Quick dismounting structure for holder of unmanned aerial vehicle
By designing a quick-release structure for the drone gimbal, a knob handle and threaded rod are used to achieve quick release, and a motor drives the adjustment roller to rotate to achieve angle adjustment. This solves the problems of imperfect quick release and angle adjustment of the drone gimbal and improves operational efficiency.
Patent Information
- Application Number
- CN202520728607.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-17
- Publication Date
- 2026-02-13
- Estimated Expiration
- 2035-04-17
AI Technical Summary
Existing drone gimbals lack sufficient functionality in quick-release and angle adjustment, affecting user operating efficiency.
A quick-release structure for a drone gimbal was designed, comprising a quick-release structure body, a mounting plate, a plug-in plate, a locking rod, a support arm, a gimbal body, a motor, and other components working together. Quick release is achieved through the connection of a knob handle and a threaded rod, and the angle is adjusted by the motor driving the adjustment roller to rotate the locking rod.
It enables quick disassembly and efficient angle adjustment of the drone gimbal, meeting users' needs for quick disassembly and self-adjustment of the angle.
Smart Images

Figure CN223905319U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to a holder quick release technical field especially relates to an unmanned aerial vehicle holder quick release structure. BACKGROUND
[0002] The unmanned aerial vehicle holder is a support device for installing and fixing task loads such as cameras, wherein the holder is a support device for installing and fixing mobile phones, cameras and video cameras, and is divided into fixed and electric holders, the holder can be rotated arbitrarily, and is convenient for users to use, when the user uses the unmanned aerial vehicle holder, the user needs to quickly release it.
[0003] Through the research, the patent with patent announcement No. CN219215406U discloses a novel unmanned aerial vehicle holder, which comprises an unmanned aerial vehicle holder and a holder protection mechanism, characterized in that: the holder protection mechanism comprises first fixing bolts, second fixing bolts, a holder protection plate, protection plate connecting bolts and connecting pieces, an upper surface of the unmanned aerial vehicle holder is provided with a holder damping mechanism, an upper surface of the holder damping mechanism is threadedly connected with an unmanned aerial vehicle, both side surfaces of the unmanned aerial vehicle holder are provided with the holder protection mechanism, and a lower surface of the unmanned aerial vehicle holder is fixedly connected with a camera.
[0004] However, the current novel unmanned aerial vehicle holder has the following problems: when the user needs to use the unmanned aerial vehicle holder, the function is not perfect, so that the use of the quick release structure by the user is affected, and when the user needs to perform angle self-adjustment of the holder, the function is not perfect, therefore, the unmanned aerial vehicle holder quick release structure is proposed. UTILITY MODEL CONTENTS
[0005] The utility model aims at the above-mentioned technical problem, provides an unmanned aerial vehicle holder quick release structure, and achieves the use effect that the user can quickly release the unmanned aerial vehicle holder and self-adjust the angle.
[0006] The technical scheme adopted by the utility model is as follows:
[0007] An unmanned aerial vehicle holder quick release structure comprises a quick release structure main body, an installation plate is installed on the upper surface of the quick release structure main body, a plug-in plate is limitedly plugged in the inner side surface of the quick release structure main body, a clamping rod is limitedly clamped on the inner side surface of the plug-in plate, and a clamping plug-in rod is limitedly plugged in the inner circle surface of the clamping rod.
[0008] The side surface of the clamping rod is fixedly connected with a support arm, the side surface of the support arm is provided with a holder main body, the bottom surface of the quick release structure main body is fixedly connected with a limiting block, the side surface of the limiting block is limitedly clamped with a nut, the inner ring surface of the nut is limitedly inserted with a threaded rod, the bottom surface of the threaded rod is provided with a knob handle, and the side surface of the clamping rod is fixedly connected with a first motor.
[0009] Preferably, the upper surface of the mounting plate is provided with a plurality of mounting openings.
[0010] The above technical scheme has the mounting openings, which can facilitate the user to install the mounting plate with bolts.
[0011] Preferably, the side surface of the quick release structure main body is provided with a clamping opening, and the size of the clamping opening and the plug-in plate matches each other.
[0012] The above technical scheme has the clamping openings, which can facilitate the user to plug in the plug-in plates.
[0013] Preferably, the bottom surface of the threaded rod is provided with a knob handle, and the knob handle is connected through the threaded rod and the nut.
[0014] The above technical scheme has the knob handle connected through the threaded rod and the nut, which can facilitate the user to connect the knob handle and the nut.
[0015] Preferably, the nut is connected between the limiting block and the quick release structure main body, and the limiting block is symmetrically arranged with the vertical center line of the nut as the axis of symmetry.
[0016] The above technical scheme has the limiting block symmetrically arranged with the vertical center line of the nut as the axis of symmetry, which can facilitate the user to stably install the nut on the quick release structure main body.
[0017] Preferably, the upper surface of the clamping plug-in rod is fixedly connected with a limiting plate, and the structure of the limiting plate and the clamping plug-in rod matches each other.
[0018] The above technical scheme has the limiting plate, which can facilitate the user to limit the clamping plug-in rod.
[0019] Preferably, the output shaft top end of the first motor is fixedly sleeved with an adjusting roller, and the adjusting roller is in contact with the outer surface of the clamping plug-in rod.
[0020] Adopting the above technical scheme, the adjusting roller in contact with the outer surface of the clamping insertion rod can facilitate the user to drive the clamping insertion rod
[0021] The utility model discloses technical effect achieved is:
[0022] The utility model discloses through the mutual cooperation and use of article quick -detach structure main part, mounting panel, installation opening, clamping opening, insertion board, limit board, clamping rod, support arm, holder main part, first motor, nut, limit block, threaded rod, knob handle, clamping insertion rod and adjusting roller, can conveniently use quick -detach of unmanned aerial vehicle holder, when the user needs quick -detach of holder, the user needs to twist knob handle, and the user can drive threaded rod in this way, so that the user can take off threaded rod on the nut, after the user takes off the nut, the user needs to push forward insertion board and takes off on quick -detach structure main part, and the user can quick detach of holder in this way, satisfy the use demand of quick -detach of holder of the user,
[0023] The utility model discloses through the first motor of the side surface fixed connection of insertion board, and after the user opens first motor, the user can drive the adjusting roller of setting, therefore the user can drive the clamping insertion rod and rotate on the clamping rod, so that the user can use angle adjustment to the holder main part of setting whole, satisfy the use demand of high -efficient angle fine adjustment of holder of the user. DRAWINGS
[0024] Figure 1 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure front view is provided for the utility model,
[0025] Figure 2 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure back view is provided for the utility model,
[0026] Figure 3 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure side sectional view is provided for the utility model,
[0027] Figure 4 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure is provided for the utility model, Figure 2 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure side sectional view is provided for the utility model,
[0028] Figure 5 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure side sectional view is provided for the utility model, Figure 3 The utility model discloses a quick -detach structure of unmanned aerial vehicle holder structure side sectional view is provided for the utility model,
[0029] In the drawings, the component list represented by each sign is as follows:
[0030] 1, quick release structure main body; 2, mounting plate; 3, mounting opening; 4, clamping opening; 5, plug-in plate; 6, limiting plate; 7, clamping rod; 8, support arm; 9, holder main body; 10, first motor; 11, nut; 12, limiting block; 13, threaded rod; 14, knob handle; 15, clamping plug-in rod; 16, adjusting roller. DETAILED DESCRIPTION
[0031] In order to make the purpose and advantages of the utility model more clear and obvious, the following will be combined with examples to specifically explain the utility model. It should be understood that the following text is only used to describe one or several specific embodiments of the utility model, and does not strictly limit the protection scope of the utility model specifically requested.
[0032] As shown in Figures 1-5 A quick release structure of a holder of a unmanned aerial vehicle, including quick release structure main body 1, the upper surface of quick release structure main body 1 is provided with mounting plate 2, the inner side surface of quick release structure main body 1 is limitedly inserted with plug-in plate 5, and the inner side surface of plug-in plate 5 is limitedly clamped with clamping rod 7.
[0033] The upper surface of mounting plate 2 is provided with mounting opening 3, and the number of mounting opening 3 is multiple, the multiple mounting opening 3 can be conveniently used by users with bolts to install mounting plate 2, the side surface of quick release structure main body 1 is provided with clamping opening 4, and the size of clamping opening 4 and plug-in plate 5 is matched with each other, and the size of clamping opening 4 and plug-in plate 5 is matched with each other, which can be conveniently used by users to plug-in plate 5.
[0034] As shown in Figures 1-5 The inner circle surface of clamping rod 7 is limitedly inserted with clamping plug-in rod 15, the side surface of clamping rod 7 is fixedly connected with support arm 8, the side surface of support arm 8 is provided with holder main body 9, the bottom surface of quick release structure main body 1 is fixedly connected with limiting block 12, the side surface of limiting block 12 is limitedly clamped with nut 11, the inner circle surface of nut 11 is limitedly inserted with threaded rod 13, the bottom surface of threaded rod 13 is provided with knob handle 14, and the side surface of clamping rod 7 is fixedly connected with first motor 10.
[0035] The bottom surface of threaded rod 13 is provided with knob handle 14, and knob handle 14 is connected between threaded rod 13 and nut 11, knob handle 14 connected between threaded rod 13 and nut 11 can be conveniently connected between knob handle 14 and nut 11 by users, nut 11 is connected between limiting block 12 and quick release structure main body 1, and limiting block 12 is symmetrically arranged with the vertical center line of nut 11 as the axis of symmetry.
[0036] According to the above structure, when the user needs to quickly disassemble the holder, the user needs to twist the knob handle 14, so that the user can drive the threaded rod 13, so that the user can take off the threaded rod 13 on the nut 11, after the user takes off the nut 11, the user needs to push the plug-in plate 5 forward and take off on the quick disassembly structure main body 1, so that the user can quickly disassemble the holder, the first motor 10 is fixedly connected to the side surface of the plug-in plate 5, and after the user opens the first motor 10, the user can drive the adjusting roller 16, so that the user can drive the clamping rod 15 to rotate on the clamping rod 7, so that the user can adjust the use angle of the holder main body 9 as a whole.
[0037] The above is only the preferred embodiment of the present application, it should be pointed out that for the ordinary skilled in the art, without departing from the principles of the present application, can make a number of improvements and refinements, these improvements and refinements should also be considered as the protection scope of the present application. The structure, device and operation method not specifically described and explained in the present application, if no special description and limitation, are implemented according to the conventional means in the art.
Claims
1. A quick release structure of a UAV gimbal, comprising a quick release structure main body (1), characterized in that, The upper surface of the quick release structure body (1) is provided with a mounting plate (2), the inner surface of the quick release structure body (1) is limitedly inserted with a plug-in plate (5), the inner surface of the plug-in plate (5) is limitedly connected with a clamping rod (7), the inner surface of the clamping rod (7) is limitedly inserted with a clamping plug-in rod (15); The side surface of the clamping rod (7) is fixedly connected with a support arm (8), the side surface of the support arm (8) is provided with a holder body (9), the bottom surface of the quick release structure body (1) is fixedly connected with a limiting block (12), the side surface of the limiting block (12) is limitedly connected with a nut (11), the inner surface of the nut (11) is limitedly inserted with a threaded rod (13), the bottom surface of the threaded rod (13) is provided with a knob handle (14), and the side surface of the clamping rod (7) is fixedly connected with a first motor (10).
2. The quick release structure of claim 1, wherein, The upper surface of the mounting plate (2) is provided with a mounting opening (3), and the mounting opening (3) is provided with a plurality of mounting openings.
3. The quick release structure of claim 1, wherein, The side surface of the quick release structure body (1) is provided with a clamping opening (4), and the size of the clamping opening (4) and the plug-in plate (5) is matched with each other.
4. The quick release structure of claim 1, wherein, The bottom surface of the threaded rod (13) is provided with a knob handle (14), and the knob handle (14) is connected through the threaded rod (13) and the nut (11).
5. The unmanned aerial vehicle holder quick release structure of claim 1, wherein, The nut (11) is connected between the limiting block (12) and the quick release structure body (1), and the limiting block (12) is symmetrically arranged with the vertical center line of the nut (11) as the axis of symmetry.
6. The quick release structure of claim 1, wherein, The upper surface of the clamping plug-in rod (15) is fixedly connected with a limiting plate (6), and the structure of the limiting plate (6) and the clamping plug-in rod (15) is matched with each other.
7. The unmanned aerial vehicle gimbal quick release structure of claim 1, wherein, The output shaft top end of the first motor (10) is fixedly sleeved with an adjusting roller (16), and the adjusting roller (16) and the outer surface of the clamping plug-in rod (15) are in contact connection.
Citation Information
Patent Citations
Novel unmanned aerial vehicle holder
CN219215406U