WO2013041025A1

WO2013041025A1 - Wing ring, and mechanism and method with same

Info

Publication number: WO2013041025A1
Application number: PCT/CN2012/081623
Authority: WO
Inventors: 罗琮贵; 丘寿勇
Original assignee: Luo Conggui; Qiu Shouyong
Priority date: 2011-09-20
Filing date: 2012-09-19
Publication date: 2013-03-28
Also published as: WO2013041025A9

Abstract

Disclosed is a wing ring comprising an annular support (1) and a plurality of vanes (2) provided on the annular support (1), wherein the plurality of vanes (2) are disposed equidistantly on the annular support (1); each vane (2) is connected to the annular support (1) and an included angle is formed between one face of each vane (2) and the circumferential face of the annular support (1); and the included angle includes an angle of 0° and 180° but does not include an angle of 90° or 270°. The wing ring dispenses with a central shaft, directly using the annular support to support the vanes from two sides, thus expanding the gross effective wing panel area, and the ring-shaped support strengthens the load bearing capacity. The wing ring of the present invention can be used for power generation and for lifting heavy objects, such as aircraft. Also disclosed are a mechanism and a method having this wing ring.

Description

Wing ring and mechanism and method with wing ring

Technical field

The present invention relates to a power device, and more particularly to a wing ring and a device therewith and a method of applying the same, and in particular to a wing ring, a wing ring with a fuel tank, a wing ring mechanism, and a wing ring wind power Institutions, high-altitude wing-ring wind power mechanisms, high-altitude water dispensers, wing-wing aircraft, wing-and-loop suspension mechanisms, crane-type transport aircraft, wing-ring wind turbines, reverse flow group energy development, utilization methods, and a construction method.

Background technique

The take-off weight of the aircraft has not reached 700 tons so far, and it cannot reach more than 10,000 tons.

Existing wind wheels can only promote small generators, and the generating capacity of wind turbine generators only reaches a fraction of large steam turbine generators. In addition, there are only ground and sea surface wind turbine generators that can really enter the practicality. Therefore, wind power is subject to low-altitude winds that are sometimes not available, and cannot sustain power generation.

Although the existing high-altitude wind turbine power generation mechanism can solve the problem of continuous and stable power generation, its power generation capacity is too small, resulting in extremely low cost performance, and it is also not competitive in the market. Brian Roberts, a professor of mechanical engineering at the University of Technology Sydney, Australia, who has been widely tested in California and San Diego in the United States, is probably the most successful spin-wing high-altitude wind turbine generator. The machine is equipped with four large-scale spinners at the four ends of a large H-shaped bracket. The four rotor blades are driven by the generator to rotate, which drives the whole machine to fly to the sky, and cuts off the power after going to the high altitude, which is reversed by the wind turbine. Drive the generator to generate electricity and supply power down. However, as this “high-altitude windmill” continues to use the central axis rotor, the maximum takeoff weight of the complete machine is unlikely to reach 210 tons (the largest twin-rotor helicopter in the world currently has a maximum takeoff weight of only 105 tons). Excluding the weight of the body 8 tons and the weight of the cable and the safety weight that must be left vacant, the weight of the generator set can only be under 180 tons, so its single power generation capacity cannot be compared with the large steam turbine generator with the weight exceeding 1,000 tons. On the same page. Another inevitable result of the use of the central axis rotor is that it can only be forced to use the tallest, finest and sharpest materials, and the cost is self-evident. Therefore, like all medium-axis wind turbine generators, it is impossible to assume the responsibility of replacing thermal power and nuclear power.

Only when the flying carrier built by ordinary materials such as steel and aluminum can send the largest generator to the sky, the high-altitude wind power can truly exert its great potential, thus having overwhelming competitiveness!

Existing wind energy vehicles have a common weakness: they must be pulled by the ground cable, otherwise they will naturally fall or drift with the wind. This makes it impossible for wind energy aircraft to achieve free universal cruising.

Since the existing power grid is not strong enough, there are still serious technical obstacles in the wind power grid-connected technology. In addition to the barriers caused by the system, the power grid has become a bottleneck restricting the power transmission of the West, and has become one of the two main bottlenecks restricting the development of China's wind power. . The addition or addition of a long-distance power grid requires over-the-counter and cross-ocean crossings. The construction period is long, the investment is huge, and the maintenance cost is extremely high, so it is almost impossible.

The existing hydropower technology is mainly based on the high-level reservoir power station, but the large-scale reservoir has huge investment, long construction period, and great damage to shipping and ecological environment.

Existing ship moorings and vehicles with windsurfing and kite-powered mechanisms can only use low-altitude wind power, while my "kite electric boat" can simultaneously use wind and wind power to tow ships, but since the ship itself must be used as a kite towing cable. The joints are therefore only suitable for large, very large vessels and cannot be used in upwind strokes. Only when the kite no longer relies on the traction cable of the ship or the ground to provide traction, the car and the ship can use the wind power generated by the high-altitude mechanism in the upwind stroke, and only when the kite no longer relies on the traction cable of the ship or the ground to provide traction, small ships and vehicles Even if the aircraft is not picked up by the high-altitude institutions, it can directly use the wind power generated by the high-altitude institutions.

The existing cranes have the disadvantages of large energy consumption, small lifting capacity, vertical lifting and short horizontal transportation distance. The existing transportation aircraft or helicopter has the disadvantages of huge energy consumption and small carrying capacity. The crane transporter belongs to a kind of high-altitude wind power, which has the flexibility, accuracy and strength of the crane, as well as the long travel and maneuverability of the transport aircraft, and the weight is ten times that of the existing crane. It is 100 times more than the existing large transport aircraft.

In response to the limitations of the prior art described above, the inventors have proposed this series of inventions.

Summary of the invention

The technical problems to be solved and the purpose of invention and innovation:

Providing a wind turbine generator with a power generation capacity exceeding that of a turbo generator, solving the technical problem that the existing wind power generation capacity is too small.

Providing a high-altitude wind turbine generator with single-unit power generation capacity overloaded thermal power and nuclear power single-unit capacity, creating a high-altitude wind power platform with installed capacity several times that of the Three Gorges Project, solving the technical problem that the existing wind power cannot sustain stable power generation and is subject to the grid bottleneck. And the wind power will eventually completely replace thermal power, nuclear power and hydropower with high reservoirs as accumulators.

An aircraft with a capacity of several hundred thousand tons is provided to solve the problem that the existing aircraft load is too small.

The utility model provides a 10,000-ton vertical take-off and landing aircraft capable of starting a ramjet engine at zero speed, and solves the problem that the locomotive efficiency of the ramjet engine is reduced when the aircraft cannot start the ramjet at zero speed and the slow flight.

Providing a vehicle, a ship or an aircraft that is completely powered by a reverse wind group or a reverse water flow group, and solves the problem that all freely cruising vehicles, ships, and aircraft must consume petrochemical energy or must supply additional power.

Providing a crane-type transport aircraft with a lifting weight of over 100,000 tons, a lifting height of up to 10,000 meters, and a transport distance for intercontinental travel, solving the lifting weight, lifting height and moving distance of existing lifting equipment are too small problem.

Provide a new type of natural energy - reverse flow group energy.

Provide an efficient and environmentally friendly new building construction method.

Technical plan and beneficial effects:

Wing ring technical solution:

The fins are equidistantly disposed on the annular bracket, and the fins are connected to the annular bracket and are not connected to the shaft; the airfoil of each fin and the circumferential surface of the annular bracket form an angle of 0° and 180°. The angle does not include any angle (angle of attack) including the 90° angle and the 270° angle.

The difference between the wing ring and the ordinary rotor, the wind wheel, the water wheel or the propeller is that the wing piece is not linked with the axis, and the axis is omitted. Even if the axis is retained, it is not for the shaft to drive the wing or the wing to drive the shaft, but to erect the spoke between the ring body and the shaft center when the wing ring rotates too fast and the centrifugal force is too large. The heart pull reaches the purpose of reinforcing the ring body. In this case, if necessary, the spokes can be designed to have a wing shape that functions both as a spoke and as a fin. The wing ring is actually equivalent to a closed loop formed by the end-to-end connection of a two-wing or single-wing fixed-wing aircraft.

Further, on the basis of the above scheme, the following arrangement is adopted: the fins are all extended to the outside of the circumference of the annular bracket, or all of them protrude to the inner side of the circumference of the annular bracket, or partially protrude outside the circumference of the annular bracket. And partially protrudes to the inner side of the circumference of the annular bracket.

Based on the above solution, the following arrangement is further adopted: the fin is directly connected to the annular bracket or indirectly connected to the annular bracket by the blade deflection mechanism.

On the basis of the above schemes, further adopt the following settings: either all of the lift type fins, or all of the non-lift type fins, or only the lift type fins on either the inner and outer sides of the annular bracket circumference. On the other side, all non-lifting fins are used. Here, the so-called lift type fin refers to a fin that cuts air to generate lift, and its cross section is longer along the line than the lower line, so the air passing through the airfoil surface is faster than the air passing under the airfoil surface, resulting in the airfoil surface. The air pressure on the lower side is stronger than the upper side of the airfoil, thereby generating a lifting force on the airfoil.

Based on the above various solutions, the following arrangement is further adopted: a small fin in the vertical direction is installed at the end of the fin. Since the radius of the wing ring can exceed 500 meters, even if the wire speed of the airfoil can only reach a very amazing degree, it is considered to install a small wing at the end of the airfoil, which is mainly used for weakening. The effect of the airflow around the lower surface of the fins on the upper surface reduces the loss of lift and improves the lift performance of the fins. It is very meaningful for wing-wing spinners or wing-wing mechanisms for wing-wing aircraft.

The beneficial effects of the wing ring:

(1) The high-efficiency wing section area can be expanded several times and dozens of times, and since the axis of the ordinary wind wheel and the inefficient and ineffective wing sections are abandoned, the weight of the high-efficiency wing section can be expanded while the weight of the whole machine can be reduced. And save raw materials. The existing rotor wind wheel can only have a few fins, and the high-efficiency wing segments of each wing piece only occupy a small part, while the high-efficiency wing segments of the wing ring can be increased to dozens of pieces to hundreds of pieces. The efficiency of turning the windmill into power or converting the power into lift is several times or even hundreds of times higher than that of a common wind turbine or rotor of the same radius. The larger the wheel diameter, the greater the difference.

The closer the wind wheel or water wheel is to the axis of the shaft, the smaller the water collecting capacity is, until it is zero, and the farther away from the axis, the greater the ability to collect wind and water, the former is the inefficient wing segment and Invalid wing segment, the latter is an efficient wing segment. In fact, the main function of the low-efficiency wing segment of the ordinary wind wheel is not to collect the wind, but to support the high-efficiency wing segment at the far end to ensure that it is linked with the shaft. It may be more suitable to call it “linkage lever”. This "leverage" has only one side support and the support point is far away from the axis. If the effective wing section is too wide and the wind is too large, it will inevitably cause severe vibration, shaking or even breaking. The actual effect is not as sharp. The wing, so the end of the wing of the ordinary wind wheel is also the high-efficiency wing segment, can not be widened, can only be tapered. The wing of the wing ring is the most efficient wing segment. It completely abandons the low and low wing segments, and instead provides support for the adjacent wings on both sides, compared to the original. The distal, one-sided axial support, the force arm is not only shortened, but also increased from one to two, and the two arms are placed on both sides of the support, the result is: only from a single wing, if The force arm is shortened by 10 times, then the support force is increased by 10 times, and the arm is increased from one to two, so the growth factor of the support force is changed from 10 times to 20 times; the one-side support becomes the support on both sides. Supporting force and stability are further improved; in terms of the number of fins, the conventional shaft wind turbine (or rotor) cannot be added with too many fins, otherwise the flaps are ineffective or inefficient as "linking levers". The wing section can overwhelm the shaft and the bearing, and the wing ring can have a number of fins as long as it does not affect the air cut by the adjacent fins, so the shaft wind wheel or rotor can only have a few fins, and the wing ring The wings can have dozens or even hundreds of pieces, and the area of each wing can be Greatly broadening, i.e. the area of efficient airfoil wing segment ring may be several times, even several times to several hundred times normal wind round the same radius (the larger the diameter, the greater the fold difference).

Therefore, it can be concluded that the wind-resistant and converted wind energy of the wing-ring wind turbine should be several times and tens of times more efficient than the ordinary wind turbine of the same radius. The lift of the wing-ring rotor (takeoff weight) should be the same radius. Ordinary rotors are several times, dozens of times or even hundreds of times.

(2) Each fin is supported by a ring bracket, that is, each fin is supported by all other fins of the entire wing ring, and each fin is also a support point of the wing ring. Each of the fins as a support point distributes the pressure of the entire wing ring. Therefore, as long as the adjacent fins do not hinder each other from cutting the air to generate lift, the number and area of the fins can be increased as much as possible, and the more the fins, the shorter the arm supported by each other, the support The more stable it is. If the rotor is likened to a bridge, the wing-rotor is a toroidal steel bridge. Each wing is its pier. The more piers and the stronger the bridge, the longer it can be. Up to ten kilometers (the radius can exceed 500 meters), as long as enough "bridge piers" (wings) are set. In contrast, a common rotor blade relies only on a shaft that is far from the center of the circle, just like a suspension with only one pier. The shaft is its only pier, and each wing is like a suspended bridge, so it It is impossible to bear too much pressure, and it is impossible to make it too long, otherwise the fins and bearings will be damaged.

Wing ring technology solution with fuel tank:

A fuel tank is provided on the basis of the above-described wing ring scheme. The fuel tank can be connected to the annular bracket or the fin, and can also be connected to the portion of the rail coupling body that rotates synchronously with the annular bracket. Fuels herein include liquid fuels, gaseous fuels, and solid fuels.

On the basis of the above scheme, the following measures can be taken further: installing a ramjet engine for the fin or the ring bracket (the specific method is detailed in the second embodiment of the wing ring with the fuel tank).

Benefits of a wing ring with a fuel tank:

(1) Solving the problem that the fins, propellers, or turbines that are directly driven by the jet engine are difficult to supply fuel at high speeds.

Since there is a fuel tank on the wing ring, no matter how high the speed of the wing ring is, the oil path from the fuel tank to the engine is exactly the same as when it is not rotating, and it will not be disconnected or leaked, nor will it be forced to reduce the supply. The amount of oil. Because the wing ring ring bracket is large enough and high enough, the fuel tank installed on it can have a very amazing capacity and will not be cut off. Even for extra long-range flights, the wing-ring fuel tank can be refueled from the fuel tank of the fuselage during flight (see the third embodiment of the "wing ring with fuel tank").

(2) Solving the problem of inefficient operation of the ramjet engine at zero speed start and low speed.

Why can a ramjet engine be combined with a wing ring with a fuel tank to solve the zero speed start problem?

Because: First, the wing ring with fuel tank solves the problem of ramjet fuel supply on the wing ring; Second, the special shape of the wing ring enables it to be equipped with numerous ramjet engines, and the large wing ring even has hundreds of ramjet engines. Space, so the engine can start to rotate the wing ring and make it speed up quickly (the wing ring is bigger, it is just a rotor, it is impossible to push several or even dozens of ramjet engines equivalent to small rockets. Third, the wing ring rotates, the airfoil cuts the air to generate lift or propulsion, and the aircraft can be lifted and accelerated. After the flight speed is fast enough, the face of the wing ring and the axis of the ramjet can be gradually formed. Adjust to parallel to the direction of the aircraft, then use the brakes or other means to fix the wing ring and the ramjet.

Why can you solve the inefficiency problem at low speed?

Because the aircraft needs low speed flight and air hovering, it can re-engage the ramjet to push the wing ring to rotate, relying on the rotation of the wing ring to provide the driving force or lift, although the speed of the aircraft slows down or even hoveres at zero speed, but the punching The engine does not move at a slow speed and still maintains a normal and efficient stamping operation.

(3) It can develop a model in which the ramjet engine and the aircraft are integrated, and solve the problem that the existing rotary ramjet engine is too large relative to the aircraft.

The result of the combination of the ramjet and the wing ring is that there is no need to add a lot of extra boosting equipment like the existing rotary ramjet, the ramjet is a simple bobbin, and the wing-wing aircraft has a huge load capacity, so even The deployment of numerous ramjet engines will not be “proportional imbalance” and will not overwhelm the aircraft.

(4) Solving the problem that the prior art rotary ramjet flight to the high speed and the rotor seriously obstructs the airflow.

Wing ring mechanism technical solution:

The wing ring mechanism relates to a wind wheel mechanism, a rotor mechanism, a water wheel mechanism or a propeller mechanism, characterized in that: the ring bracket of the wing ring is connected with the vehicle rail coupling body, and the vehicle rail coupling body is coupled with the rail car by the annular track Connected and composed (see the section "Composition of the rail coupling body" below).

Based on the above scheme, any of the following preferred schemes may be further adopted:

Two or more wing ring mechanisms are directly connected or connected by connecting the same carrier; the axis lines of each wing ring mechanism are all overlapped to the same straight line, and the wing rings are either in the same plane and have the same center but different radii (thus Forming inner and outer surrounding multi-wing ring mechanisms), or not in the same plane but the planes in which the respective wings are located are parallel to each other (thus forming a stacked parallel multi-wing mechanism)

Or at least two axial lines do not overlap each other and are parallel to each other, and the other axial lines are parallel or non-overlapping, and are parallel with one or both of the axial lines (therefore forming an axis parallel type multi-wing ring mechanism) ),

Or at least two axial lines form an angle with each other (thus forming an axis intersecting multi-wing ring mechanism).

Based on the above scheme, the following preferred arrangement can be further adopted: the mechanism is set to have both a clockwise rotating wing ring and a counterclockwise rotating wing ring, and the total torques in the two directions cancel each other out.

Based on the above scheme, the following preferred settings can be further adopted: wing ring mechanism and wing, kite, lightweight airbag, buoy, floating row, submarine, ship, tower, tower, tower, bracket, fixed-wing aircraft One or more kinds of connections in the airship. The wing ring mechanism can be connected to the tower and the tower to become a ground wind wheel mechanism. When connected with the wing, the kite and the lightweight air bag, it can become an air wheel mechanism, and the floating wheel and the floating row can be connected to the floating water wheel mechanism. It can be a new propeller propeller when connected to submarines and ships.

The introduction can be made clear that the wing ring mechanism can be divided into a single wing ring mechanism and a multi-wing ring mechanism according to the number of its wing rings. Only one wing ring is a single wing ring mechanism, and two or more wing rings are more. Wing ring mechanism. The multi-wing ring mechanism is divided into four basic structural forms: inner and outer enveloping type, laminated parallel type, axis parallel type, and axis intersecting type according to the arrangement of the central axes of the respective wing rings.

The basic components of the wing ring mechanism: the wing ring and the rail coupling body. The annular bracket of the wing ring is connected to either end of the rail coupling body to form a wing ring mechanism. Here, the term "either end of the both ends" means the left end or the right end of the rail coupling body of any of Figs. 5 to 10.

The composition of the vehicle rail coupling body: the vehicle rail coupling body is composed of a ring-shaped track and a plurality of sets of rail cars, wherein the rail car can be at least a few groups, up to hundreds or even thousands of groups, and the ring track only There can be 1 or 2, and the combination of each group of railcars and ring tracks can be seen in Figures 5-10. Preferably, the frames of each pair of rail cars can be connected in the order of connecting rods, and the connecting rods form a closed annular bracket or a polygonal bracket, so as to effectively maintain the equidistant state between the pairs of rail cars, and ensure The railcar runs stably and smoothly.

The rail coupling body can be classified into several categories, such as the number of rails, which can be divided into a monorail type rail coupling body (Fig. 5, Fig. 8) and a double rail type rail coupling body (Fig. 6, Fig. 7, Fig. 9). Figure 10) Two. The double-track type rail coupling body can be connected by the connecting rod 3-3 (as shown in Fig. 6, Fig. 7, Fig. 9, Fig. 10), or the connecting rod 3-3 can be directly connected.

Since the double-track type vehicle-rail coupling body is more complex than the single-rail type vehicle-rail coupling body, it will reduce the reliability and operating life of the operation, and also increase the manufacturing cost. Therefore, the connection between the wing-ring mechanism and the carrier is generally preferably considered. The coupling body is not the former but the latter.

The two basic components of the rail coupling body can be deformed without missing their functions. For example, the power input wheel of the generator or the power output wheel of the engine is used instead of the wheel of the railcar, and the frame of the railcar is replaced by the fuselage and the frame of the generator, the motor or the engine, for example, the friction coefficient is small. The non-wheel object replaces the wheel of the rail car, and the frame (ie, the wheel frame) is completely omitted, and the rail car and the track are replaced by a magnetic levitation mechanism, for example.

The annular track of the rail coupling body and the annular bracket of the wing ring are at the same point or the same central axis. The annular track of the rail coupling body and the annular bracket of the wing ring can be integrated.

The manner in which the wing ring mechanism is coupled to the carrier: in one wing ring mechanism, since only one end of the two ends of the rail coupling body is connected with the annular bracket of the wing ring mechanism, the other end can serve as the wing ring mechanism and its carrier Connection port. The carrier herein includes a fixed carrier and a moving carrier, and the fixed carrier refers to a tower, a tower, a base, etc., and the moving carrier refers to an aircraft, a vehicle, a ship, and the like. Alternatively, the carrier can be another wing ring mechanism.

The carrier of the wing ring mechanism may be another wing ring mechanism having the same axis line and connected to the wing ring mechanism, or may be an object that acts as a load or support or fix for the wing ring mechanism, such as a wing, Fixed-wing aircraft, airships, lightweight airbags, buoys, floating rafts, submarines, ships, towers, towers, towers, supports, pedestals, buildings, dams, walls, curtain walls or vehicles. Ships, submarines, etc. appear in this list of carriers because the wing ring mechanism can be applied not only to airflow (wind) but also to water flow.

The carrier of the wing ring mechanism often determines the function of the wing ring mechanism. If the wing ring mechanism is connected with the ground tower, it will become a ground wing ring wind wheel mechanism (such as a wing ring wind turbine generator). If it is connected to the fuselage of the aircraft, Will become a wing ring aircraft (such as a wing ring helicopter), if connected to another wing ring mechanism, it will become a high-altitude wing ring wind wheel mechanism (such as high-altitude wing ring wind power mechanism), if connected with a lightweight air bag, it will become A wing ring mechanism that is stable even when there is no low altitude in the wind (it is very suitable for use as a low-altitude wind turbine generator).

The principle that the rail car must be followed by its orbital coupling:

First, the rail car can have only one wheel, or a set of wheels. Regardless of the number of wheels, the arrangement and the axial direction of each wheel, it must ensure that all rail cars run smoothly without derailing. In order to achieve this, in a rail coupling body, it is necessary to ensure the coupling between the wheel and the rail in four directions, because the coupling of the wheel and the rail in four directions is equivalent to the four boundaries of the operating range of the wing ring. . Therefore, if the rail coupling body is on the side of the plane where the wing ring annular bracket is located (as in the vehicle rail coupling body 3 in Fig. 15, it is on the side of the plane where the wing ring 1-3 and the wing ring 1-4 are located) Then, each group of railcars should be equipped with 4 to 5 pulleys, so that they can stand in the four directions of the rail from the inside of the rail with a trough-shaped cross section (as shown in Fig. 5), or let them from four directions. Clamp the four walls of the T-shaped rail in the outer direction (as shown in Figure 8); if the rail coupling body is on the side of the circumference of the ring-shaped annular bracket, then each group of railcars can only guarantee the top by setting 3 pulleys. Live or clamp the wall in four directions of the track (as shown in Figure 6, Figure 7, Figure 9, Figure 10), or as shown in Figure 14, although the three wheels only support the wall in three directions, but because of its car The bracket 3-2 is fixedly coupled to the annular bracket of the wing ring 1-2, which in fact prevents the possibility of slipping from the fourth direction.

The advantage of the grooved track is that it is not easily contaminated by external debris. The advantage of the T-shaped track is that it is easy to overhaul.

Second, the railcars on the track should generally be no less than three (except for the railcars replaced by magnetic suspension mechanisms or similar mechanisms), and the larger the radius of the wing rings, the more railcars should be on the track.

Third, the type of track wheel and the type of track must match. For example, if the track is a smooth track shaped like a railway, then the wheel should use a wheel with a smooth wheel that is coupled with it; for example, the track is a toothed track (ie, the contact surface of the track and the wheel is toothed), then the wheel Gears that engage with it should be used; for example, if the track is replaced by a magnetic levitation mechanism, the function of the wheel should be replaced by a corresponding magnetic levitation mechanism.

The four basic structural forms of the multi-wing ring mechanism are: inner and outer enveloping type, laminated parallel type, axis parallel type, and axis intersecting type.

The beneficial effects of the wing ring mechanism:

(1) The total load that the ordinary rotor can only bear by one shaft, the wing ring mechanism is distributed to the array, dozens of groups or even hundreds of thousands of rail cars, which is equivalent to the number of axes increased by several times, dozens of times, Hundreds of times, so the mechanical strength is increased several times or even hundreds of times.

(b) If it is a wind turbine, its power is enough to drive hundreds of the current larger wind turbines; if it is a helicopter's rotorcraft, it is enough to fly more than tens of thousands of tons of objects.

At present, the largest transport aircraft is the An-225 strategic transport aircraft developed by the former Soviet Union. It has a height of 18 meters, a wingspan of 88.4 meters and a maximum takeoff weight of 640 tons. That is to say, an An-225 wing can carry 640 tons of take-off weight. . The wing ring is equivalent to an "aircraft ring" formed by the end-to-end connection of many fixed-wing aircraft. Assuming a wing ring with a radius of 500 meters and a circumference of 3.1416 kilometers, a total of 80 fins of the An-225 transport aircraft are installed. The take-off weight of this "aircraft ring" is:

80 pay × 640 tons / pay = 5.12 (ten thousand tons)

Even a small wing ring with a radius of only 50 meters can take up to 50.12 million tons of take-off weight. The largest helicopter in the world is the Mi 12 twin-rotor helicopter developed by the former Soviet Union. The maximum take-off weight is only 105 tons. And because it is too bulky, the model only produced two, one of which only flew several missions, and the other never was put into use.

In this paper, the An-225 transport aircraft wing is borrowed for convenience. However, the airspeed of a large transport aircraft must reach 600~700km/h to take off and cruise normally. Can the air-driven airfoil reach this airspeed?

Even if the windmill that the child plays is more than 1r/s under the normal wind force on the ground, and the small rotor does not multiply proportionally, the angular velocity does not change much in the same wind, so the wing ring is even in the ordinary wind on the ground. , the speed will also exceed 1r / s In the high-altitude strong wind, the speed will be much higher than 1r/s. When the speed of a large wing ring with a radius of 500 meters is only 0.1r/s, or when the speed of a small wing ring with a radius of 50 meters is only 1r/s, the line speed of the airfoil is as high as 1130.98km/h, nearly twice as much. Large transport aircraft take off airspeed! Therefore, it is not necessary to worry about the airspeed of the wing. On the contrary, it is necessary to forcefully and greatly reduce the speed of the wing ring. Otherwise, the centrifugal force is enough to completely dissipate the wing ring itself. The best way to reduce the speed of the wing ring is to increase the power generation load and use the generator to brake the wing ring to ensure safe and stable operation, achieve more power generation and better economic benefits, and make the steel suitable for manufacturing its track. And rail cars.

Since the speed of the large high-altitude wing loop is so high, will it be unstable and overturned?

will not. Due to the low angular velocity, each segment of the large wing rotor is more stable than a high-speed train with a large bend, so there is no danger of overturning.

Will the high-altitude wing ring mechanism be rough and fall?

High-altitude winds are characterized by strong, sustained, and stable winds, and there is no wind speed. Even if the accident is dangerous, as long as the wing ring has the characteristics of the spin wing, it will automatically rotate during the falling process, which will drive the air to cut the air and generate lift. Therefore, the wing ring mechanism will slowly fall like a spin wing without falling violently.

(3) The structural method of distributing the load originally carried by one shaft to multiple sets of rail cars also reduces the requirements on materials, and also reduces the manufacturing difficulty, while improving the mechanical reliability and operating life.

(d) The average distribution of all torque and load to an array to hundreds of railcars also allows several to hundreds of smaller engines to jointly propel a large, very large wing-type rotor, thus developing large, The ultra-large wing-wing aircraft does not have to be redeveloped to match large engines.

(5) Combined with the ramjet engine, it can solve the problem that the ramjet engine cannot be started in the zero speed or slow phase of the aircraft. The ramjet engine pushes the wing ring to rotate, and the wing ring generates lift or forward propulsion force to take off and accelerate the aircraft. In this process, although the overall flight speed of the aircraft is not large, the linear speed of the ramjet engine with the circular motion of the wing ring can reach the natural punching. Speed; after the airplane reaches a high speed, the wing ring can be gradually stopped, and the airfoil surface is gradually deflected to be consistent with the forward direction. The axis of the ramjet engine is also deflected to coincide with the advancing direction, and can be completely relied on the speed of the aircraft; Or to resume slow flight, just restore the angle of the airfoil and the axis of the ramjet to the state of take-off and reduce the oil supply to the engine.

(6) Cascading parallel type (such as wing ring mechanism embodiment 4, see Fig. 15 and Fig. 16) or inner and outer surrounding type (such as wing ring mechanism embodiment, see Fig. 13 and Fig. 14). The multi-wing ring mechanism not only expands the wing ring mechanism. The body shape greatly enhances the mechanical strength and smoothness of the wing ring mechanism.

Two adjacent wing ring mechanisms of the two multi-blade mechanisms, the annular track of one wing ring and the rail car of the other wing ring mechanism are coupled to each other, if we regard each wing ring as a column The "train loop" formed by the long trains connected end to end (only the wings of each car are long), then the two winged "train rings" are mutually trains and tracks each other, that is, the wing ring Running (rotating) along the orbit of the wing ring like a train, the wing ring also runs (rotates) along the orbit of the wing ring like a train, that is, whether the two wing rings share the same set of rails, rail cars, or Each has its own track and rail car. In short, the two wing rings are combined by the coupling of the rail car and the track, so that the two will not be separated and will not collide, neither hindering each other from rotating in the opposite direction, Reinforce each other to double their strength.

If the rail coupling bodies of the respective wing ring mechanisms are connected to the same bracket to form a multi-wing ring mechanism with overlapping central axes (such as wing ring mechanism embodiments 11 to 13 and seen in FIGS. 23 to 12), then each wing The rings will also be mutually supported and strengthened by this common bracket.

(7) The multi-wing ring mechanism with the parallel parallel type and the inner and outer enveloping features has sufficient mechanical strength and sufficient wind resistance due to the mutual support of the upper and lower multi-layered wing rings. Wing ring mechanisms with a radius of up to several hundred meters can also be built using ordinary steel and aluminum.

(8) The axis intersecting multi-wing ring mechanism enables a wing ring mechanism to simultaneously push thrust in multiple directions, or to convert wind energy in one direction into power or electric energy while emitting lift or thrust in one or more directions. . The axis intersecting multi-wing ring mechanism can increase the flight stability of the aircraft. By changing the rotational speed or the angle of the axis of one of the wing rings on both sides of the angle, it is also possible to break the force balance state on both sides of the aircraft, thereby realizing the aircraft turning. Or pan across.

The technical solution of the wing ring wind power mechanism:

The annular bracket of the wing ring mechanism is connected directly or indirectly to the generating winding.

Two ways of configuring the wing ring wind power mechanism:

1. The annular bracket of the wing ring is directly connected to the power generating winding. That is, the annular bracket is used as a support for the power generating winding, so that the entire annular bracket becomes a huge annular power generating winding, and then one or two annular brackets which are arranged in the same way as the annular power generating windings are formed without relying on The giant generator that drives the rotor with the shaft (herein, the "ring bracket that is set as the ring-shaped power generating winding in the same way" can be either a ring bracket of the wing ring or other ring brackets (referring to non-rotating, or a ring-shaped bracket that rotates but does not have a fin, for example, a ring-shaped bracket attached to a ring-shaped power generating winding attached to a carrier only for the core-core cutting magnetic field on the wing-ring annular bracket;

Second, the ring bracket of the wing ring is connected to the power generating winding through the rail coupling body. In this way, there are two different methods of setting: one is to directly replace the wheel of the railcar with the power input wheel of the generator (the generator that relies on the central shaft to drive the rotor to rotate), and the machine of the generator The body is connected to the frame of the railcar or directly replaces the frame of the railcar with the fuselage of the generator; the other is to fix the generator to the frame of the railcar, and to power the wheel of the railcar and the wheel of the generator. connection.

An example of the connection method between the power generation unit and the external circuit on the rotating wing ring:

Example 1: The circuit of each generator is connected with a brush, and the brush is connected with the wheel of the generator power wheel or the rail car, and the external circuit is connected with the track, and the circuit connection is achieved through the coupling contact of the wheel and the track.

Example 2: No matter how many electrodes are set in the generator, connect parallel or series in parallel or series to the same joint, then connect each joint to the corresponding brush rail, and the brush rail is attached to the wing ring groove. The outer edge of the track (the insulating isolation layer is to be provided between the brush track and the wing ring track), the brush track is in contact with the respective brushes, the external circuit is connected to the brush, and the brush does not rotate with the wing ring. Components such as railcar frames or links connecting two railcar frames are connected such that the rotating brush rails and brushes form an uninterrupted electrical connection.

The wing ring wind power mechanism can be connected to the ground carrier to become a ground wing ring wind power mechanism (such as a tower table wing ring wind turbine generator), and can be connected with a carrier in a water flow (current current, ocean current or large river, large river) to become a wing ring water. The wheel generator can also be connected to the high-altitude mechanism or become a high-altitude wing ring wind power mechanism (such as a high-altitude wing ring wind power mechanism and a pull-wing ring wind power mechanism) by setting the wing ring itself as a lift type airfoil.

The beneficial effects of the wing ring wind power mechanism:

First, the power is huge, the single-unit power generation capacity will reach or exceed the level of the steam turbine generator (see “The Benefits of the High-Air Wing Ring Wind Power Mechanism” (4)).

2. In the present invention, adjacent wing wrapping groups can mutually rotate the rotor in opposite directions, so that the relative speed of each wing surrounding group of the rotor is doubled, so that the generator shape is not enlarged, the rotor speed is not increased, The power generation capacity is doubled without increasing the electromagnetic load, so it can break through the current body shape limit and capacity limit, and develop a giant generator that cannot be imagined by current technology.

The current generator can only rotate the inner core and the winding (inner rotor) by the middle shaft, or can only rotate the outer core and the winding (outer rotor) by the outer shaft, but not the inner and outer core windings. The rotors are mutually reversed at the same time. In order to reduce the mechanical stress caused by centrifugal force and reduce wind friction, the existing rotors are generally smaller in diameter and larger in length, that is, elongated rotors, especially high-speed rotors of 3000 rpm or more. Due to the strength of the material, the diameter is strictly limited and generally cannot exceed 1.2 meters. The length of the rotor body is limited by the critical speed. When the length of the body reaches 6 times of the diameter, a large vibration may occur during operation until a shaft breakage occurs. Therefore, the size of large high-speed generator rotors is strictly limited. It is for this reason that there is a technical limit in increasing the shape of the generator. It is extremely difficult to develop a larger capacity model. The current technical measures are mainly to increase the electromagnetic load, enhance the cooling and cooling, etc., and it is difficult to achieve leap. progress.

Even if the technical advantages of the power generation capacity multiplication caused by the reverse rotation of the rotor of the present invention are not considered, the high-altitude wing-ring power generation mechanism is much more powerful and more powerful than the ordinary high-altitude wind turbine generator. It's much easier and the cost is much lower.

Technical solutions for high-altitude wing ring wind power institutions:

Based on the "wing ring wind power mechanism technical solution", the following preferred settings are made: a lifting device, such as a wing ring mechanism and any one or more types of lifting including a lightweight airbag, a lift type wing or a kite Institutional connections, such as wing ring mechanisms, directly use lift-type fins as the wings of their wing rings. If the lifting mechanism of the wing ring mechanism does not have the ability to prevent the wing ring mechanism from rotating with the one-way torque, then the high-altitude wing ring wind power mechanism should adopt a multi-wing ring mechanism, and the total torque and clockwise direction of each wing ring in the counterclockwise direction. The torques cancel each other out.

The lifting mechanism or the wing ring lifting fins enable the wing ring wind power mechanism to fly into the air to become a high-altitude wing ring wind power mechanism. The lightweight airbag in the floating mechanism has a special function compared with other floating lifting mechanisms. It can make the wing ring wind power mechanism stably suspended in the low-altitude and sometimes low-altitude wind, so as to meet the needs of low- and medium-level wind power generation. The winds in the middle and low altitudes are often variable, and it is difficult to ensure that the wings, kites, etc. get enough lift, but some houses, communities, farms and small businesses use little electricity, and there is no need or ability to obtain approval from the air traffic control authorities (1000 meters in China) Air traffic is implemented in the above airspace).

Based on the above scheme, the following arrangement may be further made: the circuit of the power generation mechanism is connected to the upper end of the cable, and the lower end of the cable is connected to the lower power installation; the upper end of the traction cable is connected to the lower end of the high-altitude mechanism without rotating the wing ring, and the lower end of the traction cable Connected to the electrical facilities below. This is a method of connecting a high-altitude wind power unit to a ground power facility (of course, the high-altitude wind power unit may not be connected to an external cable but only to a power facility on a high-altitude mechanism).

Based on the above scheme, the following preferred solution can be further adopted: the airfoil is equally spaced on the annular support to form a wing ring; the airfoil adopts a lift type airfoil, and each airfoil is like a wing of a common wind wheel. The last section (specifically, the high-efficiency wing section) forms an angle between the airfoil and the circumferential surface of the wing ring, that is, the angle of attack; the fins may protrude outward or inside the ring, or may protrude toward both sides at the same time; The angle of attack of all the fins on the wing ring is the same, and the angle of attack of the adjacent wing ring is opposite; two to three wing rings form a wing ring group, the same group of wings are in the same plane and have the same center, or each The rings are parallel to each other and the center of the circle is on the same axis. There may be only one set of wing rings in the whole machine, or two or more sets of wing rings. Each set of wing rings can form a complete power generation mechanism.

Based on the above scheme, the following preferred solution can be further adopted: two or more high-altitude air-wing wind power mechanisms are connected end to end by a traction cable and a cable, that is, a whole machine at the upper end or the lower air head, and the lower end thereof By connecting the traction cable to the upper end of another complete machine of the lower or upper wind head, the circuits of the whole machine are connected by cables and finally connected to the ground electrical facilities through the same cable. The advantage of this multi-machine serial connection is that multiple machines can use the same traction cable and the same cable, thereby reducing the load of each machine and saving a large number of traction cables and cables and reducing the weight of each single machine.

Method of releasing high-altitude wing ring wind power mechanism:

The most convenient and quick way is to use the generator as a motor, that is, to input electric energy to the power generation mechanism through the cable, so that the wing ring rotates to generate lift and fly up. If there is no electricity or less electricity, the airbag device is used, that is, an air bag is arranged in the upper part or the periphery, the middle part or even the lower part of the ring body, and the air bag is filled with light gas, so that the air bag takes off with the high-altitude wing ring wind power mechanism, and the standby body When the wind rises to a sufficient height, the wing ring will inevitably reach a sufficient speed to generate enough lift to recover the airbag.

Ways to release large, very large, high-altitude, wing-wing wind turbines with wing rings up to several hundred meters in diameter:

The power required to fly large, ultra-large high-altitude wing-ring wind power installations that do not have lightweight airbags is extremely large, and the power grid is unbearable. To this end, some of the power of the existing power grid can be used to fly several small machines, and a small number of small machines can be used to generate and fly medium-sized machines. Only a large number of medium-sized machines can generate large-scale and super-large machines.

The high-altitude wing-ring wind power mechanism that relies on the input power to lift off can stop the input power after the wind has reached a sufficiently high altitude, allowing the high-altitude wind-driven airfoil to rotate to generate lift to maintain the suspension and simultaneously generate electricity, and then send power to the ground. . The wind above 4,500 meters is strong enough and continuous, but the best wind farm is the stratosphere above 10,000 meters. Because the stratospheric wind force is 55 m / s, reaching the level of 16 strong typhoons, the maximum power generation can be achieved. There are no lightning, rain, snow and clouds, and there is not much dust. It can generate electricity continuously and minimize the depreciation speed of equipment, so the running cost is extremely low.

The beneficial effects of high-altitude wing ring wind power institutions:

First, all the advantages of the wing ring wind power mechanism.

Second, there is no need to build a high tower to achieve a height far higher than the high tower, and greatly simplify the construction of the wind turbine generator.

Third, the high-altitude wing-ring wind power mechanism connected with the lift mechanism such as light airbags, kites or wings can be suspended in the low-altitude, thus avoiding the interference of the air traffic control authorities, and is conducive to the self-power generation of houses, farms or small enterprises.

The wing ring mechanism is used for abandoning the central axis rotors that have been used for centuries, and the maximum takeoff weight of a wing ring with a radius of only 500 meters can exceed 50,000 tons (see "The Benefits of the Wing Ring Mechanism" for details) <2>) Therefore, even if there are only two wing rings with a radius of 500 meters, the maximum takeoff weight of the high-altitude wing ring wind power mechanism can exceed 100,000 tons. In this 100,000 tons, it is assumed that the weight of the fuselage is 20,000 tons, the air intake equipment is 0.5 million tons, the other facilities including the traction cable is 0.5 million tons, the vacant safety weight is 10,000 tons, and the remaining 60,000 tons is used to install the generator set. It can install 60 million kilowatt-class generator sets weighing 1,000 tons/set. Therefore, the total installed capacity of this high-altitude wing-ring wind power plant is about 60 million kilowatts (if a wing-ring type rotor generator is used, the power generation capacity is likely to increase significantly).

Even if the radius of the two wing rings is reduced to 50 meters, the maximum takeoff weight of the high-altitude wing ring wind power system is still more than 10,000 tons, and the total installed capacity still exceeds 6 million kilowatts.

Fourth, the cost is extremely low, the construction period is extremely short, the service life is extremely long, the operating cost is extremely low, and the electricity price is extremely low.

Since the flaps that can only be used for one-side and far-end support are changed to two-side and near-end supports, the torque and load that could only be carried by a single shaft are distributed to hundreds of rail cars, so the high-altitude wing ring Compared with the existing large aircraft, the wind power system is much less difficult to design and construct, and the stability of the operation is greatly improved, and the operating life is greatly extended (see "The Benefits of the Wing Ring" and "The Benefits of the Wing Ring Mechanism" in this article. Because of its zero fuel cost, the operating cost is also extremely low (see the last paragraph of "Methods for Flying High-altitude Wing Wind Power Mechanisms" in the "Technical Plan for High-altitude Wing Ring Wind Power Organizations"); due to the high-altitude wing ring The wind power system is actually a very simple spin-wing aircraft, but its shape is particularly large. Therefore, even large-scale high-altitude wing wind power plants have lower construction costs.

5. As long as the communication receiving and transmitting device is set up, the practical value of the ground communication base station and the communication satellite can be obtained greatly, and the cost is greatly reduced. Compared with communication satellites, it has short signal round-trip delay and less free space attenuation, which is conducive to miniaturization, wideband and symmetric duplex wireless access of communication terminals. Compared with terrestrial cellular systems, the role of this high-altitude station The short distance, large coverage area, and small channel attenuation can significantly reduce the transmission power, which not only greatly reduces infrastructure construction costs, but also reduces radiation pollution around the base station.

Sixth, it can fly to the upper troposphere and the stratosphere, and use the high-speed and stable wind layer of the troposphere and the stratosphere to achieve stable power generation for many years.

The wing ring technology used in the high-altitude wing-ring wind power mechanism greatly expands the high-efficiency section of the rotor wing, and at the same time greatly increases the support force obtained by the high-efficiency section of the rotor, and the lift is obtained by driving the wing ring through the cable input power source, and there is no energy. Insufficient problems are not affected by the thin air at high altitudes, so it can easily overcome the defects of existing fuel helicopters and easily rise to the stratosphere.

High-altitude water dispenser technical solution:

Any combination of a high-altitude power generating mechanism including a high-altitude wing wind power mechanism and an air water extractor is connected, and the circuit of the high-altitude generator is connected to the circuit of the air water extractor;

Based on the above scheme, the following arrangement can be further made: the circuit of the high-altitude wing ring wind power mechanism is connected with the circuit of the air water extractor; the inlet and outlet of the water tank of the air water dispenser is connected with the upper end of the water pipe, the lower end of the water pipe and the lower reservoir or water facility Connection; the water pipe can be combined with the traction cable.

There are many ways to connect the high-altitude wing ring wind power mechanism to the air water extractor, but there are two ways to operate it most easily: one is to connect one end of the rail coupling body to the bracket or outer casing of the air water dispenser, and the second is to The traction cable of the high-altitude wing wind power mechanism passes through the center of the air water extractor, and the air water extractor is suspended from the traction cable, and one, two or more can be suspended.

For the high-altitude water-discharging device whose high-altitude power generation mechanism operates in the stratosphere, its water-taker can be hung on the cable section of its ground traction cable in the troposphere, so that both the wind power of the stratosphere and the rich water vapor of the troposphere can be obtained. Stratospheric water vapor is less, and dust and other "cores" that promote water vapor condensation are rare. Therefore, water is taken from the stratosphere, and the cost may be higher than that of the troposphere.

The benefits of high-altitude water dispensers:

First, solve the water problem of high-altitude organizations.

Second, to solve the water shortage problem in deserts, islands and other serious shortages of freshwater areas.

At present, in order to increase the supply of fresh water, in addition to the use of conventional measures, such as nearby water diversion or cross-basin diversion, a favorable approach is to dilute sea or brackish water nearby. There are many methods for desalinating seawater or brackish water, but conventional methods such as distillation, ion exchange, dialysis, reverse osmosis membrane, and freezing have not only cost a lot of money, but also consume a lot of Fuel or electricity. Therefore, it is generally believed that the development of solar desalination technology is the best choice.

However, the cost of solar desalination is not very substantial, and many places that lack water are not close to the sea. Even in the offshore, solar energy cannot be used at night. Therefore, in recent years, humans have developed air water dispensers that can successfully take water. However, due to the high energy consumption of existing air water dispensers, the cost of water intake is too high to implement large-scale production, and the promotion of small models also lacks economic value. In addition, in arid areas where water is most needed (such as deserts), the low-altitude air is also extremely dry, and it is not feasible to use the prior art for air intake.

The wing ring high-altitude water dispenser completely meets several difficult requirements such as no energy consumption, low cost, large scale, and no day and night, no geographical restrictions. Since it can self-supplied electric energy at high altitude, there is no problem of excessive water cost caused by energy consumption, and it can also supply power to the ground; since the water extractor is suspended at a high altitude, especially a high-altitude water dispenser with a high-altitude wing-ring wind power mechanism as a carrier, It can also load large, giant air water extractors flying up to several kilometers or even 10,000 meters, even in the driest desert, there is a cloud above it, indicating that the water vapor is very rich, in fact, water vapor is The wind is circulating all over the world, but the desert surface and the low sky are too dry. When the air flows, the moisture has already been swept away. Even if the rain has not yet landed, it has been sucked up by the dry air. But this is only for the ground and low altitude, the impact on the airflow at high altitude is not great. Therefore, the use of the present invention for water intake in the air is not subject to geographical restrictions. Even in the desert hinterland, high-quality water can be produced without energy consumption, low cost, large-scale, and uninterrupted.

Technical solutions for wing-wing aircraft:

The wing ring mechanism or the multi-wing ring mechanism is used as a propeller mechanism, a spin wing mechanism or a rotor mechanism of the aircraft; the wing ring mechanism is connected with the power mechanism.

Based on the previous solution, any one of the following preferred settings may be further provided: the power mechanism is an engine or a transmission mechanism that is electrically connected to the engine. The so-called engines here include fossil fuel engines, various electromagnetic engines, various nuclear power engines, and steam engines.

Based on the above scheme, any one of the following preferred settings may be further provided: the fuselage of the aircraft or the fixed wing, or the wing is connected by a deflection mechanism, or the wing is not provided at all (here "wing" "Finger that moves in sync with the fuselage, not the wing on the wing ring."

Based on the above scheme, the following further settings may be further made: the annular track of the rail coupling body of the wing ring mechanism or the rail frame and the fuselage (including the nose and the tail, not just the middle of the fuselage) or The wing is connected. The fuselage may be cylindrical, ring-shaped or other shape or various brackets; its wing ring may be a wing ring with a fuel tank, or a wing ring without a fuel tank; its fins may be lift blades, or Lifting fins are not used, but as the wing-wing mechanism of the spin-wing, the fins must be lifted, otherwise the characteristics and functions of the rotor are not available.

How to set up several engines for wing-wing aircraft:

First, the setting method of the jet engine:

Jet engine (refers to all engines including ramjet engine that directly obtain propulsive force by spraying gas), placed on the wing ring or ring bracket of the wing ring (preferably the position farthest from the center of the wing ring, purpose) Is to make the jet engine get the largest possible radius of motion), the engine is fixedly connected with the wing or the ring bracket, or connected by the fin deflection mechanism, that is, the jet engine is connected to one end of the deflection mechanism, and the other end of the deflection mechanism A wing or ring bracket attached to the wing ring (the function of the deflection mechanism is to adjust the orientation of the engine's central axis at any time according to actual needs, for example, in the take-off or slow flight phase, the air vent is oriented in the opposite direction to the direction of rotation of the wing ring, In order to drive the wing ring to rotate to generate the lifting force, when the aircraft is flying at high speed, the jet port is directed in the opposite direction of the forward direction of the aircraft, so that the propulsive force is fully applied to the forward direction); the orientation of the engine jets on the same wing ring and the direction of rotation of the wing ring Conversely; the fins and the ring-ring annular bracket are either fixedly connected or connected by a flap deflection mechanism, ie The other end is connected one end connected to blade deflection mechanism airfoil blade deflection means and the annular holder ring wing. Here, the function of the fin deflecting mechanism is to bring the fins to a suitable angle of attack when the flap rotation is required to provide lift, and to make the fins completely parallel to the wind direction when the high speed flight requires the fins to let out the airflow passage, thereby avoiding blocking the high speed. The airflow passes.

Here, the blade deflection mechanism between the airfoil and the annular bracket is indispensable, and it is less, and the engine airflow is blocked when the airplane is flying at a high speed. If the jet engine is connected to the ring bracket, it must also be connected to the ring bracket by a deflection mechanism, otherwise the direction of the jet port cannot be changed; if the jet engine is connected to the fin, then it is not between the wing and the fin. Be sure to connect through the deflection mechanism, because the center axis of the jet engine will deflect as the blade deflects and the angle of attack changes, but this approach does not necessarily allow the engine to accurately deflect to the angle required for each stage, so the engine and wing Preferably, the sheets are connected by a deflection mechanism to allow the engine to be accurately deflected to accommodate different stages of the process.

If it is necessary to develop an aerospace aircraft, it is necessary to eliminate the friction of the airfoil of the wing ring (although the airfoil has been welcoming the wind with its edge, but for the very high speed aerospace aircraft, still cause great resistance and extremely high friction heat) For this reason, on the basis of the previous embodiment, the following preferred settings are made as follows:

The engine is a ramjet engine that can be mounted on the wing of the wing ring or on the ring bracket; adding a folding mechanism to the wing of the wing ring (making the blade relative to the fuselage like the blade of the folding knife relative to the shank, instead of Like the door relative to the door frame). The folding mechanism is located between the airfoil and the annular bracket. If the ramjet engine is mounted on the wing of the wing ring, that is, there is originally a wing deflection mechanism between the airfoil and the annular bracket, the folding mechanism is located at the deflection mechanism and the ring There is also a folding mechanism between the brackets or between the deflecting mechanism and the fins, and between the ramjet and the fins (the flaps are opposite to the shank of the folding knives relative to the engine), so that the ramjet is folded in the fins. Simultaneous folding during the process, so that the engine's central axis and the fuselage central axis are always consistent, and finally attached to the fuselage, so as to eliminate the frictional resistance of the airfoil to the air.

Since the wing ring must rotate when the wing ring is in zero speed start, air hover or slow flight, if the wing ring without fuel tank is used, then only the existing technology can be used, that is, some helicopters are given to the wings in the rotor. The technology of the jet engine at the end of the sheet is oiled, but it is difficult in the prior art to obtain sufficient fuel for the engine with the high-speed circular motion of the wing ring. Only the wing ring with fuel tank can fully meet the oil supply requirements of the rotation phase of the wing ring. Because the size of the ring-ring ring bracket can be very large, the capacity of the wing-ring fuel tank can fully meet the fuel requirements of the entire flight. However, it is not necessary to design the capacity of the wing ring fuel tank very large, because the time required for the zero speed start and slow flight phases of the wing ring aircraft is not too long, the aircraft will enter the high speed state faster, and enter After the high speed state, the wing ring can be braked and then replenished with oil (for details, see the second and third examples of the wing ring with fuel tank).

Second, the piston internal combustion engine setting method:

The power output wheel of the internal combustion engine is coupled to the circular orbit of the wing car and the annular track of the wing ring, and the airframe of the internal combustion engine and the annular track of the wing ring, or two adjacent single wings respectively being in line with the central axis The ring mechanism of the ring mechanism is connected, or one of the two is connected to the ring ring ring bracket and the other is connected to the aircraft.

Third, the setting method of the electric engine:

Method 1: Set according to the setting method of the internal combustion engine (just replace the fuselage of the internal combustion engine with the fuselage of the electric motor);

Method 2: The number of wing rings on the same axis is not less than two. The rotor windings are arranged on the ring brackets of these wing rings (making the wing ring become a huge coil), and the adjacent two wing rings They are mutually rotors, mutually stators, and rotate in opposite directions to each other, becoming a generator with no rotor shaft. This huge motor does not actually have a stator because each winding with a wing ring is rotating.

If an electric motor, ionization injection engine, electric boiler steam injection engine or air compression injection engine is selected, a fuel generator or a nuclear power generator should be provided on the mechanism to connect the motor circuit to the generator circuit, or in the motor and generator. A battery is provided between the battery and the motor and the generator respectively. If a fuel jet engine or an internal combustion shaft engine is selected, a fuel tank (actually a wing ring with a fuel tank), an engine and a fuel are arranged on the wing ring. The box is connected as an oil circuit.

If the endless track is shaped like a railway track, the power take-off wheel of the electric motor or internal combustion engine must be shaped like a train wheel; if the endless track is a gear track, the power take-off wheel of the electric motor or internal combustion engine must be a gear.

Wing ring aircraft with organic wings:

The position of the wing ring can be at least two: one is the wing ring connected to the fuselage (as shown in Figure 39, Figure 40), and the other is the wing ring connected to the wing (Figure 41 ~ Figure 44).

About a winged aircraft without a wing - a wing ring helicopter:

Wings of wing-wing helicopters can be lift-type or common propeller blades. If you use a lift-type wing, you will get two advantages: First, when the wing-wing aircraft is flying at a horizontal or near-horizontal level, as long as the engine for providing horizontal moving force is controlled, the wing-wing aircraft produces a proper back-tilt angle, and the wing ring The wind can be rotated to generate lift, so that the engine used to drive the rotation of the wing ring can be turned off to reduce energy consumption. The second is that the wing ring will rotate in the wind during the natural decline of the power, and the lift will make the plane land smoothly. With the characteristics of the spin-wing, the aircraft can only fall and fall at the speed of free fall.

When the wing ring helicopter has two or more wing rings whose central axes are not parallel to each other, the wing ring helicopter actually becomes an axis intersecting multi-wing ring mechanism, that is, the axial forming of the wing ring rotor Angle, the combination of this angled wing ring rotor brings two effects:

(1) By changing the axial direction of one of the wing ring mechanisms, the aircraft as a whole can achieve turning or lateral translation without relying on the rudder or the like;

(2) Increasing the wind resistance of the helicopter and increasing the flight stability. The principle is similar to the ability of some wheelchairs to intentionally form the angle between the left and right axles and increase the rollover resistance of the wheelchair.

The wing-ring helicopter can also be fitted with an auxiliary engine (eg, an engine above the "Flap Ring Aircraft Embodiment 7" cabin) in the portion of the cabin or wing ring that does not rotate with the wing ring. The auxiliary engine is mainly used for braking, turning and increasing the horizontal speed or ascending and descending speed.

Preferably, the auxiliary engine and the cabin or wing ring mechanism are connected by a steering mechanism in order to allow the engine's air vent to be flexibly turned as needed.

The auxiliary engine should generally choose a jet engine. However, if the agility and speed of steering, braking, etc. are not high, the auxiliary engine can also use the propeller engine. The number of auxiliary engines can be determined according to the principle of practicality and saving. However, it is generally best to have four, one for each of the front and rear, and a cross shape, each responsible for the power in one direction, because it can move forward, backward, brake, and agilely. Brake, turn, sharp turn and even turn at right angles. Just put the steering mechanisms on these jet engines and use them to increase the speed of ascending, descending, advancing, retreating, and turning. The air vents are upwards or upwards to accelerate the descent; the air vents are facing downwards or downwards to accelerate the rise; one, two, three or even four blast ports are oriented in the same direction or on the same side to increase forward and backward , the speed of ascending, descending, or increasing the agility of braking, braking, turning, sharp turns, such as: when one jet vents in the opposite direction of the original forward direction, while the other jet is oriented perpendicular to the original direction. Jet, you can make a right angle turn.

The wing-wing helicopter technology can be used to design and manufacture an internal wing helicopter, that is, the wing ring mechanism is placed in the ring of the annular nacelle, and no wing ring mechanism is provided on the periphery. For advance and retreat and turn, four jet engines can be placed equidistantly outside the cabin.

The beneficial effects of the wing ring aircraft:

First, the take-off weight is huge (the minimum wing mechanism of each radius of 50 meters is at least 51,200 tons, the analysis is detailed in the "beneficial effect of the wing ring mechanism").

Second, in the simplest way to properly solve the problem that the ramjet engine can not start at zero speed and low efficiency under low speed (only use the wing ring with fuel tank), so it can develop super large high-speed aircraft, space shuttle and even empty at low cost. Sky plane.

Third, even a fixed-wing wing-wing aircraft can also take off and land vertically and hover instead of flying only.

4. Wing-ring aircraft can be used as a super-large passenger aircraft and transport aircraft. It can be used as a super-large military bomber and can be used as a super-large space shuttle.

5. The wing-ring helicopter can complete the difficult movements that all airplanes can't complete, such as braking, sudden braking, sharp turn, right-angle cornering and forward reversing, with the help of the auxiliary engine. Existing helicopters can't do this because the load is too small to install an auxiliary engine, and the installation can only be placed because there is no more fuel.

Sixth, due to the absence of fins on the outside of the fuselage, not afraid of scratches and collisions, the built-in wing-ring helicopter is particularly suitable for rescue and rescue.

Seventh, the space shuttle that can integrate the ramjet engine and the fuselage can be developed.

Eight, can develop a plane capable of diving, equipped with a remotely controlled driving device.

Wing ring pull-and-fly mechanism technical solution:

Select one or more of the wing ring mechanism, the wing ring wind power mechanism, the high-altitude wing ring wind power mechanism or the wing ring aircraft to obtain the lifting force even if there is no power; the two or two sets of floating mechanism Placed in two streams of opposite flow or water, either connected by a cable or connected by a connecting rod or bracket (this group refers to a group of floating mechanisms that are placed in the same wind or water stream) One or more of the lifting mechanisms are connected to each other; any point on the cable, connecting rod or bracket connecting the two parts of the lifting mechanism or setting the pod, or no pod.

The pod is either suspended below the cable or connecting rod or bracket, or directly connected to the cable or connecting rod or bracket; the pod is either below or between two or two sets of lifting mechanisms, or between Up and down two or two sets of wing rings for vertical take-off and landing aircraft, pods and cables or connecting rods, the total weight of the brackets and the buoyancy of the two or two sets of wing rings for vertical take-off and landing must be balanced so that the two can remain appropriate Height, not excessively floating or sinking away from the two pairs of airflow or water flow equalization pull force; when considering the tension of the two floating mechanisms, must consider the wind or water flow force of the pod, and this force In the pulling force of the floating mechanism that is in the same direction as the force, the opposite pulling forces in the two directions are equal.

If the wing ring mechanism must provide both lift, then the pod should be set up. If there is no pod, the wing ring mechanism should be connected with the cage bracket. The purpose is to make the center axis of the wing ring mechanism tilt down to ensure The rotating surface of the wing ring is inclined to the wind, and the rotating surface is inclined to the wind to generate two components, one is the upwind traction and the other is the upward lift (as shown in Figure 70).

If the wing ring mechanism does not need to provide lift, such as the wing ring vertical takeoff and landing aircraft or the wing wing mechanism with fixed wings as the lifting mechanism, then you can directly connect two (or two groups) of floating up with cables or connecting rods. The mechanism can make the wing ring mechanism face the wind and exert the maximum power generation effect.

Based on the above scheme, the following measures can be taken: setting the motion mechanism. There are two kinds of sports mechanisms, one is a mechanism that can make the whole mechanism horizontally move, and the other is a mechanism that can adjust the altitude of the whole mechanism or one of the (group) floating mechanisms. The moving mechanism may be a baffle, a curtain, a rudder or an auxiliary kite, which may be a propeller engine, a wing ring engine, a steam jet engine, a compressed air engine or an ionized jet engine, and may be a wing of a wind turbine or a rotor that is controlled by a deflection mechanism. The piece can also be any other mechanism that can cause the overall mechanism to be displaced horizontally. The moving mechanism may be disposed on the floating mechanism, or may be disposed on the cable, the connecting rod or the bracket, and may be disposed at only one point or separately at multiple points.

The wing ring-to-pull suspension mechanism utilizes a rudder to achieve cross wind travel. The two levitation mechanisms in the opposite wind direction or water layer are equipped with rudders or auxiliary kites. When the two rudders or the zither body are simultaneously deflected to the same side, the wind or water flow will generate and match the entire mechanism. The vertical dynamic force of the pulling force (as shown in Figure 75). Here, the rudder is used as a representative for the convenience of expression. In fact, not only the rudder board can have this effect, but also the baffle, the curtain and the auxiliary kite can be operated in the same way and have the same effect.

The wing ring-to-pull flying mechanism utilizes a baffle, a curtain, a kite, etc. to achieve a free-flight cruise in the downwind or upwind direction and the latitude direction. If baffles, curtains, kites, etc. are used as the moving mechanism, by changing their windward, water-covering area and windward and water-facing angles, the balance of the two reverse flows can be broken. The whole will move to the larger one. For example, both sides are equipped with unloading kites. If both sides are in the unloading state, or both sides are in the nanoflow state, the two sides are balanced, when one side unloads, one side In the middle of the flow, the whole organization will move to the Naliu side. The so-called windward and water-facing angle refers to the angle formed by the windward or water-facing surface and the direction of the wind or water flow. The closer the angle is to 90° (that is, the more the baffle and the surface of the curtain are perpendicular to the flow of wind or water), The greater the force you receive. Since the reverse wind group is roughly aligned with the latitude, it is possible to achieve free global cruising in the direction of the latitude.

The wing ring-to-pull suspension mechanism utilizes its own wind power and combines with the electric engine to achieve cross wind travel. The wing ring has a huge bearing capacity for the pull-and-fly mechanism, so it can be installed with various large engines and generators. After the large-wing air ring is equipped with a power generation mechanism, the maximum power generation capacity can exceed 10 Three Gorges projects. See “The beneficial effects of the wing ring on the power generation mechanism” in this article. It is therefore possible to directly drive propeller engines, wing ring engines, ionized injection engines, compressed air engines and steam injection engines or steam piston engines with electric energy (steam injection engines, which use electric boilers to heat water into steam and steam from engine nozzles). However, the reaction force of the ejected steam pushes the mechanism to move; the compressed air injection engine relies on the air compressor to compress the air and then ejects strongly from the nozzle to obtain a reaction force), and can also be obtained by electrically driving the high-altitude water extractor. Sufficient water meets the needs of the steam engine and the operation of the aircraft, maintenance personnel or passengers.

The wing-to-pull suspension mechanism can achieve free navigation around the warp direction across the wind belt. If you do not set the power engine wing ring to pull the flying mechanism, any one (group) floating mechanism can not leave the original wind layer in the course of cruising, otherwise an accident will occur, but for some special purposes, If cruising with a windward belt (such as entering a mid-latitude westerly wind belt than a low-latitude trade wind belt), it is necessary to let the two (group) floating lifting mechanisms leave the original wind layer and enter the adjacent wind belt. In the process of getting out of the reverse wind layer of the original wind belt and not entering the reverse wind layer of another wind belt, the engine must be started, and the wing ring pull-up suspension mechanism can not only assemble the engine, but also save enough. Electrical energy (for reasons seen in the previous paragraph) completely spans the needs of the wind layer.

The wing ring can take off and land at random. A vertically-winged-wing aircraft equipped with an internal combustion engine or a jet engine is a floating-wing aircraft (see Figure 56), which is obviously free to take off and land. Even a wing-wing aircraft that is not equipped with a petrochemical engine, as long as it is equipped with a generator and a battery of sufficient capacity, can also rely on its own power to achieve more random take-off and landing as long as it has sufficient high-altitude power generation time. Only the wing ring-to-pull suspension mechanism that does not install any engine at all must be hovered or cruised in the air. This type of machine can only go up and down through the hoist or the landing gear.

Although the shape of the wing-to-pull suspension mechanism is very large, it is completely controllable and safe. As previously analyzed, the high-altitude reverse wind group provides a stable tension for the wing-to-pull suspension mechanism, and the wing-to-pull suspension mechanism not only has various mechanisms for controlling its lifting, hovering or cruising, but also has full capability. Carrying any operator required, the operator can control according to meteorological changes and mission requirements, and of course has the ability to carry any remote control system or automatic control system, so there is no fear of being unmanageable.

Why doesn't the wing ring pull the flying mechanism need to set up a more complicated control mechanism? For other high-altitude stations or high-altitude generators, it should be necessary to set up a more complicated control mechanism, because there is no other aircraft between the wing-wing and the wing-fed suspension mechanism. The quality of 100 tons determines that it is difficult to sway in the impact of forces of thousands of tons and above, and the erratic low-altitude wind will shake the cable or traction cable that weighs several tons or more. Shaking often produces hundreds of tons or even thousands of tons of pulling force, causing the high-altitude mechanism to be severely shaken or even dangerous.

However, the wing ring is different from the flying suspension mechanism, which can have the mass of thousands of tons, tens of thousands of tons or even hundreds of thousands of tons (see the third of the "beneficial effects of the flying wing flying mechanism"). This determines that it must have absolute stability on the premise of ensuring lift. In addition, the wing ring pull-up power generation mechanism does not need the ground traction cable to provide tension at all, so it is not necessary to be forced to use a very large and thus very "tractive" traction cable like other high-altitude mechanisms, only a small traction cable or cable is needed. Such a small cable, the wind it receives will also be greatly reduced. The quality of a small cable is obviously a glimpse of the flying wing suspension mechanism. This "one hair" cable draws energy from the much slower medium and low air, compared to the "elephant". The energy of the pull-wing flying suspension mechanism obtained in the two high-altitude reverse winds with much higher speeds to maintain its steady state is obviously insignificant. Even in the face of extreme conditions, such as encountering a strong typhoon, tornado, etc., it is impossible for a "hair" to shake the "elephant", because even if this "hair" pulls itself off in a strong wind, it is not enough to shake "Elephant". Compared with other high-altitude mechanisms, the wing-to-pulling suspension mechanism has the advantage of being able to cruise. When the weather forecast is too strong, the typhoon and tornado are coming, and it is possible to fly to the safety zone in advance. It can generate electricity in a safe zone and send electricity from the local area to the grid without stopping and avoiding danger.

Therefore, it is sufficient to control the traction cable or cable to sway in the wind without the need to provide a more complicated control mechanism for the wing-to-pull suspension mechanism.

The wing ring is the best high-altitude wind power mechanism. If all the wing ring mechanisms or part of the wing ring mechanism of the wing ring to fly suspension mechanism are set as the wing ring power generation mechanism, or the wing ring wind power mechanism is directly used as the floating mechanism, then the wing ring pull-up suspension mechanism becomes The wing ring pulls the power generation mechanism. The specific method of such setting and the method of connecting the external circuit of the wing ring power generation mechanism are detailed in the "Technical Solution of the Wing Ring Wind Power Mechanism".

Then, the circuits of the individual wing ring wind power mechanisms in the overall mechanism are connected in parallel or in series to a cable leading to the electrical equipment or the power grid, or the circuits of the individual wing ring wind power mechanisms are not connected, or the respective cables are Connect to the electrical equipment or the grid separately.

The wing ring pulls the power generation mechanism, and the small part supplies the wing ring to the various devices on the fly suspension mechanism. Most of them can be transported to the ground power grid by cable or directly towed by large ships and directly to the ship. The drive system is powered. Compared with the ordinary high-altitude power generation mechanism, the wing-ring pull-up power generation mechanism is free from the dependence on the traction cable. This high-hanging cable does not need to undertake the task of pulling the cable, so it is only necessary to use a common cable. The high-altitude wind power mechanism with the kite, rotor or wing ring as the lifting mechanism must be pulled by the traction cable, otherwise it will fall like a broken kite, and the diameter of the traction cable is as small as ten centimeters and as large as nearly one hundred centimeters. Its traction cable consumables and weight are amazing. The wing ring pull-up power generation mechanism can completely omit the traction cable and only retain the cable, which greatly saves materials and reduces the weight of the body, thereby improving economic performance and enabling more and larger generators to be installed on the mechanism, and increasing the power generation capacity of the mechanism. . Omit the traction cable, so that the high-altitude floating power generation mechanism is no longer afraid of storms and typhoons, tornadoes, and forced to land and shelter from the wind will be basically eliminated.

In the future, the technology of directly transmitting electric energy by microwave or laser can be used, and the electric energy can be directly transmitted to the factory building, building, car, ship, aircraft or other electric facilities by microwave or laser. At present, microwave transmission technology has been conducting practical operation tests, and in the near future, it will certainly be able to play a significant role in the power transmission of the wing ring to the power generation mechanism.

Even under current technical conditions, it is also conceivable to convert electricity into laser or microwave, spot-illuminate, heat the boiler on the ground, use the steam of the boiler to drive the generator to generate electricity, or track the boilers and trains that use the steam engine directly. Power these vehicles. Although this type of conversion has a large energy loss under the current technical conditions, considering the shape and power generation of the wing-ring type wind-powered mechanism is extremely large, it can generate electricity for a long time and with constant wind and wind direction without interruption. Petrochemical energy, so even if the loss in the transmission process is mostly, it is still very practical and economical. If the advantage of the wing ring on the traction motor and the laser power transmission method is utilized, the development of the electric boiler to provide high pressure steam is the driving force. Ships and trains will then reduce the amount of energy lost.

Is there a wind group with a reverse advection in the sky?

Have! The three-circle circulation diagram of the Earth's atmosphere shows that the low-latitude trade wind belt, the mid-latitude west wind belt and the polar easterly belt in the north and south hemispheres have upper and lower wind layers, and the wind directions of the upper and lower wind layers are opposite. Up and down reverse wind group. The stratosphere above the troposphere, the west wind that prevails at the bottom, and the stratosphere east wind above the stratosphere, this is another up-and-down reverse wind group.

The high-altitude reverse wind group resources are a huge treasure house for God to give to human beings. They are widely distributed and inexhaustible, and in terms of large-scale development, their difficulty and cost are lower than other energy sources (including oil). , coal and nuclear power, hydropower, solar power), because high-altitude wind power has neither the cost of drilling, excavation and transportation, nor the danger of collapse, water, poison and explosion, and no nuclear leakage, the collapse of the reservoir The disaster is a clean energy once and for all! The stratosphere and the troposphere have the characteristics of endless year-round and stable wind, especially the stratosphere, which is not only extremely windy, but also has no rain, snow, lightning, or even dust. The most ideal wind farm.

And the high-altitude reverse wind group resources provide the necessary conditions for humans to develop non-orbital, non-traction cables and pure wind energy aircraft without petrochemical energy consumption.

So, can the high-altitude reverse wind group hold up a large wing-to-pull suspension mechanism?

can! First, the stratospheric winds reach 55 m / s (about 200 km / h), equivalent to 16 strong typhoons, enough to overturn the car or throw adults into the air. Under the stratosphere, although the height is lower, the wind speed is slower. According to the data released by the Hong Kong Observatory's computer forecast weather map on January 31, 2012, the wind speed in most parts of China is 200 kPa (about 12,000 meters). In km/h, most of the area of 500 hectopascals (about 5,600 meters in height) has a wind speed of more than 72 km/h, and even 850 hectopascals (about 1,500 m in height) has a wind speed of 18 km/h or more. The speed is enough to support the take-off and cruising of the old-fashioned fixed-wing aircraft (the speed of the first real flight of the first human aircraft invented by the Wright brothers is only about 15 km/h). The wing ring can actually be regarded as a closed loop surrounded by a number of fixed-wing aircraft. Therefore, as long as the medium-low altitude wind of 1500 meters or more is enough to maintain the normal hovering of the pure wind wing aircraft. Or cruising.

The wing-to-pull suspension mechanism can also be placed in "two streams of opposite flow or water flow", that is,

In the vast ocean, there is also a living space for the wing-and-loop suspension mechanism. Because there are adjacent and reverse ocean currents and currents on the ocean. The most widely known is the Turkish Strait between the Black Sea and the Mediterranean Sea (composed of three parts: the Bosphorus, the Marmara Sea and the Dardanelles). This upper and lower layers also exist in other parts of the world. Reverse advection of the water layer, such as the South China Sea, "The Nansha Islands sea area has three main characteristics: the upper circulation of the Nansha River has a closed structure and a self-contained system; the lower circulation and the lower circulation of the central South China Sea form a closed circulation; the upper circulation and the lower circulation total It is the opposite direction." (Excerpted from the representative research results of the South China Sea Institute of Chinese Academy of Sciences, "Characteristics and Evolution Mechanism of the Main Dynamic Process of the South China Sea Circulation System"); and, for example, the famous Qiantang tide in China, in fact, it is also caused by two upper and lower countercurrents. The upper layer is caused by the water layer, the upper layer is the river that flows to the sea, and the lower layer is the rising tide.

The wind and water flow can also form a reverse flow group, that is, one of them is a gas flow and the other is a water flow. The wing ring-to-pulling suspension mechanism can be used as a tugboat in the reverse flow group, and can also be used as a pull-up power generation. mechanism. In addition, the wing-to-pull suspension mechanism can rely on two reverse winds to form a pull-up, or two pairs of reverse-flowing water to form a pull-up, and can also rely on a wind and a stream of water in opposite directions to form a pull-up.

The take-off method of the wing ring to pull the flying mechanism:

For wing trains that do not have power, they should be set as wing ring power generation mechanisms. When they are ready, they will be powered by cables to the wing ring power generation mechanism, and one of them will take off first, and the other will pull off the appropriate height. Take off, fly to the set height and cut off the power. As for the cable, you can take it off and leave it.

For a powered wing-wing aircraft, it can take off directly, one of which takes off first, the other takes off after pulling the appropriate height, and then flies to the set height to control the two aircraft to be horizontal, and the two machines The head is facing the opposite. Since the fixed wing of the aircraft begins to generate lift after it becomes a horizontal attitude, the overall mechanism will form a balanced pull-up state under the action of the reverse advection wind. At this point, the engine can be shut down and the reverse wind group can be relied on as the energy for hovering or cruising. .

How can we make the wing ring pull the suspension mechanism safely?

First of all, it is said that in the case of general maintenance and repair, the agency does not have to land, helicopters can be used to carry people, materials and equipment, or the hoist can be used to pull up the pods carrying people, materials and equipment through cables. If overhaul is required, there are two ways to return to the ground: one is to pull the rope back to the ground, the other is to slow down the speed of the wing ring and reduce the lift, so that the body mechanism is lowered (method one is to give the wing ring mechanism rail car) To set the brake device, it is necessary to take braking measures to slow down the speed of the wing ring when descending, and the second method is to slow down the speed of the wing ring by changing the angle of attack of the airfoil). For each of the floating mechanisms having the engine wing-to-pull suspension mechanism, the engine can be started to return to the landing.

Why does the reverse wind group enable the wing ring to fly over the suspension mechanism naturally at high altitude?

First let's see why a kite can be suspended at high altitude without falling in the wind, because it is in a large enough wind, and it has a relative motion with the wind. So why does it have a relative movement with the wind? Because it is pulled by a force opposite to the wind, this force is a horizontal component of the kite's traction line.

One of the two floating mechanisms of the wing-fed suspension mechanism is equivalent to a kite, and the two "kites" are opposite in the wind direction, and each of them receives the opposite direction of the wind, so the two can be pulled The cables are connected together to convert the respective winds to the horizontal pull required by the other party. This is the root reason why the wing ring to pull the flying suspension mechanism can abandon the ground traction cable!

For more detailed suspension and cruising principles of the wing-to-pull suspension mechanism, please refer to the section “Spiral Principles of Pulling Aircraft” in the “Technical Solution for Energy Development and Utilization of Reverse Flow Groups” (also can be seen visually). 71, Figure 72, Figure 73, Figure 74).

Since the invention can completely abandon the ground traction cable, autonomously move in any direction at any time, and can generate electricity as usual during the movement, the electric energy generated at that time can also be completely used as the kinetic energy during the cruising process.

Maintenance method of the wing ring to pull the flying mechanism:

The first method is to set up the lift cabin, and the lift cabin is to be lifted along the ground traction cable; the second method is to install brake devices for each railcar at the beginning of the construction of the mechanism. At that time, only the brakes can reduce the rotation speed of the wing ring to slowly descend; , pull back to the ground with a traction cable.

The beneficial effects of the wing ring on the flying suspension mechanism:

First, the wind vehicle will actually abandon the ground traction cable for the first time;

Second, enabling humans to truly achieve self-sufficient, non-orbital, non-inflatable, groundless traction cables for the first time;

Second, the maximum takeoff weight can reach hundreds of thousands of tons.

The front has been analyzed in the "the beneficial effects of the wing ring mechanism": a wing ring, if the radius is 500 meters, the wing of the 80 Payan-225 transport aircraft is the wing, then the maximum takeoff weight is 51,200 tons; Even if there is only two sets of wing ring mechanisms in a wing-to-pull suspension mechanism, and there are only two double-wing ring mechanisms in each group (that is, the wing ring has a total of 8 such wing rings), then the maximum take-off The weight is:

8 × 51,200 tons / piece = 409,600 tons.

The 409,600 tons is not the limit of the take-off weight of the wing-to-air suspension mechanism. The more the number of wing rings of a wing-to-pull suspension mechanism, the larger the wing area or the larger the radius of the wing ring, the more the take-off weight will be. Big.

3. Ships that achieve self-sufficient cruising in certain sea areas (can be used as barges to professionally towed ships in these areas).

Fourth, create a man-made small sun (see Example 11 of the "wing ring-to-pull suspension mechanism").

5. As a wing-to-pull power generation mechanism, its power generation is large, investment is smaller, and construction period is shorter.

In this paper, the detailed analysis of "the beneficial effects of high-altitude wing-ring wind power mechanism" shows that if a high-altitude wing-ring wind power mechanism has two wing rings and each wing ring has a radius of 500 meters, its maximum take-off weight can exceed 10 Ten thousand tons, its installed capacity can reach 60 million kilowatts. If four such high-altitude wing-ring wind power mechanisms are divided into two groups to form a wing-ring pull-up power generation mechanism, the installed capacity of the wing-ring power generation mechanism can reach 4 × 60 million kilowatts / unit = 240 million kilowatt.

6. Even if it is only used as a wing-to-pull power generation mechanism, it does not need a large traction cable at all, and only needs to keep one ordinary cable; after the microwave transmission electric technology or laser transmission electric technology is mature, the cable can be completely discarded, and it becomes completely cable-free. High-altitude wind power institutions.

VII. Even if it is only used as a wing-to-pull power generation mechanism, it does not need to set up a complicated control mechanism like some high-altitude power generation mechanisms, thus greatly simplifying the structure and reducing the cost.

8. Unless it needs major repairs, it can continue to work. It will be responsible for transportation tasks throughout the year and will continue to generate electricity for many years. Even if it encounters strong typhoons and tornadoes, it can sail to a safe area to generate electricity and send electricity through the local power grid.

Nine, you can freely cruise freely in any direction, and the power of free cruising can be exerted by the upper and lower reverse winds on the transverse movement mechanism such as the fuselage and rudder, thus generating the combined force of lateral and longitudinal movement, and also driving electric Or fuel or fuel jet or steam, jet engines move quickly.

10. Compared with the communication satellite, the invention has low construction cost, and the invention is used for communication, and has short signal round-trip delay (such as completely eliminating the dialogue delay phenomenon between the two hosts in the television picture), and less free space attenuation. It is beneficial to realize miniaturization, wideband and symmetric duplex wireless access of communication terminals; compared with terrestrial cellular systems, the high altitude station has a short working distance, a large coverage area, and small channel attenuation, so the transmission power can be significantly reduced. . Not only does it greatly reduce the cost of building a ground information infrastructure, but it also reduces the radiation pollution around the base station.

11. As a wing-to-pull power generation mechanism, the bases, outposts and oil wells in the mountains, deserts and desert islands will be supplied with sufficient fresh water and materials, so that the development and construction of extremely harsh natural conditions will greatly reduce the difficulty and cost.

12. The high-altitude wing-ring power generation mechanism that is large in shape is not only suitable for combination with large ships to form wind-driven ships, but also for vehicles and aircraft that are combined with medium-sized ships or large vehicles and aircraft to be driven by wind power. The heavy machinery is combined into a crane transporter.

In the technical solution, since the winds of the two (group) wing-wing flying mechanisms are balanced by each other, the lift of the mechanism and the gravity of the mechanism cancel each other and balance, so the high-altitude wind power mechanism towed by the ship, the vehicle or the aircraft is The shape is huge, but it is actually the same as pulling a hydrogen balloon floating in still air. Moreover, because the area or angle of attack of the windward surface of the floating mechanism can change the overall movement of the wing ring to the flying mechanism, the ship does not need to use any power to pull the "hydrogen ball". On the contrary, it can also pass the "hydrogen ball." "Using high-altitude powerful wind traction ships to move fast! Therefore, it is only necessary to remotely control the wind receiving area and the angle of attack of the high-altitude mechanism, so that the small-tonnage ship, vehicle or aircraft can “pull” the giant pull-up suspension mechanism or the pull-up generator, or let the giant pair fly over the suspension. Institutions or pull-up generators are propelling small-tonnage ships, vehicles or aircraft in full accordance with human will.

XIII. Create a reverse parallel flow water-drawing power generation mechanism with stable operation and huge power generation.

Crane transporter technical solution:

The wing ring pulls the power generating mechanism to connect the upper end of the cable, and the lower end of the cable is connected to the take-up device.

The lifting equipment generally comprises four working bodies, such as a lifting mechanism, an operating mechanism, a variable spoke mechanism and a rotating mechanism. The hoisting mechanism is used for vertically lifting materials, the running mechanism is used for horizontally moving materials, the variable spoke mechanism changes the working range by changing the length and elevation angle of the boom, and the rotating mechanism makes the boom rotate about the vertical axis of the crane. The lifting mechanism of the crane is connected with the taking device, and the picking device is a device for lifting materials by lifting, loading, sucking, clamping, supporting or other means (such as a hook, a gripping robot, Electromagnetic suction head, etc.). The wing-ring helicopter or wing-ring power generation mechanism has the functions of the running mechanism, the variable-spoke mechanism and the rotating mechanism, and also has the lifting function of the helicopter structure. Therefore, the lifting device has the complete lifting function as long as the loading device is installed. .

Although wing-wing aircraft and wing-ring helicopters have the advantages of quick climb and horizontal movement and accurate material grabbing on site, the lifting weight can exceed 10,000 tons, but it must consume a lot of oil; while the wing ring pull-up power generation mechanism is completely Self-sufficient energy, and can provide sufficient power for lifting work, and the lifting weight is much larger than that of the wing-ring helicopter, but its climbing and horizontal movement are inflexible, and it is impossible to accurately capture smaller objects. Therefore, it is necessary to The combination of advantages (see "Second Crane Transporter Example 2").

The beneficial effects of the crane transporter:

First, energy self-sufficiency can be achieved without refueling or charging.

Second, the maximum lifting height can reach more than 10,000 meters.

Third, the maximum lifting weight can reach several hundred thousand tons. The project that is impossible to implement, such as the long-distance migration installation or demolition of the giant tower, the long-distance migration installation or demolition of the large bridge, the long-distance migration of the oil rig, and the long-distance migration of large buildings; At present, the operation process is extremely difficult and slow, and the lifting, moving and installation of some overweight and oversized objects becomes a breeze.

Fourth, the lifting and lifting efficiency of giant objects is increased by a hundred times, and it is no longer subject to the obstacles of terrain and distance. It is especially suitable for long-distance or long-distance lifting, barrier-lifting and large-distance lifting, etc., where ordinary cranes cannot work, such as shallow water or berths on the shore, and loading and unloading when the ship cannot be docked, such as vehicles and ships. There are ditches, buildings and forest barriers between the cargo yards, such as lifting large machinery and equipment on the mountains or lifting large ore from the mountains to the mountain yards, as well as the long-distance transportation of ships to return to Hong Kong for repair and wrecking. Long-distance transportation, overall lifting of aerospace equipment, long-distance transportation and installation. In addition, the construction of high-rise buildings can be carried out by means of assembling large-scale prefabricated parts. It is also possible to raise the cement and sand required for the whole or the whole building into the air, and use the water produced by the high-altitude water extractor to stir the mortar and carry out the whole process. Continuous infusion of the seat or the entire layer.

Wing ring wind power boat technical solution:

The upper air mechanism is connected to the upper end of the traction cable, and the ship is connected to the lower end of the traction cable; the high altitude mechanism includes any one or more of a wing ring type spin wing mechanism, a center shaft type spin wing mechanism or a pull type flying suspension mechanism. The so-called "wing-wing rotor mechanism" refers to a wing ring mechanism in which the wing of the wing ring is a lift type wing; the "central-axis type self-rotating wing" refers to a spin wing used in a current spin-wing aircraft, and the wing is a lift type wing. The film, and each of its fins are connected in parallel with the central axis (ie, synchronous motion); and the "pull flying suspension mechanism" refers to the pull-up suspension mechanism in the "technical solution for the development and utilization of reverse flow group energy".

Based on the above scheme, the following preferred settings may be made: a high-altitude power generation mechanism including a high-altitude wing ring wind power mechanism, the lower end of the traction cable is connected to the traction point on the ship, and the cable is electrically connected with the battery or the motor of the ship.

The beneficial effects of the wing ring wind turbine:

1. Using wind or wind power to drive ships, there is almost no environmental pollution;

2. In particular, when the wing-to-pulling suspension mechanism or the wing-wing wind power mechanism is used as a high-altitude traction mechanism or power supply mechanism, regardless of the low-altitude wind direction, the high-altitude reverse wind group can be directly used for navigation in any direction (see The fifth and sixth paragraphs of the "Technical Plan for the Wing Ring Pulling Power Generation Mechanism", or the use of electric power provided by the high-altitude wind power mechanism to drive the motor, thereby achieving a free universal voyage that does not consume petrochemical energy at all.

Reverse flow group energy development and utilization method technical solution:

This is a method of using natural wind energy or advection water to fly, sail or generate electricity. It is characterized by: one or a set of two reverse advection or advection waters in the reverse wind group or the reverse water flow group in nature. a lifting mechanism, and connecting the two or two sets of floating mechanisms to each other by a cable or a connecting rod or a bracket, and using the two opposite directions of the two air currents or the water flow to form the two or two sets of floating mechanisms Pulling the flying suspension mechanism to overcome the falling effect of gravity, achieving the purpose of long-term hovering, cruising, sailing or power generation without the need to configure the engine; the floating lifting mechanism is capable of airflow, water flow or air pressure, water pressure even if it does not have power An object or mechanism that generates lift or buoyancy, and the floating mechanism may include a wing ring mechanism, a wing ring wind power mechanism, a shaft type wind wheel, a shaft type rotor, a shaft type wind wheel generator, and a kite power generating device. Rotor mechanism or power generation unit. ("Technical plan for the wing-to-pull suspension mechanism" is an example of using the "reverse flow group energy development and utilization method")

Based on the above solution, it is further possible to further set the movement mechanism, and by controlling the movement mechanism, the magnitude or direction of the force received by the mechanism is changed, or the movement of the mechanism as a whole in the horizontal direction or the vertical direction is caused. When the vertical plane where the two hoisting mechanisms coexist is not parallel to the direction of wind or water, the two reverse winds will apply a horizontal torque to the two (or two groups of) hoisting mechanisms, which will cause two (or two) Group) The floating mechanism makes an accident around the midpoint of the two, and the harmful torque can be offset at any time by manipulating the motion mechanism. The principle is shown in Fig. 74.

The moving mechanism or everything including the baffle, the curtain, the zither, the umbrella, the sail, the wing, the rudder, the airbag, the sac, etc. can change the wind, the windward facing wind, the water angle or the windward, water-facing area or The engine, or the power engine that includes the propeller engine, the wing ring engine, the compressed air injection engine, the steam injection engine, the ionization injection engine, the fuel injection engine, etc., which can actively apply thrust or tension to the gas or water body, or The flap is coupled to the flap deflecting mechanism and can be varied by a flap deflecting mechanism to change the flap angle or winglet mechanism.

By manipulating the motion mechanism, it is possible to drive the aircraft or the ship to freely lift and cruise in any direction, purely by wind or advection.

The principle of using the tail rudder to achieve cross wind driving can be found in the section "Wings of the wing ring to pull the flying suspension mechanism" in the "wing ring to pull flying suspension mechanism can use the tail rudder to achieve cross wind driving".

The principle of using the baffle, curtain, kite, etc. to achieve downwind or upwind can be found in the "Technical Plan of the Wing Ring Pulling Suspension Mechanism". "The wing ring pulls the flying suspension mechanism to realize the baffle, curtain, kite, etc. Take a section downwind or headwind.

In addition, the cable or connecting rod or bracket of the tensioning mechanism may be provided with or without a cabin, and the cabin may be suspended from a cable or a connecting rod or bracket (ie, a nacelle), which may be attached to a cable or a connecting rod or The bracket can also be built into the cable or connecting rod or bracket, or directly as a cable or a link or a section of the bracket.

The hovering principle of the pull-and-fly mechanism (shown in Figure 71, Figure 72, Figure 73, Figure 74):

Fig. 73 is a schematic diagram showing the principle of the suspension of the flying suspension mechanism without the nacelle (the plane in which the two floating mechanisms are located is parallel to the flow direction of the wind or water).

The gravity 1 and gravity 2 of this icon also share the weight of the cable or connecting rod and the bracket connecting the two floating mechanisms. The pull force 1 of the icon shows the resultant force of gravity 1 and wind 1, and the tension 2 is gravity 2 and The combined force of the wind 2, the wind 1, the wind 2 are the winds respectively received by the two floating mechanisms, wherein:

Lift 1 = Gravity 1, Lift 2 = Gravity 2

Wind 1 = wind 2, pull 1 = pull 2

These forces also form a balanced system, so the entire mechanism can be suspended at high altitude.

Fig. 74 is a schematic diagram showing the principle of the suspension of the flying suspension mechanism (the planes of the two floating mechanisms are not parallel to the flow of wind or water, and the respective forces indicated in the figure are the forces in the horizontal direction).

Wind 1 = wind 2, pull 1 = pull 2,

The component of wind 1 is tension 1 and torque 1, and the component of wind 2 is tension 2 and torque 2;

Obviously, if there is no external force to compete with the torsion 1 and the torsion 2, then the two torsion will push the two floating mechanisms to make a circular motion around their midpoints. Therefore, it is necessary to control the dynamic motion mechanism to give a direction opposite to the torsion. The force of equal force, otherwise the torque will cause the whole body to deflect. This force may be called anti-torsion, so:

Anti-torque force 1 = torque 1 , reverse torque 2 = torque 2

This creates a balanced system in which the entire mechanism remains stable without horizontal drift.

Fig. 71 is a schematic diagram showing the principle of the suspension of the flying suspension mechanism with the nacelle (the plane in which the two floating mechanisms are located is parallel to the flow direction of the wind or water).

The gravity indicated in this figure is not only the weight of the nacelle, but also the weight of the two floating mechanisms and the weight of the cables or connecting rods and brackets connecting them. The icon shows the wind 1, the wind 2 is two rising The winds received by the organization (Note: If the wind speed and wind pressure of the two reverse wind layers are not equal, the wind and wind 2 can be equalized by adjusting the wind receiving area of the floating mechanism or the wing angle of attack), A. B is the two components of gravity, A1 is the resultant force of wind 1 and lift 1, and B2 is the resultant force of wind 2 and lift 2, where:

Gravity = lift 1 + lift 2

Wind 1 = wind 2

A1=A

B2=B

These forces form a balanced system, so the entire mechanism can be suspended at high altitude.

In view of the hovering principle of the flying suspension mechanism, it must be noted in practice that the sum of the weight of the two or two sets of lifting mechanisms and the weight of the nacelle and the cable, the connecting rod or the bracket must be equal to that provided by the lifting mechanism. Buoyancy, in order to maintain the tension flying mechanism at an appropriate height, without excessive floating or sinking and leaving the two airflows or the flow of the equilibrium pull force; in consideration of the tension of the two floating mechanisms, must be considered The force of the wind and water flowing from the nacelle and the traction cable that extends downward, and the force is placed in the pulling force of the same lifting mechanism in the direction of the force, and finally the opposite pulling forces in the two directions are equal. .

However, it should be noted that the self-rotating rotorcraft moving in the horizontal direction is required to obtain upward lift. The necessary condition is that the rotor rotating surface must form an angle with the horizontal plane in the forward direction. Similarly, if the lift of the floating mechanism is only passed or mainly passed When the wing ring rotates, the windward surface of the wing ring must form an angle with the direction of the wind (as shown in Fig. 70), otherwise the wind cannot drive the rotation, and it is impossible to obtain the upward floating force. If the hoisting mechanism is a spin-wing wing mechanism, it is preferable to have an automatic or remote control between the wing ring mechanism and the entire hoisting mechanism or between the hoisting mechanism and the integral pull-up suspension mechanism (the bracket or the connecting rod). The deflecting mechanism is configured to change the angle between the rotating surface of the wing ring and the wind direction when the wind changes, and the change of the angle directly changes the magnitude of the lifting force.

Cruise method for pulling aircraft: Please refer to the principle of "wing ring to pull flying suspension mechanism to realize cross wind driving with tail rudder" and "wing ring pull flying mechanism" in this article "Technical plan for wing ring to pull flying mechanism" The use of baffles, curtains, kites, etc. to achieve the principle of downwind or headwind" two parts.

The reverse wind group or the reverse water flow group is a necessary prerequisite for the establishment of this program.

So, is there such a reverse wind group and a reverse water flow group in the sky? Yes (see "Technical Solutions for Wings and Pulling Mechanisms").

Lightweight airbags, unpowered airships and unpowered kites are the easiest aircraft to manufacture and deploy. They are also the earliest human aircraft. However, such floating mechanisms must have the constraints and traction of the ground traction cable, otherwise they will drift with the wind. I don't know what to do, no engine, they can never sail to the designated position against the wind or the wind, so they should have a bigger role but can't do more. The birth of this program has installed wind energy engines, so that they can hover or sail autonomously from above, making them extremely cheap, easy to operate, and highly practical high-altitude workstations or wind traction mechanisms. As high-altitude stations, they can solve the huge cost, long construction period, high maintenance cost, signal attenuation, dead angle, distortion, and severe electromagnetic radiation inherent in the use of satellites in the fields of communication, detection, etc. or the use of a large number of ground base stations. Such as the wind traction mechanism, they can be easily used to tow various types of ships and vehicles, regardless of the low-altitude wind direction and the same or opposite direction of the vehicle and boat does not affect its strong traction, they are especially suitable for large, The power mechanism of the super-large ship is extremely strong due to the high altitude. Therefore, several basketball court-sized kites are enough to drive the largest tanker at high speed!

The airbag type, airship type or kite type fly-pull suspension mechanism specially designed for the traction of vehicles and ships, the floating mechanism is preferably formed by a combination of an airbag or an airship and a kite, and the pair of flying suspension mechanisms can also be used for a vehicle or a ship. As part of it, the car and the ship are regarded as the pods of the flying suspension mechanism.

The advantage of the airbag, airship or kite-type flying suspension mechanism and the combination of the vehicle and the ship is that the airbag or the airship can be used to stably suspend the mechanism at high altitude, and the kite or the wind umbrella can be used to provide the wind and the wind, "windward" or The powerful traction in the crosswind direction, that is, it can tow the vehicle and the boat in any direction, not just in the downwind direction. The so-called "upwind" traction is actually the traction of the upper layer of reverse wind, and the principle of crosswind traction is: when the rudder on the two parts of the floating mechanism is simultaneously deflected to the same side, the wind in the opposite direction will produce vertical to the whole mechanism. The resultant force in the wind direction (as shown in Figure 76).

The airbag, airship or kite pull-and-pull mechanism is also very easy to apply. First of all, it is not heavy enough to squeeze a lot of load (the weight of such a mechanism is definitely less than the weight of the fuel tank and fuel that must be equipped for the same power), even it can When the ship does not need this pair of flying and flying mechanisms, the ship can be pulled down with a winch and then released when needed.

This kind of floating mechanism consisting of airbags, airships and kites, windsurfers (or water kites, water umbrellas) can only use a double-chained kite or other kite or umbrella that changes the windward area of the kite by manipulating the cable (about " Double-chain kite" See my CN2011101147334 for details. , CN2011203528410), in order to make the flying suspension mechanism have cruising ability. However, the structure based on the ordinary retractable cable machine can obtain the lifting force and can adjust the size of the lifting force so that the flying suspension mechanism can sail in two winds, but cannot use the kinetic energy of the kite or the umbrella. More meaningful work (such as power generation), so the kite and umbrella must be reciprocated so that they can drive the generator or other machinery through the cable. To achieve this goal, it is necessary to use the "reciprocating unloading kite" reasonably. Figure 64, Figure 65, Figure 66 ("Reciprocating unloading kite" is detailed in my CN2011101147334 , CN2011203528410). The use of "reciprocating unloading kites" or other similarly functioning zither mechanisms can not only use high-altitude wind energy to generate electricity or work, but also speed up the movement of the flying suspension mechanism in any direction. One of the reasons is that there is powerful electric energy. It can also drive the engine in any direction, but even if it does not generate electricity at all, it can achieve greater exercise power than the ordinary kite, because it can change the wind received at both ends by forcing the cable controller 7-2 at any time. For example, let the two zither bodies at one end be in the disengaged state. If the two zither bodies at the other end are in the nano-energy state, the fastest movement speed can be obtained, if the other end is a zither. If the body is able to dissipate energy, then the speed will be halved. Preferably, the zither body 9 and the cable control machine 7-2 are provided with a light air chamber, which is more favorable for its normal operation.

The above-mentioned airbags, airships, kites and umbrellas of Fig. 64 and Fig. 66 are actually a kind of pull-and-pull power generating mechanism, which is placed in a high-altitude reverse wind group, which is a high-altitude pull-up power generating mechanism. In the reverse flow group of the ocean, the ocean current is connected to the power generation mechanism.

The use of reverse flow group energy development and utilization methods can also permanently or automatically cruise a fixed-wing aircraft with or without power. The so-called unpowered fixed-wing aircraft here includes various unpowered gliders and full-wing aircraft that appear to have only the fuselage without the fuselage (see Figure 69). Two or two sets of fixed-wing aircraft need to form a pair of flying suspension mechanisms, which must first be connected by cables or connecting rods or brackets. Then, the unpowered fixed-wing aircraft needs to fly from other powered aircraft to a predetermined height. And they form a pull-up, and a powered fixed-wing aircraft can actively fly to a predetermined height and form a pull. When the powered fixed-wing aircraft forms a pull-up force, the engine can be shut down, and the high-altitude strong wind swept over the airfoil to obtain the floating force, thereby enabling high-altitude hovering or cruising missions.

The unpowered fixed-wing aircraft can also be combined with a kite or an umbrella to completely rely on wind cruising or power generation like an unpowered airbag or an airship. Its structure is the same as that of the airbag, airship and kite, and umbrella group described above, except that the airbag or airship is replaced with a fixed-wing aircraft.

The pull-and-fly mechanism consisting of fixed-wing aircraft can also be combined with a kite or umbrella. The combination method is basically the same as the combination method of the airbag, airship and kite and umbrella described above, the only difference being: two-way in the airbag or airship In the kite (umbrella) combination, the airbag or airship can be in a slower moving area where the two opposite directions of wind or water meet, but the fixed-wing aircraft in the two-way drift kite (umbrella) combination of the fixed-wing aircraft cannot In this area, otherwise its wings will not get enough lifting force because the wind belt is too low.

The technology of the pull-and-fly mechanism contributes to the application of the shaft-type spin-wing mechanism in the field of high-altitude power generation. Because the fins of the shaft-type rotor must be connected and linked with the central shaft, it is impossible to push large generators, and it is impossible. Bring large generators to the sky. In addition, it must also bear the weight of the ground traction cable, which must be strong enough to withstand the strong winds of high altitude, so it must be very large, and a thick and long (more than 10,000 meters) traction cable must weigh several tens of tons. Above, this has to further reduce the weight of the generator and further reduce the power generation capacity. The birth of the technology of the flying suspension mechanism can just improve this problem: not only can each group of floating mechanisms have multiple shaft rotors, but also the two sets of spin-wing power generating mechanisms form a pulling force at high altitude. Offset each other, the traction cable becomes dispensable, and after abandoning the traction cable, which may weigh up to 100 tons, a larger generator can be installed in the mechanism, the power generation capacity can be greatly improved, and economic efficiency is likely to be accepted.

The beneficial effects of energy development and utilization methods in the reverse flow group:

First, it has opened up a new form of green energy – reverse wind group energy and reverse water flow group energy, especially reverse wind group energy, which has a wide distribution and density compared with other energy sources including fossil energy. The low development cost, high operational safety, strong environmental affinity, and inexhaustible characteristics are far superior to any other existing energy forms.

2. To make the aircraft in the wind or the ship in the water flow able to resist wind and wind without any traction of the ground traction cable or anchor chain, and without any other type of energy except wind energy or water flow energy. The horizontal thrust of the water flow and the vertical attraction of the Earth.

3. The method can be used to construct a tugboat or lorry boat that does not consume petrochemical energy at all, and is dedicated to water shipping with upper and lower reverse water flow group resources.

Fourth, it can be compared with the high-altitude wing ring wind power mechanism or the wing ring to pull the flying suspension mechanism, which has much more practical value than the ground communication base station and communication satellite, but the cost and operating cost can be greatly reduced, especially the lightweight airbag. The wing-shaped aircraft or kite is the pulling mechanism of the lifting mechanism, and its construction cost and operating cost are unparalleled.

An efficient and environmentally friendly construction method:

Use the high-altitude mechanism with wing-wing mechanism as the high-altitude construction station to achieve the following purposes: either lift the cement and sand into the air (using the water produced by the high-altitude water extractor or the water supplied by the ground) to stir the mortar and infuse in the air. , or lift the stirred mortar into the air for filling, or lift the preform into the air for assembly, or lift the entire relatively small building into the air to assemble a larger building, or steel, brick The stone materials and decoration materials are upgraded to the air for construction, or the entire building is lifted and transported to other places. The high-altitude mechanism in this scheme includes a wing ring mechanism, especially a wing ring mechanism with a spin-wing property, and the best selection object is: a wing ring-to-pull suspension mechanism, a wing-ring pull-up wind mechanism, and a crane-type wing ring. Transport aircraft, high-altitude wing wind turbines or wing-wing aircraft.

The benefits of an efficient, environmentally friendly construction method:

1. The construction and electricity consumption of the entire construction site is completely self-sufficient, so that the long-distance transportation and all construction including materials can not consume petrochemical energy at all;

Second, the whole or the entire layer can be continuously infused;

Third, the project construction can be assembled with large prefabricated parts of more than 100,000 tons;

4. It is possible to raise all the decoration materials of the whole layer or several layers at one time, and the preliminary processing of the decoration materials can be carried out on the high-altitude construction station;

5. Significantly save construction time, greatly reduce the occupation area of the construction site, greatly reduce the interference of construction noise to residents, greatly reduce the pollution of waste to roads, streets and communities (the inevitable splashing of vehicles during transportation), and greatly reduce the stage of clearing. The flying of dust and dust (the whole layer of garbage is directly sucked into the garbage compartment of the high-altitude construction station), and fundamentally avoids the interference and destruction of urban transportation and urban life during the material transportation process.

DRAWINGS

1 is a schematic structural view of a first embodiment of a wing ring of the present invention, wherein the fins all extend outward of the annular bracket;

2 is a schematic structural view of a second embodiment of the wing ring of the present invention, wherein the fins all extend toward the inner side of the annular bracket;

3 is a schematic structural view of a third embodiment of the wing ring of the present invention, wherein the fin portion protrudes outward from the circumference of the annular bracket, partially protrudes to the inner side of the circumference of the annular bracket, and the inner and outer wings of the annular bracket The number of pieces is equal;

4 is a schematic structural view of a fourth embodiment of the wing ring of the present invention, wherein the wing portion protrudes outward from the circumference of the annular bracket, and a partial view of the wing ring projecting toward the inner side of the circumference of the annular bracket is annular. The number of fins on the inner and outer sides of the bracket is not equal;

Figure 5 is a schematic view of a single rail rail coupling body (the track cross section is T type);

6 and FIG. 7 are schematic diagrams of a dual-track type vehicle-rail coupling body according to an embodiment of the present invention, wherein the track cross-section is T-shaped;

FIG. 8 is a schematic diagram of a monorail type vehicle rail coupling body according to an embodiment of the present invention, wherein the rail cross section is a slot type;

9 and FIG. 10 are schematic diagrams of another dual-track vehicle rail coupling body according to an embodiment of the present invention, wherein the rail cross section is a slot type;

Figure 11 is a schematic structural view of a first embodiment of a wing ring mechanism of the present invention;

Figure 12 is a schematic structural view of a second embodiment of the wing ring mechanism of the present invention;

Figure 13 is a schematic structural view of a third embodiment of the wing ring mechanism of the present invention;

Figure 14 is a cross-sectional view of the wing ring mechanism shown in Figure 13;

Figure 15 is a schematic structural view of a fourth embodiment of the wing ring mechanism of the present invention;

Figure 16 is a cross-sectional view of the wing ring mechanism shown in Figure 15;

Figure 17 is a schematic structural view of a fifth embodiment of the wing ring mechanism of the present invention;

45 and FIG. 46 are schematic structural views of a fifth embodiment of a wing ring mechanism according to the present invention;

41-44 are schematic structural views of a seventh embodiment of a wing ring mechanism of the present invention;

Figure 19 is a schematic structural view of an eighth embodiment of a wing ring mechanism of the present invention;

20 is a schematic structural view of a ninth embodiment of a wing ring mechanism of the present invention;

Figure 18 is a schematic structural view of a tenth embodiment of a wing ring mechanism of the present invention;

21 and 22 are schematic structural views of an eleventh embodiment of a wing ring mechanism of the present invention;

23 and FIG. 24 are schematic structural views of a twelfth embodiment of a wing ring mechanism according to the present invention;

25 and FIG. 26 are schematic structural views of a thirteenth embodiment of a wing ring mechanism according to the present invention; and FIGS. 27 and 28 are schematic structural views of a fourteenth embodiment of the wing ring mechanism of the present invention;

29 is a schematic structural view of a first embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

Figure 30 is a schematic structural view of a second embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

Figure 31 is a schematic structural view of a third embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

32 is a schematic structural view of a fourth embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

33 is a schematic structural view of a fifth embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

Figure 34 is a schematic structural view of a sixth embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

35 is a schematic structural view of a seventh embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

36 is a schematic structural view of an eighth embodiment of a high-altitude wing ring wind power mechanism according to the present invention;

37 is a schematic structural view of a second embodiment of a high-altitude water dispenser according to the present invention;

Figure 38 is a schematic structural view of a third embodiment of a high-altitude water dispenser according to the present invention;

39 and FIG. 40 are schematic structural views of a first embodiment of a wing ring aircraft according to the present invention;

41 and FIG. 42 are schematic structural views of a third embodiment of a wing ring aircraft according to the present invention;

43 and FIG. 44 are schematic structural views of a fourth embodiment of a wing ring aircraft according to the present invention;

45 and FIG. 46 are schematic structural views of a fifth embodiment of a wing ring aircraft according to the present invention;

47 and FIG. 48 are schematic structural views of an eighth embodiment of a wing ring aircraft according to the present invention;

49 and FIG. 50 are schematic structural views of a ninth embodiment of a wing ring aircraft according to the present invention;

51 and 52 are schematic structural views of a tenth embodiment of a wing ring aircraft according to the present invention;

53 is a schematic structural view of a first embodiment of a wing ring pull-up suspension mechanism according to the present invention;

Figure 54 is a schematic structural view of a second embodiment of a wing ring pull-up suspension mechanism according to the present invention;

Figure 55 is a schematic structural view of a third embodiment of a wing ring pull-up suspension mechanism according to the present invention;

Figure 56 is a schematic structural view of a fifth embodiment of a wing ring pull-up suspension mechanism according to the present invention;

57 is a schematic structural view of a sixth embodiment of a wing ring pull-up suspension mechanism according to the present invention;

Figure 58 is a schematic structural view of a first embodiment of a crane conveyor of the present invention;

Figure 59 is a schematic structural view of a first embodiment of a wing ring wind power ship according to the present invention;

Figure 60 is a schematic structural view of a second embodiment of a wing ring wind power ship according to the present invention;

Figure 61 is a schematic structural view of a third embodiment of a wing ring wind power ship according to the present invention;

63 and FIG. 64 are schematic diagrams showing the application of the first embodiment of the reverse flow group energy development and utilization method of the present invention:

FIG. 65 is a schematic diagram of the application of the fourth embodiment of the method for developing and utilizing the reverse flow group energy according to the present invention:

66 is a schematic diagram of application of a fifth embodiment of a method for developing and utilizing a reverse flow group energy according to the present invention;

67 is a schematic diagram of application of a sixth embodiment of a method for developing and utilizing a reverse flow group energy according to the present invention;

68 is a schematic diagram of application of a seventh embodiment of a method for developing and utilizing a reverse flow group energy according to the present invention;

69 is a schematic diagram of application of an eighth embodiment of a method for developing and utilizing a reverse flow group energy according to the present invention;

Figure 70 is a schematic view showing the angle between the windward side of the wing ring and the direction of the incoming wind according to an embodiment of the present invention;

71 is a schematic view showing the principle of hovering suspension mechanism with a nacelle according to an embodiment of the present invention, wherein a vertical plane in which the two floating structures are co-located is parallel to the flow direction of the wind or water;

Figure 72 is a schematic view showing the principle of the suspension suspension mechanism without the pod in the embodiment of the present invention, wherein the vertical plane where the two floating mechanisms coexist is parallel to the flow direction of the wind or water; and the flying suspension mechanism without the pod Schematic diagram of the hovering principle in the up and down reverse wind group;

Figure 73 is a schematic view showing the principle of the suspension suspension mechanism of the embodiment of the present invention, wherein the vertical planes of the two floating mechanisms are not parallel to the flow direction of the wind or water, and the respective forces indicated in the figure are horizontal. force;

Fig. 74 is a schematic view showing the use of a tail rudder to make a cross-winding mechanism (perpendicular to the wind direction) using a tail rudder according to an embodiment of the present invention.

detailed description

The embodiments described below are preferred embodiments of the present invention, and are only used to assist the reader in understanding and implementing the invention, and are not intended to limit the scope of the invention, which is equivalent to the contents of the specification and the drawings. Structural or equivalent process transformations, or direct or indirect use in other related technical fields, are included within the scope of the patent protection of the present invention.

Example of a wing ring:

Embodiment 1 (shown in FIG. 1): The fins all protrude toward the outside of the annular bracket.

Embodiment 2 (shown in FIG. 2): The fins all protrude toward the inner side of the annular bracket.

Embodiment 3 (shown in FIG. 3): the fins protrude toward the inner and outer sides of the annular bracket, and the number of fins on both sides is equal.

Embodiment 4 (shown in FIG. 4): the fins protrude toward the inner and outer sides of the annular bracket, and the number of fins on both sides is not equal.

Embodiment 5: The wing ring in any of the above embodiments is selected, and all of the fins are lift-type fins.

Embodiment 6: The wing ring of any of the above embodiments is selected, and all of the fins are non-lifting fins.

Embodiment 7: The wing ring of any one of the third or fourth embodiment is selected, wherein the inner and outer fins of the annular bracket have a lifting type wing on one side and a non-lift side on the other side. Type wing.

Embodiment 8: On the basis of any one of Embodiments 1 to 7, all the fins are directly connected with the annular bracket, so that the angle of attack of all the fins is fixed.

Embodiment 9: On the basis of any one of Embodiments 1 to 7, the fin is connected to the blade deflecting mechanism, and the blade deflecting mechanism is coupled to the annular bracket, so that the angle of attack of the flap can be changed.

Example 10:

On the basis of any of the above embodiments, a small wing perpendicular to the direction in which the airfoil extends is mounted at the end of the airfoil (like a pointed small wing on a modern high-speed jet wing with its tip pointing towards the wing) Forward direction).

Example 11:

On the basis of any of the above embodiments, the fins are selected as bendable fins. These bendable fins or the whole are elastic, or only partially elastic, so that they can bend under excessive wind force and can restore the original shape after the wind is weakened; the curvature of the flap can be The setting takes place in the radial direction, and can also be set to occur in the whole, or it can be set on one side or both sides of the airfoil; if the bending of the airfoil is set in the radial direction, it can occur either in the whole segment or only in the distal end. The segment is bent.

Example of a wing ring with a fuel tank:

Embodiment 1:

Providing the fuel tank of the wing ring to the inside or the outside of the annular bracket or the airfoil can enable a synchronous circular motion with the wing ring or other annular wind wheel or annular rotor. The fuel tank may be an additional box-shaped, barrel-shaped or spherical container, and the inner space of the annular bracket is used to form an annular container as large as the annular bracket, and the inner portion of the annular container can be divided into a plurality of compartments ( There are connecting holes between the compartments, or they can be completely hollow without separation.

Embodiment 2:

On the basis of the previous embodiment, a ramjet engine is mounted to the fin or ring bracket. If the ramjet is connected to the airfoil, its central axis should be parallel or substantially parallel to the face of the airfoil (the positional relationship between the two can be modeled by the positional relationship between the existing jet wing and the jet engine, That is, connected to the upper or lower side of the airfoil, or attached to the tip or root of the wing, in order to prevent the airfoil from blocking the airflow of the engine, and the airfoil must be connected to the annular bracket by the wing deflection mechanism; if the ramjet is not It is connected to the airfoil but to the ring bracket, so it must be connected to the ring bracket by a deflection mechanism. The deflection mechanism is used to control the injection port orientation of the ramjet engine: the jet direction is aligned with the tangential direction of the circumference of the wing ring during the zero-speed engine start or the slow flight phase of the aircraft (for propelling the wing ring rotation), and the aircraft enters the high-speed flight phase. The air vent is aligned with the centerline or heading of the fuselage. That is, the ramjet engine is connected to the airfoil, and there may be a wing deflection mechanism between the engine and the airfoil, which is used to finely adjust the orientation of the blasting engine air vent, and can precisely adjust the positional relationship between the air vent and the airfoil. To meet the special requirements of different flight stages.

Embodiment 3:

Based on the previous embodiment, a fuel inlet port similar to that of a vehicle tire is provided to the fuel inlet of the wing ring fuel tank. Correspondingly, the fuel output pipe of the fuselage fuel tank is led to the side of the wing ring fuel tank, and an air outlet structure similar to that of the compressed air gun for inflating the automobile tire is provided to the pipe port. In this way, simply press the output port on the fuel inlet of the wing ring fuel tank, the oil circuit can be turned on, and the oil of the fuselage fuel tank is input into the wing ring fuel tank, and when the two interfaces are separated, two All of them will naturally return to the sealed state.

When the aircraft reaches a high speed and the engine can be punched without rotation, the wing ring stops rotating, and the flap is adjusted to the same direction as the central axis of the fuselage by the flap deflecting mechanism, so that the engine is directly punched toward the front, at this time The brake device or other means fixes the wing ring and docks the oil passage of the wing ring fuel tank with the oil passage of the fuselage fuel tank to refuel the wing ring fuel tank from the fuselage fuel tank.

Embodiment of wing ring mechanism

Embodiment 1 (shown in Figure 11):

The wind wheel of this wing ring windmill is an inner and outer surrounding multi-wing ring mechanism, which comprises an outer wing ring 1-1 and an inner wing ring 1-2, and the inner and outer wing ring mechanisms are connected by a double-track type vehicle rail coupling body (see 6, FIG. 7, FIG. 9 or FIG. 10), the annular brackets of the two wing ring mechanisms are respectively connected to one end of the rail coupling body. In this embodiment, there are four sets of such rail coupling bodies, and the spacing of the four is Equal; the tower of the wind wheel consists of three vertical support rods 11-1, 11-2, 11-3 and four diagonal support rods 11-4, 11-5, 11-6, 11-7. The top end of each support rod is connected with a set of double-track type vehicle rail coupling body, and the connection point is located in the link 3-3 of the rail coupling body (see the rail coupling body of Fig. 6, Fig. 7, Fig. 9, Fig. 10). ).

Such a wing windmill can be used to construct a tower wind turbine generator in a wind-stable stable area.

Embodiment 2 (as shown in Figure 12):

This is a “wind tunnel type wing mechanism” or “pipeline wing ring mechanism”, which is to open a hole in the dam body, wall or curtain wall, and place the wing ring mechanism in it. It is preferable to accommodate the wing ring mechanism, and the length of the hole is preferably not less than the length of the mechanism, so the dam or the wall must have a sufficient thickness. The purpose of setting up this wind tunnel or water hole is to allow airflow (wind) or water flow to flow through only this limited opening, thereby increasing the pressure of the water flow. The portion of the wing ring mechanism that does not rotate with the wing ring is directly connected to the hole wall 10 or connected by a bracket (as shown in FIG. 12, one end of the rail coupling body 3 is directly connected to the hole wall 10, if FIG. 23 to FIG. For the two wing ring mechanisms shown in I3, the rail coupling body 3 is first connected to the cage bracket 27-1, and then the cage bracket 27-1 is connected to the cave wall 10. The fins of the wing ring mechanism are not connected to the wall or the wall of the tube, but should be close to the wall 10 as much as possible.

The wind tunnel wing mechanism can be used to construct a wind tunnel type wing ring wind power mechanism or a wing ring water flow power generation mechanism, and can also be used to construct a water flow generator in a pipeline or a conveying pressure device of various pipes.

Embodiment 3 (as shown in FIG. 13 and FIG. 14):

In this embodiment, it is an "inner-and-outer-enclosed" multi-wing ring mechanism, in which each outer wing ring 1-1 and inner layer wing ring 1-2 are in the same plane and have the same center but different radii, so that a large wing ring is formed. In the pattern of the winglet ring, the two wing ring mechanisms are connected together by the rail coupling body 3 (the partial enlarged view is the detail of the joint of the two wing rings); the flaps of the two wing rings have the opposite angle of attack (ie, the direction of rotation is opposite). And the torques cancel each other out.

Embodiment 4 (as shown in Figure 15-16):

This is a "stacked parallel type" multi-wing ring mechanism. In this embodiment, the wing ring 1-3 and the wing ring 1-4 are not at the same level, and their central axes overlap with the same straight line, between the two wing rings. They are connected together by the rail coupling body 3; the flaps of the two wing rings have opposite angles of attack (ie, opposite directions of rotation), and the torques cancel each other out.

Embodiment 5 (as shown in Figure 17):

This is also a stacked parallel multi-wing ring mechanism. In this embodiment, the three wing rings 1 are respectively at different levels, and their central axes overlap with the same straight line, the upper and middle wing rings and the middle and lower wing rings. All of them are connected to each other through the double-track type rail coupling body 3, so that the three wing ring mechanisms are integrally connected; the flaps of the upper and lower wing rings have the same angle of attack (that is, the rotation direction is the same), and the wing angle of the middle wing ring is equal to the angle of attack. Contrary to the angle of attack of the other two wing rings (ie, the direction of rotation is opposite), the torque in the clockwise direction of the machine and the torque in the counterclockwise direction cancel each other out.

Embodiment 6 (as shown in FIG. 45 and FIG. 46):

This is an "axis intersecting" multi-wing ring mechanism and a wing-wing aircraft. Above each of the four sides of the aircraft fuselage 36, one wing ring steering mechanism 38 is connected, and each of the wing ring steering mechanisms 38 is connected to a wing ring mechanism 32 via a connecting rod 39, and the axis lines of the four wing ring mechanisms are crossed. Form an angle. The wing ring mechanism 32 can be either a single wing ring mechanism or a multi-wing ring mechanism.

This type of axis intersecting multi-wing ring mechanism can be applied to the design of a wing-ring helicopter. As long as there are 3 to 4 wing ring mechanisms intersecting on one helicopter, both lifting and turning can be considered. Although they do not produce vertical lift, the resultant force of several oblique lifts creates a vertical lift. When turning, you need to change the rotation speed or inclination of one or two wing rings, and the aircraft will turn. The advantage of this type of axis intersecting multi-winged ring mechanism aircraft is that the flight stability is higher, and the principle is the same as that of the common anti-rollover wheelchair. The two wheels of the wheelchair have resistance due to the intersection of the axes and the two wheels. Rollover ability.

Embodiment 7 (as shown in Figure 41-44):

The double-winged aircraft in the figure belongs to an "axis parallel type" multi-wing ring mechanism. The central axes of the two wing ring mechanisms 32 form two parallel lines. The flaps of the two wing rings have opposite angles of attack (ie, opposite directions of rotation) and the torques cancel each other out.

Embodiment 8 (as shown in Figure 19):

This is also an inner and outer enclosed multi-wing ring mechanism. Each of the wing rings is in the same plane and has the same center but each has a different radius. The wing ring 1-1-1 and the wing ring 1-1-2 are connected by the rail coupling body 3, and the wing ring 1-2-1 and the wing ring 1-2-2 are also passed through the rail coupling body 3 The wing ring 1-1-2 and the wing ring 1-2-1 are fixedly connected by the airfoil spokes 4-2, so that they are actually the same wing ring that is combined into one, this one is one. The wing ring and the adjacent two wing rings have opposite angles of attack, opposite directions of rotation, and the torques cancel each other out. The fin spokes 4-2 are spokes having a fin function.

Embodiment 9 (shown in Figure 20):

This is a multi-wing ring mechanism that combines the inner and outer enveloping features and the stacked parallel type features (in Fig. 20, the lower drawing is a cross-sectional view of the diameter, and half of the top view is taken to clearly show the correspondence of the various levels of the mechanism. Used on it for comparison). The mechanism is composed of three inner and outer surrounding multi-wing ring mechanisms of the previous embodiment, the planes of the three inner and outer surrounding multi-wing ring mechanisms are parallel to each other, and their axial lines overlap with each other. Straight line; where the rail couplings at corresponding positions between the upper and lower wing rings are connected by a connecting rod 27, the connecting point of the connecting rod 27 and the rail coupling body is located in the link between the rail car and the rail car in each rail coupling body Rod 3-3.

The multi-wing ring mechanism with both inner and outer enveloping features and laminated parallel type features is greatly suitable for building large and very large wing rings due to the multi-layered mutual support in the lateral and longitudinal directions. Institutions such as high-altitude wing-ring wind turbines and wing-wing aircraft.

Embodiment 10 (shown in Figure 18):

The two multi-wing ring mechanisms with different radii but the same axial line are stacked one on top of the other, and the two multi-wing ring mechanisms are stacked parallel. The lower wing ring 1-4 in the larger diameter multi-wing ring mechanism in the upper layer is in the same plane as the upper wing ring 1-3 in the smaller diameter multi-wing ring mechanism in the lower layer, the two wing rings passing through the wing The spokes 4-2 are integrally connected to each other and actually constitute the same wing ring. The flaps of the adjacent two wing ring mechanisms have the opposite angle of attack (ie, the direction of rotation is opposite), and the clockwise torque and the counterclockwise torque of the whole machine cancel each other out. This kind of inverted glyph structure, if used as a high-altitude mechanism connected to the ground through the traction cable, will achieve two outstanding effects: one is to maintain a stable flight and suspension attitude, and the other is to facilitate the maximum acceptance of each wing ring. Wind energy.

Embodiment 11 (as shown in FIG. 21 and FIG. 22):

This is also a laminated parallel multi-wing ring mechanism, in which a plurality of wing ring mechanisms are combined by a cage bracket 27-1, and the rail coupling body of each wing ring passes through the rail coupling body 3 and the cage bracket 27-1. Connected, the cage bracket 27-1 is surrounded by the respective wing rings.

Embodiment 12 (shown in Figures 23 and 24):

This is also a laminated parallel multi-wing ring mechanism, which is composed of a plurality of wing ring mechanisms by a cage bracket 27-1, and each wing ring is connected to the cage bracket 27-1 through the rail coupling body 3, and each wing ring It is surrounded by the cage 27-1.

Example 13:

On the basis of the previous embodiment, the cage bracket 27-1 is replaced by a cylindrical or cylindrical object or a cylindrical or cylindrical body, such as replacing the bracket 27-1 with the fuselage of the aircraft, thereby obtaining the fuselage. A vertical take-off and landing wing aircraft with multiple wing-ring rotors.

Embodiment 13 (as shown in FIG. 25 and FIG. 26):

This is a wing ring mechanism with fixed wings, which consists of three fixed wings 33 and three wing ring mechanisms (or combined wing ring mechanisms) 32 which form a wing ring mechanism with fixed wings. The middle fixed wing 33 and the left and right fixed wings 33 are each connected by four V-shaped links 4-1 (the purpose is to combine the three fixed wings into one carrier with sufficient mechanical strength, and the middle wing ring) 1 and the front and rear wing rings 1 are respectively connected by a double-track type vehicle-rail coupling body, the double-track type vehicle-track coupling body between the rail car and the rail car 3-3 and the V-shaped link 4 between the fixed wing and the fixed wing The -1 intersects and connects. The flaps of the adjacent two wing rings have the opposite angle of attack (ie, the direction of rotation is opposite), and the clockwise torque and the counterclockwise torque of the whole machine cancel each other out.

Embodiment 14 (shown in Figures 27 and 28):

This is also a wing ring mechanism with fixed wings, which consists of three fixed wings 33 and three wing ring mechanisms (or combined wing ring mechanisms) 32 which form a wing ring mechanism with fixed wings. The three fixed wings 33 are arranged in three parallel faces from top to bottom. The middle fixed wing and the upper and lower fixed wings are respectively connected by 8 connecting rods 4-1 (combining the three fixed wings into a wing ring mechanism carrier with sufficient mechanical strength); where adjacent wing ring mechanisms are The two-rail type vehicle-rail coupling body is connected, and the double-track type rail-coupled inner link rail car and the rail car between the link 3-3 and the V-shaped link 4-1 intersect and connect. It is necessary to set the torque in the clockwise direction of the whole machine to counteract the torque in the counterclockwise direction.

Wing ring wind power mechanism embodiment:

Embodiment 1:

Wing ring type wind turbine or hydroelectric generator: In any wing ring mechanism, the power transmission wheel of the shaft generator is used to directly replace the wheel of the rail car in the rail coupling body, or is connected with the wheel of the rail car, and The fuselage of the generator is either connected to the railcar frame or directly replaces the railcar frame. The so-called shaft generator refers to a generator in which the center shaft is connected to the generator rotor and moves synchronously.

The external connection method of the generator circuit with the high-speed circular motion of the wing ring is detailed in the section "Example of the connection method between the power generation part and the external circuit on the rotating wing ring". This point is applicable to the embodiment of each wing ring wind power mechanism, and the following examples will not be described again.

Embodiment 2:

Tower type wind turbine generator: Any one of the wing ring type wind turbine generators of the above embodiment connects the portion of the rail coupling body that does not rotate with the wing ring to the tower.

Embodiment 3:

Attaching the fuselage of the shaft generator to the annular bracket of a wing ring based on any of the stacked parallel multi-wing ring mechanisms (such as the third or fourth example of the "wing ring mechanism embodiment") The power input wheel is coupled to the annular track and the annular track is coupled to the adjacent other wing ring.

Embodiment 4 (as shown in FIG. 13, FIG. 14, FIG. 19):

The fuselage of the shaft generator is connected to the annular bracket of a wing ring based on any of the inner and outer surrounding multi-wing ring mechanisms (for example, the third or eighth example of the "wing ring mechanism embodiment") The power input wheel is coupled to the annular track and the annular track is coupled to the adjacent other wing ring.

Embodiment 5 (as shown in FIG. 15, FIG. 16, FIG. 17):

Based on any stacked parallel multi-wing ring mechanism (such as the third or fourth example of the "wing ring mechanism embodiment"), the annular bracket of each single-wing ring mechanism is set as a huge power generating coil and adjacent The two wings surround each other as a rotor, and each other is a stator (counter-rotating power generation), which is composed of a large generator that does not rely on the shaft to drive the rotor. Such a generator does not actually have a stator because each core winding with a wing ring is rotating. Two coaxial and adjacent wings surround the group, and when they rotate in the opposite direction, they can cut magnetic lines to generate electricity. The three coaxial wings surround the group. When the centerer rotates in the opposite direction to the one of the two sides, It is also possible to cut magnetic lines of force to generate electricity.

Embodiment 6 (as shown in FIG. 13, FIG. 14, FIG. 19):

Based on any of the inner and outer surrounding multi-wing ring mechanisms (Example 3 or Example 8 of the "wing ring mechanism embodiment"), the annular bracket of each single-wing ring mechanism is set as a huge power generating coil, and adjacent The two wings surround each other as a rotor, and each other is a stator (reverse rotation power generation), which is composed of a large generator that does not rely on the shaft to drive the rotor. Such a generator does not actually have a stator because each core winding with a wing ring is rotating. Two coaxial and adjacent wings surround the group, and when they rotate in the opposite direction, they can cut magnetic lines to generate electricity. The three coaxial wings surround the group. When the centerer rotates in the opposite direction to the one of the two sides, It is also possible to cut magnetic lines of force to generate electricity.

Embodiment 7 (shown in Figure 11)

Based on the first embodiment of the wing ring mechanism, the inner and outer wing ring mechanisms are arranged as a wing ring wind power mechanism, and the wing ring portion and the power generating portion of the wing ring wind power mechanism are actually the fourth embodiment or the implementation. The inner and outer surrounding multi-wing ring mechanism described in Example 6.

Example 8 (as shown in Figures 23 and 24):

This is also a “wind tunnel type wing ring wind power mechanism”. The wing ring mechanism of Example 12 (as shown in Fig. 23 and Fig. 2) of the “wing ring mechanism embodiment” is set as a wing ring wind power mechanism. The setting method is found in “ Example 1 or Example 2 of the Example of a Wing Ring Wind Power Mechanism; then placing the mechanism in a wind tunnel or a water hole to connect the cage bracket 27-1 to the wall of the cave.

High-altitude wing ring wind power system embodiment:

Embodiment 1 (shown in Figure 29):

The iron core and the winding are respectively arranged by the brackets of the wing ring 1-1 and the wing ring 1-2, and the two wing rings are in the same plane, have the same center but different radii; the wing ring 1-1, the wing ring 1-2 The upper and lower ends are respectively connected to the circular orbit 3-1, the track 3-1 is around the wing ring, and is actually the same as the wing ring; the cross section of the track 3-1 is a trough type, and the rail track is coupled with the rail car 3-5 ( The lower right picture is a partial enlarged view of the vehicle rail coupling body 3); the rail car is composed of the frame 3-2, the connecting rod 3-3, and the pulley 3-4; the orbits are arranged at equal distances (not less than three) The railcars 3-5, the adjacent railcars 3-5 are connected by the connecting rods 3-3, the effect is that the rails of the two different wing rings are fixed together, and the two are respectively The railcars that are coupled to different tracks can still operate freely. Therefore, although the two wing rings rotate rapidly in different directions, they always maintain the same relative position, and they will not separate or collide.

Each railcar on one track and the railcar at a corresponding position on the track of the other wing ring are connected to each other through a connecting rod 3-3; the two ends of the V-shaped connecting rod 4 are respectively connected with one connecting rod 3-3, and each strip The V-shaped links 4 intersect on the axis of the wing ring and are fixedly connected to each other at the intersection. In addition to the fixed connection at the intersection, a support bar can be welded between the intersecting V-shaped links 4 to form a triangular moment structure. If it is not enough to ensure that the relative position of each railcar does not change with the rotation of the wing ring, then all the connecting rods 3-3 of the railcars connecting the two adjacent rails between adjacent wing rings should be connected in series by connecting rods. (Forms a closed loop or polygon).

In this embodiment, the individual fins of the same wing ring must have the same area, but the wing areas of the different wing rings can be different. Since the inner ring fin collects wind energy less efficiently than the outer ring fin of the same area, the inner ring fin area must be larger than the outer ring fin area. As for the ratio of the two, a principle must be followed, that is, two The reverse rotation of the wing ring collects the same efficiency of the wind energy, so that the torsion forces cancel each other during the reverse rotation of the windward, avoiding the rotation of the wing ring with the larger torque of the whole machine, thereby ensuring the normal working of the mechanism and preventing the cable accident. .

As for the angle of attack of the airfoil, if the angle of attack of the outer wing ring is n, then the angle of attack of the inner wing ring is -n, so the direction of rotation of the two wings is inevitably opposite, and the core winding on the two wings is accompanied by the wing Reverse rotation rotates the magnetic lines of force to generate electricity. The fin of this embodiment has a spin wing tab feature.

The external connection method of the generator circuit can be found in the section "Examples of the connection method between the power generation part and the external circuit on the rotating wing ring" in the "Technical plan of the wing ring wind power mechanism" (the following examples of the high-altitude wing ring wind power mechanism are the same) Therefore, the following examples will not be repeated here.

Each of the V-shaped connecting rods 4 passes through the central axis of the wing ring, and the two ends of the two V-shaped connecting rods are respectively connected with the connecting rods 3-3 between the corresponding rail cars and the rail cars; the midpoints of the respective V-shaped connecting rods 4 intersect and are connected This intersection is connected to the upper end of the traction cable 5, and the lower end of the traction cable 5 is connected to the lower electrical installation.

The cable can be implanted inside the traction cable so that the traction cable and the cable are combined into one.

Embodiment 2 (shown in Figure 30):

Three wing rings 1 of the same diameter are arranged one above the other, their axial lines are overlapped by a straight line; the wing rings 1 at the upper and lower ends each have a track 3-1 surrounded, and the middle wing ring 1 has two tracks 3-1 around; Several (not less than three) rail cars 3-5 are arranged equidistantly on each track; the railcars of the upper wing ring are paired with the railcars on the upper wing of the middle wing ring, and the railcars and lower wing rings of the lower wing of the middle wing ring The railcars are paired, and each of the two railcars (one on top and one on the bottom) is a pair, and each pair of railcars is connected by a connecting rod 3-3.

The iron core and the winding are respectively arranged by the brackets of the three wing rings 1 , and the middle wing ring rotates in the opposite direction to the upper and lower wing rings, so that the magnetic lines of force can be cut to generate electricity, and the wings of the two uppermost and lowermost layers are welcoming. The angles are the same and the area is the same, so that the two wing rings rotate synchronously, so that the current or magnetic lines generated by their windings are the same and do not interfere with each other.

If the flap angle of the upper and lower two wing rings is n, the wing angle of the middle wing ring is -n. The fins on the same side of the same wing ring (that is, the outer side or the inner side of the ring extending uniformly) must have the same area, but the fins of different wing rings or the fins on different sides of the same wing ring may have different areas. The area is adjusted so that all windwise rotating fins and all counterclockwise rotating fins collect the same wind energy.

Each of the rails 3-1 is wound around its wing ring. In fact, it is integrated with the wing ring; the cross section of the track 3-1 is a trough type, and the trough type is coupled with the rail car. Since the two adjacent rail cars 3-2 are connected by the connecting rods 3-3, the two wing rings, although rotating in different directions, do not separate or collide with each other.

Refer to Embodiment 1 for the characteristics of the local wing, the connection relationship of the circuit, and the connection structure of the traction cable.

Embodiment 3 (as shown in Figure 31):

The inner wing ring 1-2 and the outer wing ring 1-1 are in the same plane, have the same center but different radii, and several shaft generators 6 are equally spaced on the two wing rings, and the wing ring bracket is used as the shaft type. The base of the generator 6, the power wheel 7 of the generator on each wing ring is coupled with the circular track 8 on the other wing ring (in fact, the frame of the railcar is replaced by a generator body, using a generator The power input wheel replaces the wheel of the railcar. The details are shown in a partial enlargement. The coupling of the wheel and the rail can of course follow the train and train tracks, but the best way is to use intermeshing gears and toothed rails.

Refer to Embodiment 1 for the characteristics of the local wing, the angle of attack of the airfoil, the connection relationship of the circuit, and the connection structure of the traction cable.

Embodiment 4 (as shown in Figure 32):

The upper wing ring 1-3 and the lower wing ring 1-4 are two parallel wing rings whose axis lines are overlapped by the same straight line, and a plurality of shaft generators are respectively installed on the two wing rings at equal distances. The wing ring bracket serves as a base for the shaft generator 6, and the power wheels 7 of the generators on each wing ring are coupled to the annular track 8 on the other wing ring.

Refer to Embodiment 1 for the characteristics of the local wing, the connection relationship of the circuit, and the connection structure of the traction cable. The flap angle of attack is referred to the second embodiment.

Embodiment 5 (shown in Figure 33):

The structure of the generator is identical to that of the fourth embodiment except that the axial direction of the generator changes from a vertical direction to a horizontal direction.

Embodiment 6 (as shown in Figure 34):

Figure 34 is a rear view taken along the diameter, wherein the upper view is a top view (full view is shown in Figure 19), and the lower view is a side view, with arrows between the two indicating the correspondence between the two.

The four wing rings are in the same plane, have the same center but different radii, and the wing ring 1-2-1 and the wing ring 1-1-2 are fixedly connected and rotated synchronously by the airfoil spokes 4-2, and the spokes 4-2 are wings. The flaky spokes thus function as both spokes and fins. For the connection between the wing ring 1-1-1 and the wing ring 1-1-2 and between the wing ring 1-2-1 and the wing ring 1-2-2, refer to the first embodiment, as for the characteristics of the local wing. The circuit connection relationship and the connection structure of the traction cable are referred to in the first embodiment. The wing angles of the wing ring 1-1-1 and the wing ring 1-2-2 are the same, and the wing angle of the wing ring 1-1-2 and the airfoil spoke 4-2 are the same, the wing ring 1-1-1, the angle of attack of the wing ring 1-2-2 is opposite to the angle of attack of the wing ring 1-1-2.

Embodiment 7 (shown in Figure 35):

The multi-wing ring mechanism of the present embodiment is basically the same as the "wing ring mechanism embodiment IX" (as shown in FIG. 18), but a set of the vehicle-rail coupling body 3 is added to the lowermost wing ring mechanism, and the diameter ends are respectively corresponding. Each pair of railcars 3 is connected by a connecting rod 3-3, and the connecting rod 3-3 between the railcar and the railcar is connected with the V-shaped V-shaped connecting rod 4, and the midpoint of the V-shaped connecting rod 4 It is connected to the upper end of the traction cable 5, and the traction cable 5 is connected to the ground joint; the traction cable 5 combines the traction cable and the cable. Then, the iron core and the winding are arranged by using the annular bracket of each wing ring as a bracket, so that each wing ring becomes a huge power generating winding. Since the upper and lower wing rings are opposite to the middle wing ring, this mechanism has two huge generators. For the method of externally connecting the two large generator circuits, refer to the first embodiment. The circuit of the upper generator is extended to the upper wing ring of the lower generator through the airfoil spokes 4-2. Once again, “external” to the cable to the ground. The wing angles 1-3 and wing rings 1-4 at the upper and lower ends have the same angle of attack; the wing rings 1-3 and wing rings 1-4 in the middle have the same angle of attack; the wing ring 1 in the middle 3 and the wing angle of attack of the wing ring 1-4 are opposite to the wing angles of the wing ring 1-3 and the wing ring 1-4 at the upper and lower ends.

Refer to Embodiment 1 for the characteristics of the local wing, the external connection method of the circuit, and the connection structure of the traction cable.

Embodiment 8 (as shown in FIG. 36)

The lower end of the high-altitude wing ring wind power mechanism 19-1 is connected to the upper end of the cable 5-1, the lower end of the cable 5-1 is connected to the upper end of the high-altitude wing ring wind power mechanism 19-2, and the lower end of the high-altitude wing ring wind power mechanism 19-2 is connected to the cable 5- The upper end of the cable 5-2 is connected to the upper end of the power generating ring 19-3, the lower end of the high-altitude wing ring wind power mechanism 19-3 is connected to the upper end of the traction cable 5, and the lower end of the traction cable 5 is connected to the ground facility; the high-altitude wing ring wind power mechanism The circuits of 19-1, 19-2, and 19-3 are connected in parallel or in series, and are joined together as a cable to be connected to the ground power facility, and the cable can be combined with the traction cable 5 into one.

In this embodiment, it is preferable to fly the high-altitude wing ring wind power mechanisms 19-1, 19-2, and 19-3 in the same airflow layer, so that the voltages generated by the machines are the same, and it is convenient for each machine to be connected to the grid to generate power with the same cable. Power transmission.

High-altitude water dispenser embodiment:

Embodiment 1:

The existing air air extractor is disposed above the high-altitude airfoil wind power mechanism, and the generator circuit of the high-altitude wing ring wind power mechanism is connected with the air water extractor circuit (the battery can be set if necessary), and the air outlet of the air water extractor Connected to the water pipe, the water pipe is connected to the onboard storage tank or water equipment.

Embodiment 2 (as shown in Figure 37):

The outer casing 10-1 of the water extractor is connected to the railcar 3-5 through the connecting rod 3-6, the railcar is coupled with the trough-shaped rail 3-1, and each trough-shaped rail 3-1 is wound around the respective wing ring, the wing ring 1 -3 connecting fins 2-1.3, wing rings 1-4 connecting fins 2-1.4. Both ends of the outer casing 10-1 of the water dispenser are in the shape of a bell mouth.

The water dispenser is composed of an air conditioner refrigerator 21, a condensing water collector 22, a water receiving tank 24, an air conditioner radiator 23, and a water pipe 25, and the condensing water collector is placed outside the lower air head except that the fan and the radiator are placed on the wind up head. It is basically the same as the existing air conditioner. The water extractor is connected and fixed to the wall of the air cylinder through the connecting rod 3-7, and the bottom thereof is connected with the V-shaped connecting rod 4-1, and one of the V-shaped connecting rods 4-1 is a hollow connecting rod of the connecting rod and the water pipe 4- 3. The hollow V-shaped connecting rod 4-3 is connected to the upper end, and the lower end of the water pipe and the traction cable 5-2 is connected to the ground water pipe.

Embodiment 3 (as shown in Figure 38):

The lower end of the high-altitude wing ring wind power mechanism 19-1 is connected to the lower end of the traction cable 5-4, the lower end of the traction cable 5-4 is connected to the upper end of the high-altitude water extractor 26-1, and the lower end of the high-altitude water extractor 26-1 is connected to the traction cable 5-5. The upper end of the traction cable 5-5 is connected to the upper end of the high-altitude water extractor 26-2, the lower end of the high-altitude water extractor 26-2 is connected to the upper end of the hollow traction cable 5-6, and the lower end of the traction cable 5-6 is connected to the ground facility, wherein The traction cable is bolted to the pile, and the water pipe is connected to the reservoir.

The upper end bell mouth edges of the high-altitude water extractors 26-1, 26-2 are equidistantly taken at four points, and the two ends of the two cables of the same length are respectively connected at two points on the same diameter, and the intersection of the two cables is suspended above. The connection point of the traction cable (as shown in a partially enlarged view in Figure 38).

The high-altitude wing-ring wind power mechanism 19-1 is electrically connected to three high-altitude water intakes; the water pipes of the two high-altitude water extractors are connected to the upper ends of the water pipes in the hollow traction cables 5-6.

Example of a wing ring aircraft:

Embodiment 1 (as shown in FIG. 39 and FIG. 40):

This is a wing-wing aircraft with the fuselage taking off and landing vertically in a vertical state. Its shape is basically the same as that of a normal airplane, but instead of using a common propeller, a wing-ring mechanism (or multi-wing mechanism) 32 is used. On the body, one is placed at the front of the fuselage (before the wing, behind the nacelle), one is placed at the rear of the fuselage (behind the main wing, the front of the rudder), the two wing ring mechanisms (or combined wing ring mechanism) 32 The rotation direction is opposite and the torque is balanced; the setting method of the engine can be operated according to any one of the “winging aircraft engine setting methods” in the “wing ring aircraft technical plan”; the tail rudder has the function of taking off and landing, Therefore, it is designed as a symmetrical four-page (can also be designed as three pages under the premise that the stable support body is erected on the ground), the two wings parallel to the main wing are elevators, and the two wings perpendicular to the main wing are rudders. In order to reduce the impact during landing, it is also possible to provide a three-legged landing gear without the function of the tail rudder and the landing gear. The landing gear can be designed to be telescopic. It protrudes from the fuselage during landing and is retracted into the fuselage after take-off. .

The vertical take-off and landing aircraft can be equipped with an electric engine, a piston internal combustion engine or a jet engine. The setting methods of various engines are detailed in the "wing-wing aircraft technical solution" in "the setting method of several engines of the wing-wing aircraft".

Embodiment 2 (as shown in FIG. 41 and FIG. 42):

This is a wing-wing aircraft with the fuselage taking off and landing vertically in a horizontal state. Its shape is basically the same as that of a normal airplane. The difference is that the engine adopts a wing ring mechanism (or multi-wing ring mechanism) 32, and the connection point is located at the end of the main wing. Front edge, connection mode: the airfoil is connected with the wing ring steering mechanism 38, the wing ring steering mechanism 38 is connected with the wing ring mechanism or the combined wing ring mechanism by a minimum of four links 39, and the bottom end of the connecting rod 39 is connected to the wing ring for steering The mechanism 38 has its top end connected to the rail coupling body 3 of the wing ring mechanism; the wing ring steering mechanism 38 must be capable of swinging the link 39 for 90° in order to enable the center axis of the wing ring mechanism or the combined wing ring mechanism 32 to The lifting phase is perpendicular to the main airfoil and can be parallel to the main airfoil during the horizontal flight phase.

Embodiment 3 (as shown in FIG. 43 and FIG. 44):

This is a wing-wing aircraft in which the fuselage moves up and down vertically in a horizontal state. On the basis of the previous embodiment, the original two deflection mechanisms 38 are transferred between the two wings and the fuselage to make two wings. The ring mechanism is fixedly coupled to the wing and enables the wing to be deflected by the deflection mechanism 38 while the wing ring mechanism is simultaneously deflected by the angle of rotation). The advantage of this change is that during the vertical up or down phase, the strong wind fanned out of the wing ring does not fall on the wing's airfoil, increasing the lift and stability during the vertical takeoff and landing phase.

Embodiment 4:

This is also a wing-wing aircraft with the fuselage taking off and landing vertically in a horizontal state. On the basis of the previous embodiment, the two deflection mechanisms between the wing and the wing ring mechanism of the second embodiment are restored, and the two deflection mechanisms between the wing and the fuselage are retained. The benefit is that the wing ring mechanism can fine-tune its angle relative to the wing, which is more conducive to flight control.

Embodiment 5 (as shown in FIG. 45 and FIG. 46):

This is a multi-rotor wing-ring helicopter, as detailed in Example 6 of the "Wing Ring Mechanism Embodiment".

Example 6:

This is a ramjet airfoil aircraft. Based on any of the above six embodiments, the wing ring mechanism (or multi-wing ring mechanism) 32 is further configured as a wing ring mechanism with a fuel tank, and the engine is a ramjet engine, and the ramjet engine is mounted on the wing. On the piece or on the ring bracket (the specific method is detailed in "Fourth Rings with Fuel Tanks" and "Flap Ring Aircraft Technical Plan" in "Flap Ring Aircraft Several Engines" Setting method").

Example 7:

This is a ramjet airfoil aircraft. Based on the seventh embodiment, a fuel inlet port similar to that of the automobile tire is provided to the fuel inlet of the wing ring fuel tank. Correspondingly, the fuel output pipe of the fuselage fuel tank is led to the side of the wing ring fuel tank, and an air outlet structure similar to that of the compressed air gun for inflating the automobile tire is provided to the pipe port.

Embodiment 8 (as shown in FIG. 47 and FIG. 48):

This is an outer wing ring helicopter. Two wing ring mechanisms 1-3 and 1-4 having a spin-wing feature are provided on the outer circumference of the cylindrical nacelle, and the two wing rings are set to have equal torques and opposite rotational directions. The rail coupling body 3 of the wing ring mechanism is connected with the nacelle; the wing ring mechanism of the embodiment can be configured with various engines, and the specific method is detailed in the "wing ring aircraft technical scheme" in the "wingwing aircraft several engine setting methods" "one period.

Embodiment 9 (as shown in FIG. 49 and FIG. 50):

This is an inner wing ring helicopter. Two wing ring mechanisms 1-3 and 1-4 having a spin-wing feature are provided on the inner circumference of the ring of the annular nacelle, and the two wing rings are arranged to have equal torques and opposite rotational directions. The rail coupling bodies 3 of the wing ring mechanisms 1-3 and 1-4 are connected to the nacelle; the wing ring mechanisms 1-3 and 1-4 of the present embodiment can be configured with various engines, and the specific method is detailed in the "wing ring aircraft" "Technical Solutions" section of "Setting Methods for Several Engines of Wing Ring Aircraft".

Embodiment 10 (as shown in FIG. 51 and FIG. 52):

This is a helicopter with a wing ring inside and outside. On the basis of the ninth embodiment, two wing ring mechanisms 1-3 and 1-4 having a spin-wing feature are added to the outer circumference of the annular nacelle, and the two wing rings are set to have the same torque and opposite rotation directions. The rail coupling body 3 of each wing ring mechanism is connected with the nacelle. The specific method is described in the section “How to Connect the Wing Ring Mechanism to the Carrier” in the “Technical Solution of the Wing Ring Mechanism”; the outer wing ring mechanisms of this embodiment are all Various engines can be configured. The specific methods are described in the section “Setting Methods for Several Engines of Wing Ring Aircraft” in the “Wing Ring Aircraft Technical Plan”.

Example 11:

On the basis of Example 10 or Example 11 of the "Wings of the Wing Ring Aircraft", the following settings are made: 3 to 4 jet engines are installed on the outer or top or bottom of the fuselage of the wing ring helicopter. Equal, this setting is to achieve horizontal movements, cornering, right-angle cornering, air brakes and other actions. The arrangement of the jet engines is shown in Figure 47 (four jet engines 13-3 for steering).

Example 12:

On the basis of Example 10 or Example 11 of the "Wings of the Wing Ring Aircraft", the following arrangement is made: four flow guiding nets are arranged at the lower end of the middle hole of the annular body, and the four flow guiding nets are preferably in the same flat. Each of the diversion nets is composed of deflectable blades, and both ends of each blade are connected with a "well"-shaped bracket through a blade deflection mechanism, and the well-shaped bracket is fixed at the edge of the hole in the annular fuselage.

The function of the diversion net is to achieve horizontal movement and cornering. When it is necessary to ascend or hover, the blades of the four diversion nets should be in a vertical state, so that the airflow from the wing ring is vertically downward; when horizontal horizontal motion is required, the two diversions a and b should be made. The blades of the net or c and d diversion nets are simultaneously biased to one side (while the other two diversion nets maintain the vertical state of the blades), so that the airflow from the fan ring fan is blown out obliquely; when it is required to move horizontally (this When the two flow guiding nets a and b have been turned toward one side at the same time, the blades of the two diversion nets of c and d should also be biased to one side, thereby generating another force that is perpendicular to the original horizontal direction in the horizontal direction) , so that the whole machine changes direction (that is, turning).

Example 13:

This is a diving or diving helicopter that can snorkel in the water and jump out of the water in the air.

On the basis of the above fourteen embodiments, the following settings are further made: one is strictly sealed and waterproofed to the cabin body and the door; the two are strictly waterproofed to the motor or the power generating coil of the wing ring mechanism; All exposed wheels or bearings of the organization are strictly sealed and waterproofed; the four are equipped with the inlet and drain compartments of the submarine and related institutions (that is, the equipment for the existing submarines to rise and dive in the water) inside the cabin. These facilities will undoubtedly The aircraft load is greatly increased, but the general aircraft is powerless, but the wing ring aircraft has a huge bearing capacity. Even if it has only two 50-meter-wing wing-ring rotors, its maximum take-off weight can exceed 10,000 tons (see details in " The beneficial effects of the wing ring mechanism are the second), so this solution is feasible.

This embodiment can be constructed on the basis of the above thirteenth embodiments, but it is more suitable to be constructed on the basis of any of the first embodiment or the eighth embodiment to the thirteenth embodiment. If the present embodiment is further provided on the basis of the tenth embodiment, the outer peripheral fins of the fuselage can be completely prevented from coming into contact with the reef or other objects.

Example of wing ring to pull suspension mechanism:

Embodiment 1 (shown in Figure 53):

This embodiment is a wing-to-pull flying suspension mechanism with a nacelle. The wing ring mechanism with fixed wings of the thirteenth or fourteenth embodiment of the two "wing ring mechanism embodiments" is used as the lifting mechanism 28, or two multi-wing ring mechanisms having the characteristics of the self-rotating wing are used as the lifting mechanism 28 The two float mechanisms are opposite in orientation; the two float mechanisms 28 are coupled to the nacelle 31 by traction cables or links 29, respectively.

The sum of the weight of all the lifting mechanisms 28 and the weight of the nacelle 31 and the basket bracket 27-2 must be equal to the buoyancy provided by the lifting mechanism, so that the tension flying mechanism can be maintained at an appropriate height without excessive floating or Sinking and leaving the balance of the two airflows; when considering the tension of the two sets of hoisting mechanisms, the winds received by the nacelle 31 and the basket bracket 27-2 must be considered, and this force is put into force. In the pair of pulling forces of the same group of lifting mechanisms, the opposite pulling forces in the two directions are finally balanced. This also applies to the following embodiments relating to the tensioning mechanism, in particular the embodiment of the tensioning mechanism with the nacelle in these embodiments.

Embodiment 2 (shown in Figure 54):

On the basis of the first embodiment, the lifting mechanism 28 in the upwind layer and the downwind layer are all increased from one to two, and all the lifting mechanisms 28 are wing ring mechanisms with fixed wings or both have the characteristics of a spiral wing. Multi-wing ring mechanism. Each of the floating mechanisms 28 is connected by a basket bracket 27-2, and the bottom end of the basket bracket 27-2 is connected to the nacelle 31. The two sets of hoisting mechanisms are all in the same wind belt, but only in the upper and lower two different wind layers. Therefore, the two levitation mechanisms in each group of hoisting mechanisms are side-by-side lateral windward, not front and rear. Arrange the vertical windward (different from the arrangement of the wind in Figure 63).

Embodiment 3 (shown in Figure 55):

This is a pair of wing-to-pull suspension mechanisms in which the two sets of lifting mechanisms are all in the same wind belt.

On the basis of the second embodiment, the elevator 30 is added to the basket bracket 27-2 (or on each wing ring mechanism as the floating mechanism 28), and other moving mechanisms can be added (for details, see "wing ring to pull fly". The fifth and sixth natural sections of the technical scheme of the suspension mechanism.

Embodiment 4:

This is a pair of two sets of lifting mechanisms in two different wind belts of the wing ring to pull the flying mechanism (two reverse winds are not vertically arranged, but horizontally juxtaposed).

The mechanism of this embodiment is basically the same as that of the previous embodiment, but the arrangement of the mechanism with respect to the wind direction changes from the longitudinal direction to the lateral direction. In the previous embodiment, the two sets of the two floating mechanisms 28 are arranged side by side and horizontally facing the wind (the two are connected The line is perpendicular to the wind direction, and in the present embodiment, the two sets of the two floating mechanisms 28 are longitudinally aligned in front and rear (the lines of the two are parallel to the wind direction).

In this embodiment, it is particularly necessary to pay attention to the setting and manipulation of the motion mechanism 39, so that the power mechanism is sufficient to offset the torque caused by the two horizontally arranged reverse winds to horizontally rotate the whole machine, and the whole machine gradually enters the spiral state and crashes. Such a motion mechanism 39 for correcting the whole machine should be placed at a center point as far as possible from the spiral state caused by the harmful torque, so that the motion mechanism 39 can achieve the maximum correcting effect with a minimum force. For the "sports organization", please refer to the fifth paragraph of the article "Technical plan for the wing-to-pulling suspension mechanism". This embodiment employs a power engine as the motion mechanism 39 for correcting the deviation.

The significance of this embodiment is that the wing ring-to-pull suspension mechanism not only has the ability to sail across the wind belt, but also can realize the whole machine turning or changing the direction.

Embodiment 5 (shown in Figure 56):

The present embodiment is a wing ring pull-up aircraft without a nacelle, and two vertical take-off and landing wing aircrafts are used as the lifting mechanism 28, and their orientations are opposite. The two ends of the traction cable or the connecting rod 29 are respectively connected to the two wing rings. The head of the aircraft (the upper joint of the upper machine is located on the lower side of the head, and the joint of the lower machine is located on the upper side of the head). When the two machines take off at the same time (the wing ring mechanism 32 faces upward), after the two machines reach their respective predetermined heights, the two machines will face the wind toward the front of the wing ring mechanism 32, and then the engine can be turned off, and the wing is at a strong high wind. Naturally, it will generate enough lift, while the reverse wind group will maintain the whole machine to hover or fly.

Embodiment 6 (as shown in Figure 57):

Two high-altitude wing-ring wind power mechanisms (or any wing-wing wind power mechanism with a spin-wing feature) are used as the lifting mechanism 28 to connect the nacelle 31 through a cable or a connecting rod 29, thereby forming a complete wing-ring-pull generating mechanism The bottom end of the nacelle 31 is connected to the upper end of the cable 5, and the lower end of the cable 5 is connected to the ground facility.

For the connection method of the circuit of each wing ring wind power mechanism and the cable 5, please refer to "Example of Connection Method between Power Generation Section and External Circuit on Rotating Wing Ring" in "Technical Plan of Wing Ring Wind Power Mechanism".

Example 7:

In any one of the first embodiment to the fifth embodiment, the wing ring mechanism is configured as a wing ring wind power mechanism (the method is found in the “technical solution of the wing ring wind power mechanism”), and the circuits of the respective power generation mechanisms are connected in parallel or in series, and then Connected to the upper end of the cable, the lower end of which is connected to a device or grid that requires power. This becomes the pull ring generator.

Crane transport aircraft embodiment:

Embodiment 1 (shown in Figure 58):

The lower end of the wing-to-pull power generation mechanism is connected to the upper end of the cable 29, and the lower end of the cable 29 is connected to the retractable cable machine 15 (the connection point is on the cable pulley of the retractable cable machine, and must be fixedly connected, otherwise it may be in motion In the event of a cable collapse accident, the cable 29 is wound around the cable pulley, and the length of the cable segment wound around the cable pulley is greater than the vertical distance between the highest point and the lowest point of the expected running line of the wing ring helicopter; the cable-receiving machine 15 is mounted on the crane The bottom of the compartment 31 (may also be installed on the top of the wing helicopter 40); the cable pulley is connected to the two-way motor, the two-way motor is controlled by a bidirectional switch, the bidirectional switch is controlled by a microcomputer chip; the microcomputer chip and the altitude sensor Connected, the microcomputer chip can issue a clockwise rotation, counterclockwise rotation or brake command to the bidirectional switch at any time according to the change of altitude, so that the cable is kept in an optimal tension state. The retractable cable machine 15 also has a function of lifting and landing the wing-ring helicopter together with the cargo to be lifted, thereby greatly increasing the lifting force and the lifting height. When the weight of the lifting object has exceeded the lifting capacity of the electric wing helicopter 40, the cable winding machine 15 can be instructed to recover the cable 29, which is equivalent to the wing ring pulling power generating mechanism directly playing the lifting function (the wing ring pulling power generating mechanism actually It is a kind of pull-up suspension mechanism with extremely large bearing capacity, and the lift of the electric wing-ring helicopter 40, the overall lifting force is even greater).

The electric wing ring pull-up power generation mechanism is electrically connected with the motor or battery of the wing ring helicopter 40, and the electric power line can be combined with the traction cable 29. The wing-ring helicopter 40 uses electric power as its energy source. For the configuration of its engine, please refer to the section “Setting method of electric engine” in the “wing-wing aircraft technical solution”.

The lower portion of the electric wing helicopter 40 is coupled to the hoisting mechanism 16, and the hoisting cable of the hoisting mechanism 16 or the lower end of the hoisting chain 17 is coupled to the pick-up device 18.

The electric wing helicopter 40 should be as close as possible to the ground for precise operation, and personnel should observe and operate on the electric wing helicopter 40.

The wing ring puller generator itself has a huge lifting capacity, and its maximum net lifting capacity can exceed 100,000 tons. The reason is to set up a wing ring helicopter between it and the cargo, mainly because of the pull The suspension mechanism is too far from the ground, and an intuitive operating platform close to the scene must be added to increase the accuracy and agility of the field operation; the wing-wing helicopter flying at low speed and low altitude within the diameter of the kilometer will not make the body at a high altitude. The much larger pull-up power generation unit is shaken (because the cable is ready to retract the cable at any time), so if you only need to transport the lifted items for several meters to hundreds of meters, then the pull-up generator at high altitude does not have to In any action, if it is necessary to transport the hoisted items to a farther place, then the high-altitude pull-up generators need to fly horizontally autonomously or horizontally under the towing of the wing-wing aircraft.

Embodiment 2:

On the basis of the previous embodiment, the electric wing helicopter 40 is removed, that is, the bottom of the pull-ring power generating mechanism nacelle 31 is connected to the retractable cable machine 15, and the retractable cable machine 15 is connected to the upper end of the traction cable 29, and is towed. The lower end of the cable 29 is coupled to the helicopter structure 16 and the helicopter structure 16 is coupled to the pick-up device 18 by a hoisting cable or hoisting chain 17 of the hoisting mechanism. The wing ring pull-up power generation mechanism is connected with the cable-receiving cable machine 15 and the material pick-up device 18, and a control switch is arranged on the circuit, and the operator controls the object-taking device to take objects and release objects on the wing-ring pull-generation power generation mechanism, and control the receiving The cable-receiving machine receives and releases the cable to realize lifting and lowering of objects.

Wing ring wind power boat example:

Embodiment 1 (shown in Figure 59):

The lower end of the high-altitude wing ring wind power mechanism 19 is connected to the upper end of the traction cable or cable 5 (the traction cable and the cable are combined into one), and the lower end of the traction cable or cable 5 is connected to the ship 20; the circuit of the high-altitude wing ring wind power mechanism 19 is connected to the cable. The cable is connected to the battery of the vessel 20, which is connected to the motor circuit.

Embodiment 2 (shown in Figure 60):

The nacelle 31 of the wing ring pull-up power generation mechanism is connected with the upper end of the traction cable 5, and the lower end of the traction cable 5 is connected with the splicing point of the ship 20; the wing ring pull-pull generating mechanism is electrically connected with the motor or the battery of the ship 20; the wing ring pair The two high-altitude wing-ring wind power mechanisms 19 of the pull-up power generation mechanism are respectively placed in two opposite wind layers.

Embodiment 3 (shown in Figure 61):

On the basis of the previous embodiment, the traction cable 5 between the nacelle 31 and the nacelle 31 and the ship 20 is eliminated, and the function of the nacelle 31 is replaced by the ship 20 so that the two high-altitude wing-ring wind power mechanisms 19 pass directly through the cable. 29 is connected to the boat 20.

Embodiment 4:

As a high-altitude mechanism, the third example of the "wing ring-to-pull suspension mechanism embodiment" (Fig. 55) is attached, the bottom of the nacelle 31 is connected to the upper end of the cable 29, and the lower end of the cable 29 is connected to the ship 20; The wing ring mechanism of 28 is configured as a wing ring wind power mechanism (the method is found in the "technical solution of the wing ring wind power mechanism"), and the circuits of the respective wing ring wind power mechanisms are connected in parallel, and then connected to the motor or battery of the ship 20 for circuit connection.

Since the high-altitude mechanism is provided with the motion mechanism 30, by manipulating the motion mechanism 30, the high-altitude mechanism can be used for cross-wind cruising, thereby towing the ship for crosswind sailing.

Reverse flow group energy development and utilization methods:

Embodiment 1:

On the basis of any of the above-mentioned "wing ring-to-pull suspension mechanism embodiment", the original wing-ring type float is replaced by a non-wing ring type floating mechanism such as an air bag, an airship, a kite or a center-shaft spin-wing mechanism. Lit institutions.

Embodiment 2:

On the basis of the previous embodiment, the wind turbine generator is provided to the high altitude mechanism of each embodiment.

Or kite generators or solar power facilities.

Embodiment 3 (as shown in FIG. 63 and FIG. 64):

Figure 63 is a schematic view of the overall mechanism, and Figure 64 is a partial enlarged view of the floating mechanism of Figure 63.

The two sets of floating mechanisms are each composed of an airship (or boat) 41 and a double-spinning reciprocating unloading kite. The two main control cables 9-1 and cables of the kite body 9 of the double-spinning body are reciprocally unloaded. 9-2 is connected to the motor type cable control machine 7-2, and the motor type cable control machine 7-2 controls the cable 9-1 and the cable 9-2 to alternately expand and contract, so that the two bodies are alternately in the unloading state or The nanoflow state, so that the two zither bodies alternately pull the power shaft 6-1 of the generator to rotate work; the generator 6 inside the airship is connected to the generator power wheel 7 through the coupling or the shifting mechanism 6-2 (the wheel 7 is An inner ring ratchet mechanism, an overrunning clutch or other similarly functioning mechanism consisting of an inner ring, an outer ring and an intermediate mechanism; a cable (or connecting rod) between the two floating mechanisms 29 connection.

The two sets of floating mechanisms are placed in the reverse wind group or the reverse water flow group, and the reciprocating unloading kite in the two sets of floating mechanisms will be reciprocated and unloaded under the impetus of wind or water flow, thereby pulling the generator to generate electricity (" The reciprocating unloading of the kite and its working principle are detailed in CN201210101117X, CN201220145598X or PCT/CN2012/074563).

The reciprocating unloading kite in the floating mechanism of the present embodiment can also be replaced with other forms of reciprocating unloading kites, such as the double-snake reciprocating unloading kite shown in Fig. 52 of CN201210101117X's "Instruction Drawings" (this kind The two zither bodies of the double zither body reciprocating the squad can run on the same line).

Embodiment 4 (shown in Figure 65):

On the basis of the third embodiment, the cable (or connecting rod) 29 between the two floating mechanisms is omitted, and the two airships 41 are combined into one; the two sets of the cable 29 for reciprocating the unloading of the kite are greatly extended, The two sets of reciprocating unloading kites are respectively operated in two reverse winds or two reversed water flows (actually, the floating mechanism does not include the airship 41, and the integrated airship (or boat) 41 actually becomes a connection. A portion of the traction cable or connecting rod of the two sets of lifting mechanisms.

Embodiment 5 (shown in Figure 66):

The airship (or boat) 41 has a retractable cable machine 15 at each end, and two retractable cable machines 7 are each connected with a cable 29, and the other ends of the two cables 29 are connected to a motor-type cable control machine 7 -2, the reciprocating rotating wheel of the motor type cable control machine 7-2 is connected with the two main control cables (ie, the cable 1 and the cable 2) of the double-chained kite, and the kite body 9 is the kite body of the double-chained kite (double The kite is a kite or kite that can change the state of the slab body by manipulating the expansion and contraction of the two main cables; the motor of the motor type cable control machine 7-2 and the battery on the airship (or boat) 10 For circuit connection, there are remote control bidirectional switches on the two circuits. The remote control bidirectional switch controls the bidirectional rotary motion of the reciprocating rotary wheel, and the bidirectional rotation of the reciprocating rotary wheel controls the deformation of the kite into the nanoflow state or the unloading state. This determines the change of the tension between the two sides. If the two sides pull the same force, they will hover. If the two sides pull differently, the whole body will move to the side with the strong pull.

On the airship (or boat) 41, or on the cable 29, a communication or television broadcast transceiver, radar equipment, electronic detection equipment, aerial equipment, etc., the overall mechanism becomes a hovering or cruising high-altitude electronic workstation. Since the area of the airship is large enough, solar power generation membranes and plates can be placed on the surface to solve the problem of electrical equipment used on the machine (the following examples can be used).

Embodiment 6 (shown in Figure 67):

It is basically the same as the fifth embodiment except that the positions of the two retractable cables 15 are moved to the upper or both ends of the airship (or lightweight airbag) 10. After this change, the airship (or lightweight airbag) 10 becomes a pod, and as a result, the cabin not only has the original lift as an airship or a lightweight airbag, but also the lift provided by the two kites, so this The structure can carry more weight and can carry more equipment and personnel.

With this feature, airships and lightweight airbags can be replaced by ordinary pods by first bringing the pods and kites to the upper wind with an airship, and launching the kite (umbrella) in the upper wind; then, the airship The pod descends into the lower wind and another kite (umbrella) is placed; then the airship continues to descend slowly with the pod (now paying attention to the tension of the two kites), and after dropping to the appropriate height, the two kites are pulled to the balance. In the process, the pod can be slowly separated from the airship. The advantage of this method is that the airship can be recovered, and an airship can be used to fly many such kite-to-pull suspension mechanisms.

Embodiment 7 (shown in Figure 68):

The two winged aircrafts 42 are respectively placed in a reverse wind group, which are connected by a cable (or connecting rod) 29. Because the wing will generate enough lift in the strong wind at high altitude, it can form a pulling force. If the lift is too large, when it rises to the original wind layer and approaches the excessive wind layer, the wind band slows down. Therefore, the lift will drop and the wing will return to the original wind layer, so there is no need to worry that it will leave the original wind layer, and it can be hovered permanently in the set wind layer. If it can set the remote control elevator, rudder and has the unloading port and its matching A sports organization such as a covered kite can have permanent or hovering capabilities, so it can also be used as a permanent electronic high-altitude station.

Example 8 (shown in Figure 69):

The structure of the pair of flying suspension mechanism is basically the same as that of the seventh embodiment. The difference is that the airship or the pod is replaced by the ship, and the flying task of the kite (umbrella) is carried by the lightweight airbag 41. Each of the kite's motorized cable control machines 7-2 is connected to a lightweight airbag 41. The lift of the lightweight airbag 41 must be sufficient to fly the following three pieces of equipment: a motorized cable control machine 7-2, remote control The kite body and the kite body of the double-knit kit are folded (folded into an umbrella bag). When the lightweight airbag 41 takes them to the respective wind layers, the umbrella bag can be remotely controlled, and the two umbrellas are High winds will naturally fly in the opposite direction and will naturally open after being pulled by the cable 29.

By remotely controlling two reciprocating unloading kite-type motorized cable controllers 7-2, one of the kites can be in the unloading state and the other in the nanoflow state, and the boat will be towed by the side in the nanoflow state. go ahead.

Embodiment 9 (as shown in FIG. 60 and FIG. 61):

On the basis of the second and third cases of the wing ring wind power ship, the two high-altitude wing ring wind power mechanisms 19 of the high-altitude pull-wing ring mechanism are replaced with other types of floating mechanisms (such as kites, airships or light airbags). .

Embodiment 10 (as shown in FIG. 60 and FIG. 61):

On the basis of the second and third cases of the wing-ring wind power ship, the two high-altitude wing-ring wind power mechanisms 19 of the high-altitude pull-wing ring mechanism are replaced with other types of high-altitude wind power mechanisms (such as kites, airships or lightweight airbags). High-altitude wind power mechanism formed by shaft wind turbine generator).

Example 11:

On the basis of the above embodiments of the "wing ring-to-pull suspension mechanism" and the respective "reverse flow group energy development and utilization method embodiments", illumination lamps or advertising lamps and screens are arranged on the periphery of the mechanism (mainly the lower surface). Lighting or advertising fixtures and screens can be placed on the lifting mechanism, the pod, the cable, the connecting rod or the bracket.

This embodiment can be used as a man-made sun over a city, a transportation hub, a port, a dock, a construction site, or a farm where lighting or photosynthesis is required. It can also be a very attractive advertising and publicity channel.

An efficient and environmentally friendly construction method example:

Embodiment 1:

As a high-altitude construction station, a wing-to-pull-winding mechanism or a high-altitude wing-ring wind power mechanism is provided with high-altitude water dispensers and mortar mixers to raise cement and sand into the air, and water produced by high-altitude water dispensers is used in the air. The mortar was stirred on site and the entire layer was perfused.

Embodiment 2:

Use a wing-ring helicopter or a crane-type wing-wing transport aircraft as a high-altitude construction station to lift the prefabricated parts into the air for assembly, or lift the entire relatively small building into the air for assembly, or lift the entire building Ship to other places, or upgrade steel, brick, stone, and decoration materials to the air for construction.

Claims

A wing ring, comprising: an annular bracket and a plurality of fins disposed on the annular bracket, the plurality of fins being equidistantly disposed on the annular bracket, each The fin is connected to the annular bracket, and an angle between one side of each of the fins and a circumferential surface of the annular bracket includes an angle of 0° and an angle of 180° without including 90° Angle and 270° angle.
The wing ring according to claim 1, wherein the plurality of fins extend uniformly toward the outer side of the annular bracket or uniformly protrude to the inner side of the annular bracket, or a part thereof. A portion protrudes from the inner side of the annular holder and a portion projects toward the outer side of the annular holder.
The wing ring of claim 1 wherein said flap is either directly coupled to said annular bracket or coupled to said annular bracket by a blade deflection mechanism.
The wing ring according to claim 1, wherein the fins are all lift-type fins or all non-lift-type fins; or the fins disposed on the inner side of the annular bracket are lift-type a fin, the fin disposed outside the circumference of the annular bracket is a non-lifting fin; or the fin disposed on the inner side of the annular bracket is a non-lifting fin, disposed on the annular bracket The fins on the outer side of the circumference are lift-type fins.
The wing ring of claim 4 further comprising a fuel tank disposed on said airfoil or said annular bracket.
A wing ring according to claim 5, wherein said flank or said annular support is provided with a ramjet.
A wing ring mechanism comprising at least one wing ring according to any one of claims 1 to 6 and a rail coupling body further comprising an annular bracket connected to the wing ring, the rail coupling body being annular The track and the rail car are coupled to each other.
The wing ring mechanism according to claim 7, comprising at least two of said wing rings, which are connected to each other directly by a rail coupling body or connected by a rail coupling body to the same carrier. Each of the wing ring axis lines or all overlap to the same straight line, and each of the wing rings are in the same plane and have the same center but different radii, or are not in the same plane but the planes of the wing rings are parallel to each other The face, or at least two of the axial lines do not overlap each other and are parallel to each other, or at least two of the axial lines form an angle with each other.
The wing ring mechanism according to claim 8, wherein the at least two wing rings have both a clockwise rotating wing ring and a counterclockwise rotating wing ring, and a clockwise rotating wing ring and The total torque produced by the counterclockwise rotating wing ring cancels each other out.
The wing ring mechanism according to claim 9, wherein each of the wing rings and the wing, the kite, the fixed wing aircraft, the lightweight air bag, the airship, the buoy, the floating row, the submarine, the ship, the tower, the tower, One or more connections in the tower and bracket.
A wing ring wind power mechanism comprising the wing ring mechanism of any of claims 7-10 and a power generating winding connected directly or indirectly to an annular bracket of each of the wing ring mechanisms.
The wing ring wind power mechanism according to claim 11, wherein the wing ring wind power mechanism is further connected to the floating mechanism, and the floating mechanism is one or more of a lightweight air bag, a lift type wing or a kite. Kind.
A wing ring wind power mechanism according to claim 11, further comprising a cable and a traction cable, said electric circuit of said power generating winding being connected to an upper end of said cable, said lower end of said cable being connected to said electrical installation; said The upper end of the traction cable is connected to a lower end of the wing ring mechanism that does not rotate with the wing ring, and the lower end of the traction cable is connected to the electrical installation.
A wing-ring aircraft comprising the wing ring mechanism of any of claims 7-10, the wing ring mechanism acting as a propeller mechanism, a spin-wing mechanism or a rotor mechanism of the wing-wing aircraft and coupled to a power mechanism.
A wing-wing aircraft according to claim 14 wherein said power mechanism is an engine or a transmission mechanism that is in power connection with an engine.
A wing-wing aircraft according to claim 14, wherein the fuselage of the wing-wing aircraft is connected to a stationary wing or is connected to the wing by a deflection mechanism or no wing at all.
A wing ring pull-up suspension mechanism includes at least two sets of floating mechanisms, which can be placed in the wind or in a water stream and rely on the traction of the traction cable or the connecting rod to generate a relative movement with the wind or the water flow Having a lifting force for itself, characterized in that each of the lifting mechanisms is a wing ring mechanism according to any one of claims 7 to 10, and the two sets of lifting mechanisms are disposed in two opposite flows or streams And the two sets of floating mechanisms are connected by a cable or by a connecting rod or a bracket.
The wing loop pull-up suspension mechanism of claim 17 wherein each set of lift mechanisms includes at least one lift mechanism.
The wing ring pull-up suspension mechanism according to claim 17, wherein one or more of the sets of the floating mechanism, the cable, the connecting rod or the bracket are connected with a moving mechanism.
A crane type transport machine comprising the wing ring pull-up suspension mechanism and the retractable cable machine according to any one of claims 17-19, wherein an upper end of the cable or connecting rod is connected to the wing ring pull-up flying mechanism The lower end is connected to a pickup device, and the retractable cable machine is disposed on the cable.
A wing-ring wind power ship, the wind-flight mechanism is connected to the ship by a cable, wherein the upper-air mechanism is connected to the upper end of the traction cable, and the ship is connected to the lower end of the traction cable; the high-altitude mechanism is the wing according to any one of claims 7-10. The ring mechanism or any one or more of the wing ring pull-up suspension mechanisms of claim 17.
A reverse flow group energy development and utilization method using the wing ring mechanism of claim 7, comprising the steps of: arranging one or each of two reverse advection or advection waters in a natural reverse wind group or a reverse water flow group; a set of wing ring mechanisms, and the two sets of wing ring mechanisms are connected to each other by a cable or a connecting rod or a bracket, and the two sets of wing ring mechanisms are formed into a pair of flying wings by using two opposite directions of the two air currents or water flows. The mechanism, in order to overcome the falling effect of gravity, achieves long-term hovering, cruising, sailing or power generation without the need to configure the engine.
The method for developing and utilizing a reverse flow group energy source according to claim 22, further comprising: arranging a motion mechanism, wherein the motion mechanism is operated to change a magnitude or a direction of a force received by the motion mechanism, thereby The movement mechanism moves in the horizontal direction or the vertical direction as a whole.
A method for constructing a wing ring mechanism according to claim 7, comprising: using a high-altitude mechanism including the wing ring mechanism as a high-altitude construction station, thereby lifting cement and sand into the air, stirring the mortar in the air and Infusion, or the lifting of the agitated mortar into the air for infusion, or the lifting of the preform into the air for assembly, or the lifting of a relatively small building into the air to assemble a larger building, or Lift steel, brick, stone, and decoration materials to the air for construction, or move the entire building to a preset location.