CN220367432U - Ball placing device and system applied to high-altitude image detection - Google Patents

Ball placing device and system applied to high-altitude image detection Download PDF

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Publication number
CN220367432U
CN220367432U CN202322049342.XU CN202322049342U CN220367432U CN 220367432 U CN220367432 U CN 220367432U CN 202322049342 U CN202322049342 U CN 202322049342U CN 220367432 U CN220367432 U CN 220367432U
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China
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ball placing
ball
inflation
balloon
outer balloons
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CN202322049342.XU
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Chinese (zh)
Inventor
李欣
郭启云
夏元彩
罗皓文
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CMA Meteorological Observation Centre
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CMA Meteorological Observation Centre
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

The disclosure relates to the technical field of meteorological detection, in particular to a ball placing device and system applied to high-altitude meteorological detection. The ball placing device applied to high-altitude image detection comprises a ball placing barrel and is arranged at the top of the ball placing device; the inflation release mechanism is arranged below the ball placing cylinder and is provided with a double-way inflation pipeline for simultaneously inflating the inner and outer balloons arranged on the ball placing cylinder and releasing the inner and outer balloons; and the air supply mechanism is connected with the two-way air inflation pipeline and is used for providing an air source for the inner and outer balloons. Above-mentioned technical scheme is through setting up the double-circuit gas filled line in inflating release mechanism to be connected with air feed mechanism with it, make this disclosure can be for possessing inlayer and outer double-deck sounding balloon and aerify simultaneously, convenient and fast.

Description

Ball placing device and system applied to high-altitude image detection
Technical Field
The disclosure relates to the technical field of meteorological detection, in particular to a ball placing device and system applied to high-altitude meteorological detection.
Background
Since the Assman of the German gas-image scholars in 1902 developed the atmospheric vertical detection mode by using rubber balloons and theodolites, the technology is adopted to carry out high-altitude detection internationally. Today, high-altitude meteorological detection is one of the work of the meteorological foundation business in China, and plays a very important role in the work of the meteorological business in China. 120 sounding stations in China release sounding balloons 2 times per day, and direct observation data is provided for numerical mode development, weather forecast and service.
However, in the existing high-altitude meteorological detection process, a single-layer sounding balloon is mostly adopted to carry a sounding instrument to detect meteorological observation data, and due to insufficient stability of the single-layer sounding balloon during flight, the continuity and reliability of the observation data detected by the carried sounding instrument are limited, so that the accuracy of meteorological prediction is affected.
Disclosure of Invention
In order to solve the problems in the related art, embodiments of the present disclosure provide a ball placement device and system for high-altitude image detection.
In a first aspect, embodiments of the present disclosure provide a ball placement device for use in high-altitude image detection.
Specifically, the ball placing device applied to high-altitude image detection comprises:
the ball placing cylinder is arranged at the top of the ball placing device;
the inflation release mechanism is arranged below the ball placing cylinder and is provided with a double-way inflation pipeline for simultaneously inflating the inner and outer balloons arranged on the ball placing cylinder and releasing the inner and outer balloons;
and the air supply mechanism is connected with the two-way air inflation pipeline and is used for providing an air source for the inner and outer balloons.
Optionally, the inflation release mechanism further includes:
and the gravity measuring mechanism is used for measuring the weight of the inner and outer balloons, and the inflation releasing mechanism releases the inner and outer balloons when the weight of the inner and outer balloons reaches a preset threshold value.
Optionally, an electromagnetic valve and a backfire preventer are sequentially arranged from the air inlet end to the air outlet end in each air charging branch of the two-way air charging pipeline;
the air outlet end is connected with an air charging nozzle.
Optionally, the method further comprises:
the gas flowmeter is arranged on a pipeline between the gas outlet end of the gas supply mechanism and the electromagnetic valve of the two-way gas charging pipeline.
Optionally, the method further comprises:
the explosion-proof assembly is arranged inside the ball placing device and comprises a gas leakage detector, an explosion-proof camera and an explosion-proof illuminating lamp.
Optionally, the method further comprises:
the water immersion sensor is arranged on the bottom surface and/or the side surface of the ball placing device.
Optionally, the method further comprises:
the wind shielding top cover is arranged above the ball placing barrel and hinged with the ball placing barrel, and can rotate to be perpendicular to the top surface of the ball placing barrel along the hinged position; and/or
The balloon protection net is arranged above the balloon placing cylinder.
In a second aspect, embodiments of the present disclosure provide a high-altitude image detection system.
Specifically, the high-altitude image detection system includes:
a ball placement device as claimed in any one of the first aspects for use in high-altitude image detection;
an inner balloon and an outer balloon are arranged in a ball placing barrel in the ball placing device;
and the sonde is hung below the inner and outer balloons.
Optionally, the method further comprises:
the parachute is arranged above the sonde;
and the cutting device is arranged at the outer side of the sonde and is used for separating the inner-outer balloon and the sonde.
Optionally, the method further comprises:
and the ultrasonic wind measuring device is used for measuring the wind speed and the wind direction when the inner and outer balloons are released.
The technical scheme provided by the embodiment of the disclosure can comprise the following beneficial effects:
the embodiment of the disclosure provides a ball placing device and a ball placing system applied to high-altitude image detection. The ball placing device applied to high-altitude image detection comprises a ball placing barrel and is arranged at the top of the ball placing device; the inflation release mechanism is arranged below the ball placing cylinder and is provided with a double-way inflation pipeline for simultaneously inflating the inner and outer balloons arranged on the ball placing cylinder and releasing the inner and outer balloons; and the air supply mechanism is connected with the two-way air inflation pipeline and is used for providing an air source for the inner and outer balloons. Above-mentioned technical scheme is through setting up the double-circuit gas filled line in inflating release mechanism to be connected with air feed mechanism with it, make this disclosure can be for possessing inlayer and outer double-deck sounding balloon and aerify simultaneously, convenient and fast. Because the inner and outer balloons fly in high air more stably, the sounding device is carried by the inner and outer balloons to detect high-altitude meteorological data, and the measured meteorological data are continuous and reliable, so that the accuracy of meteorological prediction is improved.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
Drawings
Other features, objects and advantages of the present disclosure will become more apparent from the following detailed description of non-limiting embodiments, taken in conjunction with the accompanying drawings. In the drawings:
fig. 1 shows a schematic configuration of a high-altitude image detection system according to an embodiment of the present disclosure.
Fig. 2 shows a plan view of a balloon apparatus for high-altitude image detection according to an embodiment of the present disclosure after deployment.
Fig. 3A illustrates a cross-sectional view of an elevation of an inflation release mechanism according to one embodiment of the present disclosure.
FIG. 3B illustrates a cross-sectional view of a side of an inflation release mechanism according to one embodiment of the present disclosure.
Fig. 4 shows a schematic structural view of a gravity measurement mechanism according to an embodiment of the present disclosure.
Fig. 5 shows a schematic structural view of a two-way inflation line according to one embodiment of the present disclosure.
A wind shielding top cover-1; ball placing cylinder-2; balloon protection net-3; an inner and outer balloon 4; a sonde-5; a cutting device-6; an ultrasonic wind measuring device-7; a gravity measuring mechanism-8; a gas flow meter-91; solenoid valve-92; a flashback arrestor-93; an inflation nozzle-94; a gas leakage detector-10; an explosion-proof camera 11; an explosion-proof lighting lamp-12; a water immersion sensor-13; a gas supply mechanism-14; an inflation release mechanism-15; a release member-16; paying-off device-17; a two-way inflation line-18; and a valve-19.
Detailed Description
Hereinafter, exemplary embodiments of the present disclosure will be described in detail with reference to the accompanying drawings so that those skilled in the art can easily implement them. In addition, for the sake of clarity, portions irrelevant to description of the exemplary embodiments are omitted in the drawings.
Moreover, those of ordinary skill in the art will appreciate that the drawings are provided herein for illustrative purposes and that the drawings are not necessarily drawn to scale.
Unless the context clearly requires otherwise, the words "comprise," "comprising," and the like in the description are to be construed in an inclusive sense as opposed to an exclusive or exhaustive sense; that is, it is the meaning of "including but not limited to".
In the description of the present disclosure, it is to be understood that the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Furthermore, in the description of the present disclosure, unless otherwise indicated, the meaning of "a plurality" is two or more.
Unless specifically stated or limited otherwise, the terms "mounted," "connected," "secured" and the like should be construed broadly, as they may be fixed, removable, or integral, for example; can be mechanically or electrically connected; either directly or indirectly, through intermediaries, or both, may be in communication with each other or in interaction with each other, unless expressly defined otherwise. The specific meaning of the terms in this disclosure will be understood by those of ordinary skill in the art as the case may be.
In addition, it should be noted that, without conflict, the embodiments of the present disclosure and features of the embodiments may be combined with each other. The present disclosure will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Since the Assman of the German gas-image scholars in 1902 developed the atmospheric vertical detection mode by using rubber balloons and theodolites, the technology is adopted to carry out high-altitude detection internationally. Today, high-altitude meteorological detection is one of the work of the meteorological foundation business in China, and plays a very important role in the work of the meteorological business in China. 120 sounding stations in China release sounding balloons 2 times per day, and direct observation data is provided for numerical mode development, weather forecast and service.
However, in the existing high-altitude meteorological detection process, a single-layer sounding balloon is mostly adopted to carry a sounding instrument to detect meteorological observation data, and due to insufficient stability of the single-layer sounding balloon during flight, the continuity and reliability of the observation data detected by the carried sounding instrument are limited, so that the accuracy of meteorological prediction is affected.
The present disclosure is provided to at least partially solve the problems in the prior art discovered by the inventors.
Fig. 1 shows a schematic configuration of a high-altitude image detection system according to an embodiment of the present disclosure.
As shown in fig. 1, the high-altitude image detection system of the present disclosure includes a balloon releasing device applied to high-altitude image detection, an inner balloon 4, an outer balloon 4 and a sonde 5, wherein the accurate control of the operation of each component in the high-altitude image detection system is realized by a host (not shown in the figure), and meanwhile, the host is also connected with a sonde (not shown in the figure), and the meteorological data detected by the sonde 5 is transmitted to the sonde by radio and then transmitted to the host for data processing and analysis, meteorological prediction and the like. The host may be, for example, a computer, a mobile terminal, or the like, which can implement a control function.
Fig. 2 shows a plan view of a balloon apparatus for high-altitude image detection according to an embodiment of the present disclosure after deployment. Fig. 3A illustrates a cross-sectional view of an elevation of an inflation release mechanism according to one embodiment of the present disclosure. FIG. 3B illustrates a cross-sectional view of a side of an inflation release mechanism according to one embodiment of the present disclosure.
As shown in fig. 1 and 2, the ball placing device for high-altitude image detection of the present disclosure includes a ball placing barrel 2 (the ball placing barrel 2 of the present disclosure is divided into an upper part and a lower part, the position marked in fig. 1 is the upper part of the ball placing barrel 2, and the position marked in fig. 2 is the lower part of the ball placing barrel 2), an inflation release mechanism 15, and an air supply mechanism 14.
Wherein, the ball placing cylinder 2 is arranged at the top of the ball placing device. The balloon releasing cylinder 2 of the present disclosure may be of various sizes to accommodate inner and outer balloons 4 having different weights after being inflated, for example, the volume of the balloon releasing cylinder 2 may be adapted to accommodate inner and outer balloons 4 having a weight of 300g to 750g after being inflated, or may be adapted to accommodate inner and outer balloons 4 having a weight of 1600g or more after being inflated, or the like. Those skilled in the art can set the setting according to the actual situation, and the disclosure is not limited thereto.
The inflation release mechanism 15 is disposed below the balloon releasing cylinder 2, and the inflation release mechanism 15 has a two-way inflation pipeline 18 (as shown in fig. 3A and 3B) for simultaneously inflating the inner and outer balloons 4 disposed on the balloon releasing cylinder 2 and releasing the inner and outer balloons 4. It can be appreciated that the release member 16 structure for releasing the inner and outer balloons 4 in the ball releasing device of the present disclosure may adopt an electromagnetic clutch, a link mechanism, a mechanical lock catch and the like in the prior art, and the inner and outer balloons 4 may be released by driving the link mechanism to push the mechanical lock catch through the electromagnetic clutch, which is not repeated in this disclosure.
Fig. 4 shows a schematic structural view of a gravity measurement mechanism according to an embodiment of the present disclosure.
As shown in fig. 4, specifically, the inflation release mechanism 15 further includes a gravity measurement mechanism 8 for measuring the weight of the inner and outer balloons 4, and when the weight of the inner and outer balloons 4 reaches a preset threshold, the inflation release mechanism 15 automatically releases the inner and outer balloons 4. The preset threshold value can be preset by an operator through a host, and in practical application, the error range between the actually measured weight of the inner and outer balloons 4 and the preset threshold value can be +/-10 g. The gravity measuring means 8 may be, for example, a sensor for measuring the net lifting force of the inner and outer balloons 4, or may be other sensors for measuring the gravity of the inner and outer balloons 4, etc.
Fig. 5 shows a schematic structural view of a two-way inflation line according to one embodiment of the present disclosure.
As shown in fig. 5, further, a solenoid valve 92 and a flashback preventer 93 are disposed in each of the two-way air charging branches of the two-way air charging pipeline 18 in sequence from the air inlet end to the air outlet end; the two air outlet ends are connected with air inlets 94, and the two air inlets 94 are respectively in butt joint with the inner-layer balloon and the outer-layer balloon of the inner-layer balloon 4. The charging connector 94 is inserted into the air inlet of the air valve 19, a 0-shaped sealing ring is arranged at the air inlet, and the charging connector 94 and the 0-shaped sealing ring are tightly matched to achieve the sealing effect. Before the inner and outer balloons 4 are released, the left and right hooks of the release member 16 fix the air valve 19, and after the inflation is completed, the left and right hooks of the release member 16 are released, and the inner and outer balloons 4 are released with the air valve 19. Preferably, each of the two-way inflation lines 18 further includes a gas flow meter 91 disposed in the line between the outlet end of the gas supply mechanism 14 and the solenoid valve 92 of the two-way inflation line 18.
Wherein, the air supply mechanism 14 is connected with the two-way inflation pipeline 18 and is used for providing an air source for the inner and outer balloons 4. The gas supply 14 may be, for example, a hydrogen cylinder and associated high pressure hose line, and/or may also be a helium cylinder and associated high pressure hose line, etc.
According to the embodiment of the disclosure, the main function of the balloon launching device applied to high-altitude meteorological detection is to release the inner and outer balloons 4 and the sonde 5 carried by the inner and outer balloons into the atmosphere together so as to detect meteorological data. Which completes the inflation and release of the inner and outer balloons 4 placed in the balloon-placing tube 2 by an inflation release mechanism 15, wherein the inflation is provided with a gas source by a gas supply mechanism 14. Specifically, the working process is as follows: when the inner and outer balloons 4 are not inflated, the electromagnetic valve 92 in each inflation branch of the two-way inflation pipeline 18 is in a closed state, and at the moment, the two-way inflation pipeline 18 is isolated; when the inner and outer balloons 4 need to be inflated, the host controls the electromagnetic valve 92 in each inflation branch of the two-way inflation pipeline 18 to be opened, and simultaneously, the gas in the gas supply mechanism 14 respectively enters the inner and outer balloons of the inner and outer balloons 4 from the two inflation branches of the two-way inflation pipeline 18 so as to inflate the inner and outer balloons at the same time, and after the inflation is completed, the electromagnetic valve 92 is closed, and the inner and outer balloons 4 are automatically bundled and released. In the process, the weight of the inner and outer balloons 4 can be measured in real time through the gravity measuring mechanism 8, and when the weight of the inner and outer balloons 4 reaches a preset threshold value, the electromagnetic valve 92 is closed, and the inflation release mechanism 15 releases the inner and outer balloons 4.
With continued reference to fig. 2, one or more safety protection or monitoring devices, such as an explosion-proof assembly and/or a water immersion sensor 13, may also be preferably provided within the ball placement device of the present disclosure for use in high-altitude image detection. The explosion-proof assembly is arranged inside the ball placing device and comprises a gas leakage detector 10, an explosion-proof camera 11 and an explosion-proof illuminating lamp 12; wherein, the water immersion sensor 13 is arranged on the bottom surface and/or the side surface of the ball placing device. It will be appreciated that in practice, the safety protection or monitoring device may be other types of devices, as well, and this disclosure is not limited in this regard.
With continued reference to fig. 2, one or more devices for protecting the inner and outer balloons 4, such as a windshield cover 1 and/or a balloon protection net 3, may also be preferably provided outside the balloon release device for high-altitude image detection of the present disclosure. The top cover 1 is arranged above the ball placing barrel 2 and hinged with the ball placing barrel 2, and the top cover 1 can rotate along the hinged position to be vertical to the top surface of the ball placing barrel 2; wherein, the balloon protection net 3 is arranged above the balloon placing cylinder 2. It will be appreciated that in practice, the means for protecting the inner and outer balloons 4 may be other types of devices, and this disclosure is not limited thereto.
With continued reference to fig. 1, according to an embodiment of the present disclosure, an inner and outer balloon 4 of the present disclosure is disposed in a balloon tube 2 in the balloon apparatus, and the inner and outer balloons 4 are double-layered sounding balloons having both inner and outer structures. In the process of meteorological detection, the inner layer and the outer layer of the double-layer sounding balloon are in an inflated state, the outer layer balloon explodes after rising to the high altitude of the preset height, and the inner layer balloon carries the sounding device 5 again to maintain floating at the height, so that the sounding device 5 can continuously detect meteorological data of the height. For example, the sonde 5 may be suspended in the stratosphere to detect the meteorological data of the stratosphere, thereby compensating for the defect of the prior art that the stratosphere detection blank occurs due to the inability to detect the stratosphere meteorological data. In addition, the types of the inflatable bodies in the inner-layer balloon and the outer-layer balloon of the inner-layer balloon 4 can be set according to specific conditions such as sounding height, for example, the inner-layer balloon and the outer-layer balloon are both inflated with hydrogen or helium; or the inner balloon is filled with hydrogen and the outer balloon is filled with helium; or the inner balloon is filled with helium, and the outer balloon is filled with hydrogen; or may be filled with other types of gas, etc. The present disclosure is not limited in this regard.
With continued reference to fig. 1, in accordance with an embodiment of the present disclosure, a sonde 5 of the present disclosure is suspended below the inner and outer balloons 4. The sonde 5 is a sonde 5 in the prior art, for example, may be a beidou sonde 5, etc., and the type of sonde 5 is not limited in this disclosure.
With continued reference to fig. 1, in accordance with an embodiment of the present disclosure, the high-altitude image detection system of the present disclosure further comprises a parachute, a cutting device 6 and/or an ultrasonic anemometer 7. Wherein, the parachute is arranged above the sonde 5; and the cutting device 6 is arranged at the outer side of the sonde 5 and is used for separating the inner and outer balloons 4 from the sonde 5. The ultrasonic wind measuring device 7 can be integrated on the balloon releasing device, can also be arranged beside the balloon releasing device and is used for testing the wind speed and the wind direction when the inner and outer balloons 4 are released. The ultrasonic wind measuring device 7 may be, for example, an ultrasonic wind meter or an ultrasonic wind meter, and the type of the ultrasonic wind measuring device 7 is not limited in the present disclosure.
According to an embodiment of the present disclosure, the operation of the high-altitude image detection system of the present disclosure is: the host is connected with the ball placing device and is connected with the sounding radar. And then acquiring wind speed and wind direction data tested by the ultrasonic wind measuring device 7 through a host computer, judging whether the current weather condition is suitable for meteorological detection, and if so, starting high-altitude detection. Specifically, the sonde 5 qualified in basic measurement is hung below the inner and outer balloons 4, then the inner and outer balloons 4, the paying-off device 17 and the sonde 5 are placed in the balloon releasing cylinder 2 in the balloon releasing device, an operator performs inflation control on the inner and outer balloons 4 through a host, when the weight of the inner and outer balloons 4 reaches a preset threshold for 15s, the wind shielding top cover 1 is controlled to be opened to the windward direction according to the wind speed and the wind direction measured by the ultrasonic wind measuring device 7 (when the wind speed measured in real time exceeds 20m/s, the wind shielding top cover 1 cannot be opened temporarily in the system standby state, when the wind speed measured in real time is less than 20m/s, the system continues to operate, the wind shielding top cover 1 is opened), when the weight of the inner and outer balloons 4 reaches the preset threshold, the wind shielding top cover 1 is automatically closed and reset to the original state after the inner and outer balloons 4 are released, and the next balloon releasing operation is waited. At this time, the inner and outer balloons 4 carry the sonde 5 to rise to the atmospheric high altitude area at a rising speed of 6m/s, the sonde 5 continuously measures and records weather data such as temperature, humidity, air pressure, air speed and air direction of different heights in the atmospheric vertical structure in the rising process, the data are transmitted to the sounding radar through radio, the data are transmitted to the host for data processing and analysis, the outer balloons explode after rising to the high altitude of 20000-30000 m, the inner balloons carry the sonde 5 again to float at the height of 20000-30000 m, so that the sonde 5 runs at the atmospheric altitude for a period of time to continuously detect weather data of the height, after the period of time of leveling, the host controls the cutting device 6 to cut off the connection between the inner and outer balloons 4 and the sonde 5, then the parachute arranged above the sonde 5 is opened, and the sonde 5 slowly descends at a speed of about 9m/s under the resistance of the parachute until the time is stopped for the operation personnel to recover, and thus the high altitude image detection is completed.
According to an embodiment of the present disclosure, a ball placement device for high-altitude image detection of the present disclosure includes: the ball placing cylinder is arranged at the top of the ball placing device; the inflation release mechanism is arranged below the ball placing cylinder and is provided with a double-way inflation pipeline for simultaneously inflating the inner and outer balloons arranged on the ball placing cylinder and releasing the inner and outer balloons; and the air supply mechanism is connected with the two-way air inflation pipeline and is used for providing an air source for the inner and outer balloons. Above-mentioned technical scheme is through setting up the double-circuit gas filled line in inflating release mechanism to be connected with air feed mechanism with it, make this disclosure can be for possessing inlayer and outer double-deck sounding balloon and aerify simultaneously, convenient and fast. Because the inner and outer balloons fly in high air more stably, the sounding device is carried by the inner and outer balloons to detect high-altitude meteorological data, and the measured meteorological data are continuous and reliable, so that the accuracy of meteorological prediction is improved.
According to an embodiment of the present disclosure, the inflation release mechanism further includes: and the gravity measuring mechanism is used for measuring the weight of the inner and outer balloons, and the inflation releasing mechanism releases the inner and outer balloons when the weight of the inner and outer balloons reaches a preset threshold value. The gravity measuring mechanism can improve the reliability of the inner and outer balloons when released, and avoid detection errors caused by insufficient or overweight weight of the inner and outer balloons.
According to the embodiment of the disclosure, an electromagnetic valve and a backfire preventer are sequentially arranged from an air inlet end to an air outlet end in each air charging branch of the two-way air charging pipeline; the air outlet end is connected with an air charging nozzle. The electromagnetic valve can realize accurate control on the inflation process of the inner and outer balloons, and ensures that the inner and outer balloons can reach preset inflation quantity; the backfire preventer can prevent the gas from flowing back into the gas supply mechanism from the inner and outer balloons, so that the stability and reliability of the inflation process are ensured; the inflating nozzle can ensure the rapid and stable inflation of the inner and outer balloons.
According to an embodiment of the present disclosure, the ball placement device further includes: the gas flowmeter is arranged on a pipeline between the gas outlet end of the gas supply mechanism and the electromagnetic valve of the two-way gas charging pipeline. The gas flowmeter is used for measuring the gas flow in the inflation process so as to realize the real-time control of the gas inflation and deflation amount and ensure the accuracy of the inflation amount of the inner balloon and the outer balloon.
According to an embodiment of the present disclosure, the ball placement device further includes: the explosion-proof assembly is arranged inside the ball placing device and comprises a gas leakage detector, an explosion-proof camera and an explosion-proof illuminating lamp. The explosion-proof assembly can ensure the safety of the ball placing device and the surrounding environment, wherein the gas leakage detector can detect the gas leakage condition in real time, so that operators can give an alarm in time or take corresponding protective measures; the explosion-proof camera and the explosion-proof illuminating lamp are convenient for operators to monitor the internal condition of the ball placing device in real time so as to discover abnormality in time.
According to an embodiment of the present disclosure, the ball placement device further includes: the water immersion sensor is arranged on the bottom surface and/or the side surface of the ball placing device. The water immersion sensor is easy to install and maintain, can accurately detect the water leakage condition in the ball placing device in a short time, and avoids equipment failure and safety problems caused by water immersion.
According to an embodiment of the present disclosure, the ball placement device further includes: the wind shielding top cover is arranged above the ball placing barrel and hinged with the ball placing barrel, and can rotate to be perpendicular to the top surface of the ball placing barrel along the hinged position; and/or a balloon protection net is arranged above the ball placing cylinder. The wind shielding top cover can effectively prevent factors such as external wind power, air flow and the like from affecting the inner and outer balloons in the ball releasing device, so that the safety of ball releasing operation is improved; the balloon protecting net can protect the inner balloon and the outer balloon from being damaged.
In accordance with an embodiment of the present disclosure, a high-altitude image detection system of the present disclosure includes: the ball placing device is applied to high-altitude image detection; an inner balloon and an outer balloon are arranged in a ball placing barrel in the ball placing device; and the sonde is hung below the inner and outer balloons. The high-altitude meteorological detection system has the advantages of high detection precision, excellent safety, low cost of each part in the system, repeated use for multiple meteorological detection, environmental protection and no pollution.
In accordance with an embodiment of the present disclosure, the high-altitude image detection system of the present disclosure further comprises: the parachute is arranged above the sonde; and the cutting device is arranged at the outer side of the sonde and is used for separating the inner-outer balloon and the sonde. The parachute can reduce the descending speed of the sonde, so that the sonde slowly descends and safely touches the ground, and the sonde is prevented from being damaged or lost due to rapid falling; the cutting device can rapidly separate the inner balloon and the outer balloon from the sonde, and is convenient for the recovery and the secondary utilization of the sonde.
In accordance with an embodiment of the present disclosure, the high-altitude image detection system of the present disclosure further comprises: and the ultrasonic wind measuring device is used for measuring the wind speed and the wind direction when the inner and outer balloons are released. The ultrasonic wind measuring device can accurately measure wind speed and wind direction, so that an operator can conveniently judge whether the current weather condition is suitable for meteorological detection, and the error of the host computer on the ball placing device caused by factors such as wind speed and wind direction is avoided.
The foregoing description is only of the preferred embodiments of the present disclosure and description of the principles of the technology being employed. It will be appreciated by those skilled in the art that the scope of the utility model referred to in this disclosure is not limited to the specific combination of features described above, but encompasses other embodiments in which any combination of features described above or their equivalents is contemplated without departing from the inventive concepts described. Such as those described above, are mutually substituted with the technical features having similar functions disclosed in the present disclosure (but not limited thereto).

Claims (10)

1. A ball placement device for high-altitude image detection, comprising:
the ball placing cylinder is arranged at the top of the ball placing device;
the inflation release mechanism is arranged below the ball placing cylinder and is provided with a double-way inflation pipeline for simultaneously inflating the inner and outer balloons arranged on the ball placing cylinder and releasing the inner and outer balloons;
and the air supply mechanism is connected with the two-way air inflation pipeline and is used for providing an air source for the inner and outer balloons.
2. The ball placement device of claim 1, wherein the inflation release mechanism further comprises:
and the gravity measuring mechanism is used for measuring the weight of the inner and outer balloons, and the inflation releasing mechanism releases the inner and outer balloons when the weight of the inner and outer balloons reaches a preset threshold value.
3. Ball placement device according to claim 1 or 2, characterized in that,
an electromagnetic valve and a backfire preventer are sequentially arranged from an air inlet end to an air outlet end in each inflation branch of the two-way inflation pipeline;
the air outlet end is connected with an air charging nozzle.
4. A ball placement device as defined in claim 3, further comprising:
the gas flowmeter is arranged on a pipeline between the gas outlet end of the gas supply mechanism and the electromagnetic valve of the two-way gas charging pipeline.
5. The ball placement device according to claim 1 or 2, further comprising:
the explosion-proof assembly is arranged inside the ball placing device and comprises a gas leakage detector, an explosion-proof camera and an explosion-proof illuminating lamp.
6. The ball placement device according to claim 1 or 2, further comprising:
the water immersion sensor is arranged on the bottom surface and/or the side surface of the ball placing device.
7. The ball placement device according to claim 1 or 2, further comprising:
the wind shielding top cover is arranged above the ball placing barrel and hinged with the ball placing barrel, and can rotate to be perpendicular to the top surface of the ball placing barrel along the hinged position; and/or
The balloon protection net is arranged above the balloon placing cylinder.
8. A high-altitude meteorological detection system, comprising:
a ball placement device for use in high-altitude image detection as claimed in any one of claims 1 to 7;
an inner balloon and an outer balloon are arranged in a ball placing barrel in the ball placing device;
and the sonde is hung below the inner and outer balloons.
9. The system of claim 8, further comprising:
the parachute is arranged above the sonde;
and the cutting device is arranged at the outer side of the sonde and is used for separating the inner-outer balloon and the sonde.
10. The system according to claim 8 or 9, further comprising:
and the ultrasonic wind measuring device is used for measuring the wind speed and the wind direction when the inner and outer balloons are released.
CN202322049342.XU 2023-08-01 2023-08-01 Ball placing device and system applied to high-altitude image detection Active CN220367432U (en)

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