or lift by crane super large, dead weight cargo (such as return port maintenance ship
Oceangoing ship, submarine, oil drilling platform etc.), can also directly as ultra-large type near-earth low spatial station or military attacking and defending Air fortress,
Patrol aircraft carrier warship.
Brief description of the drawings
First, description of symbols
1：Wing ring
1-1：Outer layer wing ring
1-1-1：Outer wing ring in outer wing ring group
1-1-2：Inner wing ring in outer wing ring group
1-2：Internal layer wing ring
1-2-1：Outer wing ring in inner wing ring group
1-2-2：Inner wing ring in inner wing ring group
1-3：Upper strata wing ring
1-4：Lower floor's wing ring
2：Fin
2-1：To overhanging unilateral fin
2-2：The unilateral fin inwardly stretched
2-3：The double fins stretched out to both sides
3：Scooter track coupled with scooter after entire combination
3-1：Grooved track
3-2：The vehicle frame of scooter
3-3：Connecting rod between scooter and scooter
3-4：Pulley
3-5：Scooter
3-8：T track
3-9：Connecting rod between scooter and support
3-10：The connection end of T track and wing ring or other figurate rigid objects of tool
4：Pass through the connecting rod of wing ring axis
4-2：Tab style spoke or connecting rod
5：Tracting cable (or tracting cable, cable are two-in-one)
6：Shaft-type generators
7：Generator power wheel
8：The track of shaft-type generators wheel
11-1：Constitute the vertical support bar of pylon
11-2：Constitute the vertical support bar of pylon
11-3：Constitute the vertical support bar of pylon
11-4：Constitute the skewed horizontal load bar of pylon
11-5：Constitute the skewed horizontal load bar of pylon
11-6：Constitute the skewed horizontal load bar of pylon
11-7：Constitute the skewed horizontal load bar of pylon
27：It is the connecting rod for mixing wing ring group mechanism by wing ring mechanism or wing ring group Mechanism Combination
27-1：It is the support for mixing wing ring group mechanism by wing ring mechanism or wing ring group Mechanism Combination
28：Unidirectional aviation mechanism of the wing ring to drawing aircraft
29：Two or two groups to the unidirectional aviation mechanism of drawing or to drawing tracting cable or connecting rod or support between wind power mechanism
30：Rudder of the wing ring to drawing aircraft
31：Gondola of the wing ring to drawing aircraft
32：Wing ring mechanism or wing ring group mechanism
33：The fixed-wing of lift can be produced
34：Elevator
35：Rudder
36：Fuselage
37：Driving cabin
38：Yi Huan steering mechanism
39：Connecting rod between wing ring mechanism or wing ring group mechanism and Yi Huan steering mechanism
40：Wing ring is to drawing wind power mechanism
41：Electricity consumption facility
2nd, drawing explanation
Fig. 1 is that (three small figures are that wing ring, the fin that fin is overhang to ring are stretched into ring respectively for the front views of three kinds of wing rings
The wing ring and fin that go out are simultaneously to the front view of the wing ring stretched out inside and outside ring)
Fig. 2 is that (left figure represents three pulleys from three not to the cross-sectional view that is coupled with two kinds of scooters of T-shaped scooter track
The equidirectional coupled modes for clamping T-shaped scooter track from outside to inside, right figure represent five scooters from four different directions by
The outer coupled modes for clamping T track inwards)
Fig. 3 is the windmill rear view that a kind of wing ring mechanism is constituted with pylon
Fig. 4 is a kind of wing ring group structural scheme of mechanism (upper figure is side cross section view, and figure below is front view)
Fig. 5 is a kind of wing ring group mechanism front view
Fig. 6 is a kind of wing ring group structural scheme of mechanism (upper figure is side cross section view, and figure below is front view)
Fig. 7 is a kind of mixing wing ring group structural scheme of mechanism (during upper figure is the symmetrical two halves of front view of each level wing ring group
Half, figure below is the sectional side view of correspondence position)
Fig. 8 be a kind of mixing wing ring group structural scheme of mechanism (in it is upper left be side cross section view, in lower right be
Front view)
Fig. 9 is that (left figure is front view to a kind of mixing wing ring group structural scheme of mechanism, during top right plot is the symmetrical two halves of front view
Half, bottom-right graph is the sectional side view of correspondence position)
Figure 10 is that (left figure is front view to a kind of mixing wing ring group structural scheme of mechanism, and top right plot is the symmetrical two halves of front view
In half, bottom-right graph is the sectional side view of correspondence position)
Figure 11 is that (the picture left above is front view to a kind of mixing wing ring group structural scheme of mechanism, and lower-left figure is the side of its correspondence position
Profile；Top right plot is the front view of the support of complete machine, and bottom-right graph is the sectional side view of its correspondence position)
Figure 12 is that (upper figure is front view to a kind of wing ring mechanism schematic diagram with fixed-wing, and figure below is that the side of correspondence position is cutd open
Face figure)
Figure 13 is that (left figure is front view to a kind of wing ring mechanism schematic diagram with fixed-wing, and right figure is that the side of correspondence position is cutd open
Face figure)
Figure 14 is a kind of wing ring type VTOL aircraft schematic diagram (left figure is front view, and right figure is side view)
Figure 15 is a kind of wing ring type VTOL aircraft schematic diagram (front view when left figure is VTOL --- wing ring
Axis and wing vertical, front view when right figure is horizontal flight --- the axis of wing ring is parallel with wing or in same flat
Face)
Figure 16 is a kind of upper bottom wing ring group and its generating mechanism combination diagram
Figure 17 is a kind of interior outer wing ring group and its generating mechanism combination diagram
Figure 18 is another upper bottom wing ring group and its generating mechanism combination diagram.
Claims (7)
1. wing ring mechanism, is related to wing ring and a kind of wind wheel organization or wheel mechanism, it is characterized in that：By wing ring, scooter track, cunning
Car composition is taken turns, wherein scooter track is of coupled connections with scooter, and the annular support of wing ring, or is connected with scooter track
And the annular support or the pulley kickstand of another wing ring mechanism of each pulley vehicle carriage and another wing ring or other there is fixed shape
The rigid objects connection of shape, or be connected with the vehicle frame of scooter and scooter track and the annular support of another wing ring or other
Figurate rigid objects connection；The connecting portion of scooter track or pulley vehicle carriage and wing ring annular support, positioned at the wing
In two sides or inner ring circumference side of ring annular support, the position of outer ring circumference side four one at, and connecting portion shape
Circularizing track or tie point turns into the equidistant points on annular trace, these positions and wing ring annular support or is joined directly together
Or be connected by connecting rod, support；Scooter track has the same center of circle with circular support and is close to annular support
Together, or its center of circle and the center of circle of annular support are on same axial line and are in parastate with annular support；One wing
Ring mechanism has the scooter track no less than one, and the scooter of every scooter orbit coupling is no less than three, same pulley
Pulley following distance on track road is equal；Scooter track is annular, and its center of circle is overlapping with the center of circle of annular support or is in
On same axial line.
2. wing ring group mechanism, is related to a kind of rotary wind type wind wheel more than two or three or water wheels and same support or same axle
Rotor formed by connection is combined, the existing rotor turned clockwise of wing ring in this rotor combination, also there is rotate counterclockwise
Rotor, and whole rotors of rotate counterclockwise and whole rotors for turning clockwise gathered within the same period wind energy or
The total amount of current energy is equal, it is characterized in that：Linked together and constituted with upper limb ring mechanism by two or three, wherein each wing ring
Or be in same plane and have the same center of circle but respective radius different, or it is not at same plane but each wing ring is each residing puts down
Face each other parallel surface and each wing ring the center of circle be in same axial line on；Adjacent wing ring mechanism direction of rotation is on the contrary, and the inverse time
The total torque of whole wing ring mechanisms of pin rotation is equal with the total torque of the whole wing ring mechanisms turned clockwise.
3. wing ring group mechanism according to claim 2, it is characterized in that：Or two adjacent wing ring mechanisms, scooter number
Amount is equal, and scooter on a wing ring mechanism and scooter on another wing ring mechanism are peering one to one, peering
Two pulley vehicle carriages, which are joined directly together, to be connect or is connected by connecting rod, or a wing ring mechanism scooter track or scooter
Vehicle frame is connected with the circular support of adjacent foil ring, or each wing ring mechanism scooter vehicle frame all with other same supports
It is connected, and they have the same center of circle or their center of circle on same axial line after be connected with same support；Each pair of pulley
Either mutually it is not attached between the connecting rod of car or all intersects with same circular support or same polygon support vertical and handing over
Point connection.
4. wing ring group mechanism is mixed, using the wing ring group mechanism described in Claims 2 or 3, it is characterized in that：More than two or three
Wing ring group mechanism linked together by support or connecting rod, or wing ring group mechanism is connected with wing ring mechanism by support or connecting rod
Together, the connecting rod on the scooter or wing ring group mechanism on each wing ring mechanism between each pair of scooter all with the support phase
Even；Either the center of circle is overlapping is same point or axle center line overlap is the same line for all wing ring mechanisms or wing ring group mechanism, or
Axial line becomes mutually parallel lines；The size and frame mode or identical or difference of each wing ring or wing ring group；Rotation counterclockwise
The total torque of whole wing ring mechanisms of the total torque of the whole wing ring mechanisms turned with turning clockwise is equal.
5. the wing ring mechanism with fixed-wing, is related to a kind of rotor mechanism and Fixed Wing AirVehicle, and according to claim 1
Mixing wing ring group mechanism described in wing ring group mechanism or 4 described in wing ring mechanism or claim 2, it is characterized in that：Wing ring mechanism,
More than one or both of three kinds of wing ring mechanisms such as wing ring group mechanism, mixing wing ring combined mechanism, every kind of mechanism is all not limited to
It is more than one, with one or both of wing aircraft, fixed wing aircraft, aerodone, paraglider, every kind of Fixed Wing AirVehicle
One is also not limited to, is connected as one, connected mode：Or the vehicle frame or scooter track of the scooter of wing ring mechanism directly with
Fixed Wing AirVehicle is connected, or is connected by connecting rod or support with Fixed Wing AirVehicle；Or adjacent foil ring in wing ring group mechanism
Directly it is connected between two paired pulley vehicle carriages of mechanism with Fixed Wing AirVehicle, or by other connecting rods or support and admittedly
Determine rotor aircraft connection；Or the support of wing ring group mechanism is directly connected with Fixed Wing AirVehicle, or pass through connecting rod or other branch
Frame is connected with Fixed Wing AirVehicle；The wing ring mechanism and the wing ring mechanism of rotate counterclockwise turned clockwise in integrated model is simultaneously
In the presence of, and the torsion of all wing ring mechanisms turned clockwise and the wing ring mechanism of all rotate counterclockwises cancels out each other.
6. the wing ring mechanism according to claim 5 with fixed-wing, it is characterized in that：The longitudinal central axis line of Fixed Wing AirVehicle
With the axis or overlapping or parallel of wing ring mechanism or each wing ring；When the quantity of Fixed Wing AirVehicle is more than 1, they
Arrangement mode either without overlapping and be listed in same plane, or they upright projection it is overlapped and they this
Status other places are in the different aspects of parallel surface each other；It is connected with each other between each Fixed Wing AirVehicle by connecting rod or support；
Fixed Wing AirVehicle is provided with can be by integrated model flight attitude from vertically changing into level or changed into from level vertical
Elevator, set or is not provided with the rudder in energy change of flight direction.
7. wing ring type original place landing aircraft, be related to a kind of fixed wing aircraft using propeller as propeller and rotary wind type go straight up to it is winged
Machine, it is characterized in that：Based on the wing ring mechanism with fixed-wing described in claim 6, or electric engine, Huo Zheshe are set
Put ramjet；
Electric engine, or the support of each wing ring sets stator core winding or rotor as support respectively using in Ge Yi ring groups mechanism
Iron core winding makes each wing ring group respectively become the big motor not against axle rotor driven, or in the circular support of wing ring
In upper side, downside, inner ring circumference, outer ring circumference one at or two at more than equidistant be provided with along the circumference of same Radius
The motor of power wheel, while the motor wheel track of the corresponding part setting annular in the circular support of another wing ring；Motor wheel
Track is joined directly together with circular support or is connected by connecting rod, so as to be close together with these positions or in parastate；
The motor wheel track of motor power wheel and adjacent another wing ring mechanism of a wing ring mechanism is allowed to be coupled；Set in mechanism
Fuel electric generator or nuclear energy generator, the circuit of motor is connected with generator circuit, or is set between motor and generator
Battery, motor and generator make circuit connection by battery；
Ramjet is then arranged at the top of wing ring fin, and the engine puff prot direction of same wing ring is consistent, in same wing ring group
The engine puff prot of adjacent both wings ring is towards conversely.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110279648.3A CN102384042B (en) | 2011-09-20 | 2011-09-20 | Wing ring mechanism and wing ring aircraft |
| PCT/CN2012/081623 WO2013041025A1 (en) | 2011-09-20 | 2012-09-19 | Wing ring, and mechanism and method with same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110279648.3A CN102384042B (en) | 2011-09-20 | 2011-09-20 | Wing ring mechanism and wing ring aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102384042A CN102384042A (en) | 2012-03-21 |
| CN102384042B true CN102384042B (en) | 2017-09-12 |
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ID=45823771
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110279648.3A Active CN102384042B (en) | 2011-09-20 | 2011-09-20 | Wing ring mechanism and wing ring aircraft |
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| Country | Link |
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| CN (1) | CN102384042B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013041025A1 (en) * | 2011-09-20 | 2013-03-28 | Luo Conggui | Wing ring, and mechanism and method with same |
| CN105416583A (en) * | 2015-12-15 | 2016-03-23 | 陆明友 | Water and air solar powered airship |
| WO2019033691A1 (en) | 2017-08-15 | 2019-02-21 | 罗琮贵 | High-speed flying method and ring wing aircraft |
| CN108344600B (en) * | 2018-03-20 | 2024-02-13 | 中国环境科学研究院 | Synchronous collection system for multiple particle size microplastic samples in water bodies of different depths |
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| CN2835639Y (en) * | 2005-11-11 | 2006-11-08 | 郭晓琳 | High efficiency fan |
| CN201212448Y (en) * | 2008-01-14 | 2009-03-25 | 邝振凯 | Disc type wind energy impeller wheel |
| CN101460736A (en) * | 2006-06-06 | 2009-06-17 | 海洋能源公司 | System for generating electricity from fluid currents |
| CN101539099A (en) * | 2009-05-06 | 2009-09-23 | 李启山 | Wind wheel or water wheel with internal thrust force and vertical shaft |
| CN101907057A (en) * | 2009-06-04 | 2010-12-08 | 姜志群 | Ring-film blade type windmill |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2835639Y (en) * | 2005-11-11 | 2006-11-08 | 郭晓琳 | High efficiency fan |
| CN101460736A (en) * | 2006-06-06 | 2009-06-17 | 海洋能源公司 | System for generating electricity from fluid currents |
| CN201212448Y (en) * | 2008-01-14 | 2009-03-25 | 邝振凯 | Disc type wind energy impeller wheel |
| CN101539099A (en) * | 2009-05-06 | 2009-09-23 | 李启山 | Wind wheel or water wheel with internal thrust force and vertical shaft |
| CN101907057A (en) * | 2009-06-04 | 2010-12-08 | 姜志群 | Ring-film blade type windmill |
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| CN102384042A (en) | 2012-03-21 |
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Address after: 536000 the Guangxi Zhuang Autonomous Region Beihai City Garden Court Yinwan Hisense building 3 unit A No. 501 Applicant after: Luo Conggui Address before: 536000 Telecom dormitory 5-503, South Sichuan Road, Haicheng District, the Guangxi Zhuang Autonomous Region, Beihai Applicant before: Luo Conggui |
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Address after: Tibet Road, Haicheng District of Beihai City Garden Yinwan 536000 the Guangxi Zhuang Autonomous Region Chishui court 8 Unit No. 102 Applicant after: Luo Conggui Address before: 536000 the Guangxi Zhuang Autonomous Region Beihai City Garden Court Yinwan Hisense building 3 unit A No. 501 Applicant before: Luo Conggui |
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Effective date of registration: 20210701 Address after: 1210, Beihai wenbang international building, 62 Sichuan Road, Haicheng District, Beihai City, Guangxi Zhuang Autonomous Region, 536000 Patentee after: Beihai wing ring Aviation Equipment Co.,Ltd. Address before: 536000 No.102, unit 8, chishuiyuan, Yinwan garden, Xizang Road, Haicheng District, Beihai City, Guangxi Patentee before: Luo Conggui |
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| TR01 | Transfer of patent right |