CN216154036U

CN216154036U - Unmanned aerial vehicle control system for geographic information mapping

Info

Publication number: CN216154036U
Application number: CN202122246706.4U
Authority: CN
Inventors: 孙国磊; 刘崇敏
Original assignee: Yunnan Shunshi Space Technology Co ltd
Current assignee: Yunnan Shunshi Space Technology Co ltd
Priority date: 2021-09-16
Filing date: 2021-09-16
Publication date: 2022-04-01
Anticipated expiration: 2031-09-16

Abstract

The utility model relates to the technical field of geographic information mapping, in particular to an unmanned aerial vehicle control system for geographic information mapping, which comprises an unmanned aerial vehicle main body, wherein a mounting groove is formed in the front end surface of a connecting seat, a storage battery is arranged in the mounting groove, a base disc is arranged on the lower surface of the connecting seat, landing gears are arranged on the circumferential outer wall of the base disc, connecting rods are also arranged on the circumferential outer wall of the unmanned aerial vehicle main body, which is close to the top, propellers are arranged on the connecting rods, and a protective device is arranged above the unmanned aerial vehicle main body; this an unmanned aerial vehicle control system for geographic information survey and drawing, cooperation detachable battery in the unmanned aerial vehicle main part, the quick replacement of being convenient for uses, the cooperation of camera is used, the aviation of being convenient for is shot and is used, a plurality of undercarriage cooperations are used, the stable take-off or descending use of being convenient for, reduce the damage that descending vibrations brought, protector's cooperation is used, be convenient for protect the screw, avoid receiving the influence of the object in the environment in the flight, cause to fall and influence the survey and drawing and shoot and use.

Description

Unmanned aerial vehicle control system for geographic information mapping

Technical Field

The utility model relates to the technical field of geographic information mapping, in particular to an unmanned aerial vehicle control system for geographic information mapping.

Background

Geographic information data production and geographic information application service capability, can survey and draw geographic information, state and earth, the domain is built, the environment, mining industry, calamity prediction, emergency treatment, etc., data production, database construction, data mining, map drawing, information technology service, etc. related to spatial location information, geographic information survey and drawing are applied to all national great survey and drawing projects from geographic state conditions, geographic information public service to global survey and drawing, put forward the innovation of the information surveying and drawing technology, actively participate in the exploration and practice of novel basic survey and drawing, relate to the fields of survey and drawing, state and earth, traffic, water conservancy, telecommunication, ground mine, exploration, urban construction planning, metallurgy, agriculture, tourism, coal, petroleum, forestry, etc.;

the unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, and can execute a more dangerous task because the unmanned aerial vehicle does not need to be driven by personnel, so that the unmanned aerial vehicle technology is widely applied to the detection, search and monitoring range and the like; general geographic information survey and drawing's unmanned aerial vehicle control system receives aerial flying object's influence easily in the flight, and the easy screw that damages of touching striking causes whole device to fall, influences the collection of survey and drawing data and uses, can not stably protect the cooperation and use.

SUMMERY OF THE UTILITY MODEL

The present invention is directed to an unmanned aerial vehicle control system for mapping geographic information, which solves the above-mentioned problems of the prior art.

In order to achieve the purpose, the utility model provides the following technical scheme:

the utility model provides an unmanned aerial vehicle control system for geographic information survey and drawing, includes the unmanned aerial vehicle main part, unmanned aerial vehicle main part lower surface is equipped with the connecting seat, the mounting groove has been seted up to the terminal surface before the connecting seat, be equipped with the battery in the mounting groove, the connecting seat lower surface is equipped with the bed plate, be equipped with a plurality of undercarriage on the bed plate circumference outer wall, it still is equipped with a plurality of connecting rod to be close to the top position on the unmanned aerial vehicle main part circumference outer wall, all be equipped with the screw on the connecting rod, unmanned aerial vehicle main part top is equipped with protector.

Preferably, protector includes fixed column and spacing ring, be connected through a plurality of horizontal pole between fixed column and the spacing ring, be close to the intermediate position on the horizontal pole and still be equipped with solid fixed ring, the horizontal pole is the equidistant distribution of annular, horizontal pole one end and fixed column welded fastening, the other end and spacing ring welded fastening, fixed column bottom and unmanned aerial vehicle main part welded fastening.

Preferably, the unmanned aerial vehicle main part is the integrated into one piece structure with the connecting seat, the width of mounting groove and the width looks adaptation of battery.

Preferably, the base plate passes through bolt fixed connection with the unmanned aerial vehicle main part, base plate lower surface central point puts and still is equipped with the camera, the camera passes through bolt and base plate fixed connection, the undercarriage is circular-arcly, just the undercarriage is the equidistant distribution of annular, undercarriage top and base plate welded fastening, the undercarriage bottom all is equipped with the rubber ball pad, the rubber ball pad bonds fixedly with the undercarriage.

Preferably, the connecting rod is welded and fixed with the unmanned aerial vehicle main body, and the propeller is fixedly connected with the connecting rod through a bolt.

Compared with the prior art, the utility model has the beneficial effects that:

1. the detachable storage battery is matched with the main body of the unmanned aerial vehicle, so that the unmanned aerial vehicle is convenient to replace and use, the camera is matched and used, aviation shooting is convenient, the landing gears are matched and used, stable takeoff or landing is convenient, damage caused by landing vibration is reduced, the protection device is matched and used, a propeller is convenient to protect, and the influence of falling on surveying, mapping and shooting caused by the influence of objects in the environment in flight is avoided.

2. The cross rod is matched with the fixing ring, so that the connection stability of the limiting ring and the fixing column is improved, the rubber ball pad is matched with the undercarriage, the friction force contacting with the ground is increased, and the unmanned aerial vehicle main body can stably rise and fall for use.

Drawings

FIG. 1 is a schematic view of the overall structure of embodiment 1 of the present invention;

FIG. 2 is a schematic structural view of a frame of a removal prevention device according to embodiment 1 of the present invention;

fig. 3 is a schematic structural view of a main frame of an unmanned aerial vehicle according to embodiment 1 of the present invention;

FIG. 4 is a schematic structural view of a frame of a guard device according to embodiment 1 of the present invention;

FIG. 5 is a schematic view of the overall structure of embodiment 2 of the present invention;

fig. 6 is an overall exploded view of embodiment 2 of the present invention.

The various reference numbers in the figures mean:

1. an unmanned aerial vehicle main body; 10. a connecting seat; 100. mounting grooves; 101. a storage battery; 11. a convex column; 110. a slot; 111. perforating;

2. a base plate; 20. a camera; 21. a landing gear; 210. a rubber ball pad;

3. a connecting rod;

4. a propeller;

5. a guard; 50. fixing a column; 500. inserting a column; 501. a circular hole; 51. a cross bar; 510. a fixing ring; 52. a limiting ring;

6. an indicator light;

7. and (6) fixing the bolt.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be considered as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a number" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

Example 1

Referring to fig. 1-4, the present embodiment provides a technical solution:

the utility model provides a data processing equipment of wind accuse business, including unmanned aerial vehicle main part 1, 1 lower surface of unmanned aerial vehicle main part is equipped with connecting seat 10, mounting groove 100 has been seted up to the terminal surface before the connecting seat 10, be equipped with battery 101 in the mounting

groove

100, 10 lower surfaces of connecting seat are equipped with base plate 2, be equipped with a plurality of undercarriage 21 on 2 circumference outer walls of base plate, it still is equipped with a plurality of connecting rod 3 to be close to the top position on 1 circumference outer wall of unmanned aerial vehicle main part, all be equipped with screw 4 on the connecting rod 3, 1 top of unmanned aerial vehicle main part is equipped with protector 5.

In this embodiment, protector 5 includes fixed column 50 and spacing ring 52, be connected through a plurality of horizontal pole 51 between fixed column 50 and the spacing ring 52, be close to the intermediate position on the horizontal pole 51 and still be equipped with solid fixed ring 510, horizontal pole 51 is the equidistant distribution of annular, horizontal pole 51 one end and fixed column 50 welded fastening, the other end and spacing ring 52 welded fastening, fixed column 50 bottom and unmanned aerial vehicle main part 1 welded fastening, horizontal pole 51 with be equipped with solid fixed ring 510 cooperation, increase the stability that fixed column 50 and spacing ring 52 are connected.

Further, unmanned aerial vehicle main part 1 is the integrated into one piece structure with connecting seat 10, the width of mounting groove 100 and the width looks adaptation of battery 101, and battery 101 is convenient for manual grafting and is installed in mounting groove 100, and convenient the change is used, and battery 101 and inside control module electric connection continue to provide power for whole device.

It should be noted that, base plate 2 passes through bolt fixed connection with unmanned aerial vehicle main part 1, 2 lower surface central point of base plate puts and still is equipped with camera 20, camera 20 passes through bolt and 2 fixed connection of base plate, undercarriage 21 is circular-arcly, and undercarriage 21 is the equidistant distribution of annular, undercarriage 21 top and 2 welded fastening of base plate, undercarriage 21 bottom all is equipped with rubber ball pad 210, rubber ball pad 210 and undercarriage 21 bonding are fixed, camera 20's installation, be convenient for survey and drawing and shoot the use, rubber ball pad 210 is used with undercarriage 21's cooperation, be convenient for stable taking off of unmanned aerial vehicle main part 1 and descending use, increase the stability of structure.

Further, connecting rod 3 and 1 welded fastening of unmanned aerial vehicle main part, screw 4 pass through bolt and 3 fixed connection of connecting rod, all cooperate screw 4 on the multiunit connecting rod 3, are convenient for rise and descend to remove and use, increase the flexibility of whole unmanned aerial vehicle main part 1.

The unmanned aerial vehicle control system for geographic information survey and drawing of this embodiment is when using, the user is manual installs camera 20 on base plate 2, undercarriage 21 cooperation

rubber ball pad

210 and 2 fixed connection of base plate, battery 101 is installed in connecting seat 10, last use for the power supply of internal control module, screw 4 uses with 3 normal running fit of connecting rod, install protector 5 in 1 top of unmanned aerial vehicle main part again, protect screw 4, avoid when flying, receive the influence of the object collision among the external environment.

Example 2

Referring to fig. 5 to 6, the present embodiment provides the following technical solutions on the basis of embodiment 1: still be equipped with a plurality of pilot lamp 6 on the 52 circumference outer walls of spacing ring, fixed column 50 bottom is equipped with inserts post 500, inserted and seted up round hole 501 on the post 500, unmanned aerial vehicle main part 1 upper surface is equipped with projection 11, the slot 110 has been seted up with the position that inserts the post 500 and correspond to projection 11 intermediate position, set up the perforation 111 that corresponds with round hole 501 on the projection 11 outer wall, be equipped with gim peg 7 in the perforation 111, gim peg 7 passes perforation 111 and pegs graft the cooperation with round hole 501.

Further, insert post 500 and fixed column 50 welded fastening, the width of inserting post 500 and the width looks adaptation of slot 110, insert post 500 and slot 110 and peg graft and join in marriage the cooperation, projection 11 and unmanned aerial vehicle main part 1 are the integrated into one piece structure, the nut has been set to the 7 tip of gim peg, nut and 7 threaded connection of gim peg, pilot lamp 6 passes through bolt and spacing ring 52 fixed connection, and pilot lamp 6 passes through wire and the inside control module electric connection of unmanned aerial vehicle main part 1, the installation of pilot lamp 6, be convenient for demonstrate the position of unmanned aerial vehicle main part 1 in real time, be convenient for pay attention to observe the use in the dim, under the cooperation of gim peg 7 and nut, be convenient for fixed post 500 and projection 11, convenient combination change uses.

When the use of this embodiment, the manual pilot lamp 6 of fixing of user is on spacing ring 52, then with fixed column 50 through inserting post 500 and projection 11 grafting cooperation, the gim peg 7 passes perforation 111 and with the cooperation of pegging graft of round hole 501, nut and gim peg 7 threaded connection increase the stability of inserting post 500 and projection 11 and being connected, increase holistic independent stability, the flight survey and drawing of being convenient for is used.

The foregoing shows and describes the general principles, essential features, and advantages of the utility model. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. An unmanned aerial vehicle control system for geographic information mapping, comprising an unmanned aerial vehicle main body (1), characterized in that: unmanned aerial vehicle main part (1) lower surface is equipped with connecting seat (10), mounting groove (100) have been seted up to the terminal surface before connecting seat (10), be equipped with battery (101) in mounting groove (100), connecting seat (10) lower surface is equipped with base plate (2), be equipped with a plurality of undercarriage (21) on base plate (2) circumference outer wall, it still is equipped with a plurality of connecting rod (3) to be close to the top position on unmanned aerial vehicle main part (1) circumference outer wall, all be equipped with screw (4) on connecting rod (3), unmanned aerial vehicle main part (1) top is equipped with protector (5).

2. The drone control system for geographic information mapping of claim 1, wherein: protector (5) are including fixed column (50) and spacing ring (52), be connected through a plurality of horizontal pole (51) between fixed column (50) and the spacing ring (52), be close to intermediate position on horizontal pole (51) and still be equipped with solid fixed ring (510), horizontal pole (51) are the equidistant distribution of annular, horizontal pole (51) one end and fixed column (50) welded fastening, the other end and spacing ring (52) welded fastening, fixed column (50) bottom and unmanned aerial vehicle main part (1) welded fastening.

3. The drone control system for geographic information mapping of claim 1, wherein: unmanned aerial vehicle main part (1) and connecting seat (10) are the integrated into one piece structure, the width of mounting groove (100) and the width looks adaptation of battery (101).

4. The drone control system for geographic information mapping of claim 1, wherein: base plate (2) pass through bolt fixed connection with unmanned aerial vehicle main part (1), base plate (2) lower surface central point puts and still is equipped with camera (20), camera (20) are through bolt and base plate (2) fixed connection, undercarriage (21) are circular-arcly, just undercarriage (21) are the equidistant distribution of annular, undercarriage (21) top and base plate (2) welded fastening, undercarriage (21) bottom all is equipped with rubber ball pad (210), rubber ball pad (210) and undercarriage (21) bonding are fixed.

5. The drone control system for geographic information mapping of claim 1, wherein: connecting rod (3) and unmanned aerial vehicle main part (1) welded fastening, screw (4) pass through bolt and connecting rod (3) fixed connection.