Remote sensing monitoring equipment for vegetation growth vigor

Abstract

The utility model discloses remote sensing monitoring equipment for vegetation growth vigor, which relates to the field of remote sensing monitoring equipment for vegetation growth vigor and comprises a machine body, a lifting frame is fixedly connected above the machine body, and a lifting block is slidably connected in the lifting frame. When the lead screw rotates, the sliding block is driven to slide, when the sliding block slides, the connecting rod pushes the lifting block to slide in the lifting frame, the height of the monitor can be changed, the monitoring range can be increased, and when the exterior of the monitor is shielded by impurities, the impurities can be scraped through up-down sliding of the lifting block in the lifting frame; by arranging a third motor, when the machine body encounters a slope or a depression, the third motor is started to drive a rotating rod to rotate, the rotating rod drives a second connecting shaft to rotate, the second connecting shaft drives a front wheel to ascend or descend to support the machine body, and the machine body is convenient to move.

Description

Technical Field

[0001] The utility model relates to the field of vegetation growth remote sensing monitoring equipment, in particular to vegetation growth remote sensing monitoring equipment. Background Art

[0002] Vegetation plays an important role in soil formation. Under different climatic conditions, there is a close relationship between various vegetation types and soil types. Effective monitoring and protection of forest cover is a very meaningful task.

[0003] Patent No. CN218142119U discloses a vegetation growth remote sensing monitoring device, including a fuselage, a built-in plate fixedly installed at the middle end of the inner wall of the fuselage, support motors fixedly installed on both sides close to the fuselage, a base fixedly installed at the bottom of the fuselage, a rotating shaft and running wheels symmetrically fixedly installed on both sides, and a monitoring device fixedly installed on the top of the fuselage. The pressing ball of the vegetation growth remote sensing monitoring device rolls along the ramp in the hollow tube, thereby triggering the second button, and the first button pops up, so that the support motor on the opposite side starts, driving the connecting shaft to rotate, so that the support wheel on the lifted side contacts the ground, and at this time the running wheel rotates, driving the support wheel to roll, so that the fuselage is successfully detached. After the detachment is completed, the center of gravity of the fuselage returns to the right position, so that the pressing ball presses the first button again along the tube wall, so that the support motor rotates in the opposite direction to before, and then returns to the control frame.

[0004] When the above-mentioned vegetation growth remote sensing monitoring equipment is in use, the monitor cannot change the monitoring position, the monitoring range is insufficient, and the monitor is easily covered by debris, which affects the monitoring results. Utility Model Content

[0005] The utility model aims to provide a vegetation growth remote sensing monitoring device to solve the problems that the monitoring position of the monitor cannot be changed, the monitoring range is insufficient, and the monitor is easily covered by debris, which affects the monitoring result.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a remote sensing monitoring device for vegetation growth, comprising a fuselage, a lifting frame fixedly connected to the top of the fuselage, a lifting block slidably connected to the inside of the lifting frame, a No. 1 motor is installed on the top of the fuselage, a screw rod is fixedly connected to the output end of the No. 1 motor, a slider is provided on the outer surface of the screw rod, one side of the slider is rotatably connected to a connecting rod, one end of the connecting rod is rotatably connected to the bottom of the lifting block, a monitor is installed on the top of the lifting block, the No. 1 motor is started to drive the screw rod to rotate, and the slider is driven to slide when the screw rod rotates, and the connecting rod pushes the lifting block to slide inside the lifting frame when the slider slides, so as to change the height of the monitor and increase the monitoring range. When the outside of the monitor is blocked by impurities, the impurities can be scraped off by the lifting block sliding up and down inside the lifting frame.

[0007] As a further solution of the utility model: a built-in plate is fixedly connected to the inside of the fuselage, a fixing frame is fixedly connected to the top of the built-in plate, a No. 2 motor is installed on one side of the fixing frame, an output end of the No. 2 motor is fixedly connected to a No. 1 connecting shaft, one end of the No. 1 connecting shaft is rotatably connected to a supporting wheel, when the fuselage is lifted up by stones, the No. 2 motor is started to make the No. 1 connecting shaft drive the supporting wheel to rotate, so that the supporting wheel contacts the ground, props up the fuselage, and makes the fuselage detach.

[0008] As a further solution of the utility model: a No. 3 motor is installed at the lower part of the fuselage, the output end of the No. 3 motor is fixedly connected to a rotating rod, one end of the rotating rod is fixedly connected to a No. 2 connecting shaft, and one end of the No. 2 connecting shaft is installed with a front wheel. When the fuselage encounters a slope or a depression, the No. 3 motor is started to drive the rotating rod to rotate, the rotating rod drives the No. 2 connecting shaft to rotate, and the No. 2 connecting shaft drives the front wheel to lift or lower the fuselage to prop up the fuselage, thereby facilitating the movement of the fuselage.

[0009] As a further solution of the utility model: rear wheels are installed under the fuselage, and the rear wheels provide power for the travel of the fuselage.

[0010] As a further solution of the utility model: a hollow tube is fixedly connected to the lower part of the interior of the fuselage, one end of the hollow tube is fixedly connected to one side of the interior of the fuselage, and a pressing ball is arranged inside the hollow tube, through which it can be monitored whether the fuselage is lifted by stones.

[0011] As a further solution of the utility model: two groups of threads with different directions are provided at both ends of the screw rod, and there are two groups of sliders, which are respectively connected to the two ends of the screw rod through threaded rotation. When the screw rod rotates, the two groups of sliders slide in the same or opposite directions, which can drive the lifting block to slide up and down inside the lifting frame.

[0012] As a further solution of the utility model: a control frame is arranged above the fuselage. When the fuselage is detached from the stone, the support wheel is reset and the control frame fixes the support wheel, thereby avoiding the shear stress of the support wheel and the No. 1 connecting shaft on the output end of the No. 2 motor, thereby increasing the service life of the device.

[0013] Compared with the prior art, the beneficial effects of the utility model are:

[0014] 1. By setting up a lifting frame, starting the No. 1 motor to drive the screw to rotate, the screw rotates to drive the slider to slide, and the connecting rod pushes the lifting block to slide inside the lifting frame when the slider slides, so as to change the height of the monitor and increase the monitoring range. When the outside of the monitor is blocked by impurities, the impurities can be scraped off by sliding the lifting block up and down inside the lifting frame;

[0015] 2. By setting the No. 3 motor, when the fuselage encounters a slope or a depression, the No. 3 motor is started to drive the rotating rod to rotate, the rotating rod drives the No. 2 connecting shaft to rotate, and the No. 2 connecting shaft drives the front wheel to lift or lower the fuselage to prop up the fuselage, making it easier to move the fuselage. BRIEF DESCRIPTION OF THE DRAWINGS

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

[0017] Figure 2 This is a schematic diagram of the lifting block structure of the utility model;

[0018] Figure 3 This is a schematic diagram of the support wheel structure of the utility model;

[0019] Figure 4 It is a schematic diagram of the front wheel structure of the utility model.

[0020] In the figure: 1. fuselage; 2. lifting frame; 3. monitor; 4. control frame; 5. support wheel; 6. rear wheel; 7. front wheel; 8. lifting block; 9. screw rod; 10. slider; 11. connecting rod; 12. No. 1 motor; 13. built-in plate; 14. fixing frame; 15. No. 2 motor; 16. No. 1 connecting shaft; 17. No. 3 motor; 18. rotating rod; 19. No. 2 connecting shaft; 20. hollow tube. DETAILED DESCRIPTION

[0021] 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.

[0022] See also Figure 1-2 In an embodiment of the utility model, a vegetation growth remote sensing monitoring device includes a fuselage 1, a lifting frame 2 is fixedly connected to the top of the fuselage 1, a lifting block 8 is slidably connected to the inside of the lifting frame 2, a No. 1 motor 12 is installed on the top of the fuselage 1, a screw rod 9 is fixedly connected to the output end of the No. 1 motor 12, a slider 10 is provided on the outer surface of the screw rod 9, a connecting rod 11 is rotatably connected to one side of the slider 10, one end of the connecting rod 11 is rotatably connected to the bottom of the lifting block 8, a monitor 3 is installed above the lifting block 8, the No. 1 motor 12 is started to drive the screw rod 9 to rotate, and the screw rod 9 drives the slider 10 to slide when it rotates, and the connecting rod 11 pushes the lifting block 8 to slide inside the lifting frame 2 when the slider 10 slides, so that the height of the monitor 3 can be changed and the monitoring range can be increased. When the outside of the monitor 3 is blocked by impurities, the impurities can be scraped off by sliding the lifting block 8 up and down inside the lifting frame 2.

[0023] In this embodiment: starting the No. 1 motor 12 drives the screw rod 9 to rotate, and when the screw rod 9 rotates, it drives the slider 10 to slide. When the slider 10 slides, the connecting rod 11 pushes the lifting block 8 to slide inside the lifting frame 2, which can change the height of the monitor 3 and increase the monitoring range. When the outside of the monitor 3 is blocked by impurities, the impurities can be scraped off by sliding the lifting block 8 up and down inside the lifting frame 2.

[0024] Please refer to Figure 3 A fixing frame 14 is fixedly connected to the top of the built-in plate 13, and a No. 2 motor 15 is installed on one side of the fixing frame 14. The output end of the No. 2 motor 15 is fixedly connected to the No. 1 connecting shaft 16, and one end of the No. 1 connecting shaft 16 is rotatably connected to the supporting wheel 5. When the fuselage 1 is lifted up by stones, the No. 2 motor 15 is started to make the No. 1 connecting shaft 16 drive the supporting wheel 5 to rotate, so that the supporting wheel 5 contacts the ground, props up the fuselage 1, and makes the fuselage 1 detach.

[0025] In this embodiment, when the fuselage 1 is lifted up by stones, the second motor 15 is started to make the first connecting shaft 16 drive the supporting wheel 5 to rotate, so that the supporting wheel 5 contacts the ground, props up the fuselage 1, and makes the fuselage 1 detach.

[0026] Please refer to Figure 4 A No. 3 motor 17 is installed at the lower part of the fuselage 1, and the output end of the No. 3 motor 17 is fixedly connected to a rotating rod 18, one end of the rotating rod 18 is fixedly connected to a No. 2 connecting shaft 19, and one end of the No. 2 connecting shaft 19 is installed with a front wheel 7. When the fuselage 1 encounters a slope or a depression, the No. 3 motor 17 is started to drive the rotating rod 18 to rotate, the rotating rod 18 drives the No. 2 connecting shaft 19 to rotate, and the No. 2 connecting shaft 19 drives the front wheel 7 to lift or lower the fuselage 1 to prop up the fuselage 1, so as to facilitate the movement of the fuselage 1.

[0027] In this embodiment: when the fuselage 1 encounters a slope or a depression, the No. 3 motor 17 is started to drive the rotating rod 18 to rotate, the rotating rod 18 drives the No. 2 connecting shaft 19 to rotate, and the No. 2 connecting shaft 19 drives the front wheel 7 to lift or lower the fuselage 1 to prop up the fuselage 1, making it easier to move the fuselage 1.

[0028] Please refer to Figure 1 A rear wheel 6 is installed under the fuselage 1, and the rear wheel 6 provides power for the movement of the fuselage 1.

[0029] In this embodiment: the rear wheels 6 provide power for the movement of the fuselage 1 .

[0030] Please refer to Figure 4 A hollow tube 20 is fixedly connected to the lower part of the fuselage 1, one end of the hollow tube 20 is fixedly connected to one side of the fuselage 1, and a pressing ball is arranged inside the hollow tube 20, by which it can be monitored whether the fuselage 1 is lifted by stones.

[0031] In this embodiment: by pressing the ball, it is possible to monitor whether the fuselage 1 is lifted up by stones.

[0032] Please refer to Figure 2 Two sets of threads with different directions are arranged at both ends of the screw rod 9, and there are two sets of sliders 10, which are respectively connected to the two ends of the screw rod 9 through threaded rotation. When the screw rod 9 rotates, the two sets of sliders 10 slide in the same or opposite directions, which can drive the lifting block 8 to slide up and down inside the lifting frame 2.

[0033] In this embodiment, when the screw rod 9 rotates, the two sets of sliders 10 slide in the same or opposite directions, and can drive the lifting block 8 to slide up and down inside the lifting frame 2.

[0034] Please refer to Figure 1 A control frame 4 is provided above the fuselage 1. When the fuselage 1 is detached from the stone, the support wheel 5 is reset, and the control frame 4 fixes the support wheel 5, thereby avoiding the shear stress of the support wheel 5 and the No. 1 connecting shaft 16 on the output end of the No. 2 motor 15, thereby increasing the service life of the device.

[0035] In this embodiment: after the fuselage 1 is detached from the stone, the support wheel 5 is reset, and the control frame 4 fixes the support wheel 5, thereby avoiding the shear stress of the support wheel 5 and the No. 1 connecting shaft 16 on the output end of the No. 2 motor 15, thereby increasing the service life of the device.

[0036] In the utility model, the use principle of the device is:

[0037] The rear wheel 6 provides power for the travel of the fuselage 1. The No. 1 motor 12 is started to drive the screw rod 9 to rotate. When the screw rod 9 rotates, it drives the slider 10 to slide. When the slider 10 slides, the connecting rod 11 pushes the lifting block 8 to slide inside the lifting frame 2, which can change the height of the monitor 3 and increase the monitoring range. When the outside of the monitor 3 is blocked by impurities, the impurities can be scraped off by sliding the lifting block 8 up and down inside the lifting frame 2. When the fuselage 1 is lifted up by stones, the No. 2 motor 15 is started to make the No. 1 connecting shaft 16 drive the supporting wheel 5 to rotate, so that the supporting wheel 5 contacts the ground, props up the fuselage 1, and makes the fuselage 1 detach. When the fuselage 1 encounters a slope or a depression, the No. 3 motor 17 is started to drive the rotating rod 18 to rotate, and the rotating rod 18 drives the No. 2 connecting shaft 19 to rotate. The No. 2 connecting shaft 19 drives the front wheel 7 to lift or lower to prop up the fuselage 1, making it convenient for the fuselage 1 to move.

[0038] What is described above is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A vegetation growth remote sensing monitoring device, comprising a body (1), characterized in that: A lifting frame (2) is fixedly connected to the top of the fuselage (1), a lifting block (8) is slidably connected to the inside of the lifting frame (2), a No. 1 motor (12) is installed on the top of the fuselage (1), a screw rod (9) is fixedly connected to the output end of the No. 1 motor (12), a slider (10) is provided on the outer surface of the screw rod (9), one side of the slider (10) is rotatably connected to a connecting rod (11), one end of the connecting rod (11) is rotatably connected to the bottom of the lifting block (8), and a monitor (3) is installed on the top of the lifting block (8).

2. A vegetation growth remote sensing monitoring device according to claim 1, characterized in that: The interior of the body (1) is fixedly connected with a built-in plate (13), the upper part of the built-in plate (13) is fixedly connected with a fixing frame (14), a No. 2 motor (15) is installed on one side of the fixing frame (14), an output end of the No. 2 motor (15) is fixedly connected with a No. 1 connecting shaft (16), and one end of the No. 1 connecting shaft (16) is rotatably connected with a supporting wheel (5).

3. The vegetation growth remote sensing monitoring device according to claim 1, characterized in that: A third motor (17) is installed at the lower part of the fuselage (1), the output end of the third motor (17) is fixedly connected to a rotating rod (18), one end of the rotating rod (18) is fixedly connected to a second connecting shaft (19), and one end of the second connecting shaft (19) is installed with a front wheel (7).

4. The vegetation growth remote sensing monitoring device according to claim 1, characterized in that: A rear wheel (6) is installed below the fuselage (1).

5. The vegetation growth remote sensing monitoring device according to claim 1, characterized in that: A hollow tube (20) is fixedly connected to the lower part of the interior of the fuselage (1), and one end of the hollow tube (20) is fixedly connected to one side of the interior of the fuselage (1).

6. The vegetation growth remote sensing monitoring device according to claim 1, characterized in that: Two groups of threads with different directions are arranged at the two ends of the screw rod (9), and the sliders (10) have two groups, which are respectively rotatably connected to the two ends of the screw rod (9) through the threads.

7. The vegetation growth remote sensing monitoring device according to claim 1, characterized in that: A control frame (4) is arranged above the fuselage (1).

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