CN212685908U

CN212685908U - Survey and drawing unmanned aerial vehicle flight platform

Info

Publication number: CN212685908U
Application number: CN202021753493.3U
Authority: CN
Inventors: 刘贺; 徐朔; 周爱家; 杨圣闯; 刘养波
Original assignee: Shandong Xindibo Engineering Management Co ltd
Current assignee: Shandong Xindibo Engineering Management Co ltd
Priority date: 2020-08-20
Filing date: 2020-08-20
Publication date: 2021-03-12
Anticipated expiration: 2030-08-20

Abstract

The utility model discloses a survey and drawing unmanned aerial vehicle flight platform, the power distribution box comprises a box body, the fixed apron of pegging graft in box top, and apron top outer wall is fixed with the limiting plate, and the relative both sides outer wall of limiting plate is opened there is the handle groove, four corners of apron bottom outer wall all are fixed with positioning mechanism, and positioning mechanism fixes pegging graft in the constant head tank of seting up on box top inner wall, threaded groove has all been opened to four corners of bottom outer wall of the box, and threaded groove internal thread is pegged graft and is had levelling mechanism. The utility model discloses can accomodate the effect to unmanned aerial vehicle, will lap the upset again for limiting plate and box upper end opening gomphosis make it form with flight supporting platform.

Description

Survey and drawing unmanned aerial vehicle flight platform

Technical Field

The utility model relates to an unmanned aerial vehicle flight platform technical field especially relates to a survey and drawing unmanned aerial vehicle flight platform.

Background

Under the current trend, the application of unmanned aerial vehicle is the focus of present novel intelligent technology, and the wide application of unmanned aerial vehicle arouses the transformation in a plurality of trades. To survey and drawing technical field, survey and drawing unmanned aerial vehicle can provide the auxiliary work a lot, for example, help collecting the data information of topography, landform, acquire high-quality influence data, also can realize the cruise planning of unmanned aerial vehicle survey and drawing, its characteristics are swift, quick and accurate, consequently are applied to the unmanned aerial vehicle in survey and drawing technical field and receive favour more.

In the existing mode, the working performance of a surveying and mapping unmanned aerial vehicle is mainly embodied in two aspects, one of which is designed for a flight system and mainly comprises an unmanned aerial vehicle control system, functions and the like; its two are the flight platform design, according to the difference of actual market demand, the specific structure difference of flight platform design is great, and there are some not enough in the use in current unmanned aerial vehicle flight platform, for example, inconvenient accomodating and putting work to unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the survey and drawing unmanned aerial vehicle flight platform who proposes.

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

the utility model provides a survey and drawing unmanned aerial vehicle flight platform, includes the box, the fixed apron of pegging graft in box top, and apron top outer wall is fixed with the limiting plate, and open the relative both sides outer wall of limiting plate has the handle groove, four corners of apron bottom outer wall all are fixed with positioning mechanism, and positioning mechanism fixes pegging graft in the constant head tank of seting up on box top inner wall, threaded groove has all been opened to four corners of bottom outer wall of the box, and the threaded groove internal thread is pegged graft and is had leveling mechanism.

Furthermore, the positioning mechanism comprises a positioning column, and a plurality of damping rings distributed annularly are fixed on the positioning column.

Furthermore, magnetic blocks are fixed at the bottom end of the positioning column and in the positioning groove.

Furthermore, the leveling mechanism comprises a stud, a supporting block is fixed at the bottom end of the stud, and an anti-skid bulge is fixed at the bottom of the supporting block.

Furthermore, the outer walls of two opposite sides of the box body are fixedly provided with connecting lugs, and handles are rotatably arranged on the connecting lugs.

Furthermore, a protective pad is fixed on the inner wall of the box body.

Further, the bottom of the box body is provided with a mounting opening, a drying mechanism is fixedly inserted in the mounting opening and comprises a drying box, a bottom plate is fixed at the bottom of the drying box, and a plurality of activated carbon plates are fixed at the top of the bottom plate.

The utility model has the advantages that:

1. can accomodate the effect to unmanned aerial vehicle through the box, the apron can carry out sealed work to the box, and the reference column can be pegged graft in the box, and damping ring and magnetic path can increase the joint strength between apron and the box, and the protection is filled up and can be formed the side protection effect to unmanned aerial vehicle.

2. The arrangement of the handle groove can facilitate workers to take the cover plate out, and the cover plate is turned, so that the limiting plate is embedded with the upper end opening of the box body to form a flying supporting platform, and the leveling mechanism can level the box body.

Drawings

Fig. 1 is a schematic sectional structure view of an embodiment 1 of a surveying and mapping unmanned aerial vehicle flight platform provided by the present invention;

fig. 2 is a schematic view of an embodiment 1 cover plate structure of a surveying and mapping unmanned aerial vehicle flight platform provided by the present invention;

fig. 3 is the utility model provides a survey and drawing unmanned aerial vehicle flight platform's embodiment 2 sectional structure schematic diagrams.

In the figure: the device comprises a box body 1, a thread groove 2, a stud 3, a supporting block 4, a connecting lug 5, a handle 6, a cover plate 7, a limiting plate 8, a handle groove 9, a positioning column 10, a damping ring 11, a magnetic block 12, a protective pad 13, a drying box 14, a bottom plate 15 and an activated carbon plate 16.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.

Example 1

Referring to fig. 1 and 2, a survey and drawing unmanned aerial vehicle flight platform, including box 1, 1 top of box is fixed to be pegged graft and is had apron 7, and apron 7 top outer wall is fixed with limiting plate 8, the relative both sides outer wall of limiting plate 8 is opened there is handle groove 9, apron 7 bottom outer wall four corners all are fixed with positioning mechanism, positioning mechanism is fixed to be pegged graft in the constant head tank of seting up on 1 top inner wall of box, thread groove 2 has all been opened to four corners of 1 bottom outer wall of box, thread groove 2 internal thread is pegged graft and is had leveling mechanism.

Positioning mechanism includes reference column 10, is fixed with a plurality of damping rings 11 that the annular distributes on the reference column 10, all is fixed with magnetic path 12 in reference column 10 bottom and the constant head tank, and levelling mechanism includes double-

screw bolt

3, and 3 bottom fixings of double-screw bolt have supporting

shoe

4, and 4 bottoms of supporting shoe are fixed with anti-skidding arch, are fixed with engaging lug 5 on the relative both sides outer wall of box 1, rotate on the engaging lug 5 and install handle 6, are fixed with protection pad 13 on the 1 inner wall of box.

The working principle of the embodiment is as follows: box 1 can accomodate the effect to unmanned aerial vehicle, apron 7 can carry out the work of sealing to box 1, reference column 10 can be pegged graft in box 1, damping ring 11 and magnetic path 12 can increase the joint strength between apron 7 and the box 1, protection pad 13 can form the side protection effect to unmanned aerial vehicle, setting up of handle groove 9 can make things convenient for the staff to take out apron 7, again will lap 7 upset 180 degrees, make limiting plate 8 and 1 upper end opening gomphosis of box, make it form with flight supporting platform, leveling mechanism can carry out leveling work to box 1.

Example 2

Referring to fig. 3, a survey and drawing unmanned aerial vehicle flight platform, this embodiment and embodiment 1 difference lie in that the box 1 bottom is opened there is the installing port, and the internal fixation of installing port is pegged graft and is had drying mechanism, and drying mechanism includes drying cabinet 14, and drying cabinet 14 bottom is fixed with bottom plate 15, and bottom plate 15 top is fixed with a plurality of activated carbon boards 16.

The working principle of the embodiment is as follows: moisture in the box body 1 penetrates into the drying box 14 from the top of the drying box 14, and the activated carbon plate 16 can adsorb the moisture, so that the drying strength in the box body 1 is improved.

In the description of this patent, it is to be understood that the terms "coaxial," "bottom," "one end," "top," "middle," "other end," "upper," "one side," "top," "inner," "front," "center," "two ends," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the patent and for simplicity in description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.

In this patent, unless expressly stated or limited otherwise, the terms "mounted," "disposed," "connected," "secured," "screwed" and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate, or they may be connected internally or in an interactive relationship with each other, and unless otherwise specifically limited, the specific meaning of the above terms in this patent will be understood by those skilled in the art according to the specific circumstances.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The utility model provides a survey and drawing unmanned aerial vehicle flight platform, includes box (1), its characterized in that, box (1) top is fixed to be pegged graft and is had apron (7), and apron (7) top outer wall is fixed with limiting plate (8), and the relative both sides outer wall of limiting plate (8) is opened there is handle groove (9), apron (7) bottom outer wall four corners all are fixed with positioning mechanism, and positioning mechanism is fixed to peg graft in the constant head tank of seting up on box (1) top inner wall, threaded groove (2) have all been opened to box (1) bottom outer wall four corners, and threaded groove (2) internal thread is pegged graft and is had leveling mechanism.

2. A mapping unmanned aerial vehicle flight platform according to claim 1, wherein the positioning mechanism comprises a positioning column (10), and a plurality of damping rings (11) distributed in a ring shape are fixed on the positioning column (10).

3. The mapping unmanned aerial vehicle flight platform of claim 2, characterized in that magnetic blocks (12) are fixed at the bottom end of the positioning column (10) and in the positioning groove.

4. The surveying and mapping unmanned aerial vehicle flight platform of claim 1, characterized in that the leveling mechanism comprises a stud (3), a support block (4) is fixed at the bottom end of the stud (3), and an anti-skid protrusion is fixed at the bottom of the support block (4).

5. The unmanned aerial vehicle flying surveying and mapping platform according to claim 1, wherein connecting lugs (5) are fixed on outer walls of two opposite sides of the box body (1), and handles (6) are rotatably mounted on the connecting lugs (5).

6. A survey and drawing unmanned aerial vehicle flight platform according to any one of claims 1-5, characterized in that, be fixed with protection pad (13) on the box (1) inner wall.

7. The unmanned aerial vehicle flying platform of surveying and mapping of claim 1, characterized in that, box (1) bottom is opened there is the installing port, and the fixed drying mechanism that pegs graft in the installing port includes drying cabinet (14), and drying cabinet (14) bottom is fixed with bottom plate (15), and bottom plate (15) top is fixed with a plurality of active carbon boards (16).