Ballast adjusting system for high-altitude balloon

Abstract

The utility model relates to a ballast adjusting system for a high-altitude balloon, and relates to the technical field of high-altitude balloons. Comprising an outer balloon, an inner balloon, a storage cabin, a ballast, a first control switch and a movable baffle. A first accommodating space is formed in the outer balloon, and the first accommodating space is filled with buoyancy lift gas; the inner balloon is arranged in the first accommodating space, and a second accommodating space is formed in the inner balloon; a third accommodating space is formed in the storage cabin, and the third accommodating space communicates with the second accommodating space; the ballast is arranged in the third containing space and used for being gasified to enter the second containing space. The first control switch is arranged at the joint of the storage cabin and the inner balloon; an opening is formed in the side, away from the inner balloon, of the storage bin and communicates with the third containing space, and the movable baffle covers the opening. The problems that the ballast adjusting system of the high-altitude balloon is poor in sustainable adjusting effect and high in energy consumption are solved by prolonging the time through phase change of the ballast and opening and closing of the movable baffle.

Description

Technical Field

[0001] The utility model relates to the technical field of high-altitude balloons, in particular to a ballast adjustment system for high-altitude balloons. Background Technique

[0002] High-altitude balloons rely on buoyant gases to float above the stratosphere and perform tasks at high altitudes.

[0003] At present, the ballast adjustment method on high-altitude balloons usually relies on throwing solid ballast or compressing and discharging air. In the case of only using solid ballast, after throwing, the balloon loses the possibility of rising and the mission faces termination. In the case of only using compressed air discharge, a large-power fan / compressor is required, consuming the energy on the balloon.

[0004] In order to achieve ballast adjustment with lower energy consumption and better sustainability.

[0005] In view of the above-mentioned related technologies, there are problems of poor sustainability adjustment effect and high energy consumption in the existing ballast adjustment system of high-altitude balloons. Content of the Utility Model

[0006] In view of the above deficiencies of the prior art, the purpose of the present utility model is to provide a ballast adjustment system for high-altitude balloons, aiming to solve the problems of poor sustainability adjustment effect and high energy consumption in the existing ballast adjustment system of high-altitude balloons.

[0007] A ballast adjustment system for high-altitude balloons provided by the present application adopts the following technical solution: A ballast adjustment system for high-altitude balloons, comprising:

[0008] An outer balloon, having a first accommodation space formed inside, and the first accommodation space is filled with a buoyant gas;

[0009] An inner balloon, disposed in the first accommodation space, and a second accommodation space is formed inside the inner balloon;

[0010] A storage compartment, on which the outer balloon and the inner balloon are disposed, a third accommodation space is formed inside the storage compartment, and the third accommodation space is communicated with the second accommodation space. Wherein, a heat preservation layer is provided on the inner wall of the storage compartment;

[0011] Ballast, disposed in the third accommodation space, and the ballast is used to vaporize and enter the second accommodation space;

[0012] A first control switch, disposed at the connection between the storage compartment and the inner balloon, and the first control switch is used for the communication or isolation between the second accommodation space and the third accommodation space;

[0013] The movable baffle, an opening is provided on the side of the storage compartment facing away from the inner balloon, the opening communicates with the third accommodation space, the movable baffle covers the opening, and the movable baffle is used to open or close the opening.

[0014] Optionally, the ballast adjustment system for the high-altitude balloon includes a heating element, the heating element is arranged in the third accommodation space, and the heating element is used to accelerate the gasification of the ballast.

[0015] Optionally, the ballast adjustment system for the high-altitude balloon includes a control element, the control element is electrically connected to the heating element, and the control element is used to control the start or stop of the heating element.

[0016] Optionally, the control element is electrically connected to the movable baffle, and the control element is used to control the movable baffle to open or close the opening.

[0017] Optionally, the movable baffle includes a baffle substrate and an electromagnet, one side of the baffle substrate is hinged to the storage compartment, the electromagnet is arranged on the other side of the baffle substrate, and the electromagnet is electrically connected to the control element;

[0018] A magnetic attracting element is arranged on the storage compartment, and the magnetic attracting element is used to adsorb the electromagnet;

[0019] When the electromagnet is energized, the electromagnet has the magnetism to adsorb the magnetic attracting element;

[0020] When the electromagnet is de-energized, the magnetism of the electromagnet disappears.

[0021] Optionally, the control element is electrically connected to the first control switch, and the control element is used to control the first control switch to connect or isolate the third accommodation space and the second accommodation space.

[0022] Optionally, the ballast adjustment system for the high-altitude balloon includes an altimeter, the altimeter is arranged on the storage compartment, and the altimeter is electrically connected to the control element.

[0023] Optionally, the ballast adjustment system for the high-altitude balloon includes a second control switch, and the second control switch is arranged at the connection between the storage compartment and the outer balloon;

[0024] The control element is electrically connected to the second control switch, and the control element is used to control the second control switch to connect or isolate the third accommodation space and the first accommodation space.

[0025] Optionally, the ballast adjustment system for the high-altitude balloon includes a solar drive element, and the solar drive element is arranged on the storage compartment;

[0026] The solar energy driving member is electrically connected to the control member, and the solar energy driving member is used to supply power to the ballast adjustment system for the high-altitude balloon.

[0027] Optionally, the lifting gas is one of helium and hydrogen.

[0028] Compared with the prior art, the embodiment of the present utility model has the following advantages:

[0029] When the high-altitude balloon operates at night, since the volume of the lifting gas will be compressed due to the decrease in temperature at night, the outer balloon will drop significantly. At this time, it is necessary to squeeze the internal lifting gas of the outer balloon to increase the buoyancy.

[0030] Open the first control switch to connect the second accommodation space and the third accommodation space. The ballast gasifies and enters the second accommodation space. At this time, the inner balloon will expand as the gasified ballast is filled, thereby squeezing the outer balloon to increase the buoyancy. Then close the first control switch to isolate the second accommodation space and the third accommodation space.

[0031] When the buoyancy of the outer balloon is seriously insufficient, the movable bottom plate can be opened to discard the remaining ballast in the storage compartment to reduce the total load mass and make the balloon rise again.

[0032] When the altitude approaches the highest threshold, open the first control switch again to connect the second accommodation space and the third accommodation space, and discharge the gasified ballast in the inner balloon to avoid the outer balloon from expanding too much and bursting, extend the mission time, improve the sustainability of the ballast adjustment system, and do not require a high-power blower or compressor, reduce the overall energy consumption, and solve the problems of poor sustainability adjustment effect and high energy consumption of the existing ballast adjustment system for high-altitude balloons. Description of the Drawings

[0033] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model or the prior art, the following will briefly introduce the drawings required for the description of the embodiments or the prior art. Obviously, the drawings in the following description are only some embodiments recorded in the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0034] Figure 1 It is a schematic structural diagram of the ballast adjustment system for the high-altitude balloon in the embodiment of the present application when the ballast does not gasify and enter the second accommodation space;

[0035] Figure 2 It is a schematic structural diagram of the ballast adjustment system for the high-altitude balloon in the embodiment of the present application when the ballast gasifies and enters the second accommodation space;

[0036] Figure 3 It is a schematic structural diagram of the opening of the movable baffle of the ballast adjustment system for high-altitude balloons and the discharge range of the vaporized ballast from the second accommodation space in the embodiments of the present application.

[0037] Description of the reference numerals:

[0038] 01, outer balloon; 011, first accommodation space; 02, inner balloon; 021, second accommodation space; 03, storage cabin; 031, storage body; 032, connecting part; 033, third accommodation space; 0331, storage space; 0332, air passage; 04, ballast; 05, first control switch; 06, movable baffle; 07, heating element; 08, control element; 09, solar drive element; 10, power storage module. Detailed implementation manners

[0039] In order to enable those skilled in the art to better understand the solution of the present utility model, the technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0040] The following further details the present application with reference to the accompanying drawings of the specification.

[0041] The embodiments of the present application disclose a ballast adjustment system for high-altitude balloons.

[0042] As Figure 1 、 Figure 2 and Figure 3As shown in the figure, a ballast adjustment system for a high-altitude balloon includes an outer balloon 01, an inner balloon 02, a storage compartment 03, ballast 04, a first control switch 05, and a movable baffle 06. A first accommodation space 011 is formed inside the outer balloon 01, and a lifting gas is filled in the first accommodation space 011; the inner balloon 02 is arranged in the first accommodation space 011, and a second accommodation space 021 is formed inside the inner balloon 02; the outer balloon 01 and the inner balloon 02 are arranged on the storage compartment 03, a third accommodation space 033 is formed inside the storage compartment 03, and the third accommodation space 033 is communicated with the second accommodation space 021; the ballast 04 is arranged in the third accommodation space 033, and the ballast 04 is used to gasify and enter the second accommodation space 021; the first control switch 05 is arranged at the connection between the storage compartment 03 and the inner balloon 02, and the first control switch 05 is used for the communication or isolation between the second accommodation space 021 and the third accommodation space 033; an opening is arranged on one side of the storage compartment 03 facing away from the inner balloon 02, the opening is communicated with the third accommodation space 033, and the movable baffle 06 covers the opening, and the movable baffle 06 is used to open or close the opening.

[0043] The lifting gas filled in the first accommodation space 011 is one of helium and hydrogen. In this embodiment, helium is selected as the lifting gas.

[0044] When the high-altitude balloon operates at night, since the volume of the lifting gas will be compressed due to the decrease in temperature at night, the outer balloon 01 will drop significantly. At this time, it is necessary to squeeze the internal lifting gas of the outer balloon 01 to increase the buoyancy.

[0045] Open the first control switch 05 to communicate the second accommodation space 021 and the third accommodation space 033. The ballast 04 gasifies and enters the second accommodation space 021. At this time, the inner balloon 02 will expand as the gasified ballast 04 is filled, thereby squeezing the outer balloon 01 to increase the buoyancy, and then close the first control switch 05 to isolate the second accommodation space 021 and the third accommodation space 033.

[0046] When the buoyancy of the outer balloon 01 is seriously insufficient, the movable bottom plate can be opened to discard the remaining ballast 04 in the storage compartment 03 to reduce the total load mass and make the balloon rise again.

[0047] When the altitude approaches the highest threshold, the first control switch 05 is turned on again to connect the second accommodation space 021 and the third accommodation space 033, and the vaporized ballast 04 in the inner balloon 02 is discharged to prevent the outer balloon 01 from over-expanding and bursting, extend the mission time, improve the sustainability of the ballast 04 adjustment system, and eliminate the need for a high-power blower or compressor, reducing the overall energy consumption and solving the problems of poor sustainability adjustment effect and high energy consumption of the existing ballast 04 adjustment system for high-altitude balloons.

[0048] The ballast adjustment system for a high-altitude balloon includes a heating element 07, which is arranged in the third accommodation space 033 and is used to accelerate the vaporization of the ballast 04.

[0049] Specifically, since the lowest temperature at the altitude where the high-altitude balloon flies is -70 °C to -90 °C, and the phase change vaporization point of dry ice is -78.5 °C, it can remain in a substantially solid state without heating at high altitude. Therefore, dry ice is selected as the ballast 04 in this embodiment.

[0050] The storage compartment 03 includes a storage body 031 and a connecting part 032. One end of the connecting part 032 is arranged on the storage body 031, and the outer balloon 01 and the inner balloon 02 are respectively arranged at the other end of the connecting part 032.

[0051] The third accommodation space 033 includes a storage space 0331 and a gas passage 0332. Among them, the storage space 0331 is formed inside the storage body 031, the gas passage 0332 is formed inside the connecting part 032, one end of the gas passage 0332 communicates with the storage space 0331, and the other end communicates with the second accommodation space 021.

[0052] The ballast 04 is arranged in the storage space 0331, and the first control switch 05 is arranged at the connection between the connecting part 032 and the inner balloon 02.

[0053] When the ballast 04 vaporizes into carbon dioxide gas, the first control switch 05 is turned on, and the carbon dioxide gas can enter the second accommodation space 021 through the gas passage 0332.

[0054] The heating element 07 is a heating wire, which is located in the storage space 0331 and is arranged on the top wall of the storage body 031.

[0055] When the heating element 07 heats up, it can raise the temperature in the storage space 0331, thereby accelerating the vaporization of dry ice.

[0056] Furthermore, a heat-insulating layer is arranged in the storage compartment 03, and the heat-insulating layer has the function of heat insulation, which helps to slow down the vaporization speed of dry ice.

[0057] The ballast adjustment system for the high-altitude balloon includes a control member 08, which is electrically connected to the heating member 07, and the control member 08 is used to control the start or shutdown of the heating member 07.

[0058] The control member 08 is electrically connected to the movable baffle 06, and the control member 08 is used to control the movable baffle 06 to open or close the opening.

[0059] The control member 08 is electrically connected to the first control switch 05, and the control member 08 is used to control the first control switch 05 to connect or isolate the third accommodation space 033 and the second accommodation space 021.

[0060] Specifically, the control member 08 is a circuit board, and the control member 08 is arranged outside the storage compartment 03. To reduce damage to the control member 08 from the outside, a protective shell is arranged outside the control member 08.

[0061] A long-distance wireless control module, such as an LR-WIFI module, is arranged on the control member 08. The control member 08 can give signal feedback to the ground operator and the operator can perform command operations on the control member 08 on the ground.

[0062] The first control switch 05 is an electric valve, and its on-off can be controlled by being powered on.

[0063] The control member 08 is electrically connected to the heating member 07, the movable baffle 06 and the first control switch 05 respectively.

[0064] When the outer balloon 01 needs to squeeze the lifting gas inside the outer balloon 01 to increase the buoyancy at night when its volume shrinks, the first control switch 05 is first opened through the control member 08 to connect the gas passing channel 0332 with the second accommodation space 021. Then, the heating member 07 is started through the control member 08 to heat the storage space 0331. The dry ice is heated and accelerated to gasify into carbon dioxide gas, and the carbon dioxide gas enters the second accommodation space 021. At this time, the inner balloon 02 will expand as it is filled with carbon dioxide gas and thus squeeze the outer balloon 01 to increase the buoyancy. When the buoyancy meets the actual requirements, the first control switch 05 is closed through the control member 08 to isolate the gas passing channel 0332 from the second accommodation space 021.

[0065] When the buoyancy of the outer balloon 01 is seriously insufficient, the movable bottom plate is opened through the control member 08 to discard the remaining dry ice in the storage compartment 03 to reduce the total load mass and make the balloon rise again.

[0066] When the altitude approaches the maximum threshold, the first control switch 05 is opened again through the control component 08 to connect the second accommodating space 021 and the third accommodating space 033, and the carbon dioxide gas in the inner balloon 02 is discharged to prevent the outer balloon 01 from over-expanding and bursting, thereby extending the mission time and solving the problems of poor sustainable adjustment effect and high energy consumption of the existing high-altitude balloon ballast 04 adjustment system.

[0067] Furthermore, the movable baffle 06 includes a baffle substrate and an electromagnet.

[0068] One side of the baffle substrate is hinged to the side of the storage compartment 03 away from the inner balloon 02, that is, the baffle substrate is hinged to the bottom wall of the storage compartment 03, and the baffle substrate can be attached to the bottom wall of the storage compartment 03. When the baffle substrate is attached to the bottom wall of the storage compartment 03, the baffle substrate can completely cover the opening, thereby preventing the dry ice in the third storage space 033 from leaking out of the opening.

[0069] The electromagnet is arranged on the other side of the baffle substrate, and a magnetic attraction component is arranged on the storage compartment 03. When the baffle substrate is attached to the bottom wall of the storage compartment 03, the electromagnet can abut against the magnetic attraction component.

[0070] The electromagnet is electrically connected to the control component 08. When the electromagnet is energized, it has strong magnetism and is attracted to the magnetic element, so that the baffle substrate abuts against the bottom wall of the storage compartment 03, completely covering the opening.

[0071] When the electromagnet is not energized, the strong magnetism of the electromagnet disappears. At this time, the electromagnet and the magnetic attraction part are no longer attracted. Under the action of gravity, the baffle substrate rotates and no longer abuts against the bottom wall of the storage compartment 03. At this time, the opening is no longer covered by the baffle substrate, and the dry ice in the storage space 0331 can be dumped to the outside.

[0072] It should be noted that the structure of the movable baffle 06 is not limited to this, as long as the movable baffle 06 can be opened or closed when powered.

[0073] The ballast adjustment system for the high-altitude balloon includes an altimeter, which is disposed on the storage cabin 03 and is electrically connected to the control component 08 .

[0074] Specifically, the altitude information collected by the altimeter can be known to the operator in real time, so that the subsequent inflation, deflation and casting operations can be performed through the control unit 08.

[0075] The ballast regulating system for high-altitude balloons includes a second control switch, which is arranged at the connection between the storage cabin 03 and the outer balloon 01;

[0076] The control member 08 is electrically connected to the second control switch, and the control member 08 is configured to control the second control switch to connect or isolate the third accommodation space 033 and the first accommodation space 011.

[0077] Specifically, the second control switch is an electric valve, and the electric valve can control the second control switch to connect the third accommodation space 033 and the first accommodation space 011, so that the floating gas in the first accommodation space 011 is discharged to the outside through the third accommodation space 033, thereby enabling the descent or recovery of the high-altitude balloon.

[0078] It should be noted that the second control switch may not be provided. That is, when the floating gas is not sufficient to support the floating of the high-altitude balloon, it can freely land and wait for the recovery personnel to recover it.

[0079] The ballast adjustment system for the high-altitude balloon includes a solar drive member 09, and the solar drive member 09 is disposed on the storage compartment 03;

[0080] The solar drive member 09 is electrically connected to the control member 08, and the solar drive member 09 is configured to supply power to the ballast adjustment system for the high-altitude balloon.

[0081] Specifically, the solar drive member 09 is a solar panel, and the solar drive member 09 can convert solar energy into electrical energy, thereby providing energy for the circuit of the entire ballast adjustment system for the high-altitude balloon.

[0082] The ballast adjustment system for the high-altitude balloon further includes a power storage module 10. The power storage module 10 is electrically connected to the solar drive member 09, and the power storage module 10 can store the excess electrical energy converted by the solar drive member 09 for use when the ballast adjustment system for the high-altitude balloon operates in the absence of sunlight, such as at night or on cloudy days.

[0083] The setting of the solar drive member 09 ensures a stable power supply and reduces the usage cost of the ballast adjustment system for the high-altitude balloon.

[0084] In summary, a ballast adjustment system for a high-altitude balloon includes an outer balloon 01, an inner balloon 02, a storage compartment 03, ballast 04, a first control switch 05, and a movable baffle 06. A first accommodation space 011 is formed inside the outer balloon 01, and the first accommodation space 011 is filled with a lifting gas; the inner balloon 02 is disposed in the first accommodation space 011, and a second accommodation space 021 is formed inside the inner balloon 02; the outer balloon 01 and the inner balloon 02 are disposed on the storage compartment 03, and a third accommodation space 033 is formed inside the storage compartment 03, and the third accommodation space 033 communicates with the second accommodation space 021; the ballast 04 is disposed in the third accommodation space 033, and the ballast 04 is used to gasify and enter the second accommodation space 021; the first control switch 05 is disposed at the connection between the storage compartment 03 and the inner balloon 02, and the first control switch 05 is used to connect or isolate the second accommodation space 021 and the third accommodation space 033; an opening is provided on one side of the storage compartment 03 facing away from the inner balloon 02, the opening communicates with the third accommodation space 033, and the movable baffle 06 covers the opening, and the movable baffle 06 is used to open or close the opening.

[0085] When the outer balloon 01 shrinks in volume at night and it is necessary to squeeze the internal lifting gas of the outer balloon 01 to increase buoyancy, the first control switch 05 is opened to connect the second accommodation space 021 and the third accommodation space 033, and the ballast 04 gasifies and enters the second accommodation space 021. At this time, the inner balloon 02 expands as the gasified ballast 04 is filled, thereby squeezing the outer balloon 01 to increase buoyancy. Then, the first control switch 05 is closed to isolate the second accommodation space 021 and the third accommodation space 033.

[0086] When the buoyancy of the outer balloon 01 is seriously insufficient, the movable bottom plate can be opened to discard the remaining ballast 04 in the storage compartment 03 to reduce the total load mass and make the balloon rise again.

[0087] When the altitude approaches the highest threshold, the first control switch 05 is opened again to connect the second accommodation space 021 and the third accommodation space 033, and the gasified ballast 04 in the inner balloon 02 is discharged to prevent the outer balloon 01 from expanding too much and bursting, extend the mission time, improve the sustainability of the ballast 04 adjustment system, and eliminate the need to set up high-power fans or compressors, reduce the overall energy consumption, and solve the problems of poor sustainability adjustment effect and high energy consumption of the existing ballast 04 adjustment system for high-altitude balloons.

[0088] It should be noted that, without conflict, the embodiments in the present application and the features in the embodiments can be combined with each other.

[0089] It should be noted that the present utility model takes a ballast adjustment system for high-altitude balloons as an example to introduce the specific structure and working principle of the present utility model. However, the application of the present utility model is not limited to a ballast adjustment system for high-altitude balloons, and it can also be applied to the production and use of other similar workpieces.

[0090] It should be understood that the present utility model is not limited to the precise structure already described and shown in the drawings, and various modifications and changes can be made without departing from its scope. The scope of the present utility model is only limited by the appended claims.

[0091] The above are only the preferred embodiments of the present utility model, and are not intended to limit the present utility model. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included in the protection scope of the present utility model.

Claims

1. A ballast regulating system for a high-altitude balloon, characterized in that: include: The outer balloon has a first accommodation space formed therein, and the first accommodation space is filled with buoyancy gas; an inner balloon, disposed in the first accommodation space, wherein a second accommodation space is formed in the inner balloon; A storage cabin, the outer balloon and the inner balloon are arranged on the storage cabin, a third accommodation space is formed inside the storage cabin, the third accommodation space is communicated with the second accommodation space, wherein an inner wall of the storage cabin is provided with a heat preservation layer; Ballast material is arranged in the third accommodation space, and the ballast material is used to be gasified and enter into the second accommodation space; a first control switch, disposed on the storage compartment, for connecting or isolating the second storage space and the third storage space; A movable baffle, an opening is provided on a side of the storage compartment away from the inner balloon, the opening is connected to the third accommodating space, the movable baffle covers the opening, and the movable baffle is used to open or close the opening.

2. The ballast regulating system for high altitude balloons according to claim 1, characterized in that: The ballast regulating system for a high-altitude balloon includes a heating element, which is disposed in the third containing space and is used to accelerate the gasification of the ballast.

3. The ballast regulating system for high altitude balloons according to claim 2, characterized in that: The ballast regulating system for a high-altitude balloon comprises a control element, wherein the control element is electrically connected to the heating element, and the control element is used to control the activation or deactivation of the heating element.

4. The ballast regulating system for high altitude balloons according to claim 3, characterized in that: The control member is electrically connected to the movable baffle, and is used to control the movable baffle to open or close the opening.

5. The ballast regulating system for high-altitude balloons according to claim 4, characterized in that: The movable baffle includes a baffle substrate and an electromagnet, one side of the baffle substrate is hinged to the storage compartment, the electromagnet is arranged on the other side of the baffle substrate, and the electromagnet is electrically connected to the control member; The storage compartment is provided with a magnetic attraction member, and the magnetic attraction member is used to be adsorbed with the electromagnet; When the electromagnet is energized, the electromagnet has the magnetism to attract the magnetic attraction member; When the electromagnet is not energized, the magnetism of the electromagnet disappears.

6. The ballast regulating system for high altitude balloons according to claim 3, characterized in that: The control element is electrically connected to the first control switch, and is used to control the first control switch to connect or isolate the third accommodation space from the second accommodation space.

7. The ballast regulating system for high-altitude balloons according to claim 6, characterized in that: The ballast adjustment system for a high-altitude balloon includes an altimeter, which is disposed on the storage cabin and is electrically connected to the control element.

8. The ballast regulating system for high altitude balloons according to claim 3, characterized in that: The ballast regulating system for high-altitude balloons includes a second control switch, which is arranged at the connection between the storage compartment and the outer balloon; The control element is electrically connected to the second control switch, and the control element is used to control the second control switch to connect or isolate the third accommodation space from the first accommodation space.

9. The ballast regulating system for high altitude balloons according to claim 3, characterized in that: The ballast regulating system for high-altitude balloons includes a solar-powered drive member, and the solar-powered drive member is disposed on the storage cabin; The solar-powered driving component is electrically connected to the control component, and the solar-powered driving component is used to supply power to the ballast regulating system for the high-altitude balloon.

10. The ballast regulating system for a high altitude balloon according to claim 1, characterized in that: The buoyancy gas is one of helium and hydrogen.

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