Vibration reduction mechanism for shooting lens of traversing machine

Abstract

The utility model provides a vibration reduction mechanism for a shooting lens of a traversing machine, and belongs to the technical field of traversing machines. The shock absorption mechanism for the shooting lens of the traversing machine comprises a buffer assembly and a connecting assembly, elastic blocks are correspondingly arranged on the two sides of the interior of a concave plate, a rack is slidably clamped with the concave plate through the elastic blocks, a camera is arranged on one side of the rack, and the shock absorption and buffering effects can be achieved through a buffer seat; according to the crossing machine, the camera can be prevented from being damaged by vibration generated when the crossing machine body falls to the ground, the protection effect can be achieved, the rack is slidably connected with the concave plate in a clamped mode through the elastic block, the rack and the camera can be conveniently disassembled and installed through the clamping connection mode, and the practicability is high. According to the invention, the rack and the camera can be dismounted and mounted without using a special tool, so that the camera can be dismounted and mounted conveniently, the dismounting and mounting are more convenient, and meanwhile, the camera can be prevented from being damaged by vibration in the landing process of the crossing machine body, so that the practicability is improved.

Description

Technical Field

[0001] The present application relates to the field of drones, and in particular to a vibration reduction mechanism for a drone shooting lens. Background Art

[0002] FPV drones, also known as "FPV quad-rotor drones", are an extreme sport of model aircraft that has emerged worldwide in recent years. Although FPV drones are quad-rotor drones, they are different from general consumer drones in that they can reach speeds of more than 200 kilometers per hour and can perform various complex aerial stunts, such as spiral flips, inverted flights, rapid ascents and descents, etc. However, the existing FPV drones have a vibration reduction mechanism for the camera lens. Usually, the camera is fixed to the FPV drone by screws, and special tools are required for disassembly and installation. Disassembly and installation are relatively cumbersome. Secondly, the vibration reduction effect is poor, and the vibration during landing can easily cause damage to the camera, thereby reducing practicality. Utility Model Content

[0003] In order to make up for the above shortcomings, the present application provides a vibration reduction mechanism for the camera lens of a FPV drone, which aims to improve the existing vibration reduction mechanism for the camera lens of a FPV drone. Usually, the camera is fixed to the FPV drone by screws, and special tools are required for disassembly and installation. The disassembly and installation are relatively cumbersome. Secondly, the shock absorption effect is poor, and the vibration occurring during the landing process can easily cause damage to the camera, thereby reducing the practicality.

[0004] An embodiment of the present application provides a vibration reduction mechanism for a drone shooting lens, including a buffer component and a connection component.

[0005] The buffer assembly includes a drone body and a buffer seat, wherein the buffer seat is arranged at one end of the drone body, and the connecting assembly includes a concave plate, an elastic block, a frame and a camera, wherein the concave plate is arranged at one side of the buffer seat, and the elastic block is correspondingly arranged at two sides inside the concave plate, the frame is slidably connected with the concave plate through the elastic block, and the camera is arranged at one side of the frame.

[0006] In a specific embodiment, the buffer seat includes a base plate, a support plate, a first spring and a damper, the support plate is slidably connected to the base plate, a plurality of first springs are arranged inside the base plate, the support plate is fixedly connected to the first spring, a plurality of dampers are arranged inside the base plate, and the support plate is fixedly connected to the damper.

[0007] In the above implementation process, the bottom plate and the support plate can play a role of limiting support, and the first spring and the damper can cooperate to play a role of buffering and shock absorption.

[0008] In a specific embodiment, a cavity is provided inside the bottom plate, and the support plate is slidably connected to the cavity.

[0009] In the above implementation process, a cavity is provided inside the bottom plate, and the cavity can play a role of limiting.

[0010] In a specific embodiment, slide grooves are arranged on both sides of the concave plate.

[0011] In the above implementation process, slide grooves are arranged on both sides of the concave plate, and the slide grooves can play a role of limiting.

[0012] In a specific embodiment, through holes are correspondingly arranged on both sides of the interior of the concave plate.

[0013] In the above implementation process, through holes are correspondingly arranged on both sides of the concave plate, and the through holes can play a role of limiting.

[0014] In a specific implementation, the elastic block includes a second spring and an arc surface block, the second spring is arranged on both sides of the through hole, the arc surface block is fixedly connected to the second spring, and the arc surface block is slidably connected to the through hole.

[0015] In the above implementation process, the second spring and the arc surface block can play a clamping role.

[0016] In a specific implementation manner, grooves are correspondingly arranged on both sides of the frame, and the arc surface blocks are in contact with the grooves.

[0017] In the above implementation process, grooves are correspondingly arranged on both sides of the frame, and the grooves can play a role of limiting.

[0018] In a specific implementation manner, limit bars are provided on both sides of the frame, and the limit bars are slidably connected to the slide grooves.

[0019] In the above implementation process, limit bars are set on both sides of the frame. When the camera needs to be disassembled, the user can pull the frame, and the groove can squeeze the arc block to move the arc block into the through hole. Then the groove and the arc block are misaligned to move the limit bar out of the slide slot, so that the frame and the camera can be disassembled, and the opposite operation can be performed to install them.

[0020] Compared with the prior art, the present application has the following beneficial effects: firstly, the buffer seat can play a role of shock absorption and buffering, which can prevent the vibration generated when the drone body falls to the ground from causing damage to the camera, and can play a protective effect; secondly, since the frame is slidably connected with the concave plate through the elastic block, the frame and the camera can be easily disassembled and installed by adopting the card connection method, and the frame and the camera can be disassembled and installed without using special tools, thereby facilitating the disassembly and installation of the camera, and the disassembly and installation are relatively convenient. At the same time, the vibration generated during the landing of the drone body can be prevented from causing damage to the camera, thereby improving practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the technical solutions of the implementation methods of the present application, the drawings required for use in the implementation methods will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0022] Figure 1 This is a schematic diagram of the first-perspective structure of a vibration reduction mechanism of a camera lens for a flying drone provided in an embodiment of the present application;

[0023] Figure 2 A schematic diagram of the structure of the buffer seat from a second viewing angle provided in an embodiment of the present application;

[0024] Figure 3 A schematic diagram of the concave plate structure provided in an embodiment of the present application;

[0025] Figure 4 A schematic diagram of the rack structure provided for an implementation manner of the present application.

[0026] In the figure: 100-buffer assembly; 110-Flying machine body; 120-buffer seat; 121-bottom plate; 1211-cavity; 122-support plate; 123-first spring; 124-damper; 200-connecting assembly; 210-concave plate; 211-slide groove; 212-through hole; 220-elastic block; 221-second spring; 222-arc block; 230-frame; 231-groove; 232-limiting strip; 240-camera. DETAILED DESCRIPTION

[0027] The technical solutions in the embodiments of the present application will be described below in conjunction with the drawings in the embodiments of the present application.

[0028] In order to make the purpose, technical solutions and advantages of the implementation methods of this application clearer, the technical solutions in the implementation methods of this application will be clearly and completely described below in conjunction with the drawings in the implementation methods of this application. Obviously, the described implementation methods are part of the implementation methods of this application, not all of the implementation methods. Based on the implementation methods in this application, all other implementation methods obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0029] See also Figure 1-4 The present application provides a vibration reduction mechanism for a drone shooting lens, including a buffer component 100 and a connecting component 200. The buffer component 100 can play a role in buffering and shock reduction, and the connecting component 200 can facilitate disassembly and installation.

[0030] See also Figure 1-2 The buffer assembly 100 includes a drone body 110 and a buffer seat 120. The buffer seat 120 is arranged at one end of the drone body 110. The buffer seat 120 includes a bottom plate 121, a support plate 122, a first spring 123 and a damper 124. The support plate 122 is slidably connected to the bottom plate 121. Several first springs 123 are arranged inside the bottom plate 121. The support plate 122 is fixedly connected to the first spring 123. Several dampers 124 are arranged inside the bottom plate 121. The support plate 122 is fixedly connected to the damper 124. The bottom plate 121 and the support plate 122 can play a role of limiting support. The first spring 123 and the damper 124 can cooperate to play a role of buffering and shock absorption. A cavity 1211 is arranged inside the bottom plate 121. The support plate 122 is slidably connected to the cavity 1211. The cavity 1211 can play a role of limiting.

[0031] See also Figure 1 , Figure 3 and Figure 4 The connecting assembly 200 includes a concave plate 210, an elastic block 220, a frame 230 and a camera 240. The concave plate 210 is arranged on one side of the buffer seat 120, and the elastic block 220 is correspondingly arranged on both sides of the concave plate 210. The frame 230 is slidably connected with the concave plate 210 through the elastic block 220. The camera 240 is arranged on one side of the frame 230. Slide grooves 211 are arranged on both sides of the concave plate 210. The slide grooves 211 can play a role in limiting. Through holes 212 are correspondingly arranged on both sides of the concave plate 210. The through holes 212 can play a role in limiting.

[0032] In some specific implementation schemes, the elastic block 220 includes a second spring 221 and a curved surface block 222. The second spring 221 is arranged on both sides of the through hole 212. The curved surface block 222 is fixedly connected to the second spring 221. The curved surface block 222 is slidably connected to the through hole 212. The second spring 221 and the curved surface block 222 can play a role of clamping. The two sides of the frame 230 are correspondingly provided with grooves 231. The curved surface block 222 contacts the groove 231. The groove 231 can play a role of limiting. The frame 2 Limiting strips 232 are provided on both sides of 30, and the limiting strips 232 are slidably connected with the slide groove 211. When the camera 240 needs to be disassembled, the user can pull the frame 230, and the groove 231 can squeeze the arc surface block 222, so that the arc surface block 222 moves into the through hole 212, and then the groove 231 and the arc surface block 222 are misaligned, and the limiting strips 232 are moved out from the slide groove 211, so that the frame 230 and the camera 240 can be disassembled, and the reverse operation can be performed to install them.

[0033] The working principle of the vibration reduction mechanism of the camera lens of the drone is as follows: the bottom plate 121 and the support plate 122 can play the role of limiting support, and the first spring 123 and the damper 124 can cooperate to play the role of buffering and shock reduction, which can prevent the vibration generated when the drone body 110 falls to the ground from causing damage to the camera 240, and can play a protective effect. When the camera 240 needs to be disassembled, the user can pull the frame 230, and the groove 231 can squeeze the arc block 222, so that the arc block 222 moves toward the inside of the through hole 212, and then the groove 231 and the arc block 2 22 is misaligned, and the limit bar 232 is moved out from the inside of the slide groove 211, so that the frame 230 and the camera 240 can be disassembled, and vice versa, they can be installed. The card connection method can facilitate the disassembly and installation of the frame 230 and the camera 240, and no special tools are needed to disassemble and install the frame 230 and the camera 240, thereby facilitating the disassembly and installation of the camera 240. The disassembly and installation are relatively convenient, and at the same time, the vibration caused by the landing of the flying machine body 110 can be prevented from causing damage to the camera 240, thereby improving practicality.

[0034] It should be noted that the specific model specifications of the FPV body 110 and the camera 240 need to be selected and determined based on the actual specifications of the device, and the specific selection calculation method adopts the existing technology in the field, so it will not be described in detail.

[0035] The power supply and principle of the drone body 110 and the camera 240 are clear to those skilled in the art and will not be described in detail here.

[0036] The above description is only an embodiment of the present application and is not intended to limit the scope of protection of the present application. For those skilled in the art, the present application may have various changes and variations. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present application should be included in the scope of protection of the present application. It should be noted that similar reference numerals and letters represent similar items in the following drawings, so once an item is defined in one drawing, it does not need to be further defined and explained in the subsequent drawings.

[0037] The above is only a specific implementation of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application. Therefore, the protection scope of the present application should be based on the protection scope of the claims.

Claims

1. A vibration reduction mechanism for a camera lens of a flying drone, characterized in that: include A buffer assembly (100), the buffer assembly (100) comprising a drone body (110) and a buffer seat (120), the buffer seat (120) being arranged at one end of the drone body (110); A connecting assembly (200), the connecting assembly (200) comprising a concave plate (210), an elastic block (220), a frame (230) and a camera (240), the concave plate (210) being arranged on one side of the buffer seat (120), the elastic block (220) being arranged on two sides of the interior of the concave plate (210) correspondingly, the frame (230) being slidably engaged with the concave plate (210) via the elastic block (220), and the camera (240) being arranged on one side of the frame (230).

2. The vibration reduction mechanism for a drone camera lens according to claim 1, characterized in that: The buffer seat (120) comprises a base plate (121), a support plate (122), a first spring (123) and a damper (124); the support plate (122) is slidably connected to the base plate (121); a plurality of first springs (123) are arranged inside the base plate (121); the support plate (122) and the first spring (123) are fixedly connected; a plurality of dampers (124) are arranged inside the base plate (121); and the support plate (122) and the damper (124) are fixedly connected.

3. The vibration reduction mechanism for a drone camera lens according to claim 2, characterized in that: A cavity (1211) is provided inside the bottom plate (121), and the support plate (122) is slidably connected to the cavity (1211).

4. The vibration reduction mechanism for a drone camera lens according to claim 1, characterized in that: Slide grooves (211) are arranged on both sides of the concave plate (210).

5. The vibration reduction mechanism for a drone shooting lens according to claim 1, characterized in that: Through holes (212) are correspondingly arranged on two sides of the interior of the concave plate (210).

6. The vibration reduction mechanism for a camera lens of a flying drone according to claim 5, characterized in that: The elastic block (220) comprises a second spring (221) and a curved surface block (222); the second spring (221) is arranged on both sides of the through hole (212); the curved surface block (222) is fixedly connected to the second spring (221); and the curved surface block (222) is slidably connected to the through hole (212).

7. The vibration reduction mechanism for a drone camera lens according to claim 6, characterized in that: Grooves (231) are correspondingly arranged on both sides of the frame (230), and the arc surface block (222) is in contact with the grooves (231).

8. The vibration reduction mechanism for a drone camera lens according to claim 4, characterized in that: Limiting bars (232) are arranged on both sides of the frame (230), and the limiting bars (232) are slidably connected to the sliding grooves (211).

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