Emergency rescue high-altitude cabin provided with wind excitation lift force equipment

Abstract

The invention relates to an emergency rescue high-altitude cabin provided with wind excitation lift force equipment, belongs to the technical field of emergency rescue equipment, and solves the problems that a high-altitude cabin in the prior art generally depends on external energy to maintain buoyancy and stability and may face insufficient energy or supply interruption in an emergency. The emergency rescue high-altitude cabin provided with the wind-excited lift force equipment comprises a high-altitude cabin body, the wind excitation lift force equipment comprises a shaft body, a wind cup stress mechanism is arranged at the top of the shaft body, and a paddle power mechanism is arranged at the bottom of the shaft body; and the inhaul cable connecting mechanism is configured to connect the wind-excited lift force equipment to a high-altitude cabin. According to the high-altitude cabin, stable buoyancy and lift force are achieved through natural wind power, and self-adaptive stability and high efficiency of the high-altitude cabin in emergency rescue are achieved.

Description

Technical Field

[0001] The present application belongs to the technical field of emergency rescue equipment, and specifically relates to an emergency rescue high-altitude cabin equipped with a wind-driven lifting device. Background Art

[0002] During high-altitude operations and rescues, the high-altitude cabin is an important equipment that can provide a safe and stable platform. However, existing high-altitude cabins generally rely on external energy to maintain buoyancy and stability. Due to the high dependence of existing high-altitude cabins on external energy, energy shortages or supply interruptions may occur in emergency situations such as harsh environments, making it difficult to ensure stability and requiring high maintenance complexity.

[0003] Therefore, there is an urgent need to provide an emergency rescue high-altitude cabin that does not require external energy and relies on natural wind to provide lift and stability. Summary of the invention

[0004] In view of the above analysis, an embodiment of the present invention aims to provide an emergency rescue high-altitude cabin equipped with a wind-driven lift device, so as to solve the problem that high-altitude cabins in the prior art generally rely on external energy to maintain buoyancy and stability, and may face energy shortages or supply interruptions in emergency situations.

[0005] The object of the present invention is achieved in that: An emergency rescue high altitude cabin provided with a wind-excited lifting device, comprising: A high altitude cabin having a cabin body; A wind-excited lift device, the wind-excited lift device comprising a shaft, a wind cup force mechanism is provided on the top of the shaft, and a blade power mechanism is provided on the bottom of the shaft; The cable connection mechanism is configured to connect the wind-excited lift device to the high-altitude cabin.

[0006] Furthermore, a bearing is provided on the shaft body, and the cable connection mechanism is connected to the bearing; the bearing includes an upper bearing and a lower bearing, the upper bearing is located above the high-altitude cabin, and the lower bearing is located below the high-altitude cabin.

[0007] Furthermore, a wind-excited lift device is arranged at the center of the cabin.

[0008] Furthermore, the cable connection mechanism includes an upper cable and a lower cable, the first end of the upper cable is connected to the upper bearing, the first end of the lower cable is connected to the lower bearing, and the second end of the upper cable and the second end of the lower cable are evenly connected to the cabin.

[0009] Furthermore, the first end of the upper cable is hinged to the outer ring of the upper bearing, and the first end of the lower cable is hinged to the outer ring of the lower bearing; a plurality of fixing rings are evenly arranged on the cabin body, and the second end of the upper cable and the second end of the lower cable are both hinged to the fixing rings.

[0010] Furthermore, a plurality of wind-induced lift devices are evenly arranged on the periphery of the cabin.

[0011] Furthermore, the shafts of the plurality of wind-excited lift devices are parallel to the axis of the cabin and are symmetrically arranged.

[0012] Furthermore, the cable connection mechanism includes an upper support rod, a lower support rod, an upper transverse cable and a lower transverse cable, and the shaft body is connected to the cabin body through the upper support rod and the lower support rod; wherein, the upper support rod and the lower support rod are rigid rods, the first end of the upper support rod is connected to the upper bearing, and the first end of the lower support rod is connected to the lower bearing; the two ends of the upper transverse cable are connected to two adjacent upper bearings, and the two ends of the lower transverse cable are connected to two adjacent lower bearings.

[0013] Furthermore, the wind cup force bearing mechanism includes a plurality of wind cups, and the plurality of wind cups are evenly distributed on the top of the shaft.

[0014] Furthermore, a transmission device is provided between the wind cup force bearing mechanism and the blade power mechanism.

[0015] Furthermore, the transmission device adopts a differential, and the differential is arranged in the middle of the shaft body.

[0016] Compared with the prior art, the present invention can achieve at least one of the following beneficial effects: a) The emergency rescue high-altitude cabin provided with a wind-excited lift device provided by the present invention does not require external energy supply and completely relies on natural wind power to provide stable lift and buoyancy. It is suitable for emergency rescue scenarios that cannot rely on external energy, thereby providing stable and efficient high-altitude rescue services in emergency rescue.

[0017] b) The emergency rescue high-altitude cabin provided by the present invention with a wind-driven lifting device does not require additional power equipment, has a simple structure, is easy to maintain, does not need to consider the endurance problem, and has broad application prospects.

[0018] c) The emergency rescue high-altitude cabin provided by the present invention with a wind-driven lifting device is connected by cables and bearings to ensure the stability and flexibility of the overall structure.

[0019] d) The emergency rescue high-altitude cabin provided by the present invention is provided with a wind-excited lifting device. The modular design of the wind-excited lifting device enables it to be flexibly configured according to the specific use environment, further enhancing the adaptability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the embodiments of this specification or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the embodiments of this specification. For ordinary technicians in this field, other drawings can also be obtained based on these drawings.

[0021] Figure 1 A schematic diagram of the first angle structure of the first emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention; Figure 2 A second angle structural schematic diagram of the first emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention; Figure 3 A schematic structural diagram of the connection between the cable connection mechanism and the shaft body of the first emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention; Figure 4 A schematic diagram of the first angle structure of a second emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention; Figure 5 A second angle structural schematic diagram of a second emergency rescue high altitude cabin provided with a wind-excited lifting device provided by the present invention; Figure 6 A schematic diagram of the structure of a wind-excited lifting device for a second emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention Figure 1 ; Figure 7 for Figure 6 A partial enlarged view of the middle A area; Figure 8 A schematic structural diagram of another wind-excited lift device provided by the present invention.

[0022] Reference numerals: 1. Cabin body; 1-1. Fixing ring; 2. Wind-excited lift device; 2-1. Shaft body; 2-11. Upper shaft; 2-12. Lower shaft; 2-2. Wind cup force mechanism; 2-3. Blade power mechanism; 2-4. Upper bearing; 2-41. Upper ear plate; 2-5. Lower bearing; 2-51. Lower ear plate; 2-6. Differential; 3. Cable connection mechanism; 3-1. Upper cable; 3-2. Lower cable; 3-3. Upper support rod; 3-4. Lower support rod; 3-5. Upper transverse cable; 3-6. Lower transverse cable. DETAILED DESCRIPTION

[0023] In order to make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme in the embodiments of the present application will be clearly and completely described in combination with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all of the embodiments. It should be noted that, in the absence of conflict, the embodiments in the present disclosure and the features in the embodiments can be combined, separated, interchanged and / or rearranged with each other. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of this application.

[0024] In the accompanying drawings, the size and relative size of components may be exaggerated for clarity and / or descriptive purposes. When the exemplary embodiments may be implemented differently, a specific process sequence may be performed in a different order than described. For example, two successively described processes may be performed substantially simultaneously or in an order opposite to the order described. In addition, the same reference numerals represent the same components.

[0025] The terms used here are for the purpose of describing specific embodiments, and are not intended to be restrictive. As used here, unless the context clearly indicates otherwise, the singular forms "one (kind, person)" and "said (the)" are also intended to include plural forms. In addition, when the terms "comprise" and / or "include" and their variations are used in this specification, it is explained that there are stated features, integral bodies, steps, operations, parts, assemblies and / or their groups, but it is not excluded that there are or add one or more other features, integral bodies, steps, operations, parts, assemblies and / or their groups. It should also be noted that, as used here, the terms "substantially", "approximately" and other similar terms are used as approximate terms and not as degree terms, so that they are used to explain the inherent deviations of the measured values, calculated values ​​and / or the values ​​provided that will be recognized by those of ordinary skill in the art.

[0026] Example 1 A specific embodiment of the present invention, as Figures 1 to 7 As shown, an emergency rescue high-altitude cabin equipped with a wind-excited lifting device is disclosed, which may be referred to as the "emergency rescue high-altitude cabin" hereinafter. The emergency rescue high-altitude cabin includes: A high-altitude cabin, the high-altitude cabin is a ring-shaped structure, and the high-altitude cabin has a cabin body 1, and the interior of the cabin body 1 is filled with a light gas with a density lower than that of air to ensure buoyancy and stability, for example, the light gas is helium; A wind-excited lift device 2, wherein the wind-excited lift device 2 comprises a shaft 2-1, a wind cup force mechanism 2-2 is provided at the top of the shaft 2-1, and a blade power mechanism 2-3 is provided at the bottom of the shaft 2-1; The cable connection mechanism 3 is configured to connect the wind-excited lift device 2 to the high-altitude cabin.

[0027] In this embodiment, the wind-excited lift device 2 and the high-altitude cabin adopt a modular design, which is convenient for quick disassembly and maintenance. The emergency rescue high-altitude cabin can be equipped with one wind-excited lift device 2 or multiple wind-excited lift devices 2 to adapt to different use environments and conditions. Among them, the height of the shaft 2-1 of the wind-excited lift device 2 is greater than the axial height of the high-altitude cabin, so that the wind cup force mechanism 2-2 and the blade power mechanism 2-3 are located on the upper and lower sides of the high-altitude cabin.

[0028] like Figure 1 to Figure 2 As shown, in the technical solution of setting a wind-excited lift device 2 at the center of the cabin 1, the wind-excited lift device 2 is installed at the center of the high-altitude cabin, and the shaft 2-1 of the wind-excited lift device 2 coincides with the axis of the high-altitude cabin.

[0029] like Figures 4 to 5 As shown, in the technical solution of arranging multiple wind-excited lifting devices 2 on the periphery of the cabin 1, the multiple wind-excited lifting devices 2 are evenly arranged on the outside of the high-altitude cabin, and the shafts 2-1 of the multiple wind-excited lifting devices 2 are parallel to the axis of the high-altitude cabin, and are symmetrically arranged. Exemplarily, four wind-excited lifting devices 2 are evenly distributed around the high-altitude cabin, the shafts 2-1 of the four wind-excited lifting devices 2 are parallel and located on the four edges of the same rectangular parallelepiped, and the shafts 2-1 of the four wind-excited lifting devices 2 are symmetrically distributed around the axis of the high-altitude cabin.

[0030] In order to ensure structural stability and flexibility, a bearing is provided on the shaft 2-1 of the wind-excited lift device 2, and the cable connection mechanism 3 is connected to the bearing. An upper bearing 2-4 and a lower bearing 2-5 are provided on the shaft 2-1. The upper bearing 2-4 is located above the high-altitude cabin, and the lower bearing 2-5 is located below the high-altitude cabin.

[0031] In the technical solution of setting a wind-excited lift device 2 at the center of the cabin 1, the cable connection mechanism 3 includes an upper cable 3-1 and a lower cable 3-2, the shaft 2-1 of the wind-excited lift device 2 is set at the center of the high-altitude cabin, the shaft 2-1 is connected to the high-altitude cabin through the upper cable 3-1 and the lower cable 3-2, the upper cable 3-1 and the lower cable 3-2 are arranged obliquely, the first end of the upper cable 3-1 is connected to the upper bearing 2-4, the first end of the lower cable 3-2 is connected to the lower bearing 2-5, and the second end of the upper cable 3-1 and the second end of the lower cable 3-2 are evenly connected to the cabin 1. Further, the first end of the upper cable 3-1 is hinged to the outer ring of the upper bearing 2-4, and the first end of the lower cable 3-2 is hinged to the outer ring of the lower bearing 2-5; a plurality of fixing rings 1-1 are also evenly arranged on the cabin 1 of the high-altitude cabin, and the second end of the upper cable 3-1 and the second end of the lower cable 3-2 are both hinged to the fixing ring 1-1. Optionally, the fixing ring 1-1 can be made of the material of a safety belt. By adding a flexible fixing ring 1-1 to the main body of the high-altitude cabin, it is easy to connect with the main body of the high-altitude cabin, which is convenient for processing. The safety belt has high strength and light weight, and is guaranteed in terms of structural safety. In the technical solution of arranging multiple wind-excited lifting devices 2 on the periphery of the cabin body 1, the cable connection mechanism 3 includes an upper support rod 3-3, a lower support rod 3-4, an upper transverse cable 3-5 and a lower transverse cable 3-6. The shaft 2-1 of the wind-excited lifting device 2 is connected to the high-altitude cabin through the upper support rod 3-3 and the lower support rod 3-4. The upper support rod 3-3 and the lower support rod 3-4 are rigid rods. The upper support rod 3-3 and the lower support rod 3-4 are arranged obliquely. The first end of the upper support rod 3-3 is connected to the upper bearing 2-4, and the first end of the lower support rod 3-4 is connected to the lower bearing 2-5. The upper transverse cable 3-5 is connected to the upper part of two adjacent shaft bodies 2-1, the lower transverse cable 3-6 is connected to the lower part of two adjacent shaft bodies 2-1, and both ends of the upper transverse cable 3-5 are connected to two adjacent upper bearings 2-4, and both ends of the lower transverse cable 3-6 are connected to two adjacent lower bearings 2-5.

[0032] In one of the optional embodiments, a plurality of ear plates are provided on the outer ring of the upper bearing 2-4 and the outer ring of the lower bearing 2-5, and the plurality of ear plates are evenly arranged on the side walls of the outer rings of the bearings. Specifically, a plurality of upper ear plates 2-41 are provided on the outer ring of the upper bearing 2-4, and a plurality of lower ear plates 2-51 are provided on the outer ring of the lower bearing 2-5. In the technical solution of setting a wind-excited lift device 2 at the center of the cabin 1, the second end of the upper cable 3-1 and the second end of the lower cable 3-2 are both hinged to the ear plates on the corresponding bearings, that is, the second end of the upper cable 3-1 is hinged to the upper ear plate 2-41 on the upper bearing 2-4, and the second end of the lower cable 3-2 is hinged to the lower ear plate 2-51 on the lower bearing 2-5; in the technical solution of setting multiple wind-excited lift devices 2 on the periphery of the cabin 1, the second end of the upper support rod 3-3 and the two ends of the upper transverse cable 3-5 are both hinged to the upper ear plate 2-41 on the outer ring of the upper bearing 2-4; the second end of the lower support rod 3-4 and the two ends of the lower transverse cable 3-6 are both hinged to the lower ear plate 2-51 on the outer ring of the lower bearing 2-5. Among them, the connection method at the ear plate is pin connection.

[0033] In one of the optional embodiments, the emergency rescue high-altitude cabin with built-in wind-excited lift equipment 2 also includes an adaptive control system. The adaptive control system includes sensors for high-altitude environment monitoring. The sensors are arranged on the wind cup force-bearing mechanism. The type and number of sensors are set according to needs. The sensors can capture parameters including wind speed, wind direction, air pressure, humidity, temperature, etc. The posture and position of the high-altitude cabin are monitored in real time through sensors according to changes in wind speed and wind direction. The data obtained by the sensors are judged and the angles of the wind cups and blades are automatically adjusted to ensure the stability of the high-altitude cabin. The sensors can be set at the upper bearings 2-4. The adaptive control system automatically adjusts the tension of the mooring rope in the corresponding direction through data such as wind force and direction sensed by the sensors, so that the cabin 1 as a whole maintains a relatively balanced state. In one optional embodiment, the emergency rescue high-altitude cabin with built-in wind-excited lift device 2 also includes an emergency brake device, which quickly stops the rotation of the wind cup and the blade in an emergency by mechanical or electronic means to ensure the safety of the high-altitude cabin. Specifically, the brake device is installed at the bearing. The braking device requires manual control, such as manual braking at a ground station when the mooring device fails or the attitude of the high-altitude cabin is out of control.

[0034] In this embodiment, the manufacturing process of the high-altitude cabin needs to be tested for air tightness to ensure that the light gas filled inside the high-altitude cabin will not leak, and helium is used to ensure sufficient buoyancy. All externally exposed parts of the emergency rescue high-altitude cabin, such as the outer shell material of the cabin 1 of the high-altitude cabin, are made of weather-resistant materials, with anti-ultraviolet coating and anti-corrosion treatment to improve the durability and environmental resistance of the equipment. In order to ensure that the emergency high-altitude cabin can operate normally at extreme temperatures, low-temperature lubricants and high-temperature resistant materials are used at the hinged parts of the equipment to ensure normal operation under various climatic conditions.

[0035] In this embodiment, the cup force mechanism 2-2 at the top of the shaft 2-1 rotates by capturing high-altitude wind force, driving the blade power mechanism 2-3 at the bottom to rotate. Each cup force mechanism 2-2 includes multiple cups, and multiple cups are evenly distributed on the top of the shaft 2-1 to maximize the capture of wind force. For example, three cups are connected to the top of the shaft 2-1 as a whole. The blade power mechanism 2-3 located at the bottom of the shaft 2-1 is provided with multiple blades, and the multiple blades are evenly distributed. The blades rotate synchronously when the cup force mechanism 2-2 rotates to provide lift. Among them, the blades are made of high-strength lightweight materials to improve durability and efficiency. The shaft 2-1 is made of high-strength alloy material to ensure stability under high loads.

[0036] In one of the optional embodiments, a transmission device is provided between the cup force mechanism 2-2 and the blade power mechanism 2-3, and the transmission device may be a differential 2-6. The cup force mechanism 2-2 at the top of the shaft 2-1 rotates by capturing the high-altitude wind force, and increases the rotation speed through the differential 2-6, thereby driving the blade power mechanism 2-3 at the bottom to rotate and provide additional lift. The differential 2-6 is provided in the middle of the shaft 2-1, and the differential 2-6 is located at the midpoint between the cup force mechanism 2-2 and the blade power mechanism 2-3. Specifically, as Figure 8 As shown, the shaft body 2-1 includes an upper shaft rod 2-11 and a lower shaft rod 2-12, the upper end of the upper shaft rod 2-11 is connected to the wind cup force mechanism 2-2, the lower end of the lower shaft rod 2-12 is connected to the blade power mechanism 2-3, and the lower end of the upper shaft rod 2-11 is connected to the upper end of the lower shaft rod 2-12 through a differential 2-6. The differential 2-6 includes a gear set and matching parts, which can realize the rotation speed adjustment of the upper shaft rod 2-11 and the lower shaft rod 2-12. When the wind cup force mechanism 2-2 rotates under the influence of wind force, it is accelerated through the differential 2-6, so that the rotation speed of the blade power mechanism 2-3 is higher than the rotation speed of the wind cup force mechanism 2-2, so that the lift provided is enhanced.

[0037] When the diameter of the main cabin is relatively small, only one set of wind-excited lift equipment 2 can be set at the center. The ear plates on the outer ring of the upper bearing 2-4 and the outer ring of the lower bearing 2-5 are connected to the cabin 1 through the upper cable 3-1 and the lower cable 3-2 to form a spoke-type tension structure; the spoke-type structure can evenly disperse the force, improve the stability and bearing capacity of the structure, and reduce the use of materials to achieve the purpose of lightweight and cost saving. In addition, the spoke-type design also shows convenience in maintenance and expansion. It is not only easy to locate and repair faults, but also supports easy expansion of the system, while being beautiful and flexible.

[0038] When the diameter of the main cabin is large, multiple wind-excited lift devices 2 are arranged around the main cabin. At this time, the ear plates on the outer ring of the upper bearing 2-4 and the outer ring of the lower bearing 2-5 are not only connected to the upper support rod 3-3 and the lower support rod 3-4, but also can be connected to the shaft body 2-1 of two adjacent wind-excited lift devices 2 through the flexible upper transverse cable 3-5 and the lower transverse cable 3-6 to form an overall tensioning structure to ensure the stability of the overall structural strength after installing multiple wind-excited lift devices 2. That is to say, in the technical solution of setting up multiple wind-excited lift devices 2, the upper bearing 2-4 and the lower bearing 2-5 of two adjacent shaft bodies 2-1 are connected to the upper bearing 2-4 and the lower bearing 2-5 on the adjacent shaft body 2-1 through the flexible upper transverse cable 3-5 and the lower transverse cable 3-6, respectively, to form a laterally stable force-bearing structure, and the upper bearing 2-4 and the lower bearing 2-5 on each shaft body 2-1 are connected to the cabin 1 through a rigid support rod, and there are two rigid support rods at each bearing. The rigid support is mainly used for compression, and the flexible upper transverse cable 3-5 and the lower transverse cable 3-6 are mainly tensile after forming. The two work together to form an overall tensioning structure to ensure the stability of the overall structure. The prestress ensures the stability of the structure, and it can maintain a good shape even under dynamic loads. This structural design is flexible and can present a variety of geometric shapes. It is both economical and environmentally friendly, and often has detachability.

[0039] Table 1 gives the relevant parameter combinations of the emergency high-altitude cabin's lift altitude, cabin outer diameter, number of wind-excited lift devices, and single blade diameter.

[0040] Table 1 Compared with the prior art, the emergency rescue high-altitude cabin provided with a wind-excited lifting device provided in this embodiment has the following beneficial effects: Energy self-sufficiency: The high-altitude cabin does not require external energy supply and relies entirely on natural wind power to provide lift and buoyancy. The wind cup force mechanism captures the high-altitude wind and drives the blade power mechanism to rotate synchronously, thereby providing the necessary lift for the high-altitude cabin. This design eliminates dependence on external energy such as electricity or fuel, ensuring normal operation in any emergency situation.

[0041] Adaptive stability: The adaptive control system monitors the attitude and position of the high-altitude cabin in real time through sensors, automatically adjusts the length of the mooring ropes, and balances the tension of each mooring rope to ensure the stability of the high-altitude cabin under various wind conditions. Even in severe weather conditions, the high-altitude cabin can remain stable, providing a safe and reliable platform for rescue operations.

[0042] Structural flexibility and adaptability: The modular design allows the wind-excited lift equipment to be flexibly configured according to different usage environments and conditions. Users can choose to install the equipment in the center or around the periphery of the high-altitude cabin to suit specific operating requirements. This modular design also simplifies the installation, removal and maintenance process of the equipment, improving ease of use and operational flexibility.

[0043] Easy maintenance: All external exposed parts are made of weather-resistant materials, such as UV-resistant coatings and anti-corrosion materials, which greatly extends the service life of the equipment and reduces maintenance frequency and costs. The modular design also facilitates the rapid replacement and maintenance of components, further reducing operating costs.

[0044] High safety: The emergency brake device is designed to achieve braking in an emergency by setting an electronic brake in the bearing. This brake includes a spring, a friction plate, a brake disc, and a caliper. This device has low power consumption and only needs to be switched on and off by a button battery. The spring in the brake system is located at the center of the brake system. Its function is to maintain a sufficient gap between the brake disc and the friction plate when the brake is not activated to avoid unnecessary friction loss; the friction plate is a key component in the brake system, usually made of wear-resistant materials, and is used to contact the brake disc to generate friction. When the brake system is activated, the friction plate will press the brake disc and prevent the rotation of the bearing through friction; the brake disc is fixed on the bearing and rotates synchronously with the bearing. When the friction plate presses the brake disc, the friction between the two is converted into heat energy, thereby slowing down and eventually stopping the rotation of the bearing; the caliper is a clamping mechanism that controls the distance between the friction plate and the brake disc. When the brake signal is issued, the caliper moves, pushing the friction plate to fit the brake disc to achieve the braking effect. The rotation of the wind cup and the blade is quickly stopped to ensure that the high-altitude cabin will not get out of control, thereby ensuring the safety of personnel and equipment. In addition, the cable connection mechanism is equipped with bearings to ensure the stability and flexibility of the structure, further improving the overall safety.

[0045] Strong environmental adaptability: The equipment design fully considers the impact of extreme climatic conditions, using low-temperature lubricants and high-temperature resistant materials to ensure normal operation under various climatic conditions. Whether in high or low temperatures, high humidity or strong winds, the high-altitude cabin can operate reliably.

[0046] Wide application: Due to its unique energy self-sufficiency and adaptive control system, the high-altitude cabin of the present invention can be widely used in various emergency rescue scenarios, such as high-altitude rescue at disaster sites such as earthquakes, floods, fires, and other emergency situations that require rapid response and deployment.

[0047] The specific implementation methods described above further illustrate the purpose, technical solutions and beneficial effects of the present application in detail. It should be understood that the above description is only the specific implementation method of the present application and is not intended to limit the scope of protection of the present application. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present application should be included in the scope of protection of the present application.

Claims

1. An emergency rescue high altitude cabin equipped with a wind-driven lifting device, characterized in that: include: A high altitude cabin having a cabin body; A wind-excited lift device, the wind-excited lift device comprising a shaft, a wind cup force mechanism is provided on the top of the shaft, and a blade power mechanism is provided on the bottom of the shaft; The cable connection mechanism is configured to connect the wind-excited lift device to the high-altitude cabin.

2. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 1, characterized in that: A bearing is provided on the shaft body, and the cable connection mechanism is connected to the bearing; The bearing comprises an upper bearing and a lower bearing, wherein the upper bearing is located above the high-altitude cabin and the lower bearing is located below the high-altitude cabin.

3. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 2 is characterized in that: A wind-excited lift device is arranged at the center of the cabin.

4. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 3 is characterized in that: The cable connection mechanism comprises an upper cable and a lower cable, wherein the first end of the upper cable is connected to the upper bearing, the first end of the lower cable is connected to the lower bearing, and the second end of the upper cable and the second end of the lower cable are evenly connected to the cabin.

5. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 4, characterized in that: The first end of the upper cable is hinged to the outer ring of the upper bearing, and the first end of the lower cable is hinged to the outer ring of the lower bearing; A plurality of fixing rings are evenly arranged on the cabin body, and the second ends of the upper pull cables and the second ends of the lower pull cables are both hinged to the fixing rings.

6. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 2, characterized in that: A plurality of wind-induced lift devices are evenly arranged on the periphery of the cabin.

7. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 6, characterized in that: The shafts of the multiple wind-excited lift devices are all parallel to the axis of the cabin and are symmetrically arranged.

8. The emergency rescue high altitude cabin equipped with a wind-excited lifting device according to claim 6 or 7, characterized in that: The cable connection mechanism includes an upper support rod, a lower support rod, an upper transverse cable and a lower transverse cable, and the shaft body is connected to the cabin body through the upper support rod and the lower support rod; wherein, the upper support rod and the lower support rod are rigid rods, the first end of the upper support rod is connected to the upper bearing, and the first end of the lower support rod is connected to the lower bearing; the two ends of the upper transverse cable are connected to two adjacent upper bearings, and the two ends of the lower transverse cable are connected to two adjacent lower bearings.

9. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 1, characterized in that: The wind cup force bearing mechanism includes a plurality of wind cups, and the plurality of wind cups are evenly distributed on the top of the shaft body.

10. The emergency rescue high altitude cabin equipped with wind-excited lifting equipment according to claim 1, characterized in that: A transmission device is arranged between the wind cup force bearing mechanism and the blade power mechanism.

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