Aviation meteorological detection device

Abstract

The utility model discloses an aviation meteorological detection device, which belongs to the technical field of meteorological detection, and is provided with a detection assembly, an inflation assembly, a protection assembly and a protection assembly, a sonde for detecting weather is installed inside a storage basket during use, and the part, used for detection, of the sonde is exposed outside the storage basket, so that the detection is more convenient. Then the sonde is sent to the high altitude through the meteorological balloon, so that the meteorological on the high altitude is detected, the stability of the meteorological balloon can be improved through a first protection ring, a connecting strip and a second protection ring, the meteorological balloon can be protected through a protection strip and a protection ring, and the meteorological balloon is prevented from colliding with a flyer to explode in the high altitude; when the gas content in the meteorological balloon is insufficient, the gas in the temporal part of the gas tank can be inflated into the meteorological balloon through the gas pump, so that the sonde can be used for detecting the weather in the air, the accuracy of meteorological data is improved, and meanwhile, the safety and cruising ability of the meteorological balloon can be ensured.

Description

Technical Field

[0001] The utility model relates to the technical field of meteorological detection, in particular to an aviation meteorological detection device. Background Art

[0002] Aviation meteorological detection refers to the use of meteorological observation data and technology to monitor, predict and report weather conditions in the aviation field to ensure aviation safety and operational efficiency. Aviation meteorological detection is a vital link in the field of air transportation and has a direct impact on flight takeoff and landing, route selection, flight altitude and flight safety.

[0003] Existing aviation meteorological collection devices are all split-type designs. During on-site installation, the installer needs to fix the meteorological sensor to the bracket with screws, the bracket is installed on the pole with a U-shaped clamp, and the junction box needs to be fixed with screws separately, which is inconvenient to install;

[0004] The existing patent (publication number: CN218119189U) is an aviation meteorological collection device. This utility model sets the box-shaped part and the meteorological sensor on the mounting bracket, and realizes the tight connection between the box cover and the box-shaped part by setting an annular mounting plate and a captive screw, so that the aviation meteorological collection device is integrated in design, which can effectively prevent the connection parts from falling off during installation and use, and is simple to operate and easy to install.

[0005] In view of the above problems, existing patents have provided solutions, but in actual use, they can only collect and detect weather in a fixed area, resulting in inaccurate detection data. At the same time, the detection altitude is low and cannot be well adapted to the requirements of aviation meteorological collection and detection.

[0006] Therefore, an aviation meteorological detection device is proposed. Utility Model Content

[0007] The purpose of the utility model is to provide an aviation meteorological detection device, which can solve the problem that the existing aviation meteorological detection devices can only collect and detect the weather in a fixed area during actual use, resulting in inaccurate detection data, and at the same time the detection height is low and cannot be well adapted to the requirements of aviation meteorological collection and detection.

[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation meteorological detection device, comprising a base, a detection component is arranged on the top of the base, an inflation component is arranged on one side of the detection component, a protection component is arranged on one side of the detection component, a protection component is arranged on one side of the protection component, a limit component is arranged on the top of the base, and a recovery component is arranged on one side of the base;

[0009] The detection assembly includes a storage basket, a sonde, a connecting rope and a weather balloon. The storage basket is movably connected to the top of the base, the sonde is arranged inside the storage basket, a plurality of connecting ropes are arranged on the top of the storage basket, and the weather balloon is arranged on the top of a plurality of connecting ropes and used in conjunction with the storage basket.

[0010] Preferably, the inflation assembly includes a gas tank, an air pump and a connecting pipe, the gas tank is arranged inside the storage basket, the air pump is arranged on one side of the gas tank and used in conjunction with the gas tank, one end of the connecting pipe is arranged at the output end of the air pump and the other end is arranged inside the weather balloon.

[0011] Preferably, the protective assembly includes a first protective ring, a connecting strip and a second protective ring, the first protective ring is arranged at the bottom of the weather balloon, a plurality of the connecting strips are fixedly connected to the top of the first protective ring, and the second protective ring is fixedly connected between the plurality of connecting strips.

[0012] Preferably, the protection assembly comprises a protection strip and a protection ring, a plurality of the protection strips are welded to the top of the second protection ring, and the protection ring is welded between the plurality of protection strips.

[0013] Preferably, the limit assembly includes a limit block, a limit rope, a limit hook and a limit hook, a plurality of the limit blocks are fixedly connected to the top of the base, the limit rope is arranged at the top of the limit block, the limit hook is fixedly connected to the end of the limit rope away from the limit block, and a plurality of the limit hooks are fixedly connected to one side of the second protective ring and used in conjunction with the limit hook.

[0014] Preferably, the recovery component includes a recovery trough, a recovery plate, a wire wheel, a recovery rope, a motor and a connecting block, the recovery trough is opened on one side of the base, the two recovery plates are fixedly connected to the bottom of the base, the wire wheel is rotatably connected between the two recovery plates, the recovery rope is arranged on one side of the wire wheel, the motor is arranged on one side of the recovery plate and the output end is fixedly connected to one side of the wire wheel, and the connecting block is fixedly connected to the bottom of the storage basket and fixedly connected to one end of the recovery rope.

[0015] Preferably, a warning light is provided on the top of the protection ring, and the warning light is used to warn high-altitude flying objects.

[0016] Preferably, a guide groove is provided on one side of the recovery groove, and the guide groove is used to guide the recovery rope.

[0017] Compared with the prior art, the beneficial effects of the utility model are:

[0018] 1. The present application is provided with a detection component, an inflation component, a protection component and a protection component. When in use, the sonde for detecting the weather is installed inside the storage basket, and the detection part of the sonde is exposed to the outside of the storage basket. The sonde is then sent to high altitude by a weather balloon to detect the weather at high altitude. The first protection ring, the connecting strip and the second protection ring can improve the stability of the weather balloon. The protection strip and the protection ring can protect the weather balloon to prevent the weather balloon from colliding with flying objects and exploding at high altitude. When the air content inside the weather balloon is insufficient, the gas in the temporal part of the gas tank can be filled into the weather balloon through an air pump, so that the sonde can be used to detect the weather at high altitude, thereby improving the accuracy of weather data and ensuring the safety and endurance of the weather balloon.

[0019] 2. The present application sets a limit assembly, a recovery assembly, a warning light and a guide groove. When in use, when the weather balloon has not been released, the limit hook can be hung on the limit hook to limit the weather balloon and prevent it from flying high in the sky in preparation for debugging the sounding instrument. The warning light can warn of high-altitude flying objects to improve the safety of the weather balloon. Then the recovery rope is fixed to the bottom of the connecting block. When the limit hook is released to release the weather balloon, one end of the recovery rope will fly high in the sky. The motor is started to drive the reel to rotate, and the length of the recovery rope can be adjusted. The guide groove can make the recovery reel slide more smoothly inside the recovery groove, so that the height of the weather balloon can be controlled, the effect of detecting weather is improved, and the recovery of the weather balloon is convenient. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the specific implementation methods of the utility model or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0021] Figure 1 This is the overall structural view of the utility model;

[0022] Figure 2 It is a front view of the utility model;

[0023] Figure 3 For this utility model Figure 2 Schematic diagram of the cross-sectional three-dimensional structure at AA in the middle;

[0024] Figure 4 for Figure 3 Schematic diagram of the local structure;

[0025] Figure 5It is a cross-sectional three-dimensional structural schematic diagram of the right view of the utility model.

[0026] Description of reference numerals:

[0027] 1. Base; 2. Detection component; 3. Inflatable component; 4. Protection component; 5. Protection component; 6. Limit component; 7. Recovery component; 201. Storage basket; 202. Sounding instrument; 203. Connecting rope; 204. Weather balloon; 301. Gas tank; 302. Air pump; 303. Connecting pipe; 401. First protective ring; 402. Connecting strip; 403. Second protective ring; 501. Protection strip; 502. Protection ring; 601. Limit block; 602. Limit rope; 603. Limit hook; 604. Limit hook; 701. Recovery trough; 702. Recovery board; 703. Wire wheel; 704. Recovery rope; 705. Motor; 706. Connecting block; 8. Warning light; 9. Diversion trough. DETAILED DESCRIPTION

[0028] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0029] See also Figures 1 to 5 , the utility model provides a technical solution:

[0030] An aviation meteorological detection device comprises a base 1, a detection component 2 is arranged on the top of the base 1, an inflation component 3 is arranged on one side of the detection component 2, a protection component 4 is arranged on one side of the detection component 2, a protection component 5 is arranged on one side of the protection component 4, a limit component 6 is arranged on the top of the base 1, and a recovery component 7 is arranged on one side of the base 1;

[0031] The detection component 2 includes a storage basket 201, a sonde 202, a connecting rope 203 and a weather balloon 204. The storage basket 201 is movably connected to the top of the base 1, the sonde 202 is arranged inside the storage basket 201, a plurality of connecting ropes 203 are arranged on the top of the storage basket 201, and the weather balloon 204 is arranged on the top of the plurality of connecting ropes 203 and is used in conjunction with the storage basket 201.

[0032] Specifically, Figure 4As shown, the inflation component 3 includes a gas tank 301, an air pump 302 and a connecting pipe 303. The gas tank 301 is arranged inside the storage basket 201, the air pump 302 is arranged on one side of the gas tank 301 and is used in conjunction with the gas tank 301, one end of the connecting pipe 303 is arranged at the output end of the air pump 302 and the other end is arranged inside the weather balloon 204.

[0033] Specifically, Figure 5 As shown, the protection assembly 4 includes a first protection ring 401, a connecting strip 402 and a second protection ring 403. The first protection ring 401 is arranged at the bottom of the weather balloon 204, a plurality of connecting strips 402 are fixedly connected to the top of the first protection ring 401, and the second protection ring 403 is fixedly connected between the plurality of connecting strips 402.

[0034] Specifically, Figure 4 As shown, the protection assembly 5 includes a protection strip 501 and a protection ring 502 . A plurality of protection strips 501 are welded to the top of the second protection ring 403 , and the protection ring 502 is welded between the plurality of protection strips 501 .

[0035] When in use, the sonde 202 for detecting the weather is installed inside the storage basket 201, and the detection part of the sonde 202 will be exposed outside the storage basket 201, and then the sonde 202 will be sent to high altitude by the weather balloon 204 to detect the weather at high altitude. The first protective ring 401, the connecting strip 402 and the second protective ring 403 can improve the stability of the weather balloon 204, and the protective strip 501 and the protective ring 502 can protect the weather balloon 204 to prevent the weather balloon 204 from colliding with flying objects at high altitude and exploding. When the air content inside the weather balloon 204 is insufficient, the gas in the top of the gas tank 301 can be filled into the weather balloon 204 through the air pump 302, so that the sonde 202 can be used to detect the weather at high altitude, thereby improving the accuracy of the weather data and ensuring the safety and endurance of the weather balloon 204.

[0036] Specifically, Figure 5 As shown, the limit assembly 6 includes a limit block 601, a limit rope 602, a limit hook 603 and a limit hook 604, a plurality of limit blocks 601 are fixedly connected to the top of the base 1, the limit rope 602 is arranged at the top of the limit block 601, the limit hook 603 is fixedly connected to the end of the limit rope 602 away from the limit block 601, and a plurality of limit hooks 604 are fixedly connected to one side of the second protective ring 403 and used in conjunction with the limit hook 603.

[0037] Specifically, Figure 5As shown, the recovery component 7 includes a recovery trough 701, a recovery plate 702, a reel 703, a recovery rope 704, a motor 705 and a connecting block 706. The recovery trough 701 is opened on one side of the base 1, the two recovery plates 702 are fixedly connected to the bottom of the base 1, the reel 703 is rotatably connected between the two recovery plates 702, the recovery rope 704 is arranged on one side of the reel 703, the motor 705 is arranged on one side of the recovery plate 702 and the output end is fixedly connected to one side of the reel 703, and the connecting block 706 is fixedly connected to the bottom of the storage basket 201 and fixedly connected to one end of the recovery rope 704.

[0038] Specifically, Figure 4 As shown, a warning light 8 is provided on the top of the protection ring 502, and the warning light 8 is used to warn high-altitude flying objects.

[0039] Specifically, Figure 4 As shown, a guide groove 9 is provided on one side of the recovery groove 701 , and the guide groove 9 is used to guide the recovery rope 704 .

[0040] When in use, when the weather balloon 204 has not been released yet, the limit hook 603 can be hung on the limit hook 604 to limit the weather balloon 204 and prevent the weather balloon 204 from flying high in order to prepare for the debugging of the sounding instrument 202. The warning light 8 can warn high-altitude flying objects to improve the safety of the weather balloon 204. Then the recovery rope 704 is fixed to the bottom of the connecting block 706. When the limit hook 603 is released to release the weather balloon 204, one end of the recovery rope 704 will fly high in the sky. The motor 705 is started to drive the reel 703 to rotate, and the length of the recovery rope 704 can be adjusted. The guide groove 9 can make the recovery reel 703 slide more smoothly inside the recovery groove 701, so that the height of the weather balloon 204 can be controlled, the effect of detecting weather is improved, and the weather balloon 204 is convenient to recover.

[0041] By adopting the above technical solution, the problem that the existing aviation meteorological detection devices can only collect and detect the weather in a fixed area during actual use, resulting in inaccurate detection data, and the detection altitude is low and cannot be well adapted to the requirements of aviation meteorological collection and detection is solved.

[0042] Working principle: When the present application is in use, the sonde 202 for detecting weather is first installed inside the storage basket 201, and the detection part of the sonde 202 is exposed outside the storage basket 201. Then the sonde 202 is sent to high altitude through the weather balloon 204, so as to detect the weather at high altitude. The first protective ring 401, the connecting strip 402 and the second protective ring 403 can improve the stability of the weather balloon 204. The protective strip 501 and the protective ring 502 can protect the weather balloon 204 to prevent the weather balloon 204 from colliding with flying objects and exploding at high altitude. When the air content inside the weather balloon 204 is insufficient, the gas in the temporal part of the gas tank 301 can be filled into the weather balloon 204 through the air pump 302, so that the sonde 202 can be used to detect weather at high altitude, thereby improving the accuracy of weather data and ensuring that the weather balloon 204 The safety and endurance of the flight can be improved. When the weather balloon 204 has not been released, the limit hook 603 can be hung on the limit hook 604 to limit the weather balloon 204 and prevent the weather balloon 204 from flying to a high altitude in preparation for debugging the sounding instrument 202. The warning light 8 can warn high-altitude flying objects to improve the safety of the weather balloon 204. Then the recovery rope 704 is fixed to the bottom of the connecting block 706. When the limit hook 603 is released to release the weather balloon 204, one end of the recovery rope 704 will fly to a high altitude together. The motor 705 is started to drive the reel 703 to rotate, and the length of the recovery rope 704 can be adjusted. The guide groove 9 can make the recovery reel 703 slide more smoothly inside the recovery groove 701, so that the height of the weather balloon 204 can be controlled, the effect of detecting the weather is improved, and the weather balloon 204 is convenient to recover.

[0043] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit it. Although the utility model has been described in detail with reference to the aforementioned embodiments, ordinary technicians in this field should understand that they can still modify the technical solutions recorded in the aforementioned embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not make the essence of the corresponding technical solution deviate from the scope of the technical solution of the embodiments of the utility model.

Claims

1. An aviation meteorological detection device, comprising a base (1), characterized in that: A detection component (2) is arranged on the top of the base (1), an inflation component (3) is arranged on one side of the detection component (2), a protection component (4) is arranged on one side of the detection component (2), a protection component (5) is arranged on one side of the protection component (4), a limit component (6) is arranged on the top of the base (1), and a recovery component (7) is arranged on one side of the base (1); The detection assembly (2) comprises a storage basket (201), a sonde (202), a connecting rope (203) and a weather balloon (204); the storage basket (201) is movably connected to the top of the base (1); the sonde (202) is arranged inside the storage basket (201); a plurality of connecting ropes (203) are arranged on the top of the storage basket (201); and the weather balloon (204) is arranged on the top of a plurality of connecting ropes (203) and is used in conjunction with the storage basket (201).

2. An aviation meteorological detection device according to claim 1, characterized in that: The inflation assembly (3) comprises a gas tank (301), an air pump (302) and a connecting pipe (303); the gas tank (301) is arranged inside the storage basket (201); the air pump (302) is arranged on one side of the gas tank (301) and is used in conjunction with the gas tank (301); one end of the connecting pipe (303) is arranged at the output end of the air pump (302) and the other end is arranged inside the weather balloon (204).

3. An aviation meteorological detection device according to claim 1, characterized in that: The protection assembly (4) comprises a first protection ring (401), a connecting strip (402) and a second protection ring (403); the first protection ring (401) is arranged at the bottom of the weather balloon (204); a plurality of connecting strips (402) are fixedly connected to the top of the first protection ring (401); and the second protection ring (403) is fixedly connected between the plurality of connecting strips (402).

4. An aviation meteorological detection device according to claim 3, characterized in that: The protection assembly (5) comprises a protection strip (501) and a protection ring (502); a plurality of the protection strips (501) are welded to the top of the second protection ring (403); and the protection ring (502) is welded between the plurality of protection strips (501).

5. The aviation meteorological detection device according to claim 1, characterized in that: The limiting assembly (6) comprises a limiting block (601), a limiting rope (602), a limiting hook (603) and a limiting hook (604); a plurality of the limiting blocks (601) are fixedly connected to the top of the base (1); the limiting rope (602) is arranged on the top of the limiting block (601); the limiting hook (603) is fixedly connected to one end of the limiting rope (602) away from the limiting block (601); and a plurality of the limiting hooks (604) are fixedly connected to one side of the second protective ring (403) and used in conjunction with the limiting hook (603).

6. An aviation meteorological detection device according to claim 1, characterized in that: The recovery component (7) comprises a recovery trough (701), a recovery plate (702), a wire wheel (703), a recovery rope (704), a motor (705) and a connection block (706); the recovery trough (701) is opened on one side of the base (1); the two recovery plates (702) are fixedly connected to the bottom of the base (1); the wire wheel (703) is rotatably connected between the two recovery plates (702); the recovery rope (704) is arranged on one side of the wire wheel (703); the motor (705) is arranged on one side of the recovery plate (702) and the output end is fixedly connected to one side of the wire wheel (703); the connection block (706) is fixedly connected to the bottom of the storage basket (201) and fixedly connected to one end of the recovery rope (704).

7. An aviation meteorological detection device according to claim 4, characterized in that: A warning light (8) is provided on the top of the protection ring (502), and the warning light (8) is used to warn of high-altitude flying objects.

8. An aviation meteorological detection device according to claim 6, characterized in that: A guide groove (9) is provided on one side of the recovery groove (701), and the guide groove (9) is used to guide the recovery rope (704).

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