CN219884105U

CN219884105U - Mobile agricultural environment information acquisition control device

Info

Publication number: CN219884105U
Application number: CN202320951465.XU
Authority: CN
Inventors: 黄宝春
Original assignee: Miluo Guangshang Agricultural Products Co ltd
Current assignee: Miluo Guangshang Agricultural Products Co ltd
Priority date: 2023-04-25
Filing date: 2023-04-25
Publication date: 2023-10-24
Anticipated expiration: 2033-04-25

Abstract

The utility model discloses a mobile agricultural environment information acquisition control device which comprises an unmanned aerial vehicle main body, a propeller, a landing gear, a data acquisition unit and a multifunctional assembly mechanism. According to the utility model, the multifunctional assembly mechanism is arranged in the middle of the bottom surface of the unmanned aerial vehicle main body, the butt joint piece can be pulled out from the inner side of the butt joint seat from front to back by pressing the pulling piece downwards, the data collector and the unmanned aerial vehicle main body can be separated, the operation is simple and quick, no tool is needed in the process, the use is more convenient, the auxiliary balance mechanism is arranged between the mounting seat and the butt joint piece, the screw rod is rotated to the direction corresponding to the gravity center deviation of the unmanned aerial vehicle main body, and then the positions of nuts on the screw rods at the two ends are adjusted to level the gravity center of the unmanned aerial vehicle main body, so that the unmanned aerial vehicle main body can fly more stably, and the operation difficulty is reduced.

Description

Mobile agricultural environment information acquisition control device

Technical Field

The utility model relates to the field of agricultural unmanned aerial vehicles, in particular to a mobile agricultural environment information acquisition control device.

Background

China is used as a large agricultural country, a large amount of agricultural plant protection operations are needed each year, along with the development of science and technology, unmanned aerial vehicles are widely applied to agriculture, the climate environment is very important for the growth of crops, and the unmanned aerial vehicles can be provided with temperature and humidity sensors to monitor the environment and climate, prevent extreme weather and ensure the yield of crops.

The prior patent application number is: CN202222619917.2 an unmanned aerial vehicle real-time supervision system for ecological environment monitoring, including fuselage, blade oar, support, cushion, gas detector, through real-time supervision's setting, the camera can start through the motor, and the drive of output shaft carries out the circumference and rotates, when unmanned aerial vehicle flies in the sky, need look over around the mirror image and need not change the fuselage, can pass through the start of motor, drive the camera and carry out all around the observation of making a video recording, has solved unmanned aerial vehicle and has not real-time supervision to need the trouble problem of all-round monitoring turning around.

The above patent describes an unmanned aerial vehicle equipped with an information acquisition device (sensor), the sensor is used to monitor the climate environment, the sensor is usually mounted on the body of the unmanned aerial vehicle by screw locking, so as to ensure that the unmanned aerial vehicle can stably carry the sensor for flying operation, but when the unmanned aerial vehicle is idle, the sensor should be detached and stored separately, so as to ensure the service life of the sensor, but the sensor and the unmanned aerial vehicle need to be assembled and disassembled frequently, so that the assembling structure of the unmanned aerial vehicle needs to be improved to realize rapid assembling and disassembling operation, and in addition, the sensor additionally mounted on the unmanned aerial vehicle easily damages the gravity center balance of the body, although the unmanned aerial vehicle can maintain the balance of the body through a balance system, the difficulty of unmanned aerial vehicle flying control is increased, and the unmanned aerial vehicle needs to be perfected according to the above problems.

Disclosure of Invention

Accordingly, in order to solve the above-mentioned drawbacks, the present utility model provides a mobile agricultural environment information acquisition control apparatus.

In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides a portable agricultural environment information acquisition controlling means, includes unmanned aerial vehicle main part, screw, undercarriage, data collection station and multi-functional assembly mechanism, the screw is installed at the support end of unmanned aerial vehicle main part corner everywhere, the undercarriage is all installed to unmanned aerial vehicle main part bottom surface left and right sides, unmanned aerial vehicle main part bottom surface mid-mounting has the data collection station, and the data line on the data collection station docks with the interface in the unmanned aerial vehicle main part, unmanned aerial vehicle main part bottom surface middle part is provided with multi-functional assembly mechanism, multi-functional assembly mechanism includes mount pad, docking piece, recess, fixture block, plectrum, docking seat, draw-in groove and auxiliary balance mechanism, the mount pad is fixed in data collection station terminal surface, the docking piece is connected to be fixed with in the mount pad top, the recess is seted up on the terminal surface of docking piece, the recess is link up to the docking piece back, the recess front side wall is provided with the fixture block, unmanned aerial vehicle main part bottom surface mid-mounting has the docking seat inboard, the inboard top surface of docking seat has seted up the draw-in groove, inboard fixture block upwards advances between clamping groove and the auxiliary balance mechanism.

Preferably, the mounting seat is X-shaped, and the screw penetrates through the through groove at the tail end of the mounting seat to be locked with the data acquisition device.

Preferably, the mounting base, the butt joint piece and the butt joint base are all made of light materials.

Preferably, the auxiliary balance mechanism comprises a connecting seat, a screw rod and a counterweight nut, wherein a stand column is arranged between the mounting seat and the butt joint piece, the connecting seat is rotationally sleeved on the outer surface of the stand column, the screw rods are symmetrically arranged on two sides of the connecting seat, the counterweight nut is sleeved on the surface of the screw rod, and the counterweight nut is in threaded connection with the surface of the screw rod.

Preferably, after the butt joint piece is fastened and fixed with the butt joint seat, the gravity centers of the mounting seat, the butt joint piece and the connecting seat and the gravity center of the unmanned aerial vehicle main body are positioned in the same vertical direction.

Preferably, the rotation angle range of the connecting seat is not less than 360 degrees.

Preferably, rubber rings are adhered to the middle part of the top surface of the mounting seat and the middle part of the bottom surface of the connecting seat, and the two groups of rubber rings are tightly abutted.

The utility model has the beneficial effects that:

according to the utility model, the multifunctional assembly mechanism is arranged in the middle of the bottom surface of the unmanned aerial vehicle main body, the butt joint piece can be pulled out from the inner side of the butt joint seat from front to back by pressing the poking piece downwards, so that the data collector and the unmanned aerial vehicle main body can be separated, the operation is simple and quick, tools are not needed in the process, and the use is more convenient.

According to the utility model, the auxiliary balance mechanism is arranged between the mounting seat and the butt joint part, the screw rod is rotated to the direction corresponding to the gravity center deviation of the unmanned aerial vehicle main body, and then the positions of the nuts on the screw rods at the two ends are adjusted, so that the gravity center of the unmanned aerial vehicle main body is leveled, the unmanned aerial vehicle main body can fly more stably, and the operation difficulty is reduced.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic view of the propeller of FIG. 1 with the propeller removed;

FIG. 3 is a schematic view of the structure of the data collector of the present utility model with the data collector removed;

FIG. 4 is a schematic view of the data acquisition unit of FIG. 3 with the data acquisition unit removed;

FIG. 5 is a right-hand view of the machine body according to the present utility model;

FIG. 6 is a schematic view of the bottom structure of the docking station of the present utility model;

FIG. 7 is a schematic view of the structure of the docking station of the present utility model after the docking station is disassembled;

FIG. 8 is a schematic view of the dock of FIG. 4 with the dock removed;

FIG. 9 is a schematic view of the structure of the mounting base of the present utility model;

fig. 10 is a schematic bottom structure of the connecting seat in the present utility model.

Wherein: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body-1, a propeller-2, a landing gear-3, a data collector-4, a multifunctional assembly mechanism-5, a mounting seat-51, a butt joint piece-52, a groove-53, a clamping block-54, a poking piece-55, a butt joint seat-56, a clamping groove-57, an auxiliary balance mechanism-58, a connecting seat-581, a screw rod-582, a counterweight nut-583 and a rubber ring-584.

Detailed Description

In order to further explain the technical scheme of the utility model, the following is explained in detail through specific examples.

Referring to fig. 1-2, the utility model provides a mobile agricultural environment information acquisition control device, which comprises an unmanned aerial vehicle main body 1, a propeller 2, landing gears 3, a data acquisition unit 4 and a multifunctional assembly mechanism 5, wherein the propeller 2 is arranged at the tail end of a bracket at four corners of the unmanned aerial vehicle main body 1, the landing gears 3 are arranged at the left side and the right side of the bottom surface of the unmanned aerial vehicle main body 1, the data acquisition unit 4 is arranged in the middle of the bottom surface of the unmanned aerial vehicle main body 1, the multifunctional assembly mechanism 5 is arranged in the middle of the bottom surface of the unmanned aerial vehicle main body 1, the unmanned aerial vehicle main body 1 is connected and fixed with the data acquisition unit 4 through the multifunctional assembly mechanism 5, and a data line on the data acquisition unit 4 is in butt joint with an interface on the unmanned aerial vehicle main body 1 so as to realize data transmission between the data acquisition unit 4 and the unmanned aerial vehicle main body 1.

Referring to fig. 3-7, the multifunctional assembly mechanism 5 of the present utility model includes a mounting seat 51, a docking member 52, a groove 53, a clamping block 54, a pulling sheet 55, a docking seat 56, a clamping groove 57 and an auxiliary balancing mechanism 58, wherein the mounting seat 51 is locked on the top end surface of the data collector 4 by a screw, the docking member 52 is fixedly connected to the top end of the mounting seat 51, the rectangular groove 53 is provided on the top end surface of the docking member 52, the groove 53 penetrates backwards to the back of the docking member 52, the clamping block 54 is welded on the front side wall of the groove 53, the pulling sheet 55 is integrally provided on the rear portion of the clamping block 54, the pulling sheet 55 extends out of the groove 53 and is located behind the docking member 52, so that a user presses the clamping block 54 downwards into the groove 53 through the pulling sheet 55, the middle portion of the bottom surface of the unmanned aerial vehicle main body 1 is screwed with the docking seat 56, the docking member 52 can be locked on the inner side of the docking seat 56 by a screw, when the docking member 52 is locked on the inner side of the docking seat 56, the inner side surface of the docking member 54 can be locked on the inner side of the clamping groove 57, so that the clamping block 54 can be locked on the inner side of the clamping groove 57 when the docking member 52 is locked on the inner side of the docking seat 56, thereby fixing the docking member 52 on the inner side of the docking seat 56, and the docking member 52, the user by the auxiliary balancing mechanism is provided between the mounting seat 52 and the docking member 52.

Further, the mounting seat 51 is in an X shape, and the screw is fastened to the data collector 4 through the through slot at the end of the mounting seat 51, so that the X shape can cut at least 40% of the weight of the mounting seat 51, and the structure is lighter to balance the weight increased by the counterweight nut 583, compared with a conventional rectangle.

Further, the mounting base 51, the butt joint member 52 and the butt joint base 56 are made of light materials, which are carbon fiber composite materials, and are widely applied to unmanned aerial vehicle components, so that weight can be effectively reduced, and the weight increased by the counterweight nut 583 can be balanced.

Referring to fig. 8-10, the auxiliary balancing mechanism 58 of the present utility model includes a connecting base 581, a screw rod 582 and a weight nut 583, wherein a stand column is integrally provided between the mounting base 51 and the butt joint member 52, the connecting base 581 is sleeved on the outer surface of the stand column and is rotationally connected with the stand column through a bearing, the screw rod 582 is symmetrically welded on both sides of the connecting base 581, the weight nut 583 is sleeved on the surface of the screw rod 582, and the weight nut 583 is in threaded connection with the surface of the screw rod 582.

Further, after the docking member 52 and the docking seat 56 are fastened and fixed, the center of gravity of the mounting seat 51, the docking member 52 and the connecting seat 581 and the center of gravity of the unmanned aerial vehicle main body 1 are located in the same vertical direction, so as to ensure that the multifunctional assembly mechanism 5 does not damage the balance of the unmanned aerial vehicle main body 1.

Further, the rotation angle range of the connection base 581 is not less than 360 degrees, the connection base 581 can be rotated to any angle, and the inclination in any direction can be leveled, so that the adjustability is strong.

Further, the middle part of the top surface of the mounting base 51 and the middle part of the bottom surface of the connecting base 581 are both adhered and provided with rubber rings 584, and the two groups of rubber rings 584 are tightly abutted against each other, so that the friction force generated by the rubber rings 584 can increase the torque required by the rotation of the connecting base 581, the connecting base 581 can stay at will within the rotation angle range, and the direction of the screw rod 582 can be conveniently adjusted.

The working principle is as follows:

first, before using, first need be full of the electric quantity for unmanned aerial vehicle main part 1, guarantee that unmanned aerial vehicle main part 1 has sufficient electric quantity to carry out the continuation of the journey, because data collection ware 4 is precision element, need save alone, still need assemble data collection ware 4 and unmanned aerial vehicle main part 1 before the use, in the equipment process, because mount pad 51 is fixed at data collection ware 4 top, and mount pad 51 top is provided with docking piece 52, only need detain docking piece 52 from the back forward and inject the docking seat 56 inboard of unmanned aerial vehicle main part 1 bottom, let fixture block 54 upwards lock advance draw-in groove 57 inboard, can make docking piece 52 firmly detain in docking seat 56 inboard, thereby accomplish the equipment with data collection ware 4 with the unmanned aerial vehicle main part 1 bottom, the installation operation of data collection ware 4 is swift.

Second, after the installation of the data collector 4 is completed, because the additionally installed data collector 4 may damage the balance of the unmanned aerial vehicle body 1, although the unmanned aerial vehicle body 1 can maintain the balance of the unmanned aerial vehicle body through the balance system, the difficulty of the flight control of the unmanned aerial vehicle body 1 is still increased, so that the unmanned aerial vehicle body 1 can be firstly tried and flown for balance debugging, and the debugging operation is as follows: if the center of gravity of the unmanned aerial vehicle main body 1 deviates, the screw 582 is rotated to the direction corresponding to the deviation of the center of gravity of the unmanned aerial vehicle main body 1, then nuts 583 on the screw 582 at two ends are screwed, when the nuts 583 on the screw 582 are far away from the center of gravity of the unmanned aerial vehicle main body 1, under the leverage, the center of gravity of the unmanned aerial vehicle main body 1 can deviate towards the nuts 583, the position of the nuts 583 on the screw 582 at two ends is adjusted to level the center of gravity of the unmanned aerial vehicle main body 1, the unmanned aerial vehicle main body 1 can fly more stably, the control difficulty is reduced, in addition, the rubber ring 584 is arranged on the top surface of the mounting seat 51 and the bottom surface of the connecting seat 581, the torque required by the rotation of the connecting seat 581 can be increased due to the friction force generated by the rubber ring 584, the connecting seat 581 can stay at will in the rotation angle range, and the direction of the screw 582 cannot deviate by itself.

Thirdly, because the weather environment is crucial to the growth of crops, can let unmanned aerial vehicle main part 1 carry on data collection system 4 and monitor the weather environment, during the use, unmanned aerial vehicle main part 1 utilizes the lift of rotatory production of screw 2 to take off, can carry on data collection system 4 to each regional data such as detection humiture, can monitor the weather environment, prevent the work to extremely end weather, guarantee the output of crops, after accomplishing the monitoring task, unmanned aerial vehicle main part 1 returns to the journey, landing gear 3 at first contacts ground when dropping, provides the support for unmanned aerial vehicle main part 1, avoid data collection system 4 of its bottom to receive the striking.

Fourth, since the data collector 4 is a precision element, it is usually required to store separately, and when the unmanned aerial vehicle main body 1 is idle, the data collector 4 needs to be detached, and the specific detachment process is as follows: the user presses down the plectrum 55 downwards, lets plectrum 55 bring the fixture block 54 into in the recess 53, and fixture block 54 breaks away from with draw-in groove 57 this moment to make butt joint piece 52 and butt joint seat 56 release fixedly, can extract the butt joint piece 52 from the butt joint seat 56 inboard from the front to back, just can accomplish the separation of data collection station 4 and unmanned aerial vehicle main part 1, easy operation is swift, and the in-process need not with the help of the instrument, and it is more convenient to use.

The utility model provides a mobile agricultural environment information acquisition control device, wherein a multifunctional assembly mechanism 5 is arranged in the middle of the bottom surface of an unmanned aerial vehicle main body 1, a butt joint piece 52 can be pulled out from the inner side of a butt joint seat 56 from front to back by pressing a pulling piece 55 downwards, the separation of a data acquisition device 4 and the unmanned aerial vehicle main body 1 can be completed, the operation is simple and quick, tools are not needed in the process, the use is more convenient, an auxiliary balance mechanism 58 is arranged between an installation seat 51 and the butt joint piece 52, the screw 582 is rotated to a direction corresponding to the gravity center offset of the unmanned aerial vehicle main body 1, the position of a nut 583 on the screw 582 at two ends is adjusted, the gravity center of the unmanned aerial vehicle main body 1 is leveled, the unmanned aerial vehicle main body 1 can fly more stably, and the operation difficulty is reduced.

The foregoing is merely a preferred example of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims

1. The utility model provides a portable agricultural environment information acquisition controlling means, includes unmanned aerial vehicle main part (1), screw (2), undercarriage (3) and data collection station (4), screw (2) are installed at the support end of unmanned aerial vehicle main part (1) four corners, undercarriage (3) are all installed to unmanned aerial vehicle main part (1) bottom surface left and right sides, unmanned aerial vehicle main part (1) bottom surface mid-mounting has data collection station (4), and the interface on data collection station (4) and unmanned aerial vehicle main part (1) is docked;

the method is characterized in that: still include multi-functional assembly devices (5), unmanned aerial vehicle main part (1) bottom surface middle part is provided with multi-functional assembly devices (5), multi-functional assembly devices (5) are including mount pad (51), interfacing part (52), recess (53), fixture block (54), plectrum (55), docking station (56), draw-in groove (57) and supplementary balance mechanism (58), mount pad (51) are fixed in data collection station (4) terminal surface, interfacing part (52) are fixed with in connection of mount pad (51) top, recess (53) are seted up on interfacing part (52) top surface, recess (53) link up backward to interfacing part (52) back, recess (53) lateral wall is provided with fixture block (54), fixture block (54) rear portion is provided with plectrum (55), unmanned aerial vehicle main part (1) bottom surface mid-mounting has docking station (56), and interfacing part (52) lock in docking station (56) inboard, docking station (56) inboard have seted up draw-in groove (57), fixture block (54) inboard lock advances draw-in groove (57), set up between docking station (58) and the balance mechanism (52).

2. The mobile agricultural environment information collection control device according to claim 1, wherein: the mounting seat (51) is X-shaped, and a screw penetrates through a through groove at the tail end of the mounting seat (51) to be locked with the data acquisition device (4).

3. The mobile agricultural environment information collection control device according to claim 1, wherein: the mounting seat (51), the butt joint piece (52) and the butt joint seat (56) are made of light materials.

4. The mobile agricultural environment information collection control device according to claim 1, wherein: the auxiliary balance mechanism (58) comprises a connecting seat (581), a screw rod (582) and a counterweight nut (583), a stand column is arranged between the mounting seat (51) and the butt joint piece (52), the outer surface of the stand column is rotationally sleeved with the connecting seat (581), the screw rod (582) is symmetrically arranged on two sides of the connecting seat (581), the counterweight nut (583) is sleeved on the surface of the screw rod (582), and the counterweight nut (583) is in threaded connection with the surface of the screw rod (582).

5. The mobile agricultural environment information collection control device according to claim 4, wherein: after the butt joint piece (52) and the butt joint seat (56) are buckled and fixed, the gravity centers of the installation seat (51), the butt joint piece (52) and the connecting seat (581) and the gravity center of the unmanned aerial vehicle main body (1) are in the same vertical direction.

6. The mobile agricultural environment information collection control device according to claim 4, wherein: the rotation angle range of the connecting seat (581) is not less than 360 degrees.

7. The mobile agricultural environment information collection control device according to claim 4, wherein: rubber rings (584) are adhered to the middle part of the top surface of the mounting seat (51) and the middle part of the bottom surface of the connecting seat (581), and the two groups of rubber rings (584) are tightly abutted against each other _。