An emergency rescue high-altitude cabin equipped with wind-excited lifting equipment

Abstract

The present application relates to an emergency rescue high-altitude cabin equipped with a wind-excited lifting device, which belongs to the technical field of emergency rescue equipment and solves 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. The emergency rescue high-altitude cabin equipped with a wind-excited lifting device includes: a high-altitude cabin having a cabin body; a wind-excited lifting device, the wind-excited lifting device including a shaft, a wind cup force mechanism provided on the top of the shaft, and a blade power mechanism provided on the bottom of the shaft; and a cable connection mechanism configured to connect the wind-excited lifting device to the high-altitude cabin. The present application achieves adaptive stability and high efficiency of the high-altitude cabin in emergency rescue by utilizing natural wind power to achieve stable buoyancy and lift.

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-excited lifting device. Background Art

[0002] During high-altitude operations and rescue operations, aerial pods are essential equipment, providing a safe and stable platform. However, existing aerial pods generally rely on external energy sources to maintain buoyancy and stability. This high reliance on external energy can lead to energy shortages or supply interruptions in emergencies, such as in harsh environments. This makes stability difficult to guarantee and increases 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 power 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-excited lift device to solve the problem that high-altitude cabins in the existing technology 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 like this:

[0006] An emergency rescue high-altitude cabin equipped with a wind-excited lifting device, comprising:

[0007] A high altitude cabin having a cabin body;

[0008] A wind-excited lift device, comprising a shaft, a cup force mechanism provided on the top of the shaft, and a blade power mechanism provided on the bottom of the shaft;

[0009] The cable connection mechanism is configured to connect the wind-excited lift device to the high-altitude cabin.

[0010] 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.

[0011] Furthermore, a wind-excited lift device is provided at the center of the cabin.

[0012] 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.

[0013] 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.

[0014] Furthermore, a plurality of wind-excited lift devices are evenly arranged on the periphery of the cabin.

[0015] Furthermore, the shafts of the multiple wind-excited lift devices are all parallel to the axis of the cabin and are symmetrically arranged.

[0016] 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 end portions of the upper transverse cable are connected to two adjacent upper bearings, and the two end portions of the lower transverse cable are connected to two adjacent lower bearings.

[0017] 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.

[0018] Furthermore, a transmission device is provided between the wind cup force mechanism and the blade power mechanism.

[0019] Furthermore, the transmission device adopts a differential, and the differential is arranged in the middle of the shaft.

[0020] Compared with the prior art, the present invention can achieve at least one of the following beneficial effects:

[0021] a) The emergency rescue high-altitude cabin provided by the present invention, which is equipped with a wind-excited lift device, does not require an external energy supply and relies entirely 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.

[0022] b) The emergency rescue high-altitude cabin provided by the present invention, which is equipped with a wind-excited 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.

[0023] c) The emergency rescue high-altitude cabin provided by the present invention, which is equipped with a wind-excited lifting device, is connected by cables and bearings to ensure the stability and flexibility of the overall structure.

[0024] d) The modular design of the wind-excited lift device provided in the emergency rescue high-altitude cabin provided by the present invention enables it to be flexibly configured according to the specific use environment, further enhancing the adaptability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] 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.

[0026] Figure 1 A schematic diagram of the first angle of the structure of the first emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention;

[0027] Figure 2 A second-angle structural diagram of the first emergency rescue high-altitude cabin provided with a wind-excited lifting device provided by the present invention;

[0028] 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 equipped with a wind-excited lift device provided by the present invention;

[0029] Figure 4 A schematic structural diagram of a second type of emergency rescue high-altitude cabin equipped with a wind-excited lift device provided by the present invention from a first angle;

[0030] Figure 5 A second perspective structural diagram of a second emergency rescue high-altitude cabin equipped with a wind-excited lift device provided by the present invention;

[0031] Figure 6 The second embodiment of the present invention provides a wind-driven lifting device for an emergency rescue high-altitude cabin. Figure 1 ;

[0032] Figure 7 for Figure 6 A partial enlarged view of area A in the middle;

[0033] Figure 8 A schematic structural diagram of another wind-excited lift device provided by the present invention.

[0034] Reference numerals:

[0035] 1. Cabin body; 1-1. Fixing ring;

[0036] 2. Wind-driven lift device; 2-1. Shaft; 2-11. Upper shaft; 2-12. Lower shaft; 2-2. Cup force mechanism; 2-3. Blade power mechanism; 2-4. Upper bearing; 2-41. Upper lug; 2-5. Lower bearing; 2-51. Lower lug; 2-6. Differential;

[0037] 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

[0038] In order to make the purpose, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction 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 this disclosure and the features in the embodiments can be combined, separated, interchanged and / or rearranged with each other. Based on the embodiments in this application, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of this application.

[0039] In the accompanying drawings, the sizes and relative sizes of components may be exaggerated for clarity and / or descriptive purposes. When the exemplary embodiments can be implemented differently, the specific process sequence may be performed in a different order than described. For example, two processes described in succession may be performed substantially simultaneously or in a reverse order from the described order. In addition, the same reference numerals represent the same components.

[0040] The terms used herein are for the purpose of describing specific embodiments and are not intended to be restrictive. As used herein, 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, the features, integral bodies, steps, operations, parts, assemblies and / or their groups stated are explained, but the presence or addition of one or more other features, integral bodies, steps, operations, parts, assemblies and / or their groups is not excluded. It should also be noted that, as used herein, 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.

[0041] Example 1

[0042] 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, hereinafter referred to as the "emergency rescue high-altitude cabin", which includes:

[0043] The high-altitude cabin is a ring-shaped structure having a cabin body 1, the interior of which is filled with a light gas having a density lower than that of air to ensure buoyancy and stability. For example, the light gas is helium;

[0044] A wind-excited lift device 2, comprising a shaft 2-1, a cup force mechanism 2-2 being provided at the top of the shaft 2-1, and a blade power mechanism 2-3 being provided at the bottom of the shaft 2-1;

[0045] The cable connection mechanism 3 is configured to connect the wind-excited lift device 2 to the high-altitude cabin.

[0046] In this embodiment, the wind-excited lift device 2 and the high-altitude cabin utilize a modular design, facilitating quick disassembly and maintenance. The emergency rescue high-altitude cabin can be equipped with one or more wind-excited lift devices 2 to accommodate diverse operating environments and conditions. The shaft 2-1 of the wind-excited lift device 2 is taller than the axial height of the high-altitude cabin, allowing the cup force mechanism 2-2 and blade power mechanism 2-3 to be located above and below the high-altitude cabin.

[0047] like Figures 1 to 2 As shown, in the technical solution of setting a wind-excited lifting device 2 at the center of the cabin 1, the wind-excited lifting device 2 is installed at the center position of the high-altitude cabin, and the shaft 2-1 of the wind-excited lifting device 2 coincides with the axis of the high-altitude cabin.

[0048] like Figures 4 and 5 As shown, in a technical solution in which multiple wind-excited lift devices 2 are disposed on the periphery of a cabin 1, the multiple wind-excited lift devices 2 are evenly disposed on the outside of the high-altitude cabin, and the shafts 2-1 of the multiple wind-excited lift devices 2 are all parallel to the axis of the high-altitude cabin and symmetrically arranged. For example, four wind-excited lift devices 2 are evenly distributed around the high-altitude cabin, with the shafts 2-1 of the four wind-excited lift devices 2 being parallel and located on the four edges of the same rectangular parallelepiped, and the shafts 2-1 of the four wind-excited lift devices 2 being symmetrically distributed around the axis of the high-altitude cabin.

[0049] 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.

[0050] In a technical solution in which a wind-excited lift device 2 is disposed at the center of a cabin 1, a 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 disposed at the center of the high-altitude cabin. The shaft 2-1 is connected to the high-altitude cabin via the upper cable 3-1 and the lower cable 3-2. The upper cable 3-1 and the lower cable 3-2 are arranged at an angle. 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. Furthermore, 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 disposed on the cabin 1 of the high-altitude cabin. The second ends of the upper cable 3-1 and the second ends of the lower cable 3-2 are both hinged to the fixing rings 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 high-altitude cabin body, it is easy to connect to the high-altitude cabin body and convenient to process. The safety belt has high strength and light weight, which ensures 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 at an angle. 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, and the lower transverse cable 3-6 is connected to the lower part of two adjacent shaft bodies 2-1. In addition, the two ends of the upper transverse cable 3-5 are connected to the two adjacent upper bearings 2-4, and the two ends of the lower transverse cable 3-6 are connected to the two adjacent lower bearings 2-5.

[0051] In one of the optional embodiments, multiple 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 multiple ear plates are evenly arranged on the side walls of the outer rings of the bearings. Specifically, multiple upper ear plates 2-41 are provided on the outer ring of the upper bearing 2-4, and multiple lower ear plates 2-51 are provided on the outer ring of the lower bearing 2-5. In a technical solution in which a single wind-excited lift device 2 is provided at the center of the cabin 1, the second ends of the upper cable 3-1 and the lower cable 3-2 are both hinged to the lugs on the corresponding bearings, i.e., the second end of the upper cable 3-1 is hinged to the upper lug 2-41 on the upper bearing 2-4, and the second end of the lower cable 3-2 is hinged to the lower lug 2-51 on the lower bearing 2-5. In a technical solution in which multiple wind-excited lift devices 2 are provided on the periphery of the cabin 1, the second end of the upper support rod 3-3 and both ends of the upper transverse cable 3-5 are both hinged to the upper lug 2-41 on the outer ring of the upper bearing 2-4; the second end of the lower support rod 3-4 and both ends of the lower transverse cable 3-6 are both hinged to the lower lug 2-51 on the outer ring of the lower bearing 2-5. The connections at the lugs are all pinned.

[0052] In one of the optional embodiments, the emergency rescue high-altitude cabin with built-in wind-excited lifting equipment 2 also includes an adaptive control system. The adaptive control system includes sensors for high-altitude environment monitoring. The sensors are set on the wind cup force-bearing mechanism. The type and number of sensors are set according to needs. They 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 the sensors according to the 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 the data such as wind force and direction sensed by the sensors, so that the cabin body 1 as a whole maintains a relatively balanced state.

[0053] 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 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

[0054] The braking device requires manual control, such as manual braking at the ground station when the mooring device fails or the attitude of the high-altitude cabin is out of control.

[0055] In this embodiment, the manufacturing process of the high-altitude cabin requires airtightness testing to ensure that the lightweight gas filling the cabin will not leak. Helium is also used to ensure sufficient buoyancy. All externally exposed components of the emergency rescue high-altitude cabin, such as the cabin body 1, are made of weather-resistant materials and are coated with UV-resistant and anti-corrosion treatments to improve the equipment's durability and resistance to environmental impacts. To ensure the emergency high-altitude cabin can operate normally in extreme temperatures, low-temperature lubricants and high-temperature resistant materials are used in the equipment's hinged parts to ensure normal operation in various climates.

[0056] 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.

[0057] 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 can 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 speed through the differential 2-6, driving the blade power mechanism 2-3 at the bottom to rotate, providing additional lift. Among them, the differential 2-6 is provided in the middle of the shaft 2-1, and the differential 2-6 is located at the midpoint of 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 2-11 and a lower shaft 2-12. The upper end of the upper shaft 2-11 is connected to the cup force mechanism 2-2, and the lower end of the lower shaft 2-12 is connected to the blade power mechanism 2-3. The lower end of the upper shaft 2-11 is connected to the upper end of the lower shaft 2-12 via a differential 2-6. The differential 2-6 includes a gear set and supporting components that can adjust the speed of the upper shaft 2-11 and the lower shaft 2-12. When the cup force mechanism 2-2 rotates due to wind force, it is accelerated by the differential 2-6, causing the blade power mechanism 2-3 to rotate faster than the cup force mechanism 2-2, thereby enhancing the lift provided.

[0058] When the main cabin diameter is relatively small, a single wind-excited lift device 2 can be installed at the center. The lugs on the outer rings of the upper bearing 2-4 and the lower bearing 2-5 are connected to the cabin 1 via upper and lower cables 3-1 and 3-2, respectively, forming a spoke-type tensioned structure. This spoke-type structure evenly distributes forces, improving structural stability and load-bearing capacity while also reducing material usage, achieving lightweighting and cost savings. Furthermore, the spoke-type design facilitates maintenance and expansion, making it easier to locate and repair faults and easily expand the system. It also offers aesthetic appeal and flexibility.

[0059] When the diameter of the main cabin is large, multiple wind-excited lifting 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 realize the connection of the shafts 2-1 of two adjacent wind-excited lifting 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 lifting devices 2. That is, in the technical solution of setting up multiple wind-excited lift devices 2, the upper bearings 2-4 and lower bearings 2-5 of two adjacent shafts 2-1 are connected to the upper bearings 2-4 and lower bearings 2-5 on the adjacent shafts 2-1 through flexible upper transverse cables 3-5 and lower transverse cables 3-6, respectively, to form a laterally stable force-bearing structure, and the upper bearings 2-4 and lower bearings 2-5 on each shaft 2-1 are connected to the cabin 1 through rigid support rods. There are two rigid support rods at each bearing. The rigid support is mainly used for compression, while the flexible upper transverse cables 3-5 and lower transverse cables 3-6 are mainly tensile after being formed. 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.

[0060] 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.

[0061] Table 1

[0062]

[0063] 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:

[0064] Energy Self-Supplied: The high-altitude capsule requires no external energy supply, relying entirely on natural wind for lift and buoyancy. The cup-type force mechanism captures the high-altitude wind and drives the propeller mechanism to rotate synchronously, providing the necessary lift. This design eliminates reliance on external energy sources such as electricity or fuel, ensuring operational operation in any emergency situation.

[0065] Adaptive Stability: The adaptive control system uses sensors to monitor the cabin's attitude and position in real time, automatically adjusting the length of the mooring lines and balancing the tension of each line to ensure the cabin's stability in various wind conditions. Even in adverse weather conditions, the cabin remains stable, providing a safe and reliable platform for rescue operations.

[0066] Structural Flexibility and Adaptability: The modular design allows the wind-inspired lift device to be flexibly configured to suit different operating environments and conditions. Users can choose to install the device in the center or around the perimeter of the high-altitude cabin to suit specific operational requirements. This modular design also simplifies installation, removal, and maintenance, improving ease of use and operational flexibility.

[0067] Easy maintenance: All exposed components are made of weather-resistant materials, such as UV-resistant coatings and corrosion-resistant materials, which greatly extends the service life of the equipment and reduces maintenance frequency and costs. The modular design also facilitates rapid replacement and maintenance of components, further reducing operating costs.

[0068] High Safety: The emergency brake system is designed to apply braking in an emergency by installing an electronic brake in the bearing. This brake consists of a spring, friction pad, brake disc, and caliper. The system is low-power and operates only with a button battery. The spring is located at the center of the braking system. Its function is to maintain sufficient clearance between the brake disc and the friction pad when the brake is not activated, preventing unnecessary friction losses. The friction pad is a key component of the braking system, typically made of wear-resistant material, and is used to generate friction with the brake disc. When the braking system is activated, the friction pad presses against the brake disc, preventing the bearing from rotating through friction. The brake disc is fixed to the bearing and rotates synchronously with the bearing. When the friction pad presses against the brake disc, the friction between the two is converted into heat energy, slowing and eventually stopping the bearing's rotation. The caliper is a clamping mechanism that controls the distance between the friction pad and the brake disc. When the brake signal is received, the caliper activates, pushing the friction pad against the brake disc, achieving the braking effect. This method quickly stops the rotation of the wind cup and blades, preventing loss of control in the high-altitude cabin and protecting 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.

[0069] Strong environmental adaptability: The equipment design fully considers the impact of extreme climate conditions, using low-temperature lubricants and high-temperature resistant materials to ensure normal operation in various climates. Whether in high or low temperatures, high humidity or strong winds, the high-altitude cabin can operate reliably.

[0070] 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, and fires, as well as other emergency situations that require rapid response and deployment.

[0071] The specific implementation methods described above further illustrate the purpose, technical solutions and beneficial effects of this application. It should be understood that the above description is only the specific implementation methods of this application and is not intended to limit the scope of protection of this application. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of this application should be included in the scope of protection of this 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; The wind-excited lifting device comprises a shaft body, a cup force-bearing mechanism is provided on the top of the shaft body, and a blade power mechanism is provided at the bottom of the shaft body: the shaft body comprises an upper shaft rod and a lower shaft rod arranged vertically and coaxially, the upper end of the upper shaft rod is connected to the cup force-bearing mechanism, the lower end of the lower shaft rod is connected to the blade power mechanism, the lower end of the upper shaft rod is connected to the upper end of the lower shaft rod through a differential, and the differential is located at the midpoint between the cup force-bearing mechanism and the blade power mechanism; the cup force-bearing mechanism rotates by capturing high-altitude wind force, increases the rotation speed through the differential, and drives the blade power mechanism at the bottom to rotate synchronously to provide additional lift: an upper bearing and a lower bearing are provided on the shaft body, the upper bearing is located above the high-altitude cabin, and the lower bearing is located below the high-altitude cabin; a cable connection mechanism configured to connect the wind-excited lift device to the high-altitude cabin; Wherein, a wind-excited lift device is provided at the center of the cabin; 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; 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 also evenly provided on the cabin, and the second ends of the upper cable and the lower cable are both hinged to the fixing rings; or, A plurality of wind-excited lifting devices are evenly arranged on the periphery of the cabin; the shafts of the plurality of wind-excited lifting devices are parallel to the axis of the cabin and are symmetrically arranged; the cable connection mechanism comprises an upper support rod, a lower support rod, an upper transverse cable and a lower transverse cable, and the shaft is connected to the cabin 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 end portions of the upper transverse cable are connected to two adjacent upper bearings, and the two end portions of the lower transverse cable are connected to two adjacent lower bearings; It also includes an adaptive control system, which includes sensors for high-altitude environmental monitoring. The sensors are arranged on the wind cup force-bearing mechanism and are used to capture parameters including wind speed, wind direction, air pressure, humidity, and temperature. The attitude and position of the high-altitude cabin are monitored in real time by changes in wind speed and direction. The data obtained by the sensors are judged to automatically adjust the angles of the wind cups and blades, as well as the tension of the mooring ropes in the corresponding directions, so that the cabin as a whole maintains a relatively balanced state. It also includes an emergency braking device for quickly stopping the rotation of the wind cup and blades in an emergency; the emergency braking device includes a brake arranged in the bearing, and the brake includes a spring, a friction plate, a brake disc and a caliper; the spring is located at the center of the emergency braking device, and is used to maintain a sufficient gap between the brake disc and the friction plate when the brake is not activated; the friction plate is used to contact the brake disc to generate friction; the brake disc is fixed on the bearing and rotates synchronously with the bearing; when the emergency braking device is started, the caliper is actuated to push the friction plate to press the brake disc, thereby preventing the rotation of the bearing by friction.

2. The emergency rescue high altitude cabin equipped with a wind-excited lifting device 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.

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

Images