High-altitude wind energy flight wing rotation flight engine power system and transmission method

Abstract

This invention relates to a high-altitude wind-powered flying wing rotational flight engine power system and transmission method, belonging to the field of high-altitude wind-powered engine technology. The technical solution is as follows: A high-altitude wind-powered flying wing is installed between a high-altitude kite operating platform (8) and a ground platform. The high-altitude wind-powered flying wing includes a rotating base (7), an engine (1), a connecting rod (2), an upper crankshaft (3), an end-face wind turbine (4), an upper frame (5), a lower crankshaft (12), a support arm (13), a rotating shaft (14), and a lower frame (15). The high-altitude wind-powered flying wing is suspended between the high-altitude kite operating platform and the ground platform. High-altitude wind energy blows the wind-powered rotation mechanism, driving the rotating shaft to rotate, and the power is transmitted to the engine through the crankshaft-connecting rod mechanism. The beneficial effects of this invention are: utilizing high-altitude wind energy for long-term continuous operation at high altitudes and generating high-speed rotational power, continuously transmitting power to the wind-powered engine on the ground, it is possible to collect and utilize enormous wind energy.

Description

Technical Field

[0001] This invention relates to a power system and transmission method for a high-altitude wind-powered flying wing rotating around an axis, belonging to the field of high-altitude wind-powered engine technology. Background Technology

[0002] Wind energy is a clean and renewable energy source, and the wind energy contained in the upper atmosphere exceeds 100 times the total energy needs of human society. The characteristics of upper-altitude winds and their energy are: high wind speed, high average energy density, wide geographical distribution, high stability, and continuous supply throughout the year. How to fully utilize upper-altitude wind energy for human benefit has been a hot topic of research for scientists, and its numerous advantages have made it increasingly important to countries around the world.

[0003] The utilization of high-altitude wind energy involves collecting wind energy at high altitudes, converting it into mechanical energy, and finally converting that mechanical energy into electrical energy or other forms of energy. Currently, there are two main methods for generating electricity using high-altitude wind energy: one is to suspend the generator in the air; the other is to place the generator on the ground. High-altitude generator systems are limited by the weight and size of the system, resulting in less effective control and higher power generation. Ground-based systems relying on kites for power generation have the following problems: the kite in a kite-type high-altitude wind power generation system acts as both a balancing body and a working body, and the interplay between these two aspects hinders efficient power generation. Furthermore, the flight and control of the kite, as well as its ability to remain at high altitudes for extended periods, are crucial factors affecting the kite's power output. For example, Chinese patents CN202221696011.4 entitled "A high-altitude wind power ground generator set with series motor" and CN 201721488275.X entitled "A parallel medium-high altitude wind power ground generator set" utilize the power generated by high-altitude kites to transmit power to the ground for electricity generation. Summary of the Invention

[0004] The purpose of this invention is to provide a high-altitude wind-powered flying wing rotating around an axis power engine and a transmission method. The high-altitude wind-powered flying wing is suspended by a kite operation platform at high altitude. The high-altitude wind-powered flying wing rotates around an axis and flies, utilizing the wind energy at high altitude to operate continuously for a long time and generate high-speed rotational power, continuously transmitting the power to the wind-powered engine on the ground, thus solving the above-mentioned technical problems existing in the prior art.

[0005] The technical solution of this invention is: A high-altitude wind-powered flying wing rotational flight engine power system includes a high-altitude kite operating platform, a high-altitude wind-powered flying wing, and a ground platform. The ground platform includes a circular track, ropes, and sliders. The circular track is located on the ground, and the high-altitude kite operating platform is located at high altitude. Multiple sliders are installed on the circular track, and the high-altitude kite operating platform is connected to the sliders via multiple ropes. The sliders slide on the circular track without detaching from it. The high-altitude wind-powered flying wing is installed between the high-altitude kite operating platform and the ground platform. The high-altitude wind-powered flying wing includes a rotating base, an engine, connecting rods, an upper crankshaft, an end-face wind turbine, an upper frame, a lower crankshaft, support arms, a rotating shaft, and a lower frame. The rotating base is located at the center of the circular track. A lower frame is mounted on a rotating base, and an engine is installed on the lower frame. An upper frame is located above the lower frame and is connected to the high-altitude kite operating platform via a suspension rope. The upper frame is suspended below the high-altitude kite operating platform. A rotating shaft is provided on the upper frame, and a support arm is vertically mounted at the end of the rotating shaft. An end face wind wheel is mounted at the end of the support arm. The rotating shaft, support arm, and end face wind wheel together constitute a wind-powered rotation mechanism. The rotating shaft is connected to the upper end of a connecting rod via an upper crankshaft, and the lower end of the connecting rod is connected to the input shaft of the engine via a lower crankshaft. The high-altitude wind-powered flying wing is suspended between the high-altitude kite operating platform and the ground platform. The high-altitude wind energy blows the wind-powered rotation mechanism, which drives the rotating shaft to rotate. The power is transmitted to the engine through the crankshaft and connecting rod mechanism.

[0006] The rotating shaft is equipped with three sets of crankshaft connecting rod mechanisms that are connected to multiple engines respectively. The angle difference between the three sets of crankshafts is 120 degrees, and the upper and lower crankshafts of each set of crankshafts have completely consistent angles.

[0007] A height control rope is installed between the upper frame and the lower frame.

[0008] The upper frame and the slider are connected by positioning ropes to position the high-altitude wind-powered flight wing.

[0009] There are multiple engines, each connected to a rotating shaft via a crankshaft connecting rod mechanism. The number of support arms and end face wind turbines is multiple.

[0010] The high-altitude kite operating platform is composed of multiple parallel wind tunnels arranged together. Each wind tunnel is a long cylindrical shape with open ends, made of flexible material. Adjacent wind tunnels are connected by connectors to form the high-altitude kite operating platform. The central axis of the wind tunnel is parallel to the ground or has an angle. The larger the wind angle, the larger the angle between the central axis of the wind tunnel and the ground. The higher the wind speed at high altitude, the closer the central axis of the wind tunnel is to being parallel to the ground.

[0011] A method for transmitting power to a high-altitude wind-powered flying wing rotating around an axis and an engine is disclosed. The high-altitude wind-powered flying wing is suspended between a high-altitude kite operating platform and a ground platform. The wind-powered rotating mechanism driven by the high-altitude wind drives the rotating shaft to rotate, and the power is transmitted to the engine through a crankshaft connecting rod mechanism.

[0012] The high-altitude wind-powered flying wing suspended at high altitude is locked to the ground platform using positioning ropes to prevent the high-altitude kite operation platform from lifting the equipment to an infinite altitude.

[0013] The slider is equipped with a railcar, and the high-altitude wind-powered kite operation platform is controlled by the railcar on the circular track.

[0014] The beneficial effects of this invention are as follows: A high-altitude wind-powered flying wing is suspended on a high-altitude kite operation platform. The high-altitude wind-powered flying wing rotates around an axis and flies, utilizing the wind energy at high altitudes to operate continuously for a long time and generate high-speed rotational power. This power is continuously transmitted to the wind-powered engine on the ground, allowing for the collection and utilization of enormous wind energy. Attached Figure Description

[0015] Figure 1 This is a schematic diagram illustrating the usage state of an embodiment of the present invention; Figure 2 This is a schematic diagram of a high-altitude wind-powered flying wing according to an embodiment of the present invention; Figure 3 This is a side view schematic diagram of a high-altitude wind-powered flight wing according to an embodiment of the present invention; Figure 4 This is a top-view schematic diagram of a high-altitude wind-powered flying wing according to an embodiment of the present invention; Figure 5 This is a three-dimensional schematic diagram of a high-altitude wind-powered flying wing according to an embodiment of the present invention; Figure 6 This is a schematic diagram of the crankshaft of a high-altitude wind-powered flying wing according to an embodiment of the present invention; In the diagram: 1. Engine; 2. Connecting rod; 3. Upper crankshaft; 4. End face impeller; 5. Upper frame; 6. Height control rope; 7. Rotating base; 8. High-altitude kite operation platform; 9. Circular track; 10. Rope; 11. Slider; 12. Lower crankshaft; 13. Support arm; 14. Rotating shaft; 15. Lower frame; 16. Suspension rope; 17. Positioning rope. Detailed Implementation

[0016] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0017] A high-altitude wind-powered flying wing rotational flight engine power system includes a high-altitude kite operating platform 8, a high-altitude wind-powered flying wing, and a ground platform. The ground platform includes a circular track 9, ropes 10, and sliders 11. The circular track 9 is located on the ground, and the high-altitude kite operating platform 8 is located at high altitude. Multiple sliders 11 are arranged on the circular track 9, and the high-altitude kite operating platform 8 is connected to the sliders 11 by multiple ropes 10. The sliders 11 slide on the circular track 9 without detaching from it. A high-altitude wind-powered flying wing is arranged between the high-altitude kite operating platform 8 and the ground platform. The high-altitude wind-powered flying wing includes a rotating base 7, an engine 1, a connecting rod 2, an upper crankshaft 3, an end face wind turbine 4, an upper frame 5, a lower crankshaft 12, a support arm 13, a rotating shaft 14, and a lower frame 15. The rotating base 7 is located at the center of the circular track 9. A lower frame 15 is mounted on the base 7, and an engine 1 is installed on the lower frame 15. An upper frame 5 is mounted above the lower frame 15 and is connected to the high-altitude kite operating platform 8 via a suspension rope 16. The upper frame 5 is suspended below the high-altitude kite operating platform 8. A rotating shaft 14 is mounted on the upper frame 5, and a support arm 13 is vertically mounted at the end of the rotating shaft 14. An end face wind wheel 4 is mounted at the end of the support arm 13. The rotating shaft 14, the support arm 13, and the end face wind wheel 4 together constitute a wind-powered rotation mechanism. The rotating shaft 14 is connected to the upper end of the connecting rod 2 via an upper crankshaft 3, and the lower end of the connecting rod 2 is connected to the input shaft of the engine 1 via a lower crankshaft 12. The high-altitude wind-powered flying wing is suspended between the high-altitude kite operating platform 8 and the ground platform. The high-altitude wind energy blows the wind-powered rotation mechanism, which drives the rotating shaft 14 to rotate. The power is transmitted to the engine through the crankshaft and connecting rod mechanism.

[0018] The rotating shaft is equipped with three sets of crankshaft connecting rod mechanisms that are connected to multiple engines respectively. The angle difference between the three sets of crankshafts is 120 degrees, and the upper and lower crankshafts of each set of crankshafts have completely consistent angles.

[0019] A height control rope 6 is installed between the upper frame 5 and the lower frame 15.

[0020] The upper frame 5 and the slider 11 are connected by a positioning rope 17 to position the high-altitude wind-powered flying wing.

[0021] There are multiple engines 1, each connected to the rotating shaft 14 via a crankshaft connecting rod mechanism. The number of the support arm 13 and the end face wind turbine 4 is multiple.

[0022] The high-altitude kite operating platform 8 is composed of multiple parallel wind ducts arranged together. Each wind duct is a long cylindrical shape with open ends, made of flexible material. Adjacent wind ducts are connected by connectors to form the high-altitude kite operating platform 8. The central axis of the wind duct is parallel to the ground or has an angle. The larger the wind angle, the larger the angle between the central axis of the wind duct and the ground. The higher the wind speed at high altitude, the closer the central axis of the wind duct is to being parallel to the ground.

[0023] A method for transmitting power to a high-altitude wind-powered flying wing rotating around an axis and an engine is disclosed. The high-altitude wind-powered flying wing is suspended between a high-altitude kite operation platform 8 and a ground platform. The wind-powered rotating mechanism driven by the high-altitude wind drives the rotating shaft 14 to rotate, and the power is transmitted to the engine through a crankshaft connecting rod mechanism.

[0024] The high-altitude wind-powered flying wing suspended at high altitude is locked to the ground platform using positioning rope 17 to prevent the high-altitude kite operation platform 8 from lifting the equipment to an infinite altitude.

[0025] The slider is equipped with a railcar, and the high-altitude wind-powered kite operation platform is controlled by the railcar on the circular track.

[0026] In this embodiment, all the equipment of the high-altitude wind-powered flying wing is mounted on this disc-shaped rotating base 7. The high-altitude wind-powered flying wing is suspended in the air by the high-altitude kite-operated platform 8. The high-altitude kite-operated platform is a type of integrated array of high-altitude wind tunnels. It can be combined according to the required lift, possessing enormous lift and capable of remaining stably in the air for extended periods. The platform is controlled 360 degrees via ropes (kite line winches) on multiple railcars on a giant circular track on the ground.

[0027] Specific implementation process: The high-altitude kite operation platform is towed and launched by a railcar on a circular track on the ground. The high-altitude kite operation platform and the suspended high-altitude wind-powered flying wings are launched and suspended at high altitude for an extended period. The high-altitude wind-powered flying wings are launched one by one in sequence and suspended at a designated height. The four corners are secured by positioning ropes 17 to lock the high-altitude wind-powered flying wings in place, preventing them from being pulled to an unlimited height by the enormous lift of the high-altitude kite operation platform. The height control rope 6 is adjusted to the appropriate length.

[0028] All equipment in this invention is launched and controlled via a circular track and rope traction vehicle on a high-altitude kite operating platform. All information in the air is collected and stored wirelessly by various instruments on the platform, including: a climb rate gauge, altimeter, horizon marker, magnetic compass, gyroscope, wind turbine tachometer, ammeter, and voltmeter. Various sensors are used, including altitude sensors, wind direction, wind speed, and wind pressure sensors at different altitudes, temperature and humidity sensors, air density sensors, ultraviolet radiation sensors, and tension sensors at various points. Real-time monitoring of all equipment in the air is achieved through various monitoring and remote control transmission devices at different locations.

[0029] All the electrical equipment and sensors that require power at high altitudes are powered by high-altitude solar power generation equipment, and there are sufficient installation locations on the high-altitude kite operation platform.

[0030] In this embodiment, three sets of crankshaft connecting rod mechanisms are set on the rotating shaft and connected to multiple engines below. The angle difference between the three sets of crankshafts is 120 degrees. The distance between the three crankshafts should be as large as possible in order to prevent the ropes connecting the crankshafts at high altitude and on the ground from interfering with each other under the action of wind. The angles corresponding to the upper crankshaft and the lower crankshaft are completely consistent.

[0031] All adjustments to the aerial operation in this invention can be made via a wireless remote control system. All parts of the high-altitude ropes that require adjustment must be equipped with a wireless remote control adjustment system, and adjustments can be made wirelessly as needed.

Claims

1. A high-altitude wind-powered wing-rotating engine propulsion system, characterized in that: The system includes a high-altitude kite operation platform (8), a high-altitude wind-powered flight wing, and a ground platform. The ground platform includes a circular track (9), ropes (10), and sliders (11). The circular track (9) is set on the ground, and the high-altitude kite operation platform (8) is set at high altitude. Multiple sliders (11) are set on the circular track (9). The high-altitude kite operation platform (8) is connected to the sliders (11) by multiple ropes (10). The sliders (11) slide on the circular track (9) and do not leave the circular track (9). A high-altitude wind-powered flight wing is set between the high-altitude kite operation platform (8) and the ground platform. The high-altitude wind-powered flight wing includes a rotating base (7), an engine (1), a connecting rod (2), an upper crankshaft (3), an end face wind turbine (4), an upper frame (5), a lower crankshaft (12), a support arm (13), a rotating shaft (14), and a lower frame (15). The rotating base (7) is set at the center of the circular track (9), and the lower frame (15) is set on the rotating base (7). 5) An engine (1) is installed on the lower frame (15). An upper frame (5) is set above the lower frame (15). The upper frame (5) is connected to the high-altitude kite operating platform (8) by a suspension rope (16). The upper frame (5) is suspended below the high-altitude kite operating platform (8). A rotating shaft (14) is provided on the upper frame (5). A support arm (13) is vertically set at the end of the rotating shaft (14). An end face wind wheel (4) is set at the end of the support arm (13). The rotating shaft (14) The support arm (13) and the end face wind wheel (4) together constitute the wind power rotation mechanism; the rotating shaft (14) is connected to the upper end of the connecting rod (2) through the upper crankshaft (3), and the lower end of the connecting rod (2) is connected to the input shaft of the engine (1) through the lower crankshaft (12); the high-altitude wind energy flying wing is suspended between the high-altitude kite operation platform (8) and the ground platform. The high-altitude wind energy blows the wind power rotation mechanism to drive the rotating shaft (14) to rotate, and transmits power to the engine through the crankshaft connecting rod mechanism.

2. The high-altitude wind-powered wing-rotating engine power system according to claim 1, characterized in that: The rotating shaft is equipped with three sets of crankshaft connecting rod mechanisms that are connected to multiple engines respectively. The angle difference between the three sets of crankshafts is 120 degrees, and the upper and lower crankshafts of each set of crankshafts have completely consistent angles.

3. A high-altitude wind-powered wing-rotating engine propulsion system according to claim 1 or 2, characterized in that: A height control rope (6) is installed between the upper frame (5) and the lower frame (15).

4. A high-altitude wind-powered wing-rotating engine propulsion system according to claim 1 or 2, characterized in that: The upper frame (5) and the slider (11) are connected by a positioning rope (17).

5. A method for transmitting power to a high-altitude wind-powered wing-rotating engine, employing the high-altitude wind-powered wing-rotating engine power system as described in any one of claims 1-4, characterized in that: The high-altitude wind-powered flying wing is suspended between the high-altitude kite operation platform (8) and the ground platform. The high-altitude wind power blows the wind-powered rotating mechanism to drive the rotating shaft (14) to rotate, and the power is transmitted to the engine through the crankshaft connecting rod mechanism.

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