CN211996167U

CN211996167U - Unmanned aerial vehicle bottom loader

Info

Publication number: CN211996167U
Application number: CN202020504315.0U
Authority: CN
Inventors: 李立
Original assignee: Hangzhou Mingqi Survey And Planning Design Co ltd
Current assignee: Hangzhou Mingqi Survey And Planning Design Co ltd
Priority date: 2020-04-08
Filing date: 2020-04-08
Publication date: 2020-11-24
Anticipated expiration: 2030-04-08

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle, especially, an unmanned aerial vehicle bottom carry ware, including the unmanned aerial vehicle body, the bottom fixed mounting of unmanned aerial vehicle body has two fixed blocks, two the bottom of fixed block is all seted up flutedly, movable mounting has the card post in the recess, the equal fixed mounting in both sides of card post has the fixture block, arc draw-in groove has all been seted up on the both sides inner wall of recess, the fixture block with correspond arc draw-in groove looks adaptation, the bottom of unmanned aerial vehicle body is equipped with the carry case, the top fixed mounting of carry case has two mount pads, the mounting groove has been seted up at the top of mount pad, the ring channel has been seted up on the inner wall of mounting groove, slidable mounting has the annular piece in the. The utility model is simple in operation, be convenient for to the quick installation of carry case, be favorable to improving the efficiency that the goods and materials transported, when not using the carry case, it is convenient to dismantle simultaneously, labour saving and time saving.

Description

Unmanned aerial vehicle bottom loader

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle bottom carry ware.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the unmanned aerial vehicle can automatically land in the same way as a common aircraft during landing, can also be recovered by a parachute or a barrier net for remote control, can be repeatedly used for many times, is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like, and can be divided into military use and civil use according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, the developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology, and the unmanned aerial vehicle needs to mount various goods and materials when being transported, rescued or used as other aspects.

However, among the prior art, unmanned aerial vehicle's carry ware is more loaded down with trivial details when the installation, influences the transport efficiency of goods and materials, when not using the carry ware, dismantles also time-consuming and energy-consuming simultaneously, for this reason, provides an unmanned aerial vehicle bottom carry ware.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle bottom loader that provides.

In order to achieve the above purpose, the utility model adopts the following technical scheme: an unmanned aerial vehicle bottom carrier comprises an unmanned aerial vehicle body, wherein two fixed blocks are fixedly mounted at the bottom of the unmanned aerial vehicle body, grooves are formed in the bottoms of the two fixed blocks, clamping columns are movably mounted in the grooves, clamping blocks are fixedly mounted on two sides of the clamping columns, arc-shaped clamping grooves are formed in inner walls of two sides of the grooves, the clamping blocks are matched with the corresponding arc-shaped clamping grooves, a carrier box is arranged at the bottom of the unmanned aerial vehicle body, two mounting seats are fixedly mounted at the top of the carrier box, mounting grooves are formed in the top of the mounting seats, annular grooves are formed in the inner walls of the mounting grooves, annular blocks are slidably mounted in the annular grooves, the bottom ends of the clamping columns extend into the corresponding mounting grooves, the clamping columns are rotatably connected with the corresponding annular blocks, and first springs are fixedly mounted on the inner walls of the bottoms of the mounting grooves, the top end of the first spring is fixedly connected with the corresponding clamping column.

Preferably, two support rods are arranged in the annular groove, the top end and the bottom end of each support rod are respectively and fixedly connected with the top inner wall and the bottom inner wall of the corresponding annular groove, and the annular blocks are slidably mounted on the corresponding two support rods.

Preferably, the support rod is sleeved with a second spring, the bottom end of the second spring is fixedly connected with the inner wall of the bottom of the annular groove, and the top end of the second spring is fixedly connected with the bottom of the annular block.

Preferably, the top of the annular block is provided with a rotating hole, and the bottom end of the clamping column penetrates through the corresponding rotating hole and is rotatably connected with the inner wall of the corresponding rotating hole.

Preferably, the outer wall of the clamping column is sleeved with a bearing, and the outer ring of the bearing is fixedly connected with the inner wall of the rotating hole correspondingly.

Preferably, two sliding holes are formed in the top of the annular block, and the supporting rod is connected with the inner wall of the corresponding sliding hole in a sliding mode.

Compared with the prior art, the beneficial effects of the utility model are that: firstly, the unmanned aerial vehicle body, the fixing block, the groove, the clamping column, the clamping block, the arc-shaped clamping groove, the mounting box, the mounting seat, the mounting groove, the annular block, the first spring, the supporting rod and the second spring are matched, when materials need to be conveyed, the clamping column is in contact with the inner wall of the top of the groove, the clamping column continues to move upwards, the clamping column drives the annular block to slide, the first spring and the second spring are compressed, when the clamping block corresponds to the annular clamping groove, the clamping column is manually rotated, the clamping column drives the clamping block to rotate into the annular clamping groove, the mounting box is mounted, the mounting box can be used for placing the materials needing to be conveyed, the mounting device is convenient to mount, and the efficiency of material conveying is improved; when the mounting box needs to be detached, the steps are operated reversely and positively, so that the mounting box can be detached, and time and labor are saved.

The utility model is simple in operation, be convenient for to the quick installation of carry case, be favorable to improving the efficiency that the goods and materials transported, when not using the carry case, it is convenient to dismantle simultaneously, labour saving and time saving.

Drawings

Fig. 1 is a schematic structural view of the present invention;

FIG. 2 is an enlarged schematic view of portion A of FIG. 1;

fig. 3 is a schematic view of the top cross-sectional structure of the middle fixing block of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a fixed block; 3. a groove; 4. clamping the column; 5. a clamping block; 6. an arc-shaped clamping groove; 7. mounting a box; 8. a mounting seat; 9. mounting grooves; 10. an annular groove; 11. a ring block; 12. a first spring; 13. a support bar; 14. a second spring.

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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution: an unmanned aerial vehicle bottom carrier comprises an unmanned aerial vehicle body 1, wherein two fixed blocks 2 are fixedly installed at the bottom of the unmanned aerial vehicle body 1, grooves 3 are formed in the bottoms of the two fixed blocks 2, clamping columns 4 are movably installed in the grooves 3, clamping blocks 5 are fixedly installed on two sides of the clamping columns 4, arc-shaped clamping grooves 6 are formed in inner walls of two sides of the grooves 3, the clamping blocks 5 are matched with the corresponding arc-shaped clamping grooves 6, a carrier box 7 is arranged at the bottom of the unmanned aerial vehicle body 1, two mounting bases 8 are fixedly installed at the top of the carrier box 7, mounting grooves 9 are formed in the tops of the mounting bases 8, annular grooves 10 are formed in the inner walls of the mounting grooves 9, annular blocks 11 are slidably installed in the annular grooves 10, the bottom ends of the clamping columns 4 extend into the corresponding mounting grooves 9, the clamping columns 4 are rotatably connected with the corresponding annular blocks 11, and first springs 12 are, the top end of the first spring 12 is fixedly connected with the corresponding clamping column 4;

be equipped with two bracing pieces 13 in the ring channel 10, the top and the bottom of bracing piece 13 respectively with the top inner wall and the bottom inner wall fixed connection of corresponding ring channel 10, ring block 11 slidable mounting is on two bracing pieces 13 that correspond, the cover is equipped with second spring 14 on the bracing piece 13, the bottom of second spring 14 and the bottom inner wall fixed connection of ring channel 10, the top of second spring 14 and the bottom fixed connection of ring block 11, the rotation hole has been seted up at the top of ring block 11, the bottom of card post 4 runs through corresponding rotation hole and is connected with the inner wall rotation of corresponding rotation hole, the cover is equipped with the bearing on the outer wall of card post 4, the outer lane of bearing and the inner wall fixed connection of corresponding rotation hole, two slip holes have been seted up at the top of ring block 11, bracing piece 13 and the inner wall sliding connection of corresponding slip hole, unmanned aerial vehicle body 1 through the device, fixed block 2, The device comprises a groove 3, a clamping column 4, a clamping block 5, an arc-shaped clamping groove 6, a mounting box 7, a mounting seat 8 and a mounting groove; 9. the annular groove 10, the annular block 11, the first spring 12, the supporting rod 13 and the second spring 14 are matched, when materials need to be conveyed, the clamping column 4 is in contact with the inner wall of the top of the groove 3, the clamping column 4 continues to move upwards, the clamping column 4 drives the annular block 11 to slide, the first spring 12 and the second spring 14 are compressed, when the clamping block 5 corresponds to the annular clamping groove 6, the clamping column 4 is rotated manually, the clamping column 4 drives the clamping block 5 to rotate into the annular clamping groove 6, the mounting box 7 is mounted, the materials needing to be conveyed can be placed in the mounting box 7, the mounting device 7 is convenient to mount, and the efficiency of conveying the materials is improved; when the carry case 7 needs to be dismantled, operate above-mentioned step just reversely, alright in order to dismantle carry case 7, labour saving and time saving, the utility model is simple in operation, be convenient for to the quick installation of carry case 7, be favorable to improving the efficiency that the goods and materials transported, when not using carry case 7, it is convenient, labour saving and time saving to dismantle simultaneously.

The working principle is as follows: when materials need to be conveyed, firstly, the two clamping columns 4 are aligned to the two grooves 3, the hanging box 7 is pushed upwards to push the two clamping columns 4 to move upwards, when the clamping columns 4 are contacted with the inner walls of the tops of the grooves 3, the clamping columns 4 continue to move upwards, the clamping columns 4 drive the annular block 11 to slide downwards on the two support rods 13, the first spring 12 and the second spring 14 are compressed until the clamping block 5 corresponds to the annular clamping groove 6, the current situation is kept, the clamping columns 4 are manually rotated, the clamping columns 4 drive the two clamping blocks 5 to rotate into the two annular clamping grooves 6, the hanging box 7 is slowly loosened, the clamping block 5 can be firmly fixed in the annular clamping groove 6 under the elastic action of the first spring 12 and the second spring 14, the hanging box 7 is installed at the moment, the materials needing to be conveyed can be placed through the hanging box 7, and the hanging device 7 is convenient to install, the efficiency of material conveying is improved;

when the mounting box 7 needs to be disassembled, the steps are operated reversely and positively, so that the two clamping blocks 5 are moved out of the two clamping grooves 6, the mounting box 7 is pulled downwards, the two clamping columns 4 are moved out of the two fixing blocks 2, the mounting box 7 is disassembled, and time and labor are saved.

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 an unmanned aerial vehicle bottom loader, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein two fixing blocks (2) are fixedly mounted at the bottom of the unmanned aerial vehicle body (1), grooves (3) are formed in the bottoms of the two fixing blocks (2), clamping columns (4) are movably mounted in the grooves (3), clamping blocks (5) are fixedly mounted on the two sides of the clamping columns (4), arc-shaped clamping grooves (6) are formed in the inner walls of the two sides of the grooves (3), the clamping blocks (5) are matched with the corresponding arc-shaped clamping grooves (6), a hanging box (7) is arranged at the bottom of the unmanned aerial vehicle body (1), two mounting seats (8) are fixedly mounted at the top of the hanging box (7), a mounting groove (9) is formed in the top of each mounting seat (8), a ring groove (10) is formed in the inner wall of each mounting groove (9), a ring-shaped block (11) is slidably mounted in each ring-shaped groove (10), and the bottom ends of the, and the clamping column (4) is connected with the corresponding annular block (11) in a rotating mode, a first spring (12) is fixedly mounted on the inner wall of the bottom of the mounting groove (9), and the top end of the first spring (12) is fixedly connected with the clamping column (4) correspondingly.

2. The unmanned aerial vehicle bottom mount device of claim 1, wherein: be equipped with two bracing pieces (13) in ring channel (10), the top and the bottom of bracing piece (13) respectively with correspond the top inner wall and the bottom inner wall fixed connection of ring channel (10), annular piece (11) slidable mounting is in two that correspond on bracing piece (13).

3. The unmanned aerial vehicle bottom mount device of claim 2, wherein: the support rod (13) is sleeved with a second spring (14), the bottom end of the second spring (14) is fixedly connected with the inner wall of the bottom of the annular groove (10), and the top end of the second spring (14) is fixedly connected with the bottom of the annular block (11).

4. The unmanned aerial vehicle bottom mount device of claim 1, wherein: the top of the annular block (11) is provided with a rotating hole, and the bottom end of the clamping column (4) penetrates through the corresponding rotating hole and is rotatably connected with the inner wall of the corresponding rotating hole.

5. The unmanned aerial vehicle bottom mount device of claim 4, wherein: the outer wall of the clamping column (4) is sleeved with a bearing, and the outer ring of the bearing is fixedly connected with the inner wall of the rotating hole correspondingly.

6. The unmanned aerial vehicle bottom mount device of claim 2, wherein: two sliding holes are formed in the top of the annular block (11), and the supporting rod (13) is connected with the inner wall of the corresponding sliding hole in a sliding mode.