A drone cover separation device

Abstract

This utility model relates to the field of mechanical engineering technology and discloses a drone protective cover separation device, including two brackets. Protective shells are fixedly connected to the top of each bracket, and a separation mechanism is fixedly connected to the top of each protective shell. Fixing mechanisms are fixedly connected to the inner walls of both protective shells. A fuselage is fixedly connected to the outside of the separation mechanism, and multiple branches are fixedly connected to the outside of the fuselage. The separation mechanism includes two outer shells, the bottom of which are fixedly connected to the top of the two protective shells. A main locking plate is fixedly connected to the inner wall of one of the two outer shells. This utility model effectively solves the problem of overly complex disassembly of drone protective cover separation devices during use. It improves the efficiency of disassembly and replacement by addressing the issue of drones of different sizes shaking and colliding internally.

Description

Technical Field

[0001] This utility model relates to the field of mechanical engineering technology, and in particular to a device for separating the protective cover of a drone. Background Technology

[0002] Drone protective covers are key protective accessories for drones, primarily used to protect the fuselage and core components in various scenarios. During parking and transportation, they can withstand collisions, scratches, and bumps, reducing the risk of impact. Some sealed protective covers can also isolate sand, rain, and snow, preventing moisture and dust from entering the fuselage and protecting core components such as circuits and motors from corrosion.

[0003] The drone protective cover is designed to protect the drone's fuselage, making it particularly crucial. It is typically made of tough and elastic materials such as engineering plastics or silicone, and features a semi-enclosed design that can cover a large area of ​​the top, bottom, and sides of the drone. It only provides precise openings for key functional areas such as the battery compartment, heat dissipation vents, and data interfaces, ensuring that it does not affect the normal operation of the drone. In the event of a collision with other objects, it significantly reduces wear and deformation of the fuselage shell. Overall, it achieves targeted protection through physical isolation and scene adaptation, balancing protection with the normal operation of the drone.

[0004] In existing technologies, the disassembly of the drone protective cover separation device is too complicated during use. Too many structures will greatly increase the time required for the entire disassembly and use process, resulting in a waste of time. The overly complicated structure will significantly increase the complexity of operation. Therefore, a drone protective cover separation device is proposed to solve the above problems. Utility Model Content

[0005] To overcome the above shortcomings, this utility model provides a drone protective cover separation device, which aims to improve the problem of disassembling the drone protective cover separation device during use in the prior art.

[0006] To achieve the above objectives, the present invention adopts the following technical solution: a drone protective cover separation device, comprising two supports, each of the two supports having a protective shell fixedly connected to its outer top, a separation mechanism fixedly connected to the top of each protective shell, a fixing mechanism fixedly connected to the inner walls of each of the two protective shells, a fuselage fixedly connected to the outer side of the separation mechanism, and multiple branches fixedly connected to the outer side of the fuselage; the separation mechanism comprises two outer shells, the bottom ends of the two outer shells being fixedly connected to the top of the two protective shells, a main locking plate fixedly connected to the inner wall of one of the two outer shells, two locking pins slidably connected to the inner wall of the main locking plate, a locked plate fixedly connected to the outer side of each of the two locking pins, a locking tongue slidably connected to the inner wall of each of the two locking pins, a control pin slidably connected to the outer side of each of the two locking tongues, a connecting plate fixedly connected to the front side of each of the two control pins, and a switch assembly fixedly connected to the inner wall of the connecting plate.

[0007] As a further description of the above technical solution: the fixing mechanism includes two side plates, the far side of the two side plates is fixedly connected to the inner wall of the protective shell, two elastic columns are fixedly connected to the near side of the two side plates, a horizontal column is fixedly connected to the near side of the two elastic columns, a horizontal spring is sleeved on the outside of the multiple horizontal columns, a force-bearing column is fixedly connected to the near side of the multiple horizontal columns, a pressing column is fixedly connected to the near side of the multiple elastic columns, a fixing cap is fixedly connected to the near side of the multiple pressing columns, and two abutment plates are fixedly connected to the near side of the multiple fixing caps.

[0008] As a further description of the above technical solution: the switch assembly includes a torsion post, the rear side of which is fixedly connected to the front of the locked plate, a torsion post spring is sleeved on the outside of the torsion post, a button is fixedly connected to the front of the torsion post, and control springs are sleeved on the outside of both locking tongues.

[0009] As a further description of the above technical solution: the inner wall of the protective shell is slidably connected to the outside of the body, and the top of the bracket is fixedly connected to the outside of the body.

[0010] As a further description of the above technical solution: the rear part of the stop plate is fixedly connected to the outside of the machine body, and the front part of the main locking plate is fixedly connected to the rear part of the locked plate.

[0011] As a further description of the above technical solution: the inner wall of the outer shell is slidably connected to the outside of the torsion post, and the outside of the locked plate is fixedly connected to the other inner wall of the two outer shells.

[0012] As a further description of the above technical solution: the adjacent sides of the plurality of force-bearing columns are fixed to the distant sides of the two abutments, and the adjacent sides of the two control springs are slidably connected to the distant sides of the two control columns.

[0013] As a further description of the above technical solution: the adjacent sides of the two cross springs are fixedly connected to the distant sides of the two force-bearing columns, and the distant sides of the plurality of cross springs are fixedly connected to the adjacent sides of the plurality of elastic columns.

[0014] This utility model has the following beneficial effects:

[0015] 1. In this utility model, by pressing the button, the button extends and retracts, causing the control columns fixedly connected to both sides of the joint plate to press down. This causes the locking tongue, which is stuck in the control column, to move to both ends by the control spring, allowing the locking tongue to slide away from the locking column. This makes it easy to separate the locking column from the locked plate, allowing the separation mechanism to open easily, thereby realizing the easy separation of the entire drone protective cover separation device.

[0016] 2. In this utility model, side plates are connected to the front and rear sides inside the protective shell, and elastic columns are fixedly connected to the side plates. There are springs inside the elastic columns, so that the pressing column can spring up when pressed. At the same time, multiple force-bearing columns are added to prevent the internal structure from not fitting properly. The structures at both ends are installed at the same time to solve the problem of the drone shaking inside the non-fitted structure, thereby damaging the drone body. Attached Figure Description

[0017] Figure 1 This is a three-dimensional schematic diagram of a drone protective cover separation device proposed in this utility model;

[0018] Figure 2 This is a schematic diagram of the protective shell of a drone protective cover separation device proposed in this utility model;

[0019] Figure 3 for Figure 2 Enlarged view of point A in the middle;

[0020] Figure 4 for Figure 2 Enlarged view of point B in the middle.

[0021] Legend:

[0022] 1. Bracket; 2. Protective shell; 3. Separation mechanism; 31. Outer shell; 32. Main locking plate; 33. Locking pin; 34. Locked plate; 35. Lock tongue; 36. Control spring; 37. Control pin; 38. Connecting plate; 39. Switch assembly; 391. Torsion pin; 392. Torsion pin spring; 393. Button; 4. Fixing mechanism; 41. Side plate; 42. Elastic pin; 43. Horizontal pin; 44. Horizontal bar spring; 45. Force-bearing pin; 46. Pressing pin; 47. Fixing cap; 48. Support plate; 5. Body; 6. Support leaf. Detailed Implementation

[0023] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0024] Reference Figures 1 to 3This utility model provides an embodiment of a drone protective cover separation device, comprising two supports 1, which connect the fuselage 5 to the entire protective shell 2, mainly supporting the entire structure and ensuring its stability. The protective shell 2 is fixedly connected to the top of each of the two supports 1, ensuring the stability of the upper part of the entire structure. A separation mechanism 3 is fixedly connected to the top of the protective shell 2, which is used to separate the entire structure. The separation mechanism 3 is designed for quick disassembly of the entire structure, ensuring both rapid disassembly and installation and fixation of the entire structure. Fixing mechanisms 4 are fixedly connected to the inner walls of both protective shells 2, ensuring the overall disassembly and rapid disassembly mechanism. The fuselage 5 is fixedly connected to the outside of the separation mechanism 3; the fuselage 5 is the drone to be inserted into the device, serving as a substitute to ensure the overall structural operation. Multiple propellers 6 are fixedly connected to the outside of the fuselage 5; these propellers 6 are the drone's propellers, an important structure for the drone's takeoff.

[0025] The separation mechanism 3 includes two outer shells 31. The two outer shells 31 ensure the integrity and appearance of the structure, while also ensuring the concealment of the internal structure. The bottom ends of the two outer shells 31 are fixedly connected to the top of the two protective shells 2, and the two outer shells 31 are connected to the top of the protective shells 2.

[0026] To ensure that the protective shell 2 opens simultaneously when the outer shell 31 is opened, a main locking plate 32 is fixedly connected to the inner wall of one of the two outer shells 31. The connection of the main locking plate 32 to one outer shell 31 ensures that the structure of one side of the outer shell 31 remains intact, preventing structural collapse. Two locking pins 33 are slidably connected to the inner wall of the main locking plate 32 for locking. A locked plate 34 is fixedly connected to the outside of each locking pin 33. The locked plate 34 is primarily for connecting the two outer shells 31 together. A locking tongue 35 is slidably connected to the inner wall of each locking pin 33. The locking tongue 35 primarily holds the locking pin 33 in place to prevent it from sliding out of the locked plate 34, thus preventing the structure from easily falling off. A control pin 37 is slidably connected to the outside of each locking tongue 35. The control pin 37 primarily controls the locking tongue 35. The locking and unlocking are achieved by moving the locking tongue 35. A connecting plate 38 is fixedly connected to the front side of each of the two control posts 37. The connecting plate 38 is used to operate the two control posts 37 simultaneously to prevent the switch from jamming. A switch assembly 39 is fixedly connected to the inner wall of the connecting plate 38. The switch assembly 39 is the manually operated part.

[0027] Reference Figures 2 to 4The fixing mechanism 4 includes two side plates 41. The fixing mechanism 4 is located on the side plates 41 inside the entire protective shell 2. The opposite sides of the two side plates 41 are fixedly connected to the inner wall of the protective shell 2 to ensure the fit of the inner wall to the body 5. The entire fixing mechanism 4 is installed. Two elastic columns 42 are fixedly connected to the adjacent sides of the two side plates 41. The elastic columns 42 are mainly to ensure the elastic energy of the entire mechanism and maintain the clamping of the intermediate structure. A horizontal column 43 is fixedly connected to the adjacent sides of the two elastic columns 42. The horizontal column 43 is used to install multiple forces applied to the intermediate structure to ensure the stability of the structure and prevent shaking.

[0028] Multiple horizontal columns 43 are fitted with horizontal springs 44. When the horizontal springs 44 move, the force-bearing column 45 transmits the force from the abutment plate 48 to the spring. The reaction force pushes the entire abutment back, ensuring that the abutment plate 48 fits the intermediate structure. Multiple horizontal columns 43 are fixedly connected to force-bearing columns 45 on adjacent sides, ensuring that the force-bearing column 45 moves towards the horizontal bar when under force to prevent it from falling. Multiple elastic columns 42 are fixedly connected to pressing columns 46 on adjacent sides. Multiple pressing columns 46 are fixedly connected to fixing caps 47 on adjacent sides. The fixing caps 47 stabilize the pressing column 46 connected to the abutment plate 48 and transmit the force of the abutment plate 48 to the elastic column 42. Multiple fixing caps 47 are fixedly connected to two abutment plates 48 on adjacent sides, fixing the entire structure and ensuring the stability of the abutment plate 48.

[0029] Reference Figures 1 to 3 The switch assembly 39 includes a torsion post 391, which receives the force transferred from the button 393 and converts it into a force on the connecting plate 38. The rear side of the torsion post 391 is fixedly connected to the front of the locked plate 34, fixing the entire switch assembly 39 and preventing the assembly from falling. A torsion post spring 392 is sleeved on the outside of the torsion post 391. When the button 393 is pressed, it will press down, and when the button 393 is released, it can automatically pop out. The front of the torsion post 391 is fixedly connected to the button 393. The button 393 is pressed when the device needs to be disassembled or installed. The two locking tongues 35 are each sleeved with a control spring 36. The spring can ensure that the locking post 33 will not disengage from the locking tongue 35 when the locking tongue 35 is not disassembled. The inner wall of the protective shell 2 is slidably connected to the outside of the body 5 to ensure the stability and adaptability of the body 5.

[0030] The top of bracket 1 is fixedly connected to the outside of body 5. Bracket 1 is connected to body 5 to ensure the stability of body 5. The rear of abutment plate 48 is fixedly connected to the outside of body 5, fitting against body 5 to ensure stability and prevent collisions. The front of main locking plate 32 is fixedly connected to the rear of locked plate 34. In order to fix the outer shells 31 on both sides to ensure the function and installation of the structure, the inner wall of outer shell 31 is slidably connected to the outside of torsion column 391. The outside of locked plate 34 is fixedly connected to the other inner wall of the two outer shells 31 to fix the other outer shell 31. The near side of multiple force-bearing columns 45 is fixed to the far side of two abutment plates 48. The near side of two control springs 36 is slidably connected to the far side of two control columns 37. The near side of two crossbar springs 44 is fixedly connected to the far side of two force-bearing columns 45. The far side of multiple crossbar springs 44 is fixedly connected to the near side of multiple elastic columns 42 to ensure that the crossbar springs 44 move towards the elastic columns 42 and prevent them from deviating from the force trajectory.

[0031] Working principle: When the operator needs to use the drone, they can press button 393 to move the torsion column 391 connected to button 393 under the force of torsion spring 392. When moving backward, the connecting plate 38 fixedly connected to the torsion column 391 moves simultaneously. Control columns 37 are fixed at both ends of the connecting plate 38. When the connecting plate 38 moves inward, the two control columns 37 move. There are slots inside the control columns 37 that hold the middle part of the entire locking tongue 35. During movement, the protruding parts on the outside of the locking tongue 35 are engaged into the control columns 37. The groove in the part allows the locking tongue 35 to move only left and right when the control column moves back and forth. A cross spring 44 is fitted on the far side of the two locking tongues 35. The cross spring 44 can keep the locking tongue 35 extended and lock the locking column 33 to prevent it from easily leaving the lock when not needed, which would cause the structure to fall apart automatically. Pressing the button 393 makes the locking tongue 35 leave the locking column 33. At this time, the locking column 33 can easily slide away from the locked plate 34, so that the two sides of the separation mechanism 3 can be easily separated, making the whole operation process simpler and more convenient.

[0032] When the drone body 5 is placed into the protective cover separation device, drones of different sizes are placed inside the device. The protective shell 2 is fixed at both ends. There are multiple elastic pillars 42 on the side plate 41. The adjacent side of two elastic pillars 42 is connected to a horizontal pillar 43. There are horizontal springs 44 and force-bearing pillars 45 on the horizontal pillars 43. When the force-bearing pillar is subjected to the pressure of the abutment plate 48, the horizontal springs 44 at both ends are subjected to pressure, which increases the internal space. At the same time, spring 1 inside the elastic pillar 42 and pressing pillar 46 are fixed by the internal influence. Spring 2 is also installed on the outside to increase the tension. When the abutment plate 48 presses the fixing mechanism 4, it maintains the stability of the mechanism. Both ends move at the same time, which stabilizes the body 5 inside the protective cover and effectively prevents the body 5 from shaking inside and causing damage.

[0033] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. An unmanned aerial vehicle cover separation device comprising two supports (1), characterized in that: The two brackets (1) are fixedly connected to the outer top of each of the two brackets (1), and the top of each of the two brackets (2) is fixedly connected to a separation mechanism (3). The inner walls of the two brackets (2) are fixedly connected to a fixing mechanism (4). The outer side of the separation mechanism (3) is fixedly connected to a body (5), and the outer side of the body (5) is fixedly connected to multiple branches (6). The separation mechanism (3) includes two outer shells (31), the bottom ends of which are fixedly connected to the top of the two protective shells (2). A main locking plate (32) is fixedly connected to the inner wall of one of the two outer shells (31). Two locking pins (33) are slidably connected to the inner wall of the main locking plate (32). A locked plate (34) is fixedly connected to the outside of each of the two locking pins (33). A locking tongue (35) is slidably connected to the inner wall of each of the two locking pins (33). A control pin (37) is slidably connected to the outside of each of the two locking tongues (35). A connecting plate (38) is fixedly connected to the front side of each of the two control pins (37). A switch assembly (39) is fixedly connected to the inner wall of the connecting plate (38).

2. The UAV protective cover separation device of claim 1, wherein: The fixing mechanism (4) includes two side plates (41). The two side plates (41) are fixedly connected to the inner wall of the protective shell (2) on opposite sides. Two elastic columns (42) are fixedly connected to the adjacent sides of the two side plates (41). A horizontal column (43) is fixedly connected to the adjacent sides of the two elastic columns (42). A horizontal spring (44) is sleeved on the outside of the multiple horizontal columns (43). A force-bearing column (45) is fixedly connected to the adjacent sides of the multiple horizontal columns (43). A pressing column (46) is fixedly connected to the adjacent sides of the multiple elastic columns (42). A fixing cap (47) is fixedly connected to the adjacent sides of the multiple pressing columns (46). Two abutment plates (48) are fixedly connected to the adjacent sides of the multiple fixing caps (47).

3. The drone protective cover separation device of claim 1, wherein: The switch assembly (39) includes a torsion post (391), the rear side of which is fixedly connected to the front of the locked plate (34), a torsion post spring (392) is sleeved on the outside of the torsion post (391), a button (393) is fixedly connected to the front of the torsion post (391), and control springs (36) are sleeved on the outside of both latches (35).

4. The drone protective cover separation device of claim 2, wherein: The inner wall of the protective shell (2) is slidably connected to the outside of the body (5), and the top of the bracket (1) is fixedly connected to the outside of the body (5).

5. The drone protective cover separation device of claim 3, wherein: The two control springs (36) are slidably connected on the adjacent side to the two control posts (37) on the distant side, and the front of the main locking plate (32) is fixedly connected to the rear of the locked plate (34).

6. The drone protective cover separation device of claim 3, wherein: The inner wall of the outer shell (31) is slidably connected to the outside of the torsion post (391), and the outside of the locked plate (34) is fixedly connected to the other inner wall of the two outer shells (31).

7. The drone protective cover separation device of claim 2, wherein: The adjacent sides of the plurality of force-bearing columns (45) are fixed to the opposite sides of the two abutment plates (48), and the rear of the abutment plates (48) are fixedly connected to the outside of the fuselage (5).

8. The drone protective cover separation device of claim 2, wherein: The proximal sides of the two horizontal rod springs (44) are fixedly connected to the distal sides of the two force columns (45), and the distal sides of the multiple horizontal rod springs (44) are fixedly connected to the proximal sides of the multiple elastic columns (42).

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