CN217836038U

CN217836038U - Unmanned aerial vehicle guided missile carries device with adjustable

Info

Publication number: CN217836038U
Application number: CN202222062631.9U
Authority: CN
Inventors: 陈罗丹
Original assignee: Zhejiang Xingkong General Aviation Technology Co ltd
Current assignee: Xingyao Aviation Technology Co.,Ltd.
Priority date: 2022-08-03
Filing date: 2022-08-03
Publication date: 2022-11-18
Anticipated expiration: 2032-08-03

Abstract

The utility model relates to an unmanned air vehicle technique field just discloses an unmanned aerial vehicle guided missile carry device with adjustable, which comprises a bod, the bottom of organism is fixed mounting first installing frame and second installing frame respectively, the inside fixed mounting of first installing frame has first motor, the output shaft fixed mounting of first motor has the driving gear, movable mounting has first screw thread post before the opposite side inner wall of second installing frame, the utility model discloses a work of second motor drives second screw thread post and carries out the pivoted, and second screw thread post can drive the second movable block and remove together when rotating, and one side fixed mounting of movable block has first connecting plate, and first connecting plate is when removing together along with the movable block, and first connecting plate can drive the second connecting plate through the catch bar and remove together, and second connecting plate fixed mounting is in the outside of guard plate, and the guard plate will remove to carry the both ends of frame like this, protects the guided missile body.

Description

Unmanned aerial vehicle guided missile carries device with adjustable

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle guided missile carry device with adjustable.

Background

An unmanned aerial vehicle is an unmanned aerial vehicle which is operated by using a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and is widely applied to agriculture, military industry, traffic, news media, industry, civilian use and the like at present due to excellent performance of the unmanned aerial vehicle.

Unmanned helicopter is unmanned aerial vehicle's a, and the most operations of the guided missile carry device of current unmanned helicopter are complicated, and carry or release are inconvenient enough, influence work efficiency, and do not set up protection device at the both ends of carry frame when carry, make external factors touch carry frame easily, damage the guided missile.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle guided missile carry device with adjustable to solve the problem that proposes in the above-mentioned background art.

Technical scheme

The utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle guided missile carry device with adjustable, includes the organism, the bottom of organism respectively fixed mounting have first installing frame and second installing frame, the inside fixed mounting of first installing frame has first motor, the output shaft fixed mounting of first motor has the driving gear, movable mounting has first screw thread post before the opposite side inner wall of second installing frame, the outside threaded connection of first screw thread post has first movable block, the bottom fixed mounting of first movable block has the spliced pole, the bottom fixed mounting of spliced pole has the carry frame, the inside of carry frame has seted up places the chamber, place the inside in chamber and placed the guided missile body, the top of carry frame respectively fixed mounting have second motor and fixed plate, two adjacent movable mounting have second screw thread post before the fixed plate, the outside threaded connection of second screw thread post has the second movable block, one side fixed mounting of second movable block has first connecting plate, one side fixed mounting that the second screw thread post was kept away from to the fixed plate has the guard plate.

Preferably, one side of the first threaded column, which is close to the first mounting frame, penetrates through the second mounting frame and is fixedly provided with a driven gear, and the driving gear is in meshed connection with the driven gear.

Preferably, a first sliding column is fixedly mounted between the inner walls of the opposite sides of the second mounting frame, and a first sliding block is movably mounted on the outer side of the first sliding column.

Preferably, adjacent sides of two adjacent first sliding blocks are fixedly connected with the first moving block, and two adjacent first sliding columns are located on two sides of the first threaded column.

Preferably, one side fixed mounting of guard plate has the second connecting plate, fixed mounting has the catch bar between first connecting plate and the second connecting plate.

Preferably, the protection plate is located the tip of carrying the frame, and with the tip swing joint of carrying the frame.

Advantageous effects

Compared with the prior art, the utility model provides an unmanned aerial vehicle guided missile carry device with adjustable possesses following beneficial effect:

1. this unmanned aerial vehicle guided missile carry device with adjustable, work through first motor drives the driving gear and rotates, can drive first screw thread post through driven gear when the driving gear rotates and rotate, can drive two adjacent first movable blocks when first screw thread post rotates and remove to the equidirectional, can drive two adjacent carry frames when first movable block removes like this and remove to the equidirectional, place the guided missile body in the chamber of placing in carry frame, when the guided missile body was placed, the reversal of first motor, even get two adjacent carry frames and be close to each other, fix the inside at carry frame with the guided missile body, it is convenient to reach the carry of guided missile body.

2. This unmanned aerial vehicle guided missile carry device with adjustable, work through the second motor drives the second screw thread post and carries out the pivoted, the second screw thread post can drive the second movable block when rotating and remove together, and one side fixed mounting of movable block has first connecting plate, first connecting plate is when removing along with the movable block together, first connecting plate can drive the second connecting plate through the catch bar and remove together, second connecting plate fixed mounting is in the outside of guard plate, the guard plate will remove to the both ends of carry frame like this, protect the guided missile body.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the principles of the invention.

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

fig. 2 is a top view of the first and second mounting frames of the present invention;

fig. 3 is a sectional view of a second mounting frame of the present invention;

fig. 4 is a partial enlarged view of the top end of the hanging frame.

In the figure: 1. a body; 2. a first mounting frame; 3. a second mounting frame; 4. mounting a frame; 5. a protection plate; 6. a first motor; 7. a first threaded post; 8. a first moving block; 9. a first sliding column; 10. a missile body; 11. a first slider; 12. a second motor; 13. a fixing plate; 14. a second threaded post; 15. a second moving block; 16. a first connecting plate; 17. a push rod; 18. a second connecting plate; 19. a driving gear; 20. a driven gear.

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.

The first embodiment is as follows:

please refer to fig. 1-3, an adjustable unmanned aerial vehicle missile mounting device, including organism 1, the bottom of organism 1 is fixed with first installing frame 2 and second installing frame 3 respectively, the inside fixed mounting of first installing frame 2 has first motor 6, the output shaft end fixed mounting of first motor 6 has driving gear 19, movable mounting has first screw post 7 before the opposite side inner wall of second installing frame 3, first screw post 7 is opposite from middle two halves outside screw direction, the outside threaded connection of first screw post 7 has first movable block 8, two adjacent first movable blocks 8 are located the two halves of first screw post 7 respectively, the bottom fixed mounting of first movable block 8 has the spliced pole, the bottom fixed mounting of spliced pole has mounting frame 4, the inside of mounting frame 4 has been seted up places the chamber, the inside of placing the chamber has placed missile body 10.

In this embodiment, one side of the first threaded column 7 close to the first mounting frame 2 penetrates through the second mounting frame 3 and is fixedly mounted with the driven gear 20, and the driving gear 19 is engaged with the driven gear 20.

In this embodiment, a first sliding column 9 is fixedly installed between the inner walls of the opposite sides of the second installation frame 3, and a first sliding block 11 is movably installed on the outer side of the first sliding column 9.

In this embodiment, the adjacent sides of the two adjacent first sliding blocks 11 are fixedly connected to the first moving block 8, and the two adjacent first sliding columns 9 are located on two sides of the first threaded column 7.

The working principle of the embodiment is as follows: during the use, the driving gear 19 is driven to rotate through the work of the first motor 6, the driving gear 19 can drive the first threaded columns 7 to rotate through the driven gears 20 when rotating, the first threaded columns 7 can drive the two adjacent first movable blocks 8 to move in different directions when rotating, the two adjacent mounting frames 4 can be driven to move in different directions when the first movable blocks 8 move like this, the missile bodies 10 are placed in the placing cavities of the mounting frames 4, when the missile bodies 10 are placed, the first motor 6 rotates reversely, namely, the two adjacent mounting frames 4 are close to each other, and the missile bodies 10 are fixed inside the mounting frames 4.

The second embodiment: please refer to fig. 1, fig. 4, an adjustable unmanned aerial vehicle guided missile carry device, the bottom fixed mounting of first movable block 8 has the spliced pole, the bottom fixed mounting of spliced pole has carry frame 4, the inside of carry frame 4 has been seted up and has been placed the chamber, place the inside in chamber and placed guided missile body 10, the top of carry frame 4 is fixed mounting respectively has second motor 12 and fixed plate 13, movable mounting has second screw post 14 before two adjacent fixed plates 13, fixed connection between output shaft end and the second screw post 14 of second motor 12, the outside threaded connection of second screw post 14 has second movable block 15, one side fixed mounting of second movable block 15 has first connecting plate 16, one side fixed mounting that second screw post 14 was kept away from to fixed plate 13 has guard plate 5.

In this embodiment, a second connecting plate 18 is fixedly installed on one side of the protection plate 5, and a push rod 17 is fixedly installed between the first connecting plate 16 and the second connecting plate 18.

In this embodiment, the protection plate 5 is located at the end of the mounting frame 4 and movably connected to the end of the mounting frame 4.

The working principle of the embodiment is as follows: when the missile body 10 is completely loaded, the second threaded columns 14 are driven to rotate through the work of the second motor 12, the second threaded columns 14 can drive the second moving block 15 to move together when rotating, a first connecting plate 16 is fixedly installed on one side of the moving block 15, when the first connecting plate 16 moves along with the moving block 15, the first connecting plate 16 can drive the second connecting plate 18 to move together through the push rods 17, the second connecting plate 18 is fixedly installed on the outer side of the protection plate 5, and therefore the protection plate 5 can move to the two ends of the hanging frame 4 to protect the missile body 10.

Claims

1. The utility model provides an unmanned aerial vehicle guided missile carries device with adjustable, includes organism (1), its characterized in that: the missile protection device is characterized in that a first installation frame (2) and a second installation frame (3) are fixedly installed at the bottom end of the engine body (1) respectively, a first motor (6) is fixedly installed inside the first installation frame (2), a driving gear (19) is fixedly installed at an output shaft end of the first motor (6), a first threaded column (7) is movably installed in front of the inner wall of the opposite side of the second installation frame (3), a first moving block (8) is connected with the outer side of the first threaded column (7) in a threaded manner, a connecting column is fixedly installed at the bottom end of the first moving block (8), a hanging frame (4) is fixedly installed at the bottom end of the connecting column, a placing cavity is formed inside the hanging frame (4), missile bodies (10) are placed inside the placing cavity, a second motor (12) and a fixing plate (13) are fixedly installed at the top end of the hanging frame (4) respectively, second threaded columns (14) are movably installed in front of the fixing plates (13) for two adjacent fixing plates, second threaded columns (14) are connected with the outer side threads of the second threaded columns (14), a first connecting plate (16) is fixedly installed at one side of the second moving block (15), and a protection plate (5) is far away from one side of the fixing plate (13).

2. The adjustable unmanned aerial vehicle missile mounting device of claim 1, wherein: one side of the first threaded column (7) close to the first mounting frame (2) penetrates through the second mounting frame (3) and is fixedly provided with a driven gear (20), and the driving gear (19) is in meshed connection with the driven gear (20).

3. The adjustable unmanned aerial vehicle missile mounting device of claim 1, wherein: fixed mounting has first slip post (9) between the opposite side inner wall of second installing frame (3), the outside movable mounting of first slip post (9) has first sliding block (11).

4. An adjustable unmanned aerial vehicle missile mounting system of claim 3, wherein: the adjacent sides of the adjacent two first sliding blocks (11) are fixedly connected with the first moving block (8), and the adjacent two first sliding columns (9) are positioned on two sides of the first threaded column (7).

5. The adjustable unmanned aerial vehicle missile mounting device of claim 1, wherein: one side fixed mounting of guard plate (5) has second connecting plate (18), fixed mounting has catch bar (17) between first connecting plate (16) and second connecting plate (18).

6. The adjustable unmanned aerial vehicle missile mounting device of claim 1, wherein: the protection plate (5) is located at the end part of the mounting frame (4) and is movably connected with the end part of the mounting frame (4).