A drone thrower

Abstract

The utility model relates to unmanned aerial vehicle throwing technology field, concretely is an unmanned aerial vehicle throwing device, including the feeder, the upper surface of feeder is provided with the aircraft, and the surface of feeder is provided with mounting device, and mounting device includes the main block, and the both sides fixed connection of main block and aircraft, and the surface of main block is provided with antiskid mouth, and the lower surface fixed connection of aircraft has the stabilizing block, and the surface of stabilizing block is covered with feeder, and the both sides of feeder are provided with built -in groove, and the inside slide connection of built -in groove has the sleeve plate, and the surface of sleeve plate places in the aircraft, and the surface of sleeve plate is provided with the sleeve mouth, and the surface of sleeve mouth is covered with main block, and the surface of sleeve plate is provided with positioning assembly. The utility model, through setting up mounting device, can effectively facilitate the worker to install throwing device, avoids the time -consuming situation that the worker will appear when installing throwing device, and then reduces the inconvenient problem that the worker appears when installing throwing device.

Description

Technical Field

[0001] This utility model relates to the field of drone throwing technology, and in particular to a drone thrower. Background Technology

[0002] A drone dropper is an auxiliary device mounted on a drone. Its main function is to use the drone's aerial carrying capacity to accurately drop specific items to a target location. A drone is an aircraft that does not require a pilot to operate it. It achieves autonomous or semi-autonomous flight through radio remote control equipment or its own onboard program control device.

[0003] When workers need to drop items, they attach the items to the dropper of a drone so that the drone can control the dropper to drop the items. However, existing droppers are usually fixed with bolts, which makes it time-consuming for workers to install the dropper and causes inconvenience. Utility Model Content

[0004] The purpose of this utility model is to solve the problem of inconvenience for workers when installing the launcher in the existing technology, and to propose a drone launcher.

[0005] To achieve the above objectives, this utility model adopts the following technical solution: a drone launcher, including a feeder, an aircraft mounted on the upper surface of the feeder, and an installation device on the surface of the feeder. The installation device includes a main block, which is fixedly connected to both sides of the aircraft. The surface of the main block has anti-slip openings. A stabilizing block is fixedly connected to the lower surface of the aircraft. The feeder is fitted onto the surface of the stabilizing block. Built-in grooves are formed on both sides of the feeder. A sleeve plate is slidably connected inside the built-in grooves. The sleeve plate is placed on the surface of the aircraft. A sleeve opening is formed on the surface of the sleeve plate, which fits onto the surface of the main block. A positioning component is provided on the surface of the sleeve plate. The positioning component consists of a rod, an adjusting plate, a limiting plate, and a pushing spring. The rod is slidably connected to the inside of the sleeve plate and inserted into the anti-slip openings. An adjusting plate is fixedly connected to the bottom end of the rod, and the adjusting plate is slidably connected to the inner side of the sleeve plate. The rod can cooperate with the sleeve plate to guide its sliding. A magnetic block is installed on the lower surface of the limiting plate.

[0006] Preferably, a limiting plate is fixedly connected to one side of the adjusting plate, the limiting plate is slidably connected to the surface of the sleeve plate, and a push spring is fixedly connected between the bottom end of the insertion rod and the sleeve plate. The limiting plate can cooperate with the adjusting plate to support the limiting plate, and the insertion rod can cooperate with the push spring to restrict the sliding of the insertion rod.

[0007] Preferably, the surface of the feeder is provided with a fixing device, the fixing device including an adjusting strap, the adjusting strap being fixedly connected to the lower surface of the feeder, the adjusting strap being located below the aircraft, the adjusting strap being able to cooperate with the feeder to achieve the purpose of supporting the adjusting strap, the adjusting strap being adjustable according to the external material, and the adjusting strap being a Velcro strap.

[0008] Preferably, one end of the adjusting strap is fixedly connected to an insert block, and the lower surface of the feeder is provided with a storage cavity. The insert block is inserted into the inside of the storage cavity, and the insert block can cooperate with the adjusting strap and the storage cavity to achieve the purpose of storing the insert block.

[0009] Preferably, the inner wall of the feeder is provided with a calibration groove, and the insert block is inserted into the inside of the calibration groove. The calibration groove can cooperate with the feeder to facilitate the placement of the insert block by the worker.

[0010] Preferably, an electric cylinder is fixedly connected to the surface of the feeder, and a limit block is fixedly connected to the drive end of the electric cylinder. The limit block is inserted into the interior of the insert block and the feeder. The electric cylinder can cooperate with the feeder to support the electric cylinder. The electric cylinder can cooperate with the limit block to restrict the insert block from leaving the receiving cavity. A locking mechanism is provided inside the electric cylinder.

[0011] Compared with the prior art, the advantages and positive effects of this utility model are as follows: 1. In this utility model, by setting up an installation device, when the worker needs to install the thrower, the worker places the feeder on the lower surface of the aircraft, and the feeder is fitted onto the stabilizing block. The worker simultaneously pushes two sleeve plates closer to the aircraft, and the sleeve openings on the surface of the sleeve plates fit onto the main block. The worker pushes the limiting plate upward, and the two magnetic blocks on the surface of the limiting plate move away from the protruding blocks on the surface of the sleeve plate, pushing the spring to push the insert rod. The insert rod slides inside the sleeve plate and inserts into the anti-slip opening of the main block. By setting up the installation device, the worker can effectively and conveniently install the thrower, avoiding the time-consuming situation when installing the thrower, and thus reducing the inconvenience problem when installing the thrower.

[0012] 2. In this utility model, by setting a fixing device, when the worker needs to fix the item, the worker places the item on the feeder. After the worker adjusts the length of the adjusting strap, the worker wraps the adjusting strap around the item. The worker inserts the insert block into the storage cavity. The calibration groove guides the insert block. When the insert block slides to the designated position, the electric cylinder is activated. The electric cylinder pushes the limit block, and the limit block inserts into the insert block. By setting a fixing device, it is possible to effectively and conveniently fix the item for the worker, avoiding inconvenience when fixing the adjusting strap, thereby improving the worker's work efficiency. Attached Figure Description

[0013] Figure 1 This utility model provides a three-dimensional structural diagram of a drone launcher; Figure 2 This utility model provides a schematic diagram of the installation device for a drone launcher; Figure 3 This utility model proposes a drone launcher. Figure 2 Enlarged structural diagram at point A in the middle; Figure 4 This utility model provides a schematic diagram of the fixing device structure for a drone launcher; Figure 5 This utility model proposes a drone launcher. Figure 4 Enlarged structural diagram at point B.

[0014] Legend: 1. Feeder; 2. Aircraft; 3. Mounting device; 31. Main block; 32. Anti-slip opening; 33. Stabilizing block; 34. Internal slot; 35. Sleeve plate; 36. Push spring; 37. Adjusting plate; 38. Insert rod; 39. Limiting plate; 310. Sleeve opening; 4. Fixing device; 41. Adjusting strap; 42. Insert block; 43. Calibration slot; 44. Storage cavity; 45. Limiting block; 46. Electric cylinder. Detailed Implementation

[0015] Please see Figures 1-5 This utility model provides a technical solution: a drone launcher, including a feeder 1, an aircraft 2 is provided on the upper surface of the feeder 1, and an installation device 3 is provided on the surface of the feeder 1.

[0016] The specific setup and function of the mounting device 3 and the fixing device 4 will be described in detail below.

[0017] In this embodiment: the installation device 3 includes a main block 31, which is fixedly connected to both sides of the aircraft 2. The surface of the main block 31 is provided with an anti-slip opening 32. A stabilizing block 33 is fixedly connected to the lower surface of the aircraft 2. The feeder 1 is sleeved on the surface of the stabilizing block 33. The feeder 1 is provided with built-in grooves 34 on both sides. A sleeve plate 35 is slidably connected inside the built-in groove 34. The sleeve plate 35 is placed on the surface of the aircraft 2. A sleeve opening 310 is provided on the surface of the sleeve plate 35. The sleeve opening 310 is sleeved on the surface of the main block 31. A positioning component is provided on the surface of the sleeve plate 35. The positioning component consists of a rod 38, an adjusting plate 37, a limiting plate 39, and a pushing spring 36.

[0018] Specifically, the insertion rod 38 is internally slidably connected to the sleeve plate 35, the insertion rod 38 is internally inserted into the anti-slip port 32, the bottom end of the insertion rod 38 is fixedly connected to the adjustment plate 37, the adjustment plate 37 is slidably connected to the inner side of the sleeve plate 35, the insertion rod 38 can cooperate with the sleeve plate 35 to guide the insertion rod 38 to slide, and a magnetic block is installed on the lower surface of the limiting plate 39.

[0019] Specifically, a limiting plate 39 is fixedly connected to one side of the adjusting plate 37, the limiting plate 39 is slidably connected to the surface of the sleeve plate 35, and a push spring 36 is fixedly connected between the bottom end of the insertion rod 38 and the sleeve plate 35.

[0020] In this embodiment: the limiting plate 39 can cooperate with the adjusting plate 37 to support the limiting plate 39, and the insertion rod 38 can cooperate with the pushing spring 36 to restrict the sliding of the insertion rod 38.

[0021] In this embodiment: a fixing device 4 is provided on the surface of the feeder 1. The fixing device 4 includes an adjusting strap 41, which is fixedly connected to the lower surface of the feeder 1. The adjusting strap 41 is located below the aircraft 2. The adjusting strap 41 can cooperate with the feeder 1 to support the adjusting strap 41. The adjusting strap 41 can be adjusted according to the external material. The adjusting strap 41 is a Velcro strap.

[0022] Specifically, one end of the adjusting strap 41 is fixedly connected to the insert block 42, and the lower surface of the feeder 1 is provided with a receiving cavity 44, and the insert block 42 is inserted into the inside of the receiving cavity 44.

[0023] In this embodiment, the insert 42 can cooperate with the adjusting strap 41 and the storage cavity 44 to achieve the purpose of storing the insert 42.

[0024] Specifically, the inner wall of the feeder 1 is provided with a calibration groove 43, and the insert block 42 is inserted into the calibration groove 43. The calibration groove 43 can cooperate with the feeder 1 to facilitate the placement of the insert block 42 by the worker.

[0025] Specifically, an electric cylinder 46 is fixedly connected to the surface of the feeder 1. A limit block 45 is fixedly connected to the drive end of the electric cylinder 46. The limit block 45 is inserted into the interior of the insert block 42. The limit block 45 is inserted into the interior of the feeder 1.

[0026] In this embodiment: the electric cylinder 46 can cooperate with the feeder 1 to support the electric cylinder 46, the electric cylinder 46 can cooperate with the limiting block 45 to restrict the insertion block 42 from leaving the receiving cavity 44, and the electric cylinder 46 is provided with a locking mechanism inside.

[0027] Working Principle: By setting up the installation device 3, when the worker needs to install the thrower, the worker places the feeder 1 on the lower surface of the aircraft 2, and the feeder 1 is fitted onto the stabilizing block 33. At the same time, the worker pushes the two sleeve plates 35 closer to the aircraft 2, and the sleeve openings 310 on the surface of the sleeve plates 35 fit onto the main block 31. The worker pushes the limiting plate 39 upward, and the two magnetic blocks on the surface of the limiting plate 39 move away from the protruding blocks on the surface of the sleeve plates 35, pushing the spring 36 to push the insertion rod 38. The insertion rod 38 slides inside the sleeve plate 35 and inserts into the anti-slip opening 32 of the main block 31. By setting up the installation device 3, the worker can effectively and conveniently install the thrower, avoiding time-consuming situations during the installation process. Furthermore, this reduces the inconvenience workers encounter when installing the thrower. Additionally, by setting up the fixing device 4, when workers need to secure items, they place the items on the feeder 1, adjust the length of the adjusting strap 41, wrap the strap 41 around the item, insert the insertion block 42 into the storage cavity 44, and the calibration groove 43 guides the insertion block 42. When the insertion block 42 slides to the designated position, the electric cylinder 46 is activated, pushing the limit block 45, which then inserts into the insertion block 42. By setting up the fixing device 4, workers can effectively and conveniently secure items, avoiding inconvenience when fixing the adjusting strap 41, thereby improving work efficiency.

Claims

1. A drone launcher, comprising a feeder (1), characterized in that: The upper surface of the feeder (1) is provided with an aircraft (2). The surface of the feeder (1) is provided with an installation device (3), the installation device (3) includes a main block (31), the main block (31) is fixedly connected to both sides of the aircraft (2); The surface of the main block (31) is provided with an anti-slip opening (32). The lower surface of the aircraft (2) is fixedly connected with a stabilizing block (33). The feeder (1) is sleeved on the surface of the stabilizing block (33). The feeder (1) is provided with built-in grooves (34) on both sides. The built-in grooves (34) are slidably connected with a sleeve plate (35). The sleeve plate (35) is placed on the surface of the aircraft (2). The surface of the sleeve plate (35) is provided with a sleeve opening (310). The sleeve opening (310) is sleeved on the surface of the main block (31). The surface of the sleeve plate (35) is provided with a positioning component. The positioning component consists of a rod (38), an adjusting plate (37), a limiting plate (39), and a pushing spring (36).

2. The drone launcher according to claim 1, characterized in that: The insert rod (38) is slidably connected to the inside of the sleeve plate (35), the insert rod (38) is inserted into the inside of the anti-slip port (32), and an adjustment plate (37) is fixedly connected to the bottom end of the insert rod (38). The adjustment plate (37) is slidably connected to the inside of the sleeve plate (35).

3. The drone launcher according to claim 2, characterized in that: A limiting plate (39) is fixedly connected to one side of the adjusting plate (37), the limiting plate (39) is slidably connected to the surface of the sleeve plate (35), and a push spring (36) is fixedly connected between the bottom end of the insert rod (38) and the sleeve plate (35).

4. The drone launcher according to claim 1, characterized in that: The surface of the feeder (1) is provided with a fixing device (4), the fixing device (4) includes an adjusting strap (41), the adjusting strap (41) is fixedly connected to the lower surface of the feeder (1), and the adjusting strap (41) is located below the aircraft (2).

5. A drone launcher according to claim 4, characterized in that: One end of the adjusting strap (41) is fixedly connected to the insert (42), and the lower surface of the feeder (1) is provided with a receiving cavity (44), and the insert (42) is inserted into the inside of the receiving cavity (44).

6. A drone launcher according to claim 5, characterized in that: The inner wall of the feeder (1) is provided with a calibration groove (43), and the insert (42) is inserted into the calibration groove (43).

7. A drone launcher according to claim 6, characterized in that: An electric cylinder (46) is fixedly connected to the surface of the feeder (1). A limit block (45) is fixedly connected to the drive end of the electric cylinder (46). The limit block (45) is inserted into the interior of the insert block (42). The limit block (45) is inserted into the interior of the feeder (1).

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