Low-altitude meteorological monitoring equipment

Abstract

The utility model relates to the meteorological monitoring field, and discloses a low-altitude meteorological monitoring device comprising an unmanned aerial vehicle, the top of the unmanned aerial vehicle is provided with a monitoring mechanism, the front, back, left and right parts of the unmanned aerial vehicle are respectively provided with a protection assembly, and the lower part of the unmanned aerial vehicle is provided with a plurality of supporting mechanisms. The supporting mechanism comprises a connecting piece and a supporting piece, an air pump is arranged on the lower portion of the unmanned aerial vehicle, the supporting piece comprises a supporting pad, the upper portion of the supporting pad is fixedly connected with a connecting base, the bottom of the supporting pad is fixedly connected with a plurality of anti-slip strips, and the connecting piece comprises a connecting rod. The upper end and the lower end of the connecting rod are fixedly connected with connecting balls. According to the unmanned aerial vehicle supporting pad, the unmanned aerial vehicle and the supporting mechanism are matched with each other, and the connecting pieces, the supporting legs and the supporting pieces are matched with each other, so that the angle of the supporting pad can be better adjusted according to ground conditions to be matched with parking of the unmanned aerial vehicle, and the unmanned aerial vehicle supporting pad is more stable and practical.

Description

Technical Field

[0001] The utility model relates to the field of meteorological monitoring, in particular to a low-altitude meteorological monitoring device. Background Art

[0002] Meteorological monitoring refers to the observation and recording of meteorological elements such as temperature, humidity, air pressure, wind speed, precipitation, etc. to obtain information on weather and climate change. The main purpose of meteorological monitoring is to provide timely and accurate weather forecasts to ensure the safety of people's lives and production. Low-altitude meteorological monitoring devices are instruments used to monitor meteorological elements from the ground to the troposphere. They mostly adopt the form of a combination of unmanned aerial vehicles (UAVs) and meteorological monitoring devices to monitor low-altitude meteorology.

[0003] After retrieval, Chinese Patent Publication No.: CN221068499U discloses a UAV for meteorological monitoring. The UAV for meteorological monitoring includes: a UAV body, on which a meteorological monitor is detachably installed; a camera, which is fixedly installed on the UAV body; multiple brackets, all of which are fixedly installed on the UAV body, and the bottom ends of the multiple brackets are all fixedly installed with mounting plates; multiple bottom plates, which are respectively arranged below the multiple mounting plates, and plugging mechanisms are arranged on the multiple bottom plates. The plugging mechanism includes a threaded cylinder, a threaded rod, a driving motor, two belt pulleys and a belt. The threaded cylinder is rotatably installed on the bottom plate, and the threaded rod is threadedly installed on the threaded cylinder. The UAV for meteorological monitoring provided by the utility model has the advantages of being able to ensure the stable parking of the UAV and being able to disassemble the meteorological monitor.

[0004] Although the above device can improve the stability of the UAV parking by setting structures such as brackets and bottom plates, the structural settings between its brackets, mounting plates and bottom plates make it difficult to adjust the angle between the bottom plate and the ground to adapt to uneven ground. This leads to the situation that even if structures such as threaded rods are set, it is still very difficult for the threaded rod to insert into the ground when the ground is uneven, resulting in the UAV being difficult to park stably on uneven ground, which is not very practical. Therefore, a low-altitude meteorological monitoring device is proposed to solve the above problems. Summary of the Utility Model

[0005] In order to make up for the above deficiencies, the utility model provides a low-altitude meteorological monitoring device, aiming to improve the problem in the prior art that it is difficult to make an angle adjustment between the bottom plate and the ground to adapt to uneven ground. This leads to the situation that even if structures such as threaded rods are set, it is still very difficult for the threaded rod to insert into the ground when the ground is uneven, resulting in the UAV being difficult to park stably on uneven ground, which is not very practical.

[0006] To achieve the above object, the utility model adopts the following technical solutions: A low-altitude meteorological monitoring device includes a drone. A monitoring mechanism is arranged at the top of the drone. Protection components are arranged at the front, rear, left, and right parts of the drone. A plurality of support mechanisms are arranged at the lower part of the drone. The support mechanism includes a connecting piece and a support piece. An air pump is arranged at the lower part of the drone. The support piece includes a support pad. A connecting seat is fixedly connected to the upper part of the support pad.

[0007] As a further description of the above technical solution:

[0008] A plurality of anti-slip strips are fixedly connected to the bottom of the support pad.

[0009] As a further description of the above technical solution:

[0010] The connecting piece includes a connecting rod. Connecting balls are fixedly connected to both the upper and lower ends of the connecting rod. The connecting ball located at the lower part is rotatably connected to the connecting seat.

[0011] As a further description of the above technical solution:

[0012] Legs are movably connected to the front and rear parts of the front right side of the drone. The connecting ball located at the upper part is rotatably connected to the bottom of the leg.

[0013] As a further description of the above technical solution:

[0014] The output end of the air pump is fixedly connected to a four-way connector. Hoses are movably connected to the front, rear, left, and right parts of the four-way connector.

[0015] As a further description of the above technical solution:

[0016] A fixing ring is fixedly connected to the middle of the hose. The fixing ring is fixedly connected to the drone.

[0017] As a further description of the above technical solution:

[0018] The protection component includes an airbag. The airbag is fixedly connected to the leg. An air inlet pipe is fixedly connected to the top of the airbag. The hose is movably connected thereto. A plurality of support bars are fixedly connected to the outside of the airbag.

[0019] As a further description of the above technical solution:

[0020] A first folding surface and a second folding surface are arranged on the top surface of the airbag. A folding ring groove is jointly arranged between the first folding surface and the second folding surface.

[0021] The utility model has the following beneficial effects:

[0022] 1. In the present utility model, through the mutual cooperation between the unmanned aerial vehicle and the support mechanism, and through the mutual cooperation between the connecting piece, the leg and the support member, the support pad can better adjust the angle according to the ground conditions to cooperate with the parking of the unmanned aerial vehicle, which is more stable and practical.

[0023] 2. In the present utility model, through the mutual cooperation between the unmanned aerial vehicle, the air pump and the protection component, when the unmanned aerial vehicle is about to fall, the device can use multiple airbags to support and buffer the unmanned aerial vehicle and the monitoring mechanism, and protect the unmanned aerial vehicle and the monitoring mechanism, which is more practical. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 is a schematic perspective view of the overall upper part of a low-altitude meteorological monitoring device proposed by the present utility model;

[0025] Figure 2 is a schematic perspective view of the overall lower part of a low-altitude meteorological monitoring device proposed by the present utility model;

[0026] Figure 3 is a schematic perspective view of a partial structure of a low-altitude meteorological monitoring device proposed by the present utility model;

[0027] Figure 4 is a schematic perspective view of the split structure of the leg and the support mechanism of a low-altitude meteorological monitoring device proposed by the present utility model.

[0028] LEGEND DESCRIPTION:

[0029] 1. Unmanned aerial vehicle; 2. Monitoring mechanism; 3. Protection component; 4. Connecting piece; 5. Support member; 6. Air pump; 41. Connecting rod; 42. Connecting ball; 51. Support pad; 52. Anti-slip strip; 53. Connecting seat; 11. Leg; 61. Four-way connector; 62. Hose; 63. Fixed ring; 31. Airbag; 32. Support bar; 33. Intake pipe; 311. First folding surface; 312. Second folding surface; 313. Folding ring groove. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0030] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with 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.

[0031] Refer to Figure 1 - Figure 2, an embodiment provided by the present utility model: a low-altitude meteorological monitoring device, including a drone 1, which is used to carry a monitoring mechanism 2 to monitor low-altitude meteorology. A monitoring mechanism 2 is arranged on the top of the drone 1. It is an existing meteorological monitoring device, which can be a monitoring device for temperature, humidity, wind speed, etc. Protection components 3 are arranged on the front, back, left and right parts of the drone 1, which are used to protect the drone 1 and the monitoring mechanism 2 when the drone 1 topples during landing and parking. A plurality of support mechanisms are arranged at the lower part of the drone 1, which are used to support the drone 1 to ensure the stable parking of the drone 1. The support mechanism includes a connecting piece 4 and a support piece 5. An air pump 6 is arranged at the lower part of the drone 1, which is used to inflate the protection component 3 to make the airbag 31 bulge, so as to better protect the drone 1 and the monitoring mechanism 2 connected thereto. The air pump 6 is controlled by an induction device, which is installed on the drone 1. It can monitor the tilting angle of the drone 1 during parking through a pre-set control program. When there is a risk of the drone 1 toppling, the induction device can control the air pump 6 to start through a circuit, etc. Legs 11 are movably connected to the front and rear parts of the front right side of the drone 1, which are used to support the drone 1. The connecting ball 42 located at the upper part is rotatably connected to the bottom of the leg 11, which is used to cooperate with the connection between the support mechanism and the drone 1. The connecting ball 42 located at the upper part and the leg 11 cannot be separated.

[0032] Furthermore, the output end of the air pump 6 is fixedly connected with a four-way connector 61, which is used to connect multiple hoses 62 to enable the air pump 6 to communicate with multiple hoses 62. Hoses 62 are movably connected to the front, back, left and right parts of the four-way connector 61, which are used to cooperate with the connection between the air pump 6 and the airbag 31. A fixing ring 63 is fixedly connected to the middle of the hose 62, which is used to cooperate with the connection between the hose 62 and the drone 1. The fixing ring 63 is fixedly connected to the drone 1.

[0033] As Figure 3 - Figure 4 shown, the connecting piece 4 includes a connecting rod 41, which is used to cooperate with connecting various components. Connecting balls 42 are fixedly connected to the upper and lower ends of the connecting rod 41 respectively, which are used to connect the leg 11 and the support piece 5 respectively. The support piece 5 includes a support pad 51, which can be made of plastic, rubber and other materials and has a certain hardness. A connecting seat 53 is fixedly connected to the upper part of the support pad 51, which is used to cooperate with the connection of the connecting piece 4. The connecting ball 42 located at the lower part is rotatably connected to the connecting seat 53, which is used to cooperate with the angle adjustment of the support piece 5 to adapt to uneven ground. A plurality of anti-slip strips 52 are fixedly connected to the bottom of the support pad 51, which are used to improve the anti-slip property of the support pad 51 to improve the stability of the drone 1 during parking.

[0034] Further, the protection component 3 includes an airbag 31, which can be made of materials such as rubber and can deform. When not in use, the airbag 31 is in a deflated state. After the airbag 31 bulges, it is in the shape of a frustum with a wider upper part and a narrower lower part, which can better protect the blades of the drone 1 and the monitoring mechanism 2 on the upper part. The airbag 31 is fixedly connected to the leg 11. The top of the airbag 31 is fixedly connected with an air inlet pipe 33, which is used to connect with the hose 62, and the hose 62 is movably connected thereto. A plurality of support bars 32 are fixedly connected to the outside of the airbag 31 for cooperating with the expansion and contraction of the airbag 31. The top surface of the airbag 31 is provided with a first folding surface 311 and a second folding surface 312 to cooperate with the expansion and contraction of the airbag 31. A folding ring groove 313 is jointly arranged between the first folding surface 311 and the second folding surface 312 to cooperate with the folding of the first folding surface 311 and the second folding surface 312.

[0035] Working principle: During use, the drone 1 drives the meteorological monitoring mechanism 2 to fly into the air to monitor the low-altitude meteorology. After the monitoring is completed, the drone 1 drives the monitoring mechanism 2 back to the ground. When the drone 1 is parked and the ground where it is parked is not flat enough, when the support member 5 touches the ground, the connecting seat 53 on the support pad 51 will rotate around the lower connecting ball 42, and at the same time, the upper connecting ball 42 will also rotate within the leg 11, thereby adjusting the angle of the support pad 51 so that the drone 1 can be parked on the ground more stably.

[0036] If the drone 1 tilts during parking, at this time, the air pump 6 will be turned on. The air pump 6 will send gas through the four-way connector 61 into multiple hoses 62, and then through the hoses 62 into the airbag 31 through the air inlet pipe 33. The airbag 31 will bulge, so that it can support the drone 1 when it tilts and provide a certain degree of buffering to protect the drone 1 and the monitoring mechanism 2 connected thereto.

[0037] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. A low-altitude meteorological monitoring device, comprising a drone (1), characterized in that: A monitoring mechanism (2) is provided at the top of the drone (1). Protection components (3) are provided on the front, rear, left, and right sides of the drone (1). A plurality of support mechanisms are provided at the lower part of the drone (1). The support mechanism includes a connecting member (4) and a support member (5). An air pump (6) is provided at the lower part of the drone (1). The support member (5) includes a support pad (51). A connecting seat (53) is fixedly connected to the upper part of the support pad (51).

2. The low-altitude meteorological monitoring device according to claim 1, characterized in that: A plurality of anti-slip strips (52) are fixedly connected to the bottom of the support pad (51).

3. A low-altitude meteorological monitoring device according to claim 1, characterized in that: The connecting member (4) includes a connecting rod (41). Connecting balls (42) are fixedly connected to both the upper and lower ends of the connecting rod (41). The connecting ball (42) located at the lower part is rotatably connected to the connecting seat (53).

4. The low-altitude weather monitoring device according to claim 3, wherein: Legs (11) are movably connected to the front and rear parts of the front right side of the drone (1). The connecting ball (42) located at the upper part is rotatably connected to the bottom of the leg (11).

5. A low-altitude meteorological monitoring device according to claim 1, characterized in that: The output end of the air pump (6) is fixedly connected to a four-way connector (61). Hoses (62) are movably connected to the front, rear, left, and right parts of the four-way connector (61).

6. The low-altitude meteorological monitoring device according to claim 5, characterized in that: A fixing ring (63) is fixedly connected to the middle of the hose (62). The fixing ring (63) is fixedly connected to the drone (1).

7. The low-altitude meteorological monitoring device according to claim 5, characterized in that: The protection component (3) includes an airbag (31). The airbag (31) is fixedly connected to the leg (11). An air inlet pipe (33) is fixedly connected to the top of the airbag (31). The hose (62) is movably connected thereto. A plurality of support bars (32) are fixedly connected to the outside of the airbag (31).

8. The low-altitude weather monitoring device according to claim 7, characterized in that: A first folding surface (311) and a second folding surface (312) are provided on the top surface of the airbag (31). A folding ring groove (313) is jointly provided between the first folding surface (311) and the second folding surface (312).

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