CN219026009U - Unmanned aerial vehicle screw perforating device - Google Patents

Unmanned aerial vehicle screw perforating device Download PDF

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CN219026009U
CN219026009U CN202223524672.1U CN202223524672U CN219026009U CN 219026009 U CN219026009 U CN 219026009U CN 202223524672 U CN202223524672 U CN 202223524672U CN 219026009 U CN219026009 U CN 219026009U
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propeller
aerial vehicle
unmanned aerial
console
punching device
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吴曼
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Suqian Shuangying Intelligent Electronic Technology Co ltd
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Suqian Shuangying Intelligent Electronic Technology Co ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/10Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working

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Abstract

The utility model relates to the technical field of drilling, in particular to an unmanned aerial vehicle propeller punching device, which comprises an operation table and a propeller body, wherein a chute is formed in the upper surface of the operation table, a circular groove is formed in the upper surface of the operation table, a circular ring support member is fixedly arranged in the circular groove, the propeller body is placed on the circular ring support member, and a clamping structure is arranged on the operation table and comprises a clamping plate and a threaded rod. According to the unmanned aerial vehicle screw punching device, the two slide bars are driven to move close to each other or away from each other through rotation of the threaded rods, the two clamping plates are driven to move close to each other through the mutual close movement of the two slide bars, so that the gap between the two clamping plates is gradually reduced, the screw body can be fastened, and the punching operation can be directly performed at the moment.

Description

一种无人机螺旋桨打孔装置A drone propeller drilling device

技术领域technical field

本实用新型涉及钻孔技术领域,特别是涉及一种无人机螺旋桨打孔装置。The utility model relates to the technical field of drilling, in particular to an unmanned aerial vehicle propeller drilling device.

背景技术Background technique

钻孔是指用钻头在实体材料上加工出孔的操作。这里讲述了勘探工作里的钻孔工作,以及钻孔需要的辅助工具以及部分应急措施方法。Drilling refers to the operation of machining a hole in a solid material with a drill. Here is a description of the drilling work in the exploration work, as well as the auxiliary tools needed for drilling and some emergency measures.

无人机螺旋桨在加工过程中,需要用到打孔装置,目前,市场上的无人机螺旋桨打孔装置在实际使用过程中,对于螺旋桨的固定较为麻烦,导致对螺旋桨打孔较为不便,且现有的无人机螺旋桨打孔装置不便于对打孔过程中产生的碎屑进行收集,还需人工进行清理,使用较为不便,为此,我们提出一种无人机螺旋桨打孔装置来解决上述问题。During the processing of the UAV propeller, a drilling device is required. At present, in the actual use of the UAV propeller drilling device on the market, it is more troublesome to fix the propeller, which makes it more inconvenient to drill holes on the propeller, and The existing UAV propeller drilling device is not convenient to collect the debris generated during the drilling process, and manual cleaning is required, which is inconvenient to use. Therefore, we propose a UAV propeller drilling device to solve the problem. above question.

实用新型内容Utility model content

为了克服现有技术的不足,本实用新型提供一种无人机螺旋桨打孔装置。In order to overcome the deficiencies of the prior art, the utility model provides a drilling device for the propeller of an unmanned aerial vehicle.

为解决上述技术问题,本实用新型提供如下技术方案:一种无人机螺旋桨打孔装置,包括操作台和螺旋桨本体,所述操作台的上表面开设有滑槽,所述操作台的上表面开设有圆形槽,所述圆形槽内固定安装有圆环支撑件,所述螺旋桨本体放置在圆环支撑件上,所述操作台上设置有夹持结构,所述夹持结构包括夹持板和螺纹杆,所述夹持板的数量为两个,两个所述夹持板均设置在操作台的上方,所述螺旋桨本体的中部处于两个夹持板之间,两个所述夹持板的端部均固定安装有滑杆,两个所述滑杆均滑动设置在滑槽内,所述螺纹杆转动安装在操作台内,并活动贯穿滑槽,所述操作台的下方设置有收集结构,所述收集结构包括箱体和收集盒,所述箱体内设置有吸尘机,所述收集盒滑动设置在箱体内,所述操作台底端的四个角均固定安装有支撑腿,所述螺纹杆的端部固定安装有手轮。In order to solve the above-mentioned technical problems, the utility model provides the following technical solutions: a UAV propeller drilling device, including an operating table and a propeller body, the upper surface of the operating table is provided with a chute, and the upper surface of the operating table is A circular groove is opened, and a ring support is fixedly installed in the circular groove, the propeller body is placed on the ring support, and a clamping structure is provided on the operating table, and the clamping structure includes a clamp holding plate and threaded rod, the number of the holding plate is two, and the two holding plates are arranged on the top of the console, the middle part of the propeller body is between the two holding plates, and the two holding plates The ends of the clamping plates are all fixedly installed with slide bars, and the two slide bars are all slidably arranged in the chute, and the threaded rod is rotatably installed in the operating table and moves through the chute. A collection structure is arranged below, the collection structure includes a box body and a collection box, a vacuum cleaner is arranged in the box body, the collection box is slidably arranged in the box body, and the four corners at the bottom of the operation table are fixedly installed with The supporting leg is fixedly equipped with a hand wheel at the end of the threaded rod.

作为本实用新型的一种优选技术方案,所述圆形槽的内壁底面开设有与箱体内腔相通的漏孔,两个所述夹持板相背离的两端均固定安装有限位杆。As a preferred technical solution of the present invention, the bottom surface of the inner wall of the circular groove is provided with a leakage hole communicating with the inner cavity of the box, and the two ends of the two clamping plates facing away from each other are fixedly equipped with limit rods.

作为本实用新型的一种优选技术方案,所述操作台上端的两侧均固定安装有挡板,两个所述限位杆分别活动贯穿两个挡板。As a preferred technical solution of the present invention, baffles are fixedly installed on both sides of the upper end of the console, and the two limit rods move through the two baffles respectively.

作为本实用新型的一种优选技术方案,两个所述滑杆的表面均开设有螺纹孔,两个所述螺纹孔的螺纹方向相反,所述螺纹杆贯穿两个螺纹孔。As a preferred technical solution of the present invention, the surfaces of the two sliding rods are provided with threaded holes, the threading directions of the two threaded holes are opposite, and the threaded rods penetrate through the two threaded holes.

作为本实用新型的一种优选技术方案,所述箱体固定安装在操作台的底端,所述收集盒内腔嵌入有过滤网,所述收集盒的端部固定安装有把手。As a preferred technical solution of the utility model, the box body is fixedly installed at the bottom end of the console, a filter screen is embedded in the inner cavity of the collection box, and a handle is fixedly installed at the end of the collection box.

与现有技术相比,本实用新型能达到的有益效果是:Compared with the prior art, the beneficial effects that the utility model can achieve are:

1、通过螺纹杆的转动会带动两个滑杆相互靠近或相互远离移动,通过两个滑杆相互靠近移动会调动两个夹持板相互靠近移动,使得两个夹持板之间的间隙逐渐缩小,从而可将螺旋桨本体紧固住,此时即可直接进行打孔作业,该无人机螺旋桨打孔装置通过对螺旋桨本体进行固定,方便对螺旋桨本体进行打孔。1. The rotation of the threaded rod will drive the two sliders to move closer to each other or move away from each other. The movement of the two sliders closer to each other will mobilize the two clamping plates to move closer to each other, so that the gap between the two clamping plates gradually Shrunk down, so that the propeller body can be fastened, and the drilling operation can be carried out directly at this time. The drone propeller drilling device fixes the propeller body to facilitate drilling of the propeller body.

2、启动吸尘机,使得对螺旋桨本体打孔过程中产生的碎屑落入至圆形槽内,并从漏孔排出至收集盒内,使用者向外移动把手即可将收集盒内收集的碎屑取出,无需人工清理打孔过程中产生的碎屑,操作更加便捷,通过两个夹持板相背离的两端均固定安装有限位杆,两个限位杆分别活动贯穿挡板,对夹持板移动过程中起到了限位作用,使得两个夹持板移动更加稳定,保证了该夹持结构的稳定运行,提高了该无人机螺旋桨打孔装置的实用性。2. Start the vacuum cleaner so that the debris generated during the drilling process of the propeller body falls into the circular groove and is discharged from the leak hole into the collection box. The user can move the handle outward to collect the debris in the collection box. There is no need to manually clean up the debris generated during the drilling process, and the operation is more convenient. The two ends of the two clamping plates are fixed with limit rods, and the two limit rods move through the baffle respectively. It plays a position-limiting role in the moving process of the clamping plate, making the movement of the two clamping plates more stable, ensuring the stable operation of the clamping structure, and improving the practicability of the UAV propeller drilling device.

附图说明Description of drawings

图1为本实用新型无人机螺旋桨打孔装置的结构示意图;Fig. 1 is the structural representation of the utility model unmanned aerial vehicle propeller punching device;

图2为本实用新型圆环支撑件的结构示意图;Fig. 2 is the structural representation of the utility model circular support;

图3为本实用新型箱体的结构示意图;Fig. 3 is the structural representation of the utility model casing;

图4为本实用新型图1中A处放大的结构示意图。Fig. 4 is an enlarged structural schematic diagram of A in Fig. 1 of the present utility model.

其中:1、操作台;11、滑槽;12、圆形槽;13、挡板;14、支撑腿;2、螺旋桨本体;3、圆环支撑件;4、夹持板;41、滑杆;42、限位杆;5、螺纹杆;51、手轮;6、箱体;61、吸尘机;7、收集盒;71、过滤网;72、把手。Among them: 1. Console; 11. Chute; 12. Circular groove; 13. Baffle; 14. Support leg; 2. Propeller body; 3. Ring support; 4. Clamping plate; 41. Slider ; 42, limit rod; 5, threaded rod; 51, hand wheel; 6, cabinet; 61, vacuum cleaner; 7, collection box; 71, filter screen; 72, handle.

具体实施方式Detailed ways

为了使本实用新型实现的技术手段、创作特征、达成目的与功效易于明白了解,下面结合具体实施例,进一步阐述本实用新型,但下述实施例仅仅为本实用新型的优选实施例,并非全部。基于实施方式中的实施例,本领域技术人员在没有做出创造性劳动的前提下所获得其它实施例,都属于本实用新型的保护范围。下述实施例中的实验方法,如无特殊说明,均为常规方法,下述实施例中所用的材料、试剂等,如无特殊说明,均可从商业途径得到。In order to make the technical means, creative features, goals and effects of the utility model realized easy to understand, the utility model will be further elaborated below in conjunction with specific examples, but the following examples are only preferred embodiments of the utility model, not all . Based on the examples in the implementation manners, other examples obtained by those skilled in the art without making creative efforts all belong to the protection scope of the present utility model. The experimental methods in the following examples, unless otherwise specified, are conventional methods, and the materials, reagents, etc. used in the following examples, unless otherwise specified, can be obtained from commercial sources.

如图1、图2、图3和图4所示,一种无人机螺旋桨打孔装置,包括操作台1和螺旋桨本体2,操作台1的上表面开设有滑槽11,操作台1的上表面开设有圆形槽12,圆形槽12内固定安装有圆环支撑件3,螺旋桨本体2放置在圆环支撑件3上,操作台1上设置有夹持结构,夹持结构包括夹持板4和螺纹杆5,夹持板4的数量为两个,两个夹持板4均设置在操作台1的上方,螺旋桨本体2的中部处于两个夹持板4之间,两个夹持板4的端部均固定安装有滑杆41,两个滑杆41均滑动设置在滑槽11内,螺纹杆5转动安装在操作台1内,并活动贯穿滑槽11,操作台1的下方设置有收集结构,收集结构包括箱体6和收集盒7,箱体6内设置有吸尘机61,收集盒7滑动设置在箱体6内,操作台1底端的四个角均固定安装有支撑腿14,螺纹杆5的端部固定安装有手轮51,圆形槽12的内壁底面开设有与箱体6内腔相通的漏孔,两个夹持板4相背离的两端均固定安装有限位杆42,操作台1上端的两侧均固定安装有挡板13,两个限位杆42分别活动贯穿两个挡板13,将螺旋桨本体2放置在圆环支撑件3上,接着扭动手轮51使螺纹杆5进行转动,通过螺纹杆5的转动会带动两个滑杆41相互靠近或相互远离移动,通过两个滑杆41相互靠近移动会调动两个夹持板4相互靠近移动,使得两个夹持板4之间的间隙逐渐缩小,从而可将螺旋桨本体2紧固住,此时即可直接进行打孔作业,该无人机螺旋桨打孔装置通过对螺旋桨本体2进行固定,方便对螺旋桨本体2进行打孔,在对螺旋桨本体2打孔过程中,启动吸尘机61,使得对螺旋桨本体2打孔过程中产生的碎屑落入至圆形槽12内,并从漏孔排出至收集盒7内,使用者向外移动把手72即可将收集盒7内收集的碎屑取出,无需人工清理打孔过程中产生的碎屑,操作更加便捷,通过两个夹持板4相背离的两端均固定安装有限位杆42,两个限位杆42分别活动贯穿挡板13,对夹持板4移动过程中起到了限位作用,使得两个夹持板4移动更加稳定,保证了该夹持结构的稳定运行,提高了该无人机螺旋桨打孔装置的实用性,两个滑杆41的表面均开设有螺纹孔,两个螺纹孔的螺纹方向相反,螺纹杆5贯穿两个螺纹孔,箱体6固定安装在操作台1的底端,收集盒7内腔嵌入有过滤网71,收集盒7的端部固定安装有把手72。As shown in Fig. 1, Fig. 2, Fig. 3 and Fig. 4, a kind of unmanned aerial vehicle propeller punching device comprises operating table 1 and propeller body 2, and the upper surface of operating table 1 is provided with chute 11, and the upper surface of operating table 1 A circular groove 12 is opened on the upper surface, and a circular support 3 is fixedly installed in the circular groove 12. The propeller body 2 is placed on the circular support 3, and a clamping structure is provided on the console 1. The clamping structure includes a clamp Holding plate 4 and threaded rod 5, the quantity of clamping plate 4 is two, and two clamping plates 4 are all arranged on the top of console 1, and the middle part of propeller body 2 is between two clamping plates 4, two The ends of the clamping plate 4 are all fixedly equipped with slide bars 41, and the two slide bars 41 are all slidably arranged in the chute 11. The threaded rod 5 is rotatably installed in the console 1, and moves through the chute 11. The console 1 A collection structure is provided below the body, the collection structure includes a box body 6 and a collection box 7, a vacuum cleaner 61 is arranged in the box body 6, the collection box 7 is slidably arranged in the box body 6, and the four corners of the bottom end of the console 1 are all fixed The supporting leg 14 is installed, the end of the threaded rod 5 is fixedly equipped with a hand wheel 51, the bottom surface of the inner wall of the circular groove 12 is provided with a leakage hole communicating with the inner cavity of the box body 6, and the two ends of the two clamping plates 4 are away from each other. Both limit rods 42 are fixedly installed, and baffles 13 are fixedly installed on both sides of the upper end of the console 1. The two limit rods 42 move through the two baffles 13 respectively, and the propeller body 2 is placed on the ring support 3. , then twist the handwheel 51 to rotate the threaded rod 5, the rotation of the threaded rod 5 will drive the two slide bars 41 to move closer to each other or move away from each other, and the two slide bars 41 will move closer to each other to move the two clamping plates 4 move closer to each other, so that the gap between the two clamping plates 4 gradually narrows, so that the propeller body 2 can be fastened, and the drilling operation can be directly carried out at this time. The main body 2 is fixed to facilitate drilling of the propeller main body 2. During the process of drilling the propeller main body 2, start the vacuum cleaner 61 so that the debris generated during the drilling of the propeller main body 2 falls into the circular groove 12 and discharged from the leakage hole into the collection box 7, the user can move the handle 72 outward to take out the debris collected in the collection box 7, without manually cleaning the debris generated during the punching process, the operation is more convenient, through The opposite ends of the two clamping plates 4 are fixedly equipped with limit rods 42, and the two limit rods 42 move through the baffle plate 13 respectively, which play a position-limiting role in the moving process of the clamping plates 4, so that the two clamps The movement of the holding plate 4 is more stable, which ensures the stable operation of the clamping structure and improves the practicability of the propeller drilling device of the drone. The surfaces of the two slide bars 41 are all provided with threaded holes, and the threads of the two threaded holes Direction is opposite, threaded rod 5 runs through two threaded holes, box body 6 is fixedly installed on the bottom end of console 1, and collection box 7 inner cavity is embedded with filter screen 71, and the end of collection box 7 is fixedly installed with handle 72.

使用时,将螺旋桨本体2放置在圆环支撑件3上,接着扭动手轮51使螺纹杆5进行转动,通过螺纹杆5的转动会带动两个滑杆41相互靠近或相互远离移动,通过两个滑杆41相互靠近移动会调动两个夹持板4相互靠近移动,使得两个夹持板4之间的间隙逐渐缩小,从而可将螺旋桨本体2紧固住,此时即可直接进行打孔作业,该无人机螺旋桨打孔装置通过对螺旋桨本体2进行固定,方便对螺旋桨本体2进行打孔,在对螺旋桨本体2打孔过程中,启动吸尘机61,使得对螺旋桨本体2打孔过程中产生的碎屑落入至圆形槽12内,并从漏孔排出至收集盒7内,使用者向外移动把手72即可将收集盒7内收集的碎屑取出,无需人工清理打孔过程中产生的碎屑,操作更加便捷,通过两个夹持板4相背离的两端均固定安装有限位杆42,两个限位杆42分别活动贯穿挡板13,对夹持板4移动过程中起到了限位作用,使得两个夹持板4移动更加稳定,保证了该夹持结构的稳定运行,提高了该无人机螺旋桨打孔装置的实用性。During use, the propeller body 2 is placed on the ring support member 3, and then the handwheel 51 is twisted to rotate the threaded rod 5. The rotation of the threaded rod 5 will drive the two slide rods 41 to move closer to each other or move away from each other. The two slide bars 41 moving closer to each other will mobilize the two clamping plates 4 to move closer to each other, so that the gap between the two clamping plates 4 will gradually narrow, so that the propeller body 2 can be fastened, and the Punching operation, the UAV propeller punching device is convenient to punch the propeller body 2 by fixing the propeller body 2, and in the process of punching the propeller body 2, start the vacuum cleaner 61, so that the propeller body 2 The debris generated during the drilling process falls into the circular groove 12 and is discharged from the leak hole into the collection box 7. The user can move the handle 72 outward to take out the debris collected in the collection box 7 without manual labor. Clean up the debris generated during the drilling process, and the operation is more convenient. The two ends of the two clamping plates 4 are fixedly installed with a limit rod 42, and the two limit rods 42 move through the baffle plate 13 respectively, and the clamping The plate 4 plays a position-limiting role in the moving process, making the movement of the two clamping plates 4 more stable, ensuring the stable operation of the clamping structure, and improving the practicability of the UAV propeller drilling device.

上面结合附图对本实用新型的实施方式作了详细说明,但是本实用新型并不限于此,在所属技术领域的技术人员所具备的知识范围内,在不脱离本实用新型宗旨的前提下还可以作出各种变化。Above, the embodiment of the present utility model has been described in detail in conjunction with the accompanying drawings, but the present utility model is not limited thereto. Make various changes.

Claims (6)

1.一种无人机螺旋桨打孔装置,包括操作台(1)和螺旋桨本体(2),其特征在于,所述操作台(1)的上表面开设有滑槽(11),所述操作台(1)的上表面开设有圆形槽(12),所述圆形槽(12)内固定安装有圆环支撑件(3),所述螺旋桨本体(2)放置在圆环支撑件(3)上,所述操作台(1)上设置有夹持结构,所述夹持结构包括夹持板(4)和螺纹杆(5),所述夹持板(4)的数量为两个,两个所述夹持板(4)均设置在操作台(1)的上方,所述螺旋桨本体(2)的中部处于两个夹持板(4)之间,两个所述夹持板(4)的端部均固定安装有滑杆(41),两个所述滑杆(41)均滑动设置在滑槽(11)内,所述螺纹杆(5)转动安装在操作台(1)内,并活动贯穿滑槽(11),所述操作台(1)的下方设置有收集结构,所述收集结构包括箱体(6)和收集盒(7),所述箱体(6)内设置有吸尘机(61),所述收集盒(7)滑动设置在箱体(6)内。1. A drone propeller punching device, comprising an operating table (1) and a propeller body (2), is characterized in that, the upper surface of the operating table (1) is provided with a chute (11), and the operation The upper surface of the platform (1) is provided with a circular groove (12), and a circular support (3) is fixedly installed in the circular groove (12), and the propeller body (2) is placed on the circular support ( 3), the console (1) is provided with a clamping structure, the clamping structure includes a clamping plate (4) and a threaded rod (5), the number of the clamping plate (4) is two , the two clamping plates (4) are all arranged above the console (1), the middle part of the propeller body (2) is between the two clamping plates (4), and the two clamping plates The ends of (4) are all fixedly equipped with slide bars (41), and the two slide bars (41) are all slidably arranged in the chute (11), and the threaded rods (5) are rotatably mounted on the console (1). ), and move through the chute (11), a collection structure is provided below the operating table (1), the collection structure includes a box (6) and a collection box (7), the box (6) A dust collector (61) is arranged inside, and the collection box (7) is slidably arranged in the box body (6). 2.根据权利要求1所述的一种无人机螺旋桨打孔装置,其特征在于,所述操作台(1)底端的四个角均固定安装有支撑腿(14),所述螺纹杆(5)的端部固定安装有手轮(51)。2. a kind of unmanned aerial vehicle propeller punching device according to claim 1, is characterized in that, four corners of described console (1) bottom end are all fixedly equipped with supporting legs (14), and described threaded rod ( 5) The end is fixedly equipped with handwheel (51). 3.根据权利要求1所述的一种无人机螺旋桨打孔装置,其特征在于,所述圆形槽(12)的内壁底面开设有与箱体(6)内腔相通的漏孔,两个所述夹持板(4)相背离的两端均固定安装有限位杆(42)。3. A kind of unmanned aerial vehicle propeller punching device according to claim 1, is characterized in that, the inner wall bottom surface of described circular groove (12) offers the leakage hole that communicates with casing (6) lumen, two Limiting rods (42) are fixedly installed at opposite ends of each of the clamping plates (4). 4.根据权利要求3所述的一种无人机螺旋桨打孔装置,其特征在于,所述操作台(1)上端的两侧均固定安装有挡板(13),两个所述限位杆(42)分别活动贯穿两个挡板(13)。4. A kind of unmanned aerial vehicle propeller punching device according to claim 3, is characterized in that, the both sides of described console (1) upper end are all fixedly installed with baffle plate (13), two described position-limiting The rod (42) moves through the two baffle plates (13) respectively. 5.根据权利要求1所述的一种无人机螺旋桨打孔装置,其特征在于,两个所述滑杆(41)的表面均开设有螺纹孔,两个所述螺纹孔的螺纹方向相反,所述螺纹杆(5)贯穿两个螺纹孔。5. A kind of unmanned aerial vehicle propeller punching device according to claim 1, is characterized in that, the surface of two described slide bars (41) is all provided with threaded hole, and the thread direction of two described threaded holes is opposite , the threaded rod (5) runs through two threaded holes. 6.根据权利要求1所述的一种无人机螺旋桨打孔装置,其特征在于,所述箱体(6)固定安装在操作台(1)的底端,所述收集盒(7)内腔嵌入有过滤网(71),所述收集盒(7)的端部固定安装有把手(72)。6. A kind of unmanned aerial vehicle propeller punching device according to claim 1, is characterized in that, described casing (6) is fixedly installed on the bottom end of console (1), and in described collection box (7) A filter screen (71) is embedded in the cavity, and a handle (72) is fixedly installed at the end of the collection box (7).
CN202223524672.1U 2022-12-28 2022-12-28 Unmanned aerial vehicle screw perforating device Expired - Fee Related CN219026009U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223524672.1U CN219026009U (en) 2022-12-28 2022-12-28 Unmanned aerial vehicle screw perforating device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223524672.1U CN219026009U (en) 2022-12-28 2022-12-28 Unmanned aerial vehicle screw perforating device

Publications (1)

Publication Number Publication Date
CN219026009U true CN219026009U (en) 2023-05-16

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202223524672.1U Expired - Fee Related CN219026009U (en) 2022-12-28 2022-12-28 Unmanned aerial vehicle screw perforating device

Country Status (1)

Country Link
CN (1) CN219026009U (en)

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