Unmanned aerial vehicle launch canister convenient to adjust

Abstract

The utility model is applicable to the technical field of unmanned aerial vehicles, and provides an unmanned aerial vehicle launch canister convenient to adjust, which comprises a base, a mounting plate is fixed at the top end of the base, a first connecting block is arranged at the top end of a second connecting block, a connecting canister is fixed at the top end of the first connecting block, and a threaded groove is formed in the second connecting block. And a bolt is arranged in the threaded groove. Through arrangement of a connecting structure, symmetrical distribution of a first connecting block and a second connecting block and corresponding placement of the first connecting block and the second connecting block, a connecting cylinder can be limited at the top end of a cylinder body, the cylinder body is subjected to extension treatment, and the first connecting block is internally provided with the same threaded groove, so that a bolt can penetrate through the first connecting block and the second connecting block; and limiting of the connecting cylinder is reinforced, the cylinder body is lengthened, so that the length of the unmanned aerial vehicle launching cylinder can be adjusted, and different requirements are met.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) technology, and in particular relates to an easily adjustable UAV launch tube. Background Technology

[0002] A drone is an unmanned aircraft that is operated by radio remote control equipment and its own program control device. It can fly autonomously or be remotely controlled, and has the characteristics of high maneuverability, flexibility and efficient operation. According to its purpose, drones can be divided into military drones and civilian drones. Different types of drones are used in different industries. Drones also involve auxiliary tools when in use, so a drone launcher is involved.

[0003] When launching drones, the length of the launch tube may be insufficient for longer drones, which can affect the launch. Therefore, the designed connection structure adjusts the length of the drone launch tube, extending the tube to meet different launch requirements. Utility Model Content

[0004] This invention provides an easily adjustable drone launch tube, aiming to solve the problem that the length of a drone launch tube cannot be adjusted.

[0005] This utility model is implemented as follows: an easily adjustable drone launch tube includes a base, a mounting plate fixed to the top of the base, a connecting shaft fixed to the top of the mounting plate, a cylinder movably connected to the other end of the connecting shaft, a connecting structure provided at the top of the cylinder, a support frame movably connected to the other side of the cylinder, and a reinforcing structure provided on both sides of the base.

[0006] The connection structure includes a second connecting block, which is fixed to the top of the cylinder. A first connecting block is provided at the top of the second connecting block, and a connecting cylinder is fixed at the top of the first connecting block. A threaded groove is provided inside the second connecting block, and a bolt is provided inside the threaded groove.

[0007] Preferably, the second connecting block is provided in two sets, and the two sets of the second connecting block are symmetrically distributed about the central axis of the cylinder.

[0008] Preferably, the first connecting block is provided in two sets, and the two sets of the first connecting block are symmetrically distributed about the central axis of the connecting cylinder.

[0009] Preferably, the reinforcing structure includes a slider, which is disposed on both sides of the top and bottom of the base. A limiting plate is fixed on the outer side wall of the slider, and an insertion post is fixed on the top of the limiting plate.

[0010] Preferably, the limiting plate is provided in two sets, and the two sets of limiting plates are symmetrically distributed about the central axis of the base.

[0011] Preferably, there are two sets of insertion posts, and the two sets of insertion posts are symmetrically distributed about the central axis of the limiting plate.

[0012] Compared with the prior art, the embodiments of this application have the following main advantages:

[0013] By setting up a connection structure, through the symmetrical distribution of the first and second connecting blocks, and the corresponding placement of the first and second connecting blocks, the connecting cylinder can be limited to the top of the cylinder body, and the cylinder body is extended. The first connecting block has the same threaded groove inside, so that the bolt can pass through the first and second connecting blocks, thereby reinforcing the limitation of the connecting cylinder. Extending the cylinder body allows the length of the UAV launch tube to be adjusted to meet different needs.

[0014] By setting up a reinforcement structure, two sets of sliders are symmetrically fixed at the top and bottom of the limiting plate. The top and bottom of the base have grooves on both sides, which are adapted to the sliders. The inner diameter of the limiting plate is larger than the outer diameter of the base, so that the two sets of sliders can slide within the grooves of the base and the two sets of limiting plates are limited on both sides of the base. When the drone launch tube is in use, the insertion post can be inserted into the ground to reinforce and limit the drone launch tube and prevent displacement. Attached Figure Description

[0015] Figure 1 This is a front view cross-sectional structural diagram of the present invention;

[0016] Figure 2 This is a front view structural diagram of the present invention;

[0017] Figure 3 This is the utility model Figure 1 Enlarged structural diagram at point A in the middle;

[0018] Figure 4 This is a three-dimensional structural diagram of the reinforcement structure of this utility model.

[0019] In the diagram: 1. Base; 2. Mounting plate; 3. Connecting shaft; 4. Cylinder; 5. Connecting structure; 501. Connecting cylinder; 502. First connecting block; 503. Second connecting block; 504. Bolt; 505. Threaded groove; 6. Support frame; 7. Reinforcing structure; 701. Limiting plate; 702. Slider; 703. Insertion column. Detailed Implementation

[0020] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs; the terminology used herein in the specification of the application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application; the terms "comprising" and "having," and any variations thereof, in the specification, claims, and foregoing drawings of this application are intended to cover non-exclusive inclusion. The terms "first," "second," etc., in the specification, claims, or foregoing drawings of this application are used to distinguish different objects, not to describe a particular order.

[0021] In this document, the term "embodiment" means that a particular feature, structure, or characteristic described in connection with an embodiment may be included in at least one embodiment of this application. The appearance of this phrase in various places throughout the specification does not necessarily refer to the same embodiment, nor is it a separate or alternative embodiment mutually exclusive with other embodiments. It will be explicitly and implicitly understood by those skilled in the art that the embodiments described herein can be combined with other embodiments.

[0022] This utility model embodiment provides an easily adjustable drone launch tube, such as... Figure 1-4 As shown, it includes a base 1, a mounting plate 2 fixed to the top of the base 1, a connecting shaft 3 fixed to the top of the mounting plate 2, a cylinder 4 movably connected to the other end of the connecting shaft 3, a connecting structure 5 provided at the top of the cylinder 4, a support frame 6 movably connected to the other side of the cylinder 4, and a reinforcing structure 7 provided on both sides of the base 1.

[0023] It should be noted that, due to the inability to adjust the length of the drone launch tube, this solution addresses this issue by setting up a connecting structure 5. Through the symmetrical distribution of the first connecting block 502 and the second connecting block 503, and their corresponding placement, the connecting tube 501 can be limited to the top of the tube body 4, thus extending the tube body 4. The first connecting block 502 has the same threaded groove 505 inside, allowing the bolt 504 to pass through the first connecting block 502 and the second connecting block 503, reinforcing the limitation of the connecting tube 501. Extending the tube body 4 allows the length of the drone launch tube to be adjusted to meet different needs.

[0024] Specifically, in this embodiment, the solution mainly includes a connecting structure 5, which includes a second connecting block 503. The second connecting block 503 is fixed to the top of the cylinder 4. A first connecting block 502 is provided at the top of the second connecting block 503. A connecting cylinder 501 is fixed at the top of the first connecting block 502. A threaded groove 505 is provided inside the second connecting block 503, and a bolt 504 is provided inside the threaded groove 505. First, the threaded groove 505 is opened inside the second connecting block 503, and then the first connecting block 504 is connected to the cylinder 4. A threaded groove 505 is opened inside the 2, and then the first connecting block 502 is symmetrically fixed to the top and bottom of the connecting cylinder 501. Then the second connecting block 503 is symmetrically fixed to the top and bottom of the cylinder 4. The connecting cylinder 501 is placed at the top of the cylinder 4, so that the first connecting block 502 and the second connecting block 503 correspond to each other. Then the bolt 504 is screwed into the inside of the threaded groove 505 to limit and reinforce the connecting cylinder 501, so that the length of the UAV launch tube can be adjusted to meet the needs of different lengths.

[0025] In a further preferred embodiment of this utility model, such as Figure 1 , Figure 2 and Figure 3 As shown, there are two sets of second connecting blocks 503, which are symmetrically distributed about the central axis of the cylinder 4. There are also two sets of first connecting blocks 502, which are symmetrically distributed about the central axis of the connecting cylinder 501. The symmetrical distribution of the second connecting blocks 503 allows them to overlap with the first connecting blocks 502. The symmetrical distribution of the first connecting blocks 502 makes the two sets of first connecting blocks 502 and the two sets of second connecting blocks 503 symmetrical, making the connecting cylinder 501 more securely positioned at the top of the cylinder 4.

[0026] Specifically, in this embodiment, the solution mainly includes a reinforcing structure 7, which includes a slider 702. The slider 702 is disposed on both sides of the top and bottom of the base 1. A limiting plate 701 is fixed on the outer side wall of the slider 702. A locking post 703 is fixed on the top of the limiting plate 701. First, the slider 702 is symmetrically fixed on the top and bottom of the limiting plate 701. Then, the locking post 703 is symmetrically fixed on the top and bottom of the limiting plate 701. Then, the two sets of limiting plates 701 are symmetrically placed on both sides of the base 1 and slid, so that the slider 702 is engaged inside the base 1. The two sets of limiting plates 701 are symmetrically limited on both sides of the base 1, so that the drone launch tube can be limited and fixed by the locking post 703 when in use, making the drone launch tube more stable and less prone to displacement.

[0027] In a further preferred embodiment of this utility model, such as Figure 1 , Figure 2 and Figure 4As shown, there are two sets of limiting plates 701, which are symmetrically distributed about the central axis of the base 1. There are also two sets of insertion columns 703, which are symmetrically distributed about the central axis of the limiting plates 701. The symmetrical distribution of the limiting plates 701 allows the insertion columns 703 to be limited on both sides of the base 1. The symmetrical distribution of the insertion columns 703 makes the limiting of the UAV launch tube more stable when the insertion columns 703 are inserted into the ground.

[0028] It should be noted that, for the sake of simplicity, the foregoing embodiments are all described as a series of actions. However, those skilled in the art should understand that the present invention is not limited to the described order of actions, as some steps may be performed in other orders or simultaneously according to the present invention. Furthermore, those skilled in the art should also understand that the embodiments described in the specification are preferred embodiments, and the actions and modules involved are not necessarily essential to the present invention.

[0029] It should be understood that the disclosed apparatus can be implemented in other ways, given the several embodiments provided in this application. For example, the apparatus embodiments described above are merely illustrative. For instance, the division of units described above may be implemented in other ways in practice. For example, multiple units or components may be combined or integrated into another system, or some features may be ignored or not executed. Furthermore, the coupling or communication connections shown or discussed may be through some interfaces; indirect coupling or communication connections between devices or units may be telecommunications or other forms.

[0030] The units described above as separate components may or may not be physically separate. The components shown as units may or may not be physical units; that is, they may be located in one place or distributed across multiple network units. Some or all of the units can be selected to achieve the purpose of this embodiment according to actual needs.

[0031] The above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit the scope of protection of this utility model. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on these embodiments, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this utility model. Although this utility model has been described in detail with reference to the above embodiments, those skilled in the art can still combine, add, delete, or otherwise adjust the features of the various embodiments of this utility model according to the circumstances without conflict or creative effort, thereby obtaining different technical solutions that do not fundamentally depart from the concept of this utility model. These technical solutions are also within the scope of protection of this utility model.

Claims

1. An easily adjustable drone launch tube, characterized in that, Includes a base (1), with a mounting plate (2) fixed to the top of the base (1), a connecting shaft (3) fixed to the top of the mounting plate (2), a cylinder (4) movably connected to the other end of the connecting shaft (3), a connecting structure (5) provided at the top of the cylinder (4), a support frame (6) movably connected to the other side of the cylinder (4), and a reinforcing structure (7) provided on both sides of the base (1); The connecting structure (5) includes a second connecting block (503), which is fixed to the top of the cylinder (4). A first connecting block (502) is provided at the top of the second connecting block (503), and a connecting cylinder (501) is fixed at the top of the first connecting block (502). A threaded groove (505) is provided inside the second connecting block (503), and a bolt (504) is provided inside the threaded groove (505).

2. The adjustable UAV launch tube as described in claim 1, characterized in that, The second connecting block (503) is provided in two sets, and the two sets of the second connecting block (503) are symmetrically distributed about the central axis of the cylinder (4).

3. The adjustable UAV launch tube as described in claim 1, characterized in that, The first connecting block (502) is provided in two sets, and the two sets of the first connecting block (502) are symmetrically distributed about the central axis of the connecting cylinder (501).

4. The adjustable UAV launch tube as described in claim 1, characterized in that, The reinforcing structure (7) includes a slider (702), which is disposed on both sides of the top and bottom of the base (1). A limiting plate (701) is fixed on the outer side wall of the slider (702), and a mating post (703) is fixed on the top of the limiting plate (701).

5. The adjustable UAV launch tube as described in claim 4, characterized in that, The limiting plate (701) is provided in two sets, and the two sets of the limiting plate (701) are symmetrically distributed about the central axis of the base (1).

6. The adjustable UAV launch tube as described in claim 4, characterized in that, The insertion post (703) is provided in two sets, and the two sets of insertion posts (703) are symmetrically distributed about the central axis of the limiting plate (701).

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