Air quality detection device

By combining the mounting column, the detector body, and the drone body, and using the magnetic control unit to control the snap-fit ​​notch, the air quality detection device achieves a combination of fixed-point and cruise detection, solving the problem of limited detection range in existing technologies and improving the reliability and automation of detection results.

CN121114360AActive Publication Date: 2025-12-12山西省太原生态环境监测中心
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Patent Information

Application Number
CN202511676316.7
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-11-17
Publication Date
2025-12-12
Estimated Expiration
2045-11-17

AI Technical Summary

Technical Problem

Existing air quality detectors are fixed outdoors and can only perform point-to-point testing, which cannot expand the detection range and results in poor reliability of the test results.

Method used

The device employs a combined structure of mounting post, detector body, and drone body. The magnetic control unit controls the opening and closing of the snap-fit ​​notch, enabling a detachable connection between the detector body and the drone body. This allows the drone to carry the detector for cruise testing and return to fixed-point testing when needed.

Benefits of technology

It expands the detection range, improves the reliability of detection results, reduces the intensity of manual labor, and enhances the automation and convenience of the detection device.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention relates to an air quality detection device, and relates to the technical field of environment monitoring, the air quality detection device comprises a mounting column, a detector body and an unmanned aerial vehicle body, the detector body is mounted on the unmanned aerial vehicle body, a mounting assembly is arranged between the detector body and the mounting column, and the mounting assembly comprises a mounting seat, a connecting seat, a clamping part and a magnetic control part; the mounting seat is connected to the mounting column, the connecting seat is connected to the detector body, a clamping head is connected to the connecting seat, and the clamping part is arranged on the mounting seat and provided with a clamping notch; the magnetic control part is used for controlling opening and closing of the clamping gap based on the starting condition of the unmanned aerial vehicle body; in a state that the connecting seat is close to the mounting seat, when the unmanned aerial vehicle body is started, the magnetic control part opens the clamping notch; and under the condition that the clamping notch is opened, the clamping head can rotate in the forward direction and is clamped on the clamping part, and the clamping head can rotate in the reverse direction and is separated from the clamping part. The air quality detection device has the effect of expanding the detection range of the air quality detection device.
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Description

TECHNICAL FIELD

[0001] The application relates to the technical field of environmental monitoring, and in particular to an air quality detection device. BACKGROUND

[0002] The quality of air quality reflects the concentration of pollutants in the air, and thus outdoor air quality detection is an important means of urban environmental management.

[0003] In order to detect the outdoor environment in real time, a plurality of air quality detectors are usually fixedly installed outdoors, such as the outdoor air quality detector disclosed in Chinese Patent No. CN222014133U and the outdoor environment detection device disclosed in Chinese Patent No. CN210894269U. Since the air quality detector is fixedly installed outdoors, the air quality detector can detect and feed back the detection data of the surrounding environment in real time, but can only perform fixed-point detection and cannot expand the detection range. The detected data can only reflect the air quality at the position of the air quality detector, so that the reliability of the detection result is poor under the condition of limited detection data. SUMMARY

[0004] In order to expand the detection range of the air quality detection device and improve the reliability of the detection result, the application provides an air quality detection device.

[0005] The air quality detection device provided by the application adopts the following technical scheme: The air quality detection device comprises a mounting column, a detector body and a drone body. The mounting column is fixedly installed on the ground. The detector body is installed on the drone body. An installation assembly is arranged between the detector body and the mounting column. The installation assembly comprises a mounting seat, a connecting seat, a clamping portion and a magnetic control portion. The mounting seat is connected to the mounting column. The connecting seat is connected to the detector body. A clamping head is connected to the connecting seat. The clamping portion is arranged on the mounting seat and is provided with a clamping gap. The clamping head can be clamped to the clamping portion through the clamping gap. The magnetic control portion is arranged between the mounting seat and the connecting seat. The magnetic control portion is used to control the opening and closing of the clamping gap based on the starting state of the drone body. When the drone body is in a starting state, the magnetic control portion opens the clamping gap. When the drone body is in a shutdown state, the magnetic control portion closes the clamping gap. When the clamping gap is open, the clamping head can be clamped to the clamping portion in a forward direction under the drive of the drone body, and the clamping head can be clamped to the clamping portion in a reverse direction under the drive of the drone body.

[0006] Optionally, the clamping part comprises a first clamping ring, a second clamping ring and a closing plate, the first clamping ring and the second clamping ring are connected to the hole wall of the mounting hole formed in the middle of the mounting seat, the first clamping ring is located above the second clamping ring, the first clamping ring is provided with a clamping hole, the clamping hole forms a clamping notch of the clamping part, the closing plate is hinged to the clamping hole through a hinge shaft, the magnetic control part is used for controlling the forward swing of the closing plate and abutting to the second clamping ring to open the clamping hole, the magnetic control part is used for controlling the reverse swing of the closing plate to close the clamping hole, and the clamping head is provided with a disengaging slope capable of sliding onto the closing plate.

[0007] Optionally, the side of the first clamping ring away from the second clamping ring is connected with a guide plate, the guide plate is arranged close to the clamping hole, and the guide plate is used for guiding the clamping head to enter the clamping hole when the clamping head rotates forward.

[0008] Optionally, the magnetic control part comprises an electromagnetic ring, a permanent magnet block, a control rack and a control gear, the electromagnetic ring is embedded on the connecting seat, the permanent magnet block is slidingly arranged in a control sliding slot formed in the mounting seat, the polarity of the side of the electromagnetic ring and the permanent magnet block close to each other is the same when the unmanned aerial vehicle body is powered on, the polarity of the side of the electromagnetic ring and the permanent magnet block close to each other is opposite when the unmanned aerial vehicle body is powered off, the control rack and the control gear are arranged in a transmission groove formed in the mounting seat, the control rack is engaged with the control gear, the control rack is connected with the permanent magnet block, and the control gear is connected with the hinge shaft.

[0009] Optionally, the mounting surfaces of the mounting seat and the connecting seat close to each other are conical.

[0010] Optionally, the number of the clamping head, the clamping hole, the permanent magnet block, the control rack and the control gear is consistent in pairs, and the permanent magnet block is uniformly provided with a plurality of permanent magnet blocks around the axis direction of the mounting seat.

[0011] Optionally, the connecting seat is connected with a camera, and when the connecting seat is mounted on the mounting seat, the camera can be located in the mounting hole.

[0012] Optionally, the connecting seat is provided with a protection assembly, the number of the protection assembly is consistent with the number of the propellers on the unmanned aerial vehicle body, the protection assembly comprises a protection cylinder, a protection rack, a protection gear, a protection rod and a protection cloth, the protection cylinder, the protection rack, the protection gear and the protection rod are provided with two, and are symmetrically arranged on both sides of the propellers of the unmanned aerial vehicle body, the protection cylinder is connected to the connecting seat, the protection rack is connected to the movable end of the protection cylinder in a one-to-one correspondence, the protection gear is engaged with the protection rack in a one-to-one correspondence and is rotatably connected to the connecting seat, one end of the protection rod is connected to the protection gear in a one-to-one correspondence, the other end is connected with the protection cloth, the protection cloth is connected to the unmanned aerial vehicle body, and the two protection rods can unfold the protection cloth above the propellers of the unmanned aerial vehicle body.

[0013] Optionally, the protection cylinder is connected with a reinforcing assembly, the reinforcing assembly comprises reinforcing heads and a reinforcing ring, the number of the reinforcing heads is consistent with the number of the protection cylinders, the reinforcing heads are connected with the movable ends of the protection cylinders one by one, reinforcing nails are connected with the reinforcing heads, the reinforcing ring is connected with the mounting seat, a reinforcing rubber layer is connected with the reinforcing ring, the protection cylinders can drive the reinforcing heads to abut against the reinforcing rubber layer and drive the reinforcing nails to be fixed on the reinforcing rubber layer, and the protection cylinders can drive the protection rods to unfold the protective cloth.

[0014] Optionally, the unmanned aerial vehicle body is provided with a power supply assembly, the power supply assembly comprises a solar cell panel and a storage battery, the solar cell panel is electrically connected with the storage battery, and the storage battery is electrically connected with the detector body, the unmanned aerial vehicle body and the magnetic control part respectively.

[0015] In summary, the application has at least one of the following beneficial technical effects: 1. The air quality detection device comprises a mounting column, a detector body, an unmanned aerial vehicle body and a mounting assembly, wherein the detector body can perform fixed-point air detection at the mounting column in a normal state, when it is necessary to expand the detection range, the unmanned aerial vehicle body is started, the magnetic control part opens the clamping hole based on the state of the unmanned aerial vehicle body, the clamping head is driven to rotate reversely by the unmanned aerial vehicle body, so that the clamping head can be separated from between the first clamping ring and the second clamping ring, the unmanned aerial vehicle body can carry the detector body to perform cruise detection, after the cruise is completed, the unmanned aerial vehicle body carries the detector body to approach the mounting seat, the clamping head is driven to rotate forward by the unmanned aerial vehicle body, so that the clamping head can be clamped between the first clamping ring and the second clamping ring, the unmanned aerial vehicle body is stopped, the magnetic control part closes the clamping hole based on the state of the unmanned aerial vehicle body, so that the clamping head is difficult to be separated from between the first clamping ring and the second clamping ring, thereby the detection range of the detector body is expanded, and the reliability of the detection result is improved in a manner of fixed-point detection and regional detection cooperation. 2. The air quality detection device further comprises a protection assembly and a reinforcing assembly, wherein in severe weather, the protection cylinder can drive the protection rods to swing, so that the protective cloth is unfolded above the propeller of the unmanned aerial vehicle body, the protective cloth can shield the damage of wind and rain to the propeller of the unmanned aerial vehicle body, at the same time, the protection cylinder can drive the reinforcing heads to abut against the reinforcing rubber layer and make the reinforcing nails fixed on the reinforcing rubber layer, so as to further fix the mounting seat and the mounting seat. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 is a structural schematic diagram of an embodiment of the application; Figure 2 is a structural schematic diagram of the unmanned aerial vehicle body and the power supply assembly; Figure 3 is a structural schematic diagram of the mounting assembly; Figure 4is a structural schematic diagram of the control sliding groove and the transmission groove; Figure 5 is a structural schematic diagram of the reinforcing nail.

[0017] Explanation of reference signs: 1, mounting column; 2, detector body; 3, unmanned aerial vehicle body; 4, mounting assembly; 41, mounting seat; 411, mounting hole; 412, control sliding groove; 413, transmission groove; 42, connecting seat; 421, clamping joint; 422, escape slope; 43, clamping part; 431, first clamping ring; 4311, clamping hole; 432, second clamping ring; 433, closing plate; 434, hinged shaft; 435, guide plate; 44, magnetic control part; 441, electromagnetic ring; 442, permanent magnet block; 443, control rack; 4431, connecting rod; 444, control gear; 5, camera; 6, protection assembly; 61, protection electric cylinder; 62, protection rack; 63, protection gear; 64, protection rod; 65, protection cloth; 7, reinforcing assembly; 71, reinforcing head; 72, reinforcing ring; 73, reinforcing nail; 74, reinforcing rubber layer; 8, energy supply assembly; 81, solar panel; 82, battery. DETAILED DESCRIPTION

[0018] The following will be described in detail with reference to the accompanying drawings Figures 1-5 The present application is further described in detail.

[0019] The embodiment of the present application discloses an air quality detection device. Referring to Figure 1 An air quality detection device comprises a mounting column 1, a detector body 2 and an unmanned aerial vehicle body 3.

[0020] The mounting column 1 is fixedly installed on the ground through bolts. The detector body 2 is fixedly connected to the bottom of the unmanned aerial vehicle body 3, and a mounting assembly 4 is arranged between the detector body 2 and the mounting column 1, and the mounting assembly 4 is used for realizing detachable connection of the detector body 2 and the mounting column 1.

[0021] Referring to Figure 2 and Figure 3 , the mounting assembly 4 comprises a mounting seat 41, a connecting seat 42, a clamping part 43 and a magnetic control part 44.

[0022] Referring to Figure 1 , Figure 3 and Figure 4 , the mounting seat 41 is fixedly connected to the top end of the mounting column 1, the connecting seat 42 is fixedly connected to the bottom end of the detector body 2, the connecting seat 42 is fixedly connected with a clamping joint 421, the clamping part 43 is arranged on the mounting seat 41, and the clamping part 43 is provided with a clamping notch, and the clamping joint 421 can be clamped and rotated to the clamping part 43 through the clamping notch, so as to realize connection of the mounting seat 41 and the connecting seat 42.

[0023] Referring toFigure 2 and Figure 4 The magnetic control part 44 is arranged between the mounting base 41 and the connecting base 42, and is used to control the opening and closing of the clamping gap based on the starting condition of the UAV body 3; when the UAV body 3 is in the starting state, the magnetic control part 44 opens the clamping gap to facilitate the clamping head 421 to enter or exit the clamping gap, and when the UAV body 3 is in the shutdown state, the magnetic control part 44 closes the clamping gap to limit the clamping head 421 from disengaging from the clamping part 43; in the case that the clamping gap is opened, the clamping head 421 can be positively rotated and clamped to the clamping part 43 under the drive of the UAV body 3, and the clamping head 421 can be reversely rotated and disengaged from the clamping part 43 under the drive of the UAV body 3.

[0024] In the normal state, the UAV body 3 and the detector body 2 are connected to the mounting base 41 through the connecting base 42, and the detector body 2 can perform point air detection; when it is necessary to expand the detection range, the UAV body 3 is started, the magnetic control part 44 can open the clamping gap, and the started UAV body 3 can drive the clamping head 421 to reversely rotate to make the clamping head 421 exit the clamping part 43, so that the connection between the mounting base 41 and the connecting base 42 can be released, and the UAV body 3 can carry the detector body 2 to fly to perform regional air detection in a cruising manner, thereby expanding the detection range of the air quality detection device.

[0025] After the cruising detection is completed, the UAV body 3 carries the detector body 2 to fly back to the mounting base 41, and after the connecting base 42 approaches the mounting base 41, the UAV body 3 drives the clamping head 421 to positively rotate to make the clamping head 421 clamped to the clamping part 43 from the clamping gap, thereby realizing the connection between the connecting base 42 and the mounting base 41, stopping the UAV body 3, and closing the clamping gap by the magnetic control part 44 to make it difficult for the clamping head 421 to disengage from the clamping part 43, so that the UAV body 3 and the detector body 2 are not easy to disengage from the mounting column 1, and the detector body 2 can perform point detection.

[0026] Under the cooperation of the magnetic control part 44 and the UAV body 3, the connection and disconnection between the connecting base 42 and the mounting base 41 can be automatically realized without manual on-site operation, thereby improving the overall automation degree of the detection device, reducing the labor intensity, and enhancing the convenience of using the detection device.

[0027] Fixed-point detection data can reflect the long-term air quality around the fixed location of the detector body 2, while cruise detection data can periodically reflect the air quality in the area surrounding the detector body 2. Combining fixed-point detection data and cruise detection data can more accurately reflect the outdoor air quality, thereby expanding the detection range of the air quality detection device and improving the reliability of the detection results based on the expanded air detection data.

[0028] Specifically, refer to Figure 4 The snap-fit ​​part 43 includes a first snap ring 431, a second snap ring 432, and a closing plate 433.

[0029] Reference Figure 3 and Figure 4 The first retaining ring 431 and the second retaining ring 432 are both fixedly connected to the wall of the mounting hole 411 opened in the middle of the mounting base 41. The first retaining ring 431 is located above the second retaining ring 432. The first retaining ring 431 has a snap-fit ​​hole 4311, which forms the snap-fit ​​notch of the snap-fit ​​part 43. The closing plate 433 is hinged to the snap-fit ​​hole 4311 through the hinge shaft 434. The closing plate 433 is used to open or close the snap-fit ​​hole 4311. The wall surface of the snap-fit ​​hole 4311 near the wall of the mounting hole 411 is flush with the wall of the mounting hole 411.

[0030] The magnetic control unit 44 is used to control the sealing plate 433 to swing forward and abut against the second retaining ring 432 to open the retaining hole 4311. The magnetic control unit 44 is also used to control the sealing plate 433 to swing in the opposite direction to close the retaining hole 4311. The retaining head 421 is provided with a release ramp 422 that can slide onto the sealing plate 433 to assist the retaining head 421 in releasing itself between the first retaining ring 431 and the second retaining ring 432.

[0031] When it is necessary to connect the mounting base 41 and the connecting base 42, the magnetic control unit 44 controls the sealing plate 433 to swing forward and abut against the second retaining ring 432. During the forward rotation, the retaining connector 421 can rotate to the retaining hole 4311. The retaining connector 421 can slide along the sealing plate 433 into the space between the first retaining ring 431 and the second retaining ring 432, and can rotate continuously between the first retaining ring 431 and the second retaining ring 432. After the retaining connector 421 slides into the space between the first retaining ring 431 and the second retaining ring 432, the drone body 3 stops. The magnetic control unit 44 controls the sealing plate 433 to swing and close the retaining hole 4311, making it difficult for the retaining connector 421 to come out of the retaining hole 4311 between the first retaining ring 431 and the second retaining ring 432.

[0032] Under the unidirectional guiding action of the sealing plate 433, the forward-rotating snap-fit ​​connector 421 is difficult to disengage between the first snap ring 431 and the second snap ring 432, allowing the detection direction of the detector body 2 to be adjusted under the drive of the drone body 3. When it is necessary to disconnect the mounting base 41 from the connecting base 42, the magnetic control unit 44 controls the sealing plate 433 to swing forward and abut against the second snap ring 432. The drone body 3 drives the snap-fit ​​connector 421 to rotate in the opposite direction. The reverse-rotating snap-fit ​​connector 421 can slide up onto the sealing plate 433 through the disengagement ramp 422. Under the guiding action of the sealing plate 433, the snap-fit ​​connector 421 can disengage between the first snap ring 431 and the second snap ring 432, thereby allowing the snap-fit ​​connector 421 to disengage between the first snap ring 431 and the second snap ring 432 under the drive of the drone body 3.

[0033] Reference Figure 3 In order to facilitate the insertion of the snap-fit ​​connector 421 into the snap-fit ​​hole 4311, a guide plate 435 is fixedly connected to the side of the first snap-fit ​​ring 431 away from the second snap-fit ​​ring 432. The guide plate 435 is located close to the snap-fit ​​hole 4311 and is curved in an arc shape. The guide plate 435 is used to guide the snap-fit ​​connector 421 into the snap-fit ​​hole 4311 when the snap-fit ​​connector 421 rotates in the forward direction.

[0034] The arc-shaped guide plate 435 can guide and restrict the rotating snap-fit ​​connector 421, so that the snap-fit ​​connector 421 can only slide along the closed plate 433. This makes it less likely for the snap-fit ​​connector 421 to slip past the snap-fit ​​hole 4311 when it rotates to the snap-fit ​​hole 4311, thus making it easier for the snap-fit ​​connector 421 to slide into the snap-fit ​​hole 4311.

[0035] Specifically, refer to Figure 3 The magnetic control unit 44 includes an electromagnetic ring 441, a permanent magnet block 442, a control rack 443, and a control gear 444.

[0036] Reference Figure 3 and Figure 4 The electromagnetic ring 441 is fixedly embedded in the connecting seat 42, and the permanent magnet 442 is slidably disposed in the control groove 412 opened on the mounting seat 41, with the sliding direction being vertical. When the drone body 3 is powered on, the polarities of the electromagnetic ring 441 and the permanent magnet 442 on the side closest to each other are the same; when the drone body 3 is stopped, the polarities of the electromagnetic ring 441 and the permanent magnet 442 on the side closest to each other are opposite.

[0037] Both the control rack 443 and the control gear 444 are set in the transmission groove 413 opened on the mounting base 41. The transmission groove 413 is connected to the control slide 412. The control rack 443 meshes with the control gear 444. The control rack 443 is fixedly connected to the connecting rod 4431. The connecting rod 4431 is fixedly connected to the permanent magnet block 442. The control gear 444 is fixedly connected to the hinge shaft 434.

[0038] When the UAV body 3 is activated, the electromagnetic ring 441 and the permanent magnet block 442 are in a state of mutual repulsion. Under the action of magnetic thrust, the permanent magnet block 442 can slide down to the bottom of the control chute 412. The permanent magnet block 442 drives the control rack 443 to move through the connecting rod 4431. The control rack 443 drives the control gear 444 to rotate. The control gear 444 can drive the hinge shaft 434 to rotate. The hinge shaft 434 can drive the closing plate 433 to swing, so that the snap-fit ​​hole 4311 opens. When the UAV body 3 is stopped, the electromagnetic ring 441 and the permanent magnet block 442 can be in a state of mutual attraction. The permanent magnet block 442 can slide up to the slot position of the control slide 412. The permanent magnet block 442 can drive the sealing plate 433 to close the snap-fit ​​hole 4311 through the control rack 443 and the control gear 444. The magnetic attraction between the electromagnetic ring 441 and the permanent magnet block 442 can also apply a fixing force to the connecting seat 42 and the mounting seat 41, so that the detector body 2 is not easy to rotate freely under normal conditions.

[0039] Reference Figure 4 To facilitate the docking and installation of the mounting base 41 and the connecting base 42, the mounting surfaces of the mounting base 41 and the connecting base 42 that are close to each other are conical. By installing the connecting base 42 and the mounting base 41 through the conical mounting surfaces, the connecting base 42 is easy to position relative to the mounting base 41, which facilitates the insertion of the snap-fit ​​connector 421 into the mounting hole 411, thereby facilitating the docking of the connecting base 42 and the mounting base 41 and improving the connection efficiency between the connecting base 42 and the mounting base 41.

[0040] Reference Figure 2 and Figure 3 In order to reduce the frictional resistance of the drive connector 42 rotating on the UAV body 3, the number of the snap connector 421, snap hole 4311, permanent magnet 442, control rack 443 and control gear 444 are the same in pairs, and multiple permanent magnets 442 are evenly arranged around the axis of the mounting base 41.

[0041] The uniformly arranged permanent magnet blocks 442 can form a stable and central magnetic thrust on the electromagnetic ring 441. On the one hand, it helps the connector 421 to be inserted into the mounting hole 411 in a centered position. On the other hand, it helps to reduce the frictional resistance between the connector 42 and the mounting base 41 or between the connector 421 and the first retaining ring 431, making it easier for the UAV body 3 to drive the connector 421 to rotate.

[0042] Reference Figure 4 In order to enable the connector 42 to quickly locate and approach the mounting base 41 after the flight, a camera 5 is connected to the center of the bottom surface of the connector 42. When the connector 42 is installed on the mounting base 41, the camera 5 can be located inside the mounting hole 411. The camera 5 can capture video images of the area below the connector 42. The video images help the user to quickly locate the mounting base 41, and the user can determine the relative position of the connector 42 and the mounting base 41 based on the video images, thus speeding up the connection efficiency between the connector 42 and the mounting base 41.

[0043] Reference Figure 1 and Figure 2 In order to protect the propellers of the drone body 3 in severe weather, a protective component 6 is provided on the connecting seat 42. The number of protective components 6 is the same as the number of propellers on the drone body 3. The protective component 6 includes a protective electric cylinder 61, a protective rack 62, a protective gear 63, a protective rod 64, and a protective cloth 65.

[0044] Two protective electric cylinders 61, two protective racks 62, two protective gears 63, and two protective rods 64 are provided, and they are symmetrically arranged on both sides of the propeller of the UAV body 3. The protective electric cylinder 61 is fixed to the connecting seat 42. The protective racks 62 are fixed to the movable end of the protective electric cylinder 61. The protective gears 63 mesh with the protective racks 62 and are rotatably connected to the connecting seat 42. One end of the protective rod 64 is fixed to the protective gear 63 through a rotating shaft, and the other end is fixed to the edge of the protective cloth 65. The edge of the protective cloth 65 away from the protective rod 64 is fixed to the UAV body 3. The two protective rods 64 can unfold the protective cloth 65 above the propeller of the UAV body 3.

[0045] In this embodiment, in order to enhance the protective capability of the protective cloth 65, the protective cloth 65 can be unfolded and placed in a U-shape over the propeller of the drone body 3.

[0046] When the outdoor weather is severe, such as heavy rain or strong winds, the protective electric cylinder 61 extends, which drives the protective rack 62 to move. The protective rack 62 drives the protective gear 63 to rotate, and the protective gear 63 can drive the protective rod 64 to swing away from the detector body 2. The two protective rods 64 can unfold the protective cloth 65 and cover the propeller of the drone body 3 to protect the propeller of the drone body 3 from damage.

[0047] Reference Figure 2 In order to further secure the connecting seat 42 and the mounting seat 41 in severe weather, the protective electric cylinder 61 is connected to a reinforcing component 7, which includes a reinforcing head 71 and a reinforcing ring 72.

[0048] ReferenceFigure 2 and Figure 5 The number of reinforcing heads 71 ​​is the same as the number of protective electric cylinders 61. Each reinforcing head 71 is fixedly connected to the movable end of the protective electric cylinder 61. Two reinforcing nails 73 are fixedly connected to each reinforcing head 71. A reinforcing ring 72 is fixedly connected to the mounting base 41 and sleeved on the connecting base 42. A reinforcing rubber layer 74 is fixedly connected to the inner wall of the reinforcing ring 72. When the protective electric cylinder 61 extends, it can drive the reinforcing head 71 to press against the reinforcing rubber layer 74 and drive the reinforcing nails 73 to be driven into the reinforcing rubber layer 74. When the protective electric cylinder 61 extends, it can drive the protective rod 64 to unfold the protective cloth 65, so that the unfolding of the protective cloth 65 and the further reinforcement of the connecting base 42 relative to the mounting base 41 can be carried out simultaneously.

[0049] When the protective electric cylinder 61 extends due to severe weather, the protective electric cylinder 61 can also drive the reinforcing head 71 to abut against the reinforcing rubber layer 74, and can make the reinforcing nail 73 stick into the reinforcing rubber layer 74 to further fix the connecting seat 42 and the mounting seat 41, making it even more difficult for the connecting seat 42 to rotate relative to the mounting seat 41, so that the detector body 2 can be stably installed on the mounting column 1 in severe weather.

[0050] Reference Figure 2 and Figure 3 In order to enable the detector body 2 and the drone body 3 to easily obtain power, the drone body 3 is equipped with a power supply component 8, which includes a solar panel 81 and a battery 82. The solar panel 81 is electrically connected to the battery 82, and the battery 82 is electrically connected to the detector body 2, the drone body 3 and the magnetic control unit 44 respectively.

[0051] The battery 82 is charged by the solar panel 81, so that the battery 82 can be automatically replenished and the detector body 2, the drone body 3 and the magnetic control unit 44 can use clean energy.

[0052] Reference Figure 2 and Figure 3 In this embodiment, the solar panel 81 is located in the middle of the UAV body 3, and there are four batteries 82, which are evenly arranged around the solar panel 81. In this embodiment, the batteries 82 are electrically connected to the electromagnetic ring 441 of the magnetic control unit 44. In this embodiment, the batteries 82 are also electrically connected to the camera 5 and the protective electric cylinder 61.

[0053] The implementation principle of an air quality detection device according to an embodiment of this application is as follows: In normal use, the detector body 2 can perform fixed-point air detection on the mounting column 1. When it is necessary to expand the detection range, the drone body 3 is started, the magnetic control unit 44 opens the snap-fit ​​hole 4311, and the drone body 3 rotates in the reverse direction to drive the snap-fit ​​connector 421 to disengage from between the first snap ring 431 and the second snap ring 432 along the sealing plate 433, so that the drone body 3 can carry the detector body 2 to fly, enabling the detector body 2 to cruise and detect the air, thus expanding the detection range of the detector body 2. After completing the cruise detection, the drone body 3 carries the detector body 2 back to the mounting column 1, and the drone body 3 rotates in the forward direction to drive the snap-fit ​​connector 421 to slide into between the first snap ring 431 and the second snap ring 432 along the sealing plate 433. After the drone stops, the magnetic control unit 44 closes the snap-fit ​​hole 4311, and the detector body 2 continues to perform fixed-point detection, so that fixed-point detection and area detection can be used in combination. Area detection is performed intermittently during the fixed-point detection process, thereby improving the reliability of the detection results.

[0054] The above are all preferred embodiments of this application, and are not intended to limit the scope of protection of this application. Therefore, all equivalent changes made in accordance with the structure, shape and principle of this application should be covered within the scope of protection of this application.

Claims

1. An air quality detection device, characterized in that: The device includes a mounting post (1), a detector body (2), and a drone body (3). The mounting post (1) is fixedly installed on the ground, and the detector body (2) is installed on the drone body (3). An installation assembly (4) is provided between the detector body (2) and the mounting post (1). The installation assembly (4) includes a mounting base (41), a connecting base (42), a snap-fit ​​part (43), and a magnetic control part (44). The mounting base (41) is connected to the mounting post (1), and the connecting base (42) is connected to the detector body (2). A snap-fit ​​connector (421) is connected to the connecting base (42). The snap-fit ​​part (43) is provided on the mounting base (41), and a snap-fit ​​notch is provided on the snap-fit ​​part (43). The snap-fit ​​connector (421) can be rotated and snapped onto the snap-fit ​​part (43) through the snap-fit ​​notch. The magnetic control unit (44) is disposed between the mounting base (41) and the connecting base (42). The magnetic control unit (44) is used to control the opening and closing of the snap-fit ​​notch based on the startup status of the UAV body (3). When the connecting base (42) is close to the mounting base (41), the magnetic control unit (44) opens the snap-fit ​​notch when the UAV body (3) is in the startup state, and closes the snap-fit ​​notch when the UAV body (3) is in the shutdown state. When the snap-fit ​​notch is open, the snap-fit ​​connector (421) can rotate forward and snap onto the snap-fit ​​part (43) under the drive of the UAV body (3), and the snap-fit ​​connector (421) can rotate in the opposite direction and disengage from the snap-fit ​​part (43) under the drive of the UAV body (3).

2. The air quality detection device according to claim 1, characterized in that: The snap-fit ​​part (43) includes a first snap ring (431), a second snap ring (432), and a closing plate (433). The first snap ring (431) and the second snap ring (432) are both connected to the wall of the mounting hole (411) opened in the middle of the mounting base (41). The first snap ring (431) is located above the second snap ring (432). The first snap ring (431) has a snap-fit ​​hole (4311), which forms the snap-fit ​​notch of the snap-fit ​​part (43). The sealing plate (433) is hinged to the snap-fit ​​hole (4311) via the hinge shaft (434). The magnetic control unit (44) is used to control the sealing plate (433) to swing forward and abut against the second snap ring (432) to open the snap-fit ​​hole (4311). The magnetic control unit (44) is used to control the sealing plate (433) to swing in the opposite direction to close the snap-fit ​​hole (4311). The snap-fit ​​connector (421) is provided with a release ramp (422) that can slide onto the sealing plate (433).

3. An air quality detection device according to claim 2, characterized in that: A guide plate (435) is connected to the side of the first retaining ring (431) away from the second retaining ring (432). The guide plate (435) is located near the snap-fit ​​hole (4311). The guide plate (435) is used to guide the snap-fit ​​joint (421) into the snap-fit ​​hole (4311) when the snap-fit ​​joint (421) rotates in the forward direction.

4. An air quality detection device according to claim 2, characterized in that: The magnetic control unit (44) includes an electromagnetic ring (441), a permanent magnet (442), a control rack (443), and a control gear (444). The electromagnetic ring (441) is embedded in the connecting seat (42), and the permanent magnet (442) is slidably disposed in the control groove (412) opened on the mounting seat (41). When the UAV body (3) is powered on, the electromagnetic ring (441) and the permanent magnet (442) have the same polarity on the side closest to each other. When the human-machine body (3) stops, the electromagnetic ring (441) and the permanent magnet block (442) are opposite in polarity on the side they are close to each other. The control rack (443) and the control gear (444) are both set in the transmission groove (413) opened on the mounting base (41). The control rack (443) meshes with the control gear (444), the control rack (443) is connected to the permanent magnet block (442), and the control gear (444) is connected to the hinge shaft (434).

5. An air quality detection device according to claim 4, characterized in that: The mounting surfaces of the mounting base (41) and the connecting base (42) that are close to each other are both conical.

6. An air quality detection device according to claim 5, characterized in that: The number of the card connector (421), card hole (4311), permanent magnet (442), control rack (443) and control gear (444) are the same in pairs, and multiple permanent magnets (442) are evenly arranged around the axis of the mounting base (41).

7. An air quality detection device according to claim 2, characterized in that: A camera (5) is connected to the connector (42). When the connector (42) is installed on the mounting base (41), the camera (5) can be located in the mounting hole (411).

8. An air quality detection device according to claim 1, characterized in that: The connecting seat (42) is provided with a protective component (6). The number of protective components (6) is the same as the number of propellers on the UAV body (3). The protective component (6) includes a protective electric cylinder (61), a protective rack (62), a protective gear (63), a protective rod (64), and a protective cloth (65). There are two of each of the protective electric cylinder (61), the protective rack (62), the protective gear (63), and the protective rod (64), and they are symmetrically arranged on both sides of the propellers on the UAV body (3). The protective electric cylinder (61) is connected to... On the connecting seat (42), the protective racks (62) are connected to the movable end of the protective electric cylinder (61) in a one-to-one correspondence. The protective gears (63) are meshed with the protective racks (62) in a one-to-one correspondence and are rotatably connected to the connecting seat (42). One end of the protective rod (64) is connected to the protective gear (63) in a one-to-one correspondence, and the other end is connected to the protective cloth (65). The protective cloth (65) is connected to the UAV body (3). The two protective rods (64) can unfold the protective cloth (65) above the propeller of the UAV body (3).

9. An air quality detection device according to claim 8, characterized in that: The protective electric cylinder (61) is connected to a reinforcing component (7). The reinforcing component (7) includes a reinforcing head (71) and a reinforcing ring (72). The number of reinforcing heads (71) is the same as the number of protective electric cylinders (61). The reinforcing heads (71) are connected to the movable end of the protective electric cylinder (61) in a one-to-one correspondence. A reinforcing nail (73) is connected to the reinforcing head (71). The reinforcing ring (72) is connected to the mounting base (41). A reinforcing rubber layer (74) is connected to the reinforcing ring (72). When the protective electric cylinder (61) extends, it can drive the reinforcing head (71) to press against the reinforcing rubber layer (74) and drive the reinforcing nail (73) to be driven into the reinforcing rubber layer (74). When the protective electric cylinder (61) extends, it can drive the protective rod (64) to unfold the protective cloth (65).

10. An air quality detection device according to claim 1, characterized in that: The UAV body (3) is provided with a power supply component (8), which includes a solar panel (81) and a battery (82). The solar panel (81) and the battery (82) are electrically connected. The battery (82) is electrically connected to the detector body (2), the UAV body (3) and the magnetic control unit (44).

Citation Information

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