Air gas sampling device mounted on unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle mounted air gas sampling device which comprises an unmanned aerial vehicle body and a gas sampling mechanism telescopic assembly, the unmanned aerial vehicle body comprises a case, the gas sampling mechanism telescopic assembly comprises fixing blocks, the fixing blocks are connected to the two side ends in the case in a welded mode, and the fixing blocks are connected with the case in a welded mode. The interior of the fixed block is connected with a rotating bolt in a penetrating manner, when the gas sampling device is moved into the unmanned aerial vehicle case, vibration and impact on the gas sampling device in the long-time flight process of the unmanned aerial vehicle can be avoided, and the situation that a connecting part of the gas sampling device is loosened or falls off is avoided; the stability of the gas sampling device is influenced, and the gas sampling device is moved into the case, so that better protection measures can be provided, and the conditions that the gas sampling device is damaged by external environmental factors and the like are prevented.

Description

Technical Field

[0001] The utility model relates to the technical field of packaging equipment, in particular to an air gas sampling device mounted on an unmanned aerial vehicle. Background Art

[0002] In the fields of environmental monitoring, industrial emission detection, air quality assessment, disaster site investigation, etc., air gas sampling devices mounted on drones provide a fast, efficient and relatively low-cost solution. Compared with traditional ground monitoring stations, drones can reach remote or inaccessible areas and collect data over a large range. By carrying different types of sensors, these devices can analyze a variety of gases, such as carbon dioxide, methane, hydrogen sulfide, etc., helping researchers and decision makers better understand the state of atmospheric pollution and its impact on the environment and human health.

[0003] The prior art discloses a technical solution for a gas sampling device for an unmanned aerial vehicle. The solution includes a straight rod and a circular plate through an installation structure. The inner side of the straight rod is fixedly connected to the outer wall of a square frame, and the outer side of the straight rod is fixedly connected to the inner side of the circular plate. The outer wall of the straight rod is slidably engaged with a square plate. The square plate slides back and forth through the outer wall of the straight rod under force. A spring is sleeved on the outer wall of the straight rod. The two ends of the spring are respectively fixedly connected to the outer wall of the square frame and the inner side of the square plate. After the square plate is moved under force, it rebounds through the elastic force of the spring. The outer wall of the square plate is fixedly connected to an insert plate, and the outer wall of the insert plate is slidably engaged with the groove of the outer wall of the square frame.

[0004] In this scheme, when the gas sampling device is installed and connected to the drone and has completed the sampling work, if the gas sampling device is exposed to the outside for a long time, due to the vibration, impact and airflow changes during the flight, long-term exposure may cause the connecting parts to loosen or fall off, thereby affecting the stability of the gas sampling device. Utility Model Content

[0005] The purpose of the utility model is to provide an air gas sampling device mounted on a drone to solve the problems raised in the above-mentioned background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an air gas sampling device mounted on a drone, comprising a drone body and a telescopic assembly of a gas sampling mechanism, the drone body includes a chassis installed thereon, the telescopic assembly of the gas sampling mechanism includes a fixed block, the fixed block is connected to both side ends inside the chassis by welding, the interior of the fixed block is connected with a rotating bolt through a penetration, the outer side of the rotating bolt is connected with a connecting block through a rotation, one end of the connecting block is connected and fixed to a telescopic hydraulic cylinder by a bolt, a telescopic guide column is installed inside the telescopic hydraulic cylinder, one end of the telescopic guide column is connected to the outer end of a rotating pin by a bolt, the rotating pin is connected to the interior of the fixed block by a penetration, and the fixed block is connected to one end side of the gas sampling body by welding.

[0007] As a further preferred embodiment of the technical solution, a gas sampling hole is provided at one end of the gas sampling body, and movable bolts are installed at both side ends of the gas sampling body, and the movable bolts are connected to the inside of the first connecting rod and the second connecting rod by rotation.

[0008] As a further preferred embodiment of the technical solution, one end of the first connecting rod and the second connecting rod is connected by rotation and has a rotating bolt, and the rotating bolt is connected to the interior of the fixed block through a penetration.

[0009] As a further preferred embodiment of the present technical solution, brackets are connected to both sides of the chassis by welding, the lower ends of the brackets are fixed to the floor panels by bolts, and sliding grooves are provided inside both sides of the lower end of the chassis.

[0010] As a further preferred embodiment of the present technical solution, a first sliding rod and a second sliding rod are slidably connected inside the sliding groove, and sliding through holes are provided inside the first sliding rod and the second sliding rod.

[0011] As a further preferred embodiment of the technical solution, the interior of the first sliding rod is connected with a screw rod through rotation, an electric motor is installed at one end of the screw rod, and the electric motor is connected to one end of the chassis through bolts.

[0012] As a further preferred embodiment of the present technical solution, the interior of the second sliding rod is slidably connected to a support guide column, one end of the support guide column is provided with a mounting plate, and the lower ends of the first sliding rod and the second sliding rod are connected and fixed to the closed door by welding.

[0013] The utility model provides an air gas sampling device mounted on a drone, which has the following beneficial effects:

[0014] (1) By moving the gas sampling device to the inside of the UAV chassis, the utility model can avoid vibration and impact on the gas sampling device during the long-term flight of the UAV, and avoid loosening or falling off of the connecting parts of the gas sampling device, thereby affecting the stability of the gas sampling device. Moving the gas sampling device into the chassis can provide better protection measures to prevent external environmental factors from causing damage to the gas sampling device.

[0015] (2) The utility model recovers the gas sampling device into the interior of the UAV chassis by driving the electric motor to drive the screw rod to rotate inside the first sliding rod, and the rotation of the screw rod further drives the first sliding rod and the second sliding rod to move, and the movement of the first sliding rod and the second sliding rod further drives the closed door to move, and the lower end of the UAV chassis is closed by the movement of the closed door. By closing the lower end opening of the UAV chassis, the gas sampling device can be effectively protected from external factors, such as bad weather, accidental collision, etc., which helps to reduce the possibility of damage to the gas sampling device and ensure the safety of the sampling process. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model from the first perspective;

[0017] Figure 2 It is a schematic diagram of the overall structure of the utility model from the first perspective;

[0018] Figure 3 It is a schematic diagram of the sliding groove structure of the utility model;

[0019] Figure 4 It is a schematic diagram of the telescopic component structure of the practical gas sampling mechanism;

[0020] Figure 5 It is a schematic diagram of the closed component structure of the utility model;

[0021] In the figure: 100, drone body; 101, chassis; 102, floor panel; 103, bracket; 200, telescopic assembly of gas sampling mechanism; 201, fixed block; 202, rotating bolt; 203, first connecting rod; 204, second connecting rod; 205, movable bolt; 206, gas sampling body; 207, gas sampling hole; 208, rotating latch; 209, telescopic guide column; 210, telescopic hydraulic cylinder; 211, connecting block; 300, closing assembly; 301, sliding groove; 302, first sliding rod; 303, second sliding rod; 304, sliding through hole; 305, screw rod; 306, electric motor; 307, supporting guide column; 308, mounting plate; 309, closing door. DETAILED DESCRIPTION

[0022] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0023] The utility model provides a technical solution: Figure 1-2 , Figure 4 As shown, in the present embodiment, an air gas sampling device mounted on a drone includes a drone body 100 and a telescopic assembly 200 of a gas sampling mechanism, wherein the drone body 100 includes a chassis 101 installed thereon, and the telescopic assembly 200 of the gas sampling mechanism includes a fixed block 201, wherein the fixed block 201 is connected to both side ends inside the chassis 101 by welding, wherein the interior of the fixed block 201 is connected with a rotating bolt 202 by penetration, and the outer side of the rotating bolt 202 is connected with a connecting block 211 by rotation, and one end of the connecting block 211 is connected and fixed to a telescopic hydraulic cylinder 210 by bolts, and a telescopic guide column 209 is installed inside the telescopic hydraulic cylinder 210, and one end of the telescopic guide column 209 is connected to the outer end of a rotating pin 208 by bolts, and the rotating pin 208 is connected to the interior of the fixed block 201 by penetration, and the fixed block 201 is connected to one end side of a gas sampling body 206 by welding.

[0024] like Figure 4 As shown, a gas sampling hole 207 is provided at one end of the gas sampling body 206, and movable bolts 205 are installed on both side ends of the gas sampling body 206. The movable bolts 205 are connected to the inside of the first connecting rod 203 and the second connecting rod 204 by rotation. The inside of one end of the first connecting rod 203 and the second connecting rod 204 is connected to the rotating bolt 202 by rotation, and the rotating bolt 202 is connected to the inside of the fixed block 201 through a penetration.

[0025] The drone is started and operated, and the air gas sampling device is used to sample the air gas. When the gas sampling device is completed, the telescopic guide column 209 is moved by driving the telescopic hydraulic cylinder 210. When the telescopic guide column 209 retracts inwardly inside the telescopic hydraulic cylinder 210, the rotating latch 208 on the telescopic guide column 209 rotates on the fixed block 201, and the gas sampling body 206 moves upward and moves into the chassis 101. The connecting block 211 at one end of the telescopic hydraulic cylinder 210 rotates on the rotating bolt 202. When the gas sampling body 206 moves upward, it further drives the first connecting rod 203 and the second connecting rod 204. The connecting rod 204 moves upward, and drives the first connecting rod 203 and the second connecting rod 204 to rotate through the movable bolt 205. At the same time, the first connecting rod 203 and the second connecting rod 204 are driven to rotate through the rotating bolt 202. By moving the gas sampling device to the inside of the drone chassis 101, it can avoid vibration and impact on the gas sampling device during long-term flight of the drone, and avoid loosening or falling off of the connecting parts of the gas sampling device, thereby affecting the stability of the gas sampling device. Moving the gas sampling device into the chassis 101 can provide better protection measures to prevent external environmental factors from causing damage to the gas sampling device.

[0026] like Figure 1 , Figure 3 , Figure 5 As shown, brackets 103 are connected to both sides of the chassis 101 by welding, and the lower end of the bracket 103 is fixed to the floor panel 102 by bolts. Sliding grooves 301 are provided inside the lower end of the chassis 101 on both sides, and the first sliding rod 302 and the second sliding rod 303 are connected inside the sliding grooves 301 by sliding. Sliding through holes 304 are provided inside the first sliding rod 302 and the second sliding rod 303. A screw rod 305 is connected inside the first sliding rod 302 by rotation, and an electric motor 306 is installed at one end of the screw rod 305. The electric motor 306 is connected to one end of the chassis 101 by bolts. A support guide column 307 is connected inside the second sliding rod 303 by sliding, and a mounting plate 308 is installed at one end of the support guide column 307. The lower ends of the first sliding rod 302 and the second sliding rod 303 are connected and fixed to the closed door 309 by welding.

[0027] When the gas sampling device is recovered into the UAV chassis 101, the electric motor 306 is driven to drive the screw rod 305 to rotate inside the first sliding rod 302, and the rotation of the screw rod 305 further drives the first sliding rod 302 and the second sliding rod 303 to move. The movement of the first sliding rod 302 and the second sliding rod 303 further drives the closed door 309 to move. The lower end of the UAV chassis 101 is closed by the movement of the closed door 309. By closing the lower end opening of the UAV chassis 101, the gas sampling device can be effectively protected from external factors, such as bad weather, accidental collisions, etc., which helps to reduce the possibility of damage to the gas sampling device and ensure the safety of the sampling process.

[0028] The utility model provides an air gas sampling device mounted on a drone, and the specific working principle is as follows: the drone is started and operated, and the air gas sampling device is used to sample the air gas. When the gas sampling device is completed, the telescopic guide column 209 is driven to move by driving the telescopic hydraulic cylinder 210. When the telescopic guide column 209 is retracted inwardly inside the telescopic hydraulic cylinder 210, the rotating pin 208 on the telescopic guide column 209 rotates on the fixed block 201, and at the same time, the gas sampling body 206 moves upward and moves into the inside of the chassis 101. The connecting block 211 at one end of the telescopic hydraulic cylinder 210 rotates on the rotating bolt 202. When the gas sampling body 206 moves upward, it further drives the first connecting rod 203 and the second connecting rod 204 to move. The movable bolt 205 drives the first connecting rod 203 and the second connecting rod 204 to rotate, and the rotating bolt 202 drives the first connecting rod 203 and the second connecting rod 204 to rotate. The gas sampling device is moved to the inside of the UAV chassis 101. When the gas sampling device is recovered to the inside of the UAV chassis 101, the electric motor 306 drives the screw rod 305 to rotate inside the first sliding rod 302. The rotation of the screw rod 305 further drives the first sliding rod 302 and the second sliding rod 303 to move. The movement of the first sliding rod 302 and the second sliding rod 303 further drives the closed door 309 to move. The lower end of the chassis 101 of the UAV is closed by the movement of the closed door 309.

[0029] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An air gas sampling device mounted on an unmanned aerial vehicle, comprising an unmanned aerial vehicle body (100) and a gas sampling mechanism telescopic assembly (200), characterized in that: The unmanned aerial vehicle body (100) includes a chassis (101) installed thereon, and the telescopic assembly (200) of the gas sampling mechanism includes a fixed block (201), the fixed block (201) is connected to both side ends inside the chassis (101) by welding, the inside of the fixed block (201) is connected by a rotating bolt (202) through the inside, the outside of the rotating bolt (202) is connected by a connecting block (211) by rotation, one end of the connecting block (211) is connected and fixed to a telescopic hydraulic cylinder (210) by bolts, a telescopic guide column (209) is installed inside the telescopic hydraulic cylinder (210), one end of the telescopic guide column (209) is connected to the outer end of a rotating pin (208) by bolts, the rotating pin (208) is connected to the inside of the fixed block (201) by penetration, and the fixed block (201) is connected to one end of the gas sampling body (206) by welding.

2. The air gas sampling device mounted on a drone according to claim 1, characterized in that: A gas sampling hole (207) is provided at one end of the gas sampling body (206), and movable bolts (205) are installed on both side ends of the gas sampling body (206). The movable bolts (205) are connected to the inside of the first connecting rod (203) and the second connecting rod (204) by rotation.

3. The air gas sampling device mounted on a drone according to claim 2, characterized in that: One end of the first connecting rod (203) and the second connecting rod (204) are connected by rotation and have a rotating bolt (202), and the rotating bolt (202) is connected to the inside of the fixed block (201) by passing through.

4. The air gas sampling device mounted on a drone according to claim 1, characterized in that: Brackets (103) are connected to both sides of the chassis (101) by welding, and the lower ends of the brackets (103) are fixed to the floor panels (102) by bolts. Sliding grooves (301) are provided inside both sides of the lower end of the chassis (101).

5. The air gas sampling device mounted on a drone according to claim 4, characterized in that: The interior of the sliding groove (301) is connected by sliding with a first sliding rod (302) and a second sliding rod (303), and the interior of the first sliding rod (302) and the second sliding rod (303) is provided with a sliding through hole (304).

6. The air gas sampling device mounted on a drone according to claim 5, characterized in that: The first sliding rod (302) is internally connected to a screw rod (305) by rotation, one end of the screw rod (305) is installed with an electric motor (306), and the electric motor (306) is connected to one end of the chassis (101) by bolts.

7. The air gas sampling device mounted on a drone according to claim 6, characterized in that: The interior of the second sliding rod (303) is slidably connected to a support guide column (307), one end of the support guide column (307) is mounted with a mounting plate (308), and the lower ends of the first sliding rod (302) and the second sliding rod (303) are connected and fixed to the closed door (309) by welding.

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