Starry sky tent device suspended in air

Abstract

The invention relates to the technical field of recreational facilities, and discloses an air-suspending starry sky tent device which comprises helium balloons, a starry sky tent body, an elevator, a landing platform, a data acquisition module and a controller. According to the starry sky tent device, through a dynamic adjustment mechanism combining real-time environment parameters, real-time loads and system bearing capacity, the basic thrust, the safe operation speed and the bearing level of an elevator can be accurately calculated, the parameters can be dynamically adjusted according to real-time data, and therefore stable operation of an elevator system and personnel safety are guaranteed.

Description

Technical Field

[0001] The invention relates to the technical field of entertainment facilities, and in particular to a starry sky tent device suspended in the air. Background Art

[0002] With the continuous construction of modern high-rise buildings and people's increasing demand for aerial landscape experience, aerial suspended sightseeing platforms, as a new type of aerial sightseeing facilities, are gradually being widely used in urban landscape and tourism industries. This type of platform usually needs to be able to provide a stable and safe vertical lifting and suspension system, so precise control and adjustment are required. One of its core components is the elevator system. In the actual application of aerial suspended platforms, the load-bearing capacity, operation stability and safety of the elevator system become particularly important.

[0003] The support structure between the elevator shaft and the platform ensures the stability of the aerial suspension platform through the interaction of steel cables, helium balloons and the elevator body. In this context, how to scientifically calculate the load-bearing level of the elevator shaft and how to dynamically adjust it according to environmental factors and real-time loads has become one of the key technologies to ensure the safe operation of the aerial suspension platform. In addition, since environmental factors (such as wind speed, humidity, etc.) and real-time loads (such as the number of tourists, etc.) have an important impact on the operating safety of the elevator, how to accurately quantify the adjustment of these environmental factors on the elevator operating parameters and provide adaptive adjustment solutions is also one of the technical difficulties in this field.

[0004] At present, there have been some studies on the safe operation of elevators, load calculation and the impact of environmental factors on elevator performance, but most methods are only based on static parameters and lack real-time monitoring and adjustment of dynamic environmental changes and load fluctuations. They cannot reflect the actual carrying capacity and operating speed of the elevator under different environmental conditions in real time. Summary of the invention

[0005] In view of this, the present invention proposes an air-suspended starry sky tent device, aiming to solve the above problems.

[0006] The present invention proposes an air-suspended starry sky tent device, comprising a helium balloon, a starry sky tent body, a lifting elevator, a landing platform, a data acquisition module and a controller;

[0007] The helium balloon is connected to the starry sky tent body through an upper traction steel cable, and the helium balloon is used to apply an upward pulling force to the starry sky tent body through the upper traction steel cable; the starry sky tent body is connected to the landing platform through a lower traction steel cable;

[0008] The lift elevator comprises an elevator shaft and an elevator body; the elevator shaft is respectively connected to the landing platform and the starry sky tent body, and the elevator shaft is used to accommodate the elevator body; the starry sky tent body is provided with a groove, and the groove is used to embed the elevator body;

[0009] The controller is preset with basic mechanical parameters and preset environmental parameters of the starry sky tent device; the controller is used to set the basic thrust of the elevator shaft on the starry sky tent body according to the basic mechanical parameters; the controller is also used to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, and use the optimal thrust as the actual supporting force of the elevator shaft;

[0010] The data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state for use based on the real-time environmental parameters and the real-time number of people; when the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body based on the real-time environmental parameters and the real-time number of people.

[0011] Preferably, the basic mechanical parameters include the total weight of the starry sky tent body, the buoyancy parameters of the helium balloon, the tension parameters of the upper traction steel cable, and the tension parameters of the lower traction steel cable.

[0012] Preferably, the total weight of the starry sky tent body is calculated by the following formula:

[0013] W tent =m tent g;

[0014] Among them, W tent Indicates the total weight of the starry sky tent body; m tent represents the mass of the starry sky tent body; g represents the acceleration due to gravity.

[0015] Preferably, the buoyancy parameter of the helium balloon is calculated by the following formula:

[0016] F buoyancy =(ρ air -ρ helium )·V balloon g;

[0017] Among them, F bouyancy represents the buoyancy parameter of the helium balloon; ρ air Represents the density of air; ρ helium represents the density of helium, V balloon represents the volume of the helium balloon and g represents the acceleration due to gravity.

[0018] Preferably, the upper traction steel cables are provided with 4n pieces, n is a positive integer greater than 0, and the angle between the upper traction steel cables and the vertical direction is less than 90°; the tension parameter of the upper traction steel cables is calculated by the following calculation formula:

[0019]

[0020] Wherein, Ts represents the tension parameter of the upper traction steel cable; θ represents the angle between the upper traction steel cable and the vertical direction.

[0021] Preferably, the number of the lower traction steel cables is 4m, where m is a positive integer greater than 0, and the angle between the lower traction steel cables and the vertical direction is less than 90°; the tension parameter of the lower traction steel cables is calculated by the following formula:

[0022]

[0023] Among them, T d represents the tension parameter of the lower traction steel cable; ω represents the angle between the lower traction steel cable and the vertical direction.

[0024] Preferably, when the controller is used to set the basic operating parameters of the elevator body according to the basic mechanical parameters, it includes:

[0025] The basic thrust of the elevator shaft on the starry sky tent body is calculated by the following formula:

[0026] F elevator =W tent -F buoyancy -T s -T d ;

[0027] Among them, F elevator It represents the basic thrust of the elevator shaft on the starry sky tent body.

[0028] Preferably, the controller is further used to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, including:

[0029] The preset environmental parameters include the maximum wind speed and maximum humidity that the starry sky tent device can withstand; the optimal thrust is calculated by the following formula:

[0030]

[0031] Among them, F optimal represents the optimal thrust; α wind Represents the wind speed correction coefficient, that is, the influence of wind speed on thrust; α humidityRepresents the humidity correction factor, that is, the influence of humidity on thrust; V wind,max Indicates the maximum wind speed; V wind,nom Indicates the annual average wind speed; H max Indicates the maximum humidity; H nom Indicates the average annual humidity.

[0032] Preferably, the data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state for use according to the real-time environmental parameters and the real-time number of people, including:

[0033] According to the real-time environmental parameters and the real-time number of people, the real-time load level of the elevator is calculated by the following formula:

[0034] C elevator =C base α wind α humidity α load ;

[0035] Among them, C elevator Indicates the real-time load level of the elevator; C base It represents the basic bearing level of the elevator shaft when there is no external environmental influence and the elevator body is fully loaded; α wind , α humidity , α load They represent the adjustment coefficients of real-time wind speed, real-time humidity and real-time number of people respectively;

[0036] The maximum load capacity of the elevator body is preset, denoted as C elevator,max ;

[0037] When C elevator ≤C elevator,max When the elevator body is in a safe state for use, the judgment result is that the elevator body is in a safe state for use; otherwise, the judgment result is that the elevator body is not in a safe state for use, and at this time, the elevator body stops being used.

[0038] Preferably, when the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body according to the real-time environmental parameters and the real-time number of people, including:

[0039] The safe operating speed of the elevator body is obtained by calculating the following formula:

[0040]

[0041] Among them, V safe Indicates the safe operating speed of the elevator body; V base Indicates the preset basic operating speed of the elevator body.

[0042] Compared with the prior art, the present invention has the following beneficial effects:

[0043] Environmental adaptability: The present invention monitors environmental parameters such as wind speed, humidity, and temperature in real time and adjusts the elevator operating parameters accordingly to ensure that the elevator system can adapt to changing environmental conditions, thereby improving the safety and stability of the system. For example, when the wind speed is high, the system can automatically reduce the elevator speed to prevent overload or instability.

[0044] Dynamic adjustment capability: According to the real-time number of passengers and the load condition of the elevator shaft, the controller can flexibly adjust the elevator's operating speed and carrying capacity. For example, when the number of passengers increases, the system will adjust the elevator speed and carrying capacity accordingly to prevent overload operation; at the same time, in response to changes in environmental factors such as humidity and wind speed, the system will make real-time adjustments to ensure the safety of elevator operation.

[0045] Operation optimization: This invention combines environmental data such as wind speed and humidity with real-time load information to optimize the safe operation speed of the elevator, aiming to reduce energy consumption and ensure the stable operation of the elevator under various environmental conditions. Through precise parameter calculation, the system avoids over-design or operation in an unsuitable environment, achieving efficient resource utilization and dual security.

[0046] Enhanced safety: By real-time monitoring and calculating the load level of the elevator shaft, the present invention can instantly assess the safe operation status of the elevator. If the load capacity of the elevator shaft is detected to be insufficient, the system will automatically sound an alarm to prevent the elevator from overloading and ensure the safety of passengers.

[0047] Intelligent control mechanism: The present invention combines preset environmental parameters and basic mechanical parameters with a real-time data acquisition system to autonomously adjust the operating speed, thrust and load capacity of the elevator system. Under extreme weather or load conditions, the system can adjust the working state in time, thereby improving the adaptive ability and intelligence level of the elevator system. BRIEF DESCRIPTION OF THE DRAWINGS

[0048] Various other advantages and benefits will become apparent to those of ordinary skill in the art by reading the detailed description of the preferred embodiments below. The accompanying drawings are only for the purpose of illustrating the preferred embodiments and are not to be considered as limiting the present invention. Moreover, the same reference symbols are used throughout the accompanying drawings to represent the same components. In the accompanying drawings:

[0049] Figure 1 This is a schematic diagram of the overall structure of the starry sky tent device suspended in the air;

[0050] Figure 2 It is a cross-sectional view of the main body of the starry sky tent suspended in the air (without the elevator embedded);

[0051] Figure 3 It is a cross-sectional view of the main body of the starry sky tent (embedded with the lift) suspended in the air;

[0052] In the picture, 1. Helium balloon; 2. Upper traction steel cable; 3. Starry sky tent body; 4. Lifting elevator; 5. Lower main steel cable; 6. Lower auxiliary steel cable; 7. Water and electricity pipelines; 8. Lifting motor; 9. Landing platform; 10. Upper rest space; 11. Lifting motor; 12. Lower activity space; 13. Elevator cable. DETAILED DESCRIPTION

[0053] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the accompanying drawings, it should be understood that the present disclosure can be implemented in various forms and should not be limited by the embodiments described herein. On the contrary, these embodiments are provided in order to enable a more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the absence of conflict, the embodiments of the present invention and the features described in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.

[0054] This embodiment provides a starry sky tent device suspended in the air, including a helium balloon 1, a starry sky tent body 3, a lift 4, a landing platform 9, a data acquisition module and a controller;

[0055] The helium balloon 1 is connected to the starry sky tent body 3 through an upper traction steel cable 2, and the helium balloon 1 is used to apply an upward pulling force to the starry sky tent body 3 through the upper traction steel cable 2; the starry sky tent body 3 is connected to the landing platform 9 through a lower traction steel cable;

[0056] The lift 4 includes an elevator shaft and an elevator body; the elevator shaft is connected to the landing platform 9 and the starry sky tent body 3 respectively, and the elevator shaft is used to accommodate the elevator body; the starry sky tent body 3 is provided with a groove, and the groove is used to embed the elevator body;

[0057] The controller is preset with basic mechanical parameters and preset environmental parameters of the starry sky tent device; the controller is used to set the basic thrust of the elevator shaft on the starry sky tent body 3 according to the basic mechanical parameters; the controller is also used to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, and use the optimal thrust as the actual supporting force of the elevator shaft;

[0058] The data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state for use based on the real-time environmental parameters and the real-time number of people; when the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body based on the real-time environmental parameters and the real-time number of people.

[0059] It can be understood that the starry sky tent device of this embodiment not only provides users with a unique air accommodation experience, but also ensures safety and comfort through advanced technology. In practical applications, the size and number of helium balloons 1 can be adjusted according to the weight of the starry sky tent body 3 and the required suspension height to ensure the stability and safety of the entire structure. The design of the lift 4 allows users to easily get on and off the starry sky tent body 3, while ensuring reliable operation in various weather conditions.

[0060] As the brain of the whole system, the controller ensures the stable suspension of the starry sky tent body 3 through real-time monitoring and adjustment. It can quickly respond to environmental changes, such as changes in wind speed, temperature, humidity and other parameters, by cooperating with the data acquisition module, so as to automatically adjust the buoyancy of the helium balloon 1 and the support force of the elevator shaft to ensure the safety of the whole system.

[0061] The data acquisition module is responsible for monitoring not only environmental parameters, but also the real-time number of people in the tent, which is crucial to ensure the safe operation of the elevator body. Through precise calculations, the data acquisition module can determine the safe operating speed of the elevator body to prevent overloading or operation in adverse weather conditions.

[0062] In summary, the starry sky tent device of this embodiment provides users with a safe and romantic aerial accommodation experience by combining the buoyancy of helium balloons, the convenience of elevators, the intelligent adjustment of controllers, and the real-time monitoring of data acquisition modules.

[0063] Specifically, refer to Figures 1 to 3The present invention introduces an air-suspended starry sky tent device suitable for low-altitude accommodation and family entertainment. The device mainly utilizes the long-term floating characteristics of a helium balloon 1, and includes a helium balloon 1 located at the top to provide buoyancy for the entire device, and a starry sky tent body 3 located in the middle. The skeleton of the starry sky tent body 3 preferably adopts a lightweight steel structure to ensure that the overall quality is controllable and reduce the load of the helium balloon 1. The landing platform 9 of the device is located at the bottom of its projection, and the helium balloon 1 at the top, the starry sky tent body 3 in the middle, and the landing platform 9 below are connected by traction cables. These traction cables are made of high-strength steel, the upper traction cable 2 connects the helium balloon 1 and the starry sky tent body 3, and the lower main cable 5 and the lower auxiliary cable 6 connect the starry sky tent body 3 and the landing platform 9. The lower main cable 5 and the lower auxiliary cable 6 work together to stably position the starry sky tent body 3 at a predetermined position in the air. In addition, a lift 4 is arranged outside the main steel cable of the traction steel cable, which can realize the up and down transportation of personnel and materials under the control of the lift motor 11 inside the starry sky tent body 3.

[0064] The helium balloon 1 is located at the top of the device, providing the necessary buoyancy for the entire suspended starry sky tent device. The device preferably adopts a non-pressurized method for filling the air, and in order to ensure the safety of the entire device, a safety detection device is installed on the surface of the helium balloon 1, which can monitor the air pressure, temperature, wind speed and other data in real time, and process and analyze potential safety risks in real time.

[0065] In a preferred embodiment of the present invention, the starry sky tent body 3 is located in the middle of the device and is the functional core of the entire device. It includes a load-bearing frame for support, an upper rest space 10, a lower rest space 12, a lifting motor 11, and a part of the lower main steel cable 5. The load-bearing frame is made of high-strength square steel and is responsible for the mechanical bearing of the entire device, including the buoyancy provided by the helium balloon 1 transmitted by the upper traction steel cable 2, and the limiting downward pressure provided by the landing platform 9 transmitted by the lower main steel cable 5 and the lower auxiliary steel cable 6, and the whole presents a long-term load state. In order to reduce the load of the helium balloon 1, the entire starry sky tent body 3 is preferably wrapped with lightweight materials to form a closed structure to reduce the safety risks of personnel.

[0066] After being wrapped with lightweight materials, the main body 3 of the starry sky tent can be divided into two parts: an upper rest space 10 and a lower rest space 12. The upper rest space 10 is hemispherical, and the wrapping material is preferably made of transparent material. There are beds and corresponding facilities in the middle for people inside to rest and watch the starry sky and the external environment. The lower rest space 12 is truncated as a whole, and is equipped with basic furniture such as desks, chairs, showers and lockers. It provides daily life services such as washing, dining and storage, and is equipped with water and electricity facilities. There is space on the inner side adjacent to the main steel cable for the parking and storage of the elevator 4. In addition, a control lifting motor 3 is provided on the load-bearing frame of the lower rest space 12, which can control the lifting and lowering of the elevator 4 to achieve rapid up and down of people.

[0067] Preferably, the elevator 4 is located outside the main steel cable of the traction steel cable 3, providing a service for quickly getting on and off the starry sky tent. The lifting and lowering of the elevator 4 is controlled by the lifting motor 3 inside the starry sky tent body 3, which can complete the up and down of people in a short time, and can also provide a quick escape function when necessary to ensure the safety of the people inside.

[0068] In a preferred embodiment of the present invention, the upper traction steel cable 2, the lower main steel cable 5 and the lower auxiliary steel cable 6 are respectively located between the top helium balloon 1, the middle starry sky tent body 3 and the lower landing platform 9. The upper traction steel cable 2 bears the tension between the top helium balloon 1 and the middle starry sky tent body 3, while the lower main steel cable 5 and the lower auxiliary steel cable 6 bear the tension between the middle starry sky tent body 3 and the lower landing platform 9. The lower main steel cable 5 mainly bears the tension between the starry sky tent body 3 and the lower landing platform 9, and the lower auxiliary steel cable 6 plays a limiting role to ensure that the entire device is stable at a predetermined position.

[0069] Furthermore, some of the lower auxiliary steel cables 6 are equipped with electric wires and water pipes to provide the required electricity and water for the people inside the starry sky tent body 3 .

[0070] In addition, the bottom landing platform 9 preferably provides maintenance services such as docking, inspection, water supply and power supply for the entire starry sky tent device. It has a pressurizing device that can pump water into the starry sky tent body 3 in the sky. At the same time, the landing platform 9 is also equipped with a landing motor 8, which can control the sending and receiving of the lower main steel cable 5, thereby controlling the take-off and landing of the starry sky tent body 3.

[0071] In some embodiments of the present application, the basic mechanical parameters include the total weight of the starry sky tent body, the buoyancy parameters of the helium balloon, the tension parameters of the upper traction steel cable, and the tension parameters of the lower traction steel cable.

[0072] It is understandable that the concept of basic mechanical parameters is elaborated in detail in this embodiment, which includes multiple key physical quantities. These parameters are not limited to the total weight of the starry sky tent body, but also include the buoyancy parameters of the helium balloon used to support the tent. In addition, it also includes the tension parameters of the upper traction steel cable used to ensure the stability of the tent, and the tension parameters of the lower traction steel cable, which work together to maintain the structural stability and wind resistance of the tent.

[0073] In some embodiments of the present application, the total weight of the starry sky tent body is calculated by the following formula:

[0074] W tent =m tent g;

[0075] Among them, W tent Indicates the total weight of the starry sky tent body; m tent represents the mass of the starry sky tent body; g represents the acceleration due to gravity.

[0076] It is understandable that this embodiment explains in detail how to calculate the total weight of the starry sky tent body by using known mass and gravitational acceleration. This calculation is crucial to ensuring the stability and safety of the entire device, because it involves whether the buoyancy provided by the helium balloon is sufficient to support the weight of the tent body, and whether the traction cable can withstand the corresponding tension. The advantage of this embodiment is that it provides a method for accurately evaluating and designing the stability of the starry sky tent. By accurately calculating the total weight of the tent body, the designer can ensure that a balance is reached between the buoyancy of the helium balloon and the weight of the tent, thereby ensuring that the tent is stably suspended in the air. At the same time, by calculating the tension parameters of the upper and lower traction cables, it can be ensured that the tent can maintain structural integrity under various weather conditions, especially in strong winds. Such a design not only improves the safety of the tent, but also enhances the user experience, making camping under the stars a safe and romantic activity.

[0077] In some embodiments of the present application, the buoyancy parameters of the helium balloon are calculated by the following formula:

[0078] F buoyancy =(ρ air -ρ helium )·V balloon g;

[0079] Among them, F bouyancy represents the buoyancy parameter of the helium balloon; ρ air Represents the density of air; ρ helium represents the density of helium, V balloon represents the volume of the helium balloon and g represents the acceleration due to gravity.

[0080] It is understandable that this embodiment explains in detail how to calculate the buoyancy parameters of the helium balloon by the density difference between air and helium. The buoyancy of the helium balloon is based on the Archimedean principle, that is, the upward buoyancy of an object in a fluid is equal to the weight of the fluid it displaces. By calculation, it can be determined how much volume the helium balloon needs to provide sufficient buoyancy to support the weight of the main body of the starry sky tent. This calculation is crucial to ensure that the buoyancy and gravity of the entire device are balanced, thereby ensuring that the tent can be stably suspended in the air. The advantage of this embodiment is that it provides a scientific and precise method to design and implement the starry sky tent project. By accurately calculating the buoyancy parameters of the helium balloon, the designer can ensure the stability and safety of the tent when it is suspended in the air.

[0081] In some embodiments of the present application, 4n upper traction cables are provided, n is a positive integer greater than 0, and the angle between the upper traction cables and the vertical direction is less than 90°; the tension parameter of the upper traction cables is calculated by the following formula:

[0082]

[0083] Wherein, Ts represents the tension parameter of the upper traction steel cable; θ represents the angle between the upper traction steel cable and the vertical direction.

[0084] It can be understood that this embodiment explains in detail how to calculate the tension parameters of the steel cable by the angle between the upper traction steel cable and the vertical direction. The tension of the upper traction steel cable is based on the principle of static balance, that is, the tension exerted on the steel cable must be sufficient to support the weight of the tent body and keep it stable. Through calculation, the tension that the steel cable needs to withstand at different angles can be determined to ensure the stability and safety of the tent when it is suspended in the air. The user can use this calculation result to select a steel cable of appropriate strength and length to ensure that the tent can still maintain a predetermined height and stability under various environmental conditions. The advantage of this embodiment is that it provides a scientific and precise method to design and implement a starry sky tent project. By accurately calculating the tension parameters of the upper traction steel cable, the designer can ensure the stability and safety of the tent when it is suspended in the air.

[0085] In some embodiments of the present application, 4m lower traction steel cables are provided, where m is a positive integer greater than 0, and the angle between the lower traction steel cables and the vertical direction is less than 90°; the tension parameter of the lower traction steel cables is calculated by the following formula:

[0086]

[0087] Among them, T drepresents the tension parameter of the lower traction steel cable; ω represents the angle between the lower traction steel cable and the vertical direction.

[0088] It can be understood that this embodiment explains in detail how to calculate the tension parameters of the steel cable by the angle between the lower traction steel cable and the vertical direction. The tension of the lower traction steel cable is also based on the principle of static balance, that is, the tension exerted on the steel cable must be sufficient to support the weight of the tent body and keep it stable. Through calculation, the tension that the steel cable needs to withstand at different angles can be determined to ensure the stability and safety of the tent when it is suspended in the air. The user can use this calculation result to select a steel cable of appropriate strength and length to ensure that the tent can maintain a predetermined height and stability. The advantage of this embodiment is that it provides a scientific and precise method to design and implement a starry sky tent project. By accurately calculating the tension parameters of the lower traction steel cable, the designer can ensure the stability and safety of the tent when it is suspended in the air.

[0089] In some embodiments of the present application, when the controller is used to set the basic operating parameters of the elevator body according to the basic mechanical parameters, it includes:

[0090] The basic thrust of the elevator shaft on the starry sky tent body is calculated by the following formula:

[0091] F elevator =W tent -F buoyancy -T s -T d ;

[0092] Among them, F elevator It represents the basic thrust of the elevator shaft on the starry sky tent body.

[0093] It can be understood that this embodiment explains in detail how to calculate the basic thrust of the elevator shaft on the starry sky tent body through basic mechanical parameters. The calculation of the basic thrust is based on ensuring that the elevator shaft can stably support the weight of the tent body and keep the tent stable during the operation of the elevator. Through calculation, it is possible to determine the thrust that the elevator shaft needs to provide to ensure the stability and safety of the tent when it is suspended in the air. The user can use this calculation result to design the structure of the elevator shaft and select appropriate elevator operating parameters to ensure that the tent can still maintain a predetermined height and stability under various operating conditions. The advantage of this embodiment is that it provides a scientific and precise method to design and implement a starry sky tent project. By accurately calculating the basic thrust of the elevator shaft, the designer can ensure the stability and safety of the tent when it is suspended in the air.

[0094] In some embodiments of the present application, the controller is further configured to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, including:

[0095] The preset environmental parameters include the maximum wind speed and maximum humidity that the starry sky tent device can withstand; the optimal thrust is calculated by the following formula:

[0096]

[0097] Among them, F optimal represents the optimal thrust; α wind Represents the wind speed correction coefficient, that is, the influence of wind speed on thrust; α humidity Represents the humidity correction factor, that is, the influence of humidity on thrust; V wind,max Indicates the maximum wind speed; V wind,nom Indicates the annual average wind speed; H max Indicates the maximum humidity; H nom Indicates the average annual humidity.

[0098] It is understandable that this embodiment explains in detail how to adjust the basic thrust by presetting environmental parameters to obtain the optimal thrust. The calculation of the optimal thrust takes into account the influence of wind speed and humidity on the stability of the tent. The wind speed correction coefficient and the humidity correction coefficient represent the degree of influence of wind speed and humidity on the thrust respectively. Through calculation, the thrust that the elevator shaft needs to provide under different environmental conditions can be determined to ensure the stability and safety of the tent when it is suspended in the air. The user can use this calculation result to adjust the structure of the elevator shaft and the elevator operation parameters to ensure that the tent can still maintain a predetermined height and stability under extreme weather conditions. The advantage of this embodiment is that it provides a scientific and precise method to design and implement the starry sky tent project. By accurately calculating the optimal thrust, the designer can ensure the stability and safety of the tent when it is suspended in the air, and maintain its functionality and beauty even in harsh environmental conditions.

[0099] In some embodiments of the present application, the data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state for use according to the real-time environmental parameters and the real-time number of people, including:

[0100] According to the real-time environmental parameters and the real-time number of people, the real-time load level of the elevator is calculated by the following formula:

[0101] C elevator =C base α wind α humidity α load ;

[0102] Among them, C elevatorIndicates the real-time load level of the elevator; C base It represents the basic bearing level of the elevator shaft when there is no external environmental influence and the elevator body is fully loaded; α wind , α humidity , α load They represent the adjustment coefficients of real-time wind speed, real-time humidity and real-time number of people respectively;

[0103] The maximum load capacity of the elevator body is preset, denoted as C elevator,max ;

[0104] When C elevator ≤C elevator,max When the elevator body is in a safe state for use, the judgment result is that the elevator body is in a safe state for use; otherwise, the judgment result is that the elevator body is not in a safe state for use, and at this time, the elevator body stops being used.

[0105] It can be understood that this embodiment explains in detail how to determine whether the elevator is in a safe state of use through real-time environmental parameters and real-time number of people. The calculation of the real-time load level takes into account the impact of wind, humidity and number of people on the elevator's load capacity. By adjusting the coefficient in real time, the load level of the elevator under the current environment and passenger load can be accurately evaluated. When the real-time load level does not exceed the maximum load capacity of the elevator, it can be judged that the elevator is in a safe state of use. Conversely, if the real-time load level exceeds the maximum load capacity, the elevator will stop using to ensure the safety of passengers. This real-time monitoring and evaluation mechanism can effectively prevent the occurrence of dangerous situations such as overloading and ensure the safety of elevator operation.

[0106] In some embodiments of the present application, when the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body according to the real-time environmental parameters and the real-time number of people, including:

[0107] The safe operating speed of the elevator body is obtained by calculating the following formula:

[0108]

[0109] Among them, V safe Indicates the safe operating speed of the elevator body; V base Indicates the preset basic operating speed of the elevator body.

[0110] It is understood that this embodiment explains in detail how to determine the safe operating speed of the elevator based on the real-time environmental parameters and the real-time number of people. The calculation of the safe operating speed takes into account the impact of wind speed and humidity on the operation of the elevator. By adjusting the real-time environmental parameters and the number of people, it can be ensured that the elevator runs at an appropriate speed while ensuring safety. When the environmental conditions and passenger capacity change, the speed of the elevator can be adjusted accordingly to avoid operating risks caused by environmental factors. This dynamic adjustment mechanism helps to improve the flexibility and safety of elevator operation and ensure the comfort and safety of passengers under various environmental conditions.

[0111] Those skilled in the art will appreciate that the embodiments of the present application may be provided as methods, systems or computer program products. Therefore, the present application may adopt the form of a complete hardware embodiment, a complete software embodiment, or an embodiment in combination with software and hardware. Moreover, the present application may adopt the form of a computer program product implemented on one or more computer-usable storage media (including but not limited to disk storage, CD-ROM, optical storage, etc.) containing computer-usable program codes.

[0112] The present application is described with reference to flowcharts and / or block diagrams of methods, devices (systems) and computer program products according to embodiments of the present application. It should be understood that each process and / or box in the flowchart and / or block diagram, as well as the combination of processes and / or boxes in the flowchart and / or block diagram, can be implemented by computer program instructions. These computer program instructions can be provided to a processor of a general-purpose computer, a special-purpose computer, an embedded processor or other programmable data processing device to generate a machine, so that the instructions executed by the processor of the computer or other programmable data processing device generate instructions for implementing the processes in the flowchart and / or block diagram. Figure 1 A process or multiple processes and / or boxes Figure 1 A device that provides the functions specified in a block or multiple blocks.

[0113] These computer program instructions may also be stored in a computer-readable memory capable of directing a computer or other programmable data processing device to operate in a specific manner, so that the instructions stored in the computer-readable memory produce an article of manufacture comprising an instruction device, which implements the process Figure 1 A process or multiple processes and / or boxes Figure 1 A function specified in one or more boxes.

[0114] These computer program instructions can also be loaded onto a computer or other programmable data processing device so that a series of operating steps are executed on the computer or other programmable device to produce a computer-implemented process, thereby providing instructions for implementing the process. Figure 1 A process or multiple processes and / or boxes Figure 1The steps for the functions specified in one or more boxes.

[0115] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention rather than to limit it. Although the present invention has been described in detail with reference to the above embodiments, ordinary technicians in the relevant field should understand that the specific implementation methods of the present invention can still be modified or replaced by equivalents. Any modification or equivalent replacement that does not depart from the spirit and scope of the present invention should be covered within the scope of protection of the claims of the present invention.

Claims

1. A starry sky tent device suspended in the air, characterized in that: Including helium balloon, star tent body, elevator, landing platform, data acquisition module and controller; The helium balloon is connected to the starry sky tent body through an upper traction steel cable, and the helium balloon is used to apply an upward pulling force to the starry sky tent body through the upper traction steel cable; the starry sky tent body is connected to the landing platform through a lower traction steel cable; The lift elevator comprises an elevator shaft and an elevator body; the elevator shaft is respectively connected to the landing platform and the starry sky tent body, and the elevator shaft is used to accommodate the elevator body; the starry sky tent body is provided with a groove, and the groove is used to embed the elevator body; The controller is preset with basic mechanical parameters and preset environmental parameters of the starry sky tent device; the controller is used to set the basic thrust of the elevator shaft on the starry sky tent body according to the basic mechanical parameters; the controller is also used to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, and use the optimal thrust as the actual supporting force of the elevator shaft; The data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state for use based on the real-time environmental parameters and the real-time number of people; when the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body based on the real-time environmental parameters and the real-time number of people.

2. The air-suspended starry sky tent device according to claim 1, characterized in that: The basic mechanical parameters include the total weight of the starry sky tent body, the buoyancy parameters of the helium balloon, the tension parameters of the upper traction steel cable, and the tension parameters of the lower traction steel cable.

3. The air-suspended starry sky tent device according to claim 2, characterized in that: The total weight of the starry sky tent body is calculated by the following formula: W tent =m tent ·g; Among them, W tent Indicates the total weight of the starry sky tent body; m tent represents the mass of the starry sky tent body; g represents the acceleration due to gravity.

4. The air-suspended starry sky tent device according to claim 3, characterized in that: The buoyancy parameters of the helium balloon are calculated by the following formula: F buogancy =(ρ air -r helium )·V balloon ·g; Among them, F bouyancy represents the buoyancy parameter of the helium balloon; ρ air represents the density of air; ρ helium represents the density of helium, V balloon represents the volume of the helium balloon and g represents the acceleration due to gravity.

5. The air-suspended starry sky tent device according to claim 4, characterized in that: The upper traction steel cables are provided with 4n pieces, n is a positive integer greater than 0, and the angle between the upper traction steel cables and the vertical direction is less than 90°; the tension parameter of the upper traction steel cables is calculated by the following calculation formula: Wherein, Ts represents the tension parameter of the upper traction steel cable; θ represents the angle between the upper traction steel cable and the vertical direction.

6. The air-suspended starry sky tent device according to claim 5, characterized in that: The lower traction steel cables are provided with 4m pieces, m is a positive integer greater than 0, and the angle between the lower traction steel cables and the vertical direction is less than 90°; the tension parameter of the lower traction steel cables is calculated by the following calculation formula: Among them, T d represents the tension parameter of the lower traction steel cable; ω represents the angle between the lower traction steel cable and the vertical direction.

7. The air-suspended starry sky tent device according to claim 6, characterized in that: When the controller is used to set the basic operating parameters of the elevator body according to the basic mechanical parameters, it includes: The basic thrust of the elevator shaft on the starry sky tent body is calculated by the following formula: F elevator =W tent -F buoyaney -T s -T d ; Among them, F elevator It represents the basic thrust of the elevator shaft on the starry sky tent body.

8. The air-suspended starry sky tent device according to claim 7, characterized in that: The controller is also used to adjust the basic thrust according to the preset environmental parameters to obtain the optimal thrust, including: The preset environmental parameters include the maximum wind speed and maximum humidity that the starry sky tent device can withstand; the optimal thrust is calculated by the following formula: Among them, F optimal represents the optimal thrust; α wind Represents the wind speed correction coefficient, that is, the influence of wind speed on thrust; α humidity Represents the humidity correction factor, that is, the influence of humidity on thrust; V wind,max Indicates the maximum wind speed; V wind,nom Indicates the annual average wind speed; H max Indicates the maximum humidity; H nom Indicates the average annual humidity.

9. The air-suspended starry sky tent device according to claim 8, characterized in that: The data acquisition module is used to collect real-time environmental parameters, and judge whether the elevator body is in a safe state according to the real-time environmental parameters and the real-time number of people, including: According to the real-time environmental parameters and the real-time number of people, the real-time load level of the elevator is calculated by the following formula: C eleuator =C base ·a wind ·a humidity ·a load ; Among them, C elevator Indicates the real-time load level of the elevator; C base It represents the basic bearing level of the elevator shaft when there is no external environmental influence and the elevator body is fully loaded; α wind , α humidity , α load They represent the adjustment coefficients of real-time wind speed, real-time humidity and real-time number of people respectively; The maximum load capacity of the elevator body is preset, denoted as C elevator,max ; When C elevator ≤C elevator,max When the elevator body is in a safe state for use, the judgment result is that the elevator body is in a safe state for use; otherwise, the judgment result is that the elevator body is not in a safe state for use, and at this time, the elevator body stops being used.

10. The air-suspended starry sky tent device according to claim 9, characterized in that: When the judgment result is that the elevator body is in a safe state for use, the data acquisition module calculates the safe operating speed of the elevator body according to the real-time environmental parameters and the real-time number of people, including: The safe operating speed of the elevator body is obtained by calculating the following formula: Among them, Vsafe represents the safe operating speed of the elevator body; Vbase represents the preset basic operating speed of the elevator body.

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