CN111577056A - A rotary drive hangar door device - Google Patents
A rotary drive hangar door device Download PDFInfo
- Publication number
- CN111577056A CN111577056A CN202010440301.1A CN202010440301A CN111577056A CN 111577056 A CN111577056 A CN 111577056A CN 202010440301 A CN202010440301 A CN 202010440301A CN 111577056 A CN111577056 A CN 111577056A
- Authority
- CN
- China
- Prior art keywords
- hangar
- rotary drive
- door device
- hangar door
- hook
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/60—Power-operated mechanisms for wings using electrical actuators
- E05F15/603—Power-operated mechanisms for wings using electrical actuators using rotary electromotors
- E05F15/611—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings
- E05F15/63—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings operated by swinging arms
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/02—Suspension arrangements for wings for revolving wings
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/32—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing
- E06B3/325—Wings opening towards the outside
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/108—Application of doors, windows, wings or fittings thereof for buildings or parts thereof for hangars
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
- E05Y2900/132—Doors
Landscapes
- Engineering & Computer Science (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
Description
技术领域technical field
本发明涉及无人机技术领域,具体为一种旋转驱动机库门装置。The invention relates to the technical field of unmanned aerial vehicles, in particular to a rotary drive hangar door device.
背景技术Background technique
无人驾驶飞机简称“无人机”,英文缩写为“UAV”,是利用无线电遥控设备和自备的程序控制装置操纵的不载人飞机,或者由车载计算机完全地或间歇地自主地操作。与有人驾驶飞机相比,无人机往往更适合那些太“愚钝,肮脏或危险”的任务。无人机按应用领域,可分为军用与民用。军用方面,无人机分为侦察机和靶机。民用方面,无人机+行业应用,是无人机真正的刚需;目前在航拍、农业、植保、微型自拍、快递运输、灾难救援、观察野生动物、监控传染病、测绘、新闻报道、电力巡检、救灾、影视拍摄、制造浪漫等等领域的应用,大大的拓展了无人机本身的用途,发达国家也在积极扩展行业应用与发展无人机技术。Unmanned aerial vehicle is referred to as "unmanned aerial vehicle", and the English abbreviation is "UAV". Drones tend to be better suited for tasks that are too "dumb, dirty or dangerous" than manned aircraft. UAVs can be divided into military and civilian according to the application field. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civil use, drones + industrial applications are the real needs of drones; currently, they are used in aerial photography, agriculture, plant protection, miniature selfies, express transportation, disaster rescue, observation of wildlife, monitoring of infectious diseases, surveying and mapping, news reports, and electric power patrols. The application in the fields of inspection, disaster relief, film and television shooting, manufacturing romance, etc. has greatly expanded the use of the drone itself, and developed countries are also actively expanding industrial applications and developing drone technology.
然而,现有的无人机在使用的过程中存在以下的问题:(1)现有的无人机机体结构较为固定,一般由外壳和安装在内部的元器件组成,在使用的过程中需要人工通过专门的工具打开机体,不放在拆卸和维修,缺乏相应的开仓机构;(2)无人机机体顶部顶部一般由塑料材质的外壳进行包裹,当碎石或是冰块坠落至机体顶部时,容易导致机体外壳出现损坏,抗压能力较差。为此,需要设计相应的技术方案解决存在的技术问题。However, the existing UAVs have the following problems in the process of use: (1) The structure of the existing UAVs is relatively fixed, generally composed of a shell and components installed in the interior. The body is manually opened by special tools, not for disassembly and maintenance, and there is no corresponding opening mechanism; (2) The top of the drone body is generally wrapped by a plastic shell, and when gravel or ice falls to the body When it is on the top, it is easy to cause damage to the body shell, and the pressure resistance is poor. To this end, it is necessary to design corresponding technical solutions to solve the existing technical problems.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种旋转驱动机库门装置,解决了背景技术中所提出的问题,满足实际使用需求。The purpose of the present invention is to provide a rotary drive hangar door device, which solves the problems raised in the background art and satisfies the actual use requirements.
为实现上述目的,本发明提供如下技术方案:一种旋转驱动机库门装置,包括机架,所述机架包括机体框架和固定在机体框架上的机体外壳,所述机架的内部形成有容纳腔且顶部开设有机舱口,所述机舱口处对称安装有两组呈倾斜设置的机库门,两组所述机库门的正下方设置有安装座,所述安装座固定在容纳腔内壁上且表面垂直设置有连接杆,所述连接杆的上端开设有穿口,所述穿口内水平穿插有铰接轴,所述铰接轴的上端固定连接有旋转臂,所述旋转臂的顶部与机库门的内壁铰接且末端安装有传动副,所述传动副包括从动轮和位于从动轮内侧的传动轮,所述从动轮末端固定有与铰接轴同轴的旋转轴,所述从动轮和传动轮啮合连接,所述传动轮的下方还安装有驱动装置,所述驱动装置包括安装板和固定在安装板上的驱动电机,所述驱动电机的动力输出端安装有驱动轮,所述驱动轮与传动轮啮合连接。In order to achieve the above purpose, the present invention provides the following technical solutions: a rotary drive hangar door device, comprising a frame, the frame includes a body frame and a body shell fixed on the body frame, the interior of the frame is formed with The accommodating cavity is provided with an organic hatch at the top. Two sets of inclined hangar doors are symmetrically installed at the hatches of the locomotive. The two sets of hangar doors are provided with mounting seats directly under the two sets of hangar doors, and the mounting seats are fixed in the accommodating cavity. A connecting rod is arranged vertically on the inner wall and on the surface, the upper end of the connecting rod is provided with a through hole, a hinge shaft is inserted horizontally in the through hole, and a rotating arm is fixedly connected to the upper end of the hinge shaft, and the top of the rotating arm is connected with the rotating arm. The inner wall of the hangar door is hinged and a transmission pair is installed at the end. The transmission pair includes a driven wheel and a transmission wheel located inside the driven wheel. The end of the driven wheel is fixed with a rotating shaft coaxial with the hinge shaft. The driven wheel and The transmission wheels are meshed and connected, and a driving device is also installed below the transmission wheel. The driving device includes a mounting plate and a driving motor fixed on the mounting plate. A driving wheel is installed at the power output end of the driving motor. The wheel is meshed with the transmission wheel.
作为本发明的一种优选实施方式,所述机体框架由若干组金属杆组成,若干组金属杆组成长方体结构,相邻两组所述金属杆之间设置有套管,所述金属杆的一端套嵌于套管内。As a preferred embodiment of the present invention, the body frame is composed of several groups of metal rods, and several groups of metal rods form a cuboid structure, and a sleeve is arranged between the adjacent two groups of the metal rods, and one end of the metal rods Nested in the casing.
作为本发明的一种优选实施方式,所述安装座包括固定在容纳腔底部的基座和对称安装在基座上的两组支撑块,所述连接杆和安装板均固定在支撑块上。As a preferred embodiment of the present invention, the mounting seat includes a base fixed on the bottom of the accommodating cavity and two sets of support blocks symmetrically mounted on the base, and the connecting rod and the mounting plate are both fixed on the support blocks.
作为本发明的一种优选实施方式,所述旋转臂整体呈倒置的钩状结构且包括上端的钩杆和位于下方的主杆,所述钩杆与主杆一体成型。As a preferred embodiment of the present invention, the rotating arm has an inverted hook-shaped structure as a whole and includes a hook rod at the upper end and a main rod located below, and the hook rod and the main rod are integrally formed.
作为本发明的一种优选实施方式,所述旋转臂上加工成型有加固机构,所述加固机构包括钩状板和均匀焊接于钩状板两侧的若干组加固板。As a preferred embodiment of the present invention, a reinforcement mechanism is formed on the rotating arm, and the reinforcement mechanism includes a hook-shaped plate and several groups of reinforcement plates uniformly welded on both sides of the hook-shaped plate.
作为本发明的一种优选实施方式,若干组所述加固板呈倾斜状设置在钩状板的两侧,所述加固机构整体呈鱼骨状结构。As a preferred embodiment of the present invention, several groups of the reinforcing plates are disposed on both sides of the hook-shaped plate in an inclined shape, and the reinforcing mechanism has a fishbone-like structure as a whole.
作为本发明的一种优选实施方式,所述机库门与旋转臂无相对运动,两组所述机库门处于闭合状态时,两组机库门之间形成人字形“屋脊”结构。As a preferred embodiment of the present invention, there is no relative movement between the hangar door and the rotating arm. When the two groups of the hangar doors are in a closed state, a herringbone "ridge" structure is formed between the two groups of hangar doors.
作为本发明的一种优选实施方式,所述驱动装置可以是电机也可以是电机与减速机的组合。As a preferred embodiment of the present invention, the driving device may be a motor or a combination of a motor and a reducer.
作为本发明的一种优选实施方式,所述传动副可以是齿轮副、链传动副和带传动副。As a preferred embodiment of the present invention, the transmission pair may be a gear pair, a chain transmission pair and a belt transmission pair.
与现有技术相比,本发明的有益效果如下:Compared with the prior art, the beneficial effects of the present invention are as follows:
1.本方案对无人机机体的结构进行了改进,在机体的顶部设计有可自动开启的机库门机构,当需要对机体进行检修时可以通过内部的驱动机构将机库门打开进行操作,该结构可以有效的提高无人机机体的智能化程度和自动化程度,并且采用的旋转式开启方式占用空间小且结构更加简单,使机体更加轻量化。1. This scheme improves the structure of the drone body. The top of the body is designed with a hangar door mechanism that can be opened automatically. When the body needs to be repaired, the hangar door can be opened through the internal drive mechanism for operation. , the structure can effectively improve the degree of intelligence and automation of the drone body, and the rotary opening method adopted takes up less space and has a simpler structure, making the body more lightweight.
2.将位于机体顶部的机库门设计为倾斜状机构,当顶部受到冲击时具有较好的卸力效果,并且配合内部的旋转臂可以达到更好的支撑效果。2. The hangar door located at the top of the body is designed as an inclined mechanism, which has a better unloading effect when the top is impacted, and can achieve a better support effect with the internal rotating arm.
附图说明Description of drawings
图1为本发明的整体结构图;Fig. 1 is the overall structure diagram of the present invention;
图2为本发明所述传动副与驱动装置连接结构图;Fig. 2 is the connection structure diagram of the transmission pair and the drive device according to the present invention;
图3为本发明所述旋转臂结构图。FIG. 3 is a structural diagram of the rotating arm according to the present invention.
图中:1-机体框架,2-机体外壳,3-容纳腔,4-机舱口,5-机库门,6-安装座,7-连接杆,8-穿口,9-铰接轴,10-旋转臂,11-传动副,12-从动轮,13-传动轮,14-旋转轴,15-驱动装置,16-安装板,17-驱动电机,18-驱动轮,19-金属杆,20-套管,21-基座,22-支撑块,23-钩杆,24-主杆,25-钩状板,26-加固板。In the picture: 1-body frame, 2-body shell, 3-accommodating cavity, 4-machine hatch, 5-hangar door, 6-mounting seat, 7-connecting rod, 8-through opening, 9-hinge shaft, 10 - Rotating arm, 11- transmission pair, 12- driven wheel, 13- driving wheel, 14- rotating shaft, 15- driving device, 16- mounting plate, 17- driving motor, 18- driving wheel, 19- metal rod, 20 -Sleeve, 21- Base, 22- Support block, 23- Hook rod, 24- Main rod, 25- Hook plate, 26- Reinforcement plate.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
请参阅图1-3,本发明提供一种技术方案:一种旋转驱动机库门装置,包括机架,机架包括机体框架1和固定在机体框架1上的机体外壳2,机架的内部形成有容纳腔3且顶部开设有机舱口4,机舱口4处对称安装有两组呈倾斜设置的机库门5,两组机库门5的正下方设置有安装座6,安装座6固定在容纳腔3内壁上且表面垂直设置有连接杆7,连接杆7的上端开设有穿口8,穿口8内水平穿插有铰接轴9,铰接轴9的上端固定连接有旋转臂10,旋转臂10的顶部与机库门5的内壁铰接且末端安装有传动副11,传动副11包括从动轮12和位于从动轮12内侧的传动轮13,从动轮12末端固定有与铰接轴9同轴的旋转轴14,从动轮12和传动轮13啮合连接,传动轮13的下方还安装有驱动装置15,驱动装置15包括安装板16和固定在安装板16上的驱动电机17,驱动电机17的动力输出端安装有驱动轮18,驱动轮18与传动轮13啮合连接。1-3, the present invention provides a technical solution: a rotary drive hangar door device, including a frame, the frame includes a
进一步改进地,如图1所示:机体框架1由若干组金属杆19组成,若干组金属杆19组成长方体结构,相邻两组金属杆19之间设置有套管20,金属杆19的一端套嵌于套管20内,这样的设计方式便于机体框架1各部分金属感19之间的组装和拆卸,提高安装和拆卸的便捷性和效率。Further improved, as shown in Figure 1: the
进一步改进地,如图1所示:安装座6包括固定在容纳腔3底部的基座21和对称安装在基座21上的两组支撑块22,连接杆7和安装板16均固定在支撑块22上,设计有安装座6可以对驱动装置15、传动副11以及旋转臂10达到较好的支撑效果和转动连接的目的。Further improved, as shown in FIG. 1: the mounting seat 6 includes a
进一步改进地,如图3所示:旋转臂10整体呈倒置的钩状结构且包括上端的钩杆23和位于下方的主杆24,钩杆23与主杆24一体成型,将旋转臂10设计为钩状结构便于对机库门5进行旋转调节。Further improved, as shown in FIG. 3 : the rotating
进一步改进地,如图3所示:旋转臂10上加工成型有加固机构,加固机构包括钩状板25和均匀焊接于钩状板25两侧的若干组加固板26,在旋转臂10的两侧均设计有加固机构,可以提高旋转臂10的抗压性。Further improved, as shown in FIG. 3 : a reinforcement mechanism is formed on the
进一步改进地,如图3所示:若干组加固板26呈倾斜状设置在钩状板25的两侧,加固机构整体呈鱼骨状结构,将加固机构设计为鱼骨状结构可以很多程度上提高旋转臂10各部位的强度和抗压性。Further improved, as shown in Figure 3: several groups of
进一步改进地,如图1所示:机库门5与旋转臂10无相对运动,两组机库门5处于闭合状态时,两组机库门5之间形成人字形“屋脊”结构,通过将两组机库门5闭合时呈人字形结构可以提高机库门5的抗压能力,并配合内部的旋转臂10可以增加机架顶部的强度。Further improved, as shown in Figure 1: the hangar door 5 and the
进一步改进地,如图2所示:驱动装置15可以是电机也可以是电机与减速机的组合,通过电机或是电机与减速机的组合来驱动传动副11运作,提供动力来源。Further improvement, as shown in FIG. 2 : the driving
具体地,传动副11可以是齿轮副、链传动副和带传动副,可以及时的需要选择不同种类的传动副11来满足驱动的需要。Specifically, the
在使用时:本发明当需要对机架进行开机库门5时,可以通过驱动电机17带动驱动轮18转动,驱动轮18在转动的过程中带动传动轮13转动,传动轮13带动从动轮12转动,从动轮12转动的过程中通过旋转轴14带动旋转臂10的底部向外转动,从而带动机库门5打开,当需要进行关闭上,驱动电机17反向转动即可通过旋转臂10带动机库门5向内侧转动,达到关闭的目的,对无人机机体的结构进行了改进,在机体的顶部设计有可自动开启的机库门5机构,当需要对机体进行检修时可以通过内部的驱动机构将机库门5打开进行操作,该结构可以有效的提高无人机机体的智能化程度和自动化程度,并且采用的旋转式开启方式占用空间小且结构更加简单,使机体更加轻量化。In use: the present invention can drive the
最后应说明的是:以上所述仅为本发明的优选实施例而已,并不用于限制本发明,尽管参照前述实施例对本发明进行了详细的说明,对于本领域的技术人员来说,其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。Finally, it should be noted that the above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, the The technical solutions described in the foregoing embodiments may be modified, or some technical features thereof may be equivalently replaced. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
Claims (9)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010440301.1A CN111577056A (en) | 2020-05-22 | 2020-05-22 | A rotary drive hangar door device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010440301.1A CN111577056A (en) | 2020-05-22 | 2020-05-22 | A rotary drive hangar door device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111577056A true CN111577056A (en) | 2020-08-25 |
Family
ID=72121236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010440301.1A Pending CN111577056A (en) | 2020-05-22 | 2020-05-22 | A rotary drive hangar door device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111577056A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113539620A (en) * | 2021-09-15 | 2021-10-22 | 江苏鑫鸿电气设备有限公司 | Oil-immersed transformer protection casing |
| CN116834868A (en) * | 2023-07-04 | 2023-10-03 | 张家港扬子江冷轧板有限公司 | A kind of silicon steel annealing furnace inspection car |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103452443A (en) * | 2013-08-08 | 2013-12-18 | 贵州航天天马机电科技有限公司 | Hatch cover structure |
| CN204433025U (en) * | 2014-11-19 | 2015-07-01 | 中国航空工业集团公司西安飞机设计研究所 | A kind of outer receipts formula air baggage chamber door opener |
| US20180245365A1 (en) * | 2015-08-17 | 2018-08-30 | H3 Dynamics Holdings Pte. Ltd. | Drone box |
| CN108945387A (en) * | 2018-07-27 | 2018-12-07 | 贵州航天天马机电科技有限公司 | A kind of aircraft door opening device |
| CN208363905U (en) * | 2018-06-26 | 2019-01-11 | 东莞动源机电科技有限公司 | A kind of container of the electronic headstock gear of band |
| CN109779437A (en) * | 2019-02-19 | 2019-05-21 | 贵州航天天马机电科技有限公司 | A kind of car door drive |
| CN210000076U (en) * | 2019-03-29 | 2020-01-31 | 潍柴动力股份有限公司 | Outer hem structure of passenger car and passenger car provided with same |
| CN212773960U (en) * | 2020-05-22 | 2021-03-23 | 上海芝松航空科技有限公司 | Rotary driving garage door device |
-
2020
- 2020-05-22 CN CN202010440301.1A patent/CN111577056A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103452443A (en) * | 2013-08-08 | 2013-12-18 | 贵州航天天马机电科技有限公司 | Hatch cover structure |
| CN204433025U (en) * | 2014-11-19 | 2015-07-01 | 中国航空工业集团公司西安飞机设计研究所 | A kind of outer receipts formula air baggage chamber door opener |
| US20180245365A1 (en) * | 2015-08-17 | 2018-08-30 | H3 Dynamics Holdings Pte. Ltd. | Drone box |
| CN208363905U (en) * | 2018-06-26 | 2019-01-11 | 东莞动源机电科技有限公司 | A kind of container of the electronic headstock gear of band |
| CN108945387A (en) * | 2018-07-27 | 2018-12-07 | 贵州航天天马机电科技有限公司 | A kind of aircraft door opening device |
| CN109779437A (en) * | 2019-02-19 | 2019-05-21 | 贵州航天天马机电科技有限公司 | A kind of car door drive |
| CN210000076U (en) * | 2019-03-29 | 2020-01-31 | 潍柴动力股份有限公司 | Outer hem structure of passenger car and passenger car provided with same |
| CN212773960U (en) * | 2020-05-22 | 2021-03-23 | 上海芝松航空科技有限公司 | Rotary driving garage door device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113539620A (en) * | 2021-09-15 | 2021-10-22 | 江苏鑫鸿电气设备有限公司 | Oil-immersed transformer protection casing |
| CN116834868A (en) * | 2023-07-04 | 2023-10-03 | 张家港扬子江冷轧板有限公司 | A kind of silicon steel annealing furnace inspection car |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111577056A (en) | A rotary drive hangar door device | |
| CN203767061U (en) | Door-less weather tight invisible ventilation device | |
| CN212773960U (en) | Rotary driving garage door device | |
| CN104803013B (en) | Three degree of freedom spherical motion platform | |
| CN105329443A (en) | Ornithopter capable of realizing flapping-reversing coupled motion | |
| CN209479338U (en) | A kind of land, water and air three are dwelt quadrotor drone | |
| CN110077616A (en) | A kind of the unmanned plane arresting gear and unmanned plane closing method of energy wireless charging | |
| CN114408175A (en) | Bionic sparrow unmanned aerial vehicle | |
| CN106945828B (en) | A kind of unmanned plane with transportation function | |
| CN109131886B (en) | a life-saving drone | |
| RU180861U1 (en) | Land vehicle equipped with a module for storing and automatically launching a UAV | |
| CN205113712U (en) | Two degree of freedom flapping wing aircraft | |
| CN221738166U (en) | A clamshell drone nest | |
| CN211844904U (en) | Unmanned aerial vehicle is patrolled and examined to electric power that possesses protect function | |
| CN112340001A (en) | Unmanned plane | |
| CN212709970U (en) | Unmanned aerial vehicle inspection device | |
| CN111577064A (en) | Push rod driver storehouse door gear | |
| CN219428356U (en) | Scalable unmanned aerial vehicle horn device | |
| CN108469357A (en) | A kind of unmanned plane with river water sampling function based on Internet of Things | |
| CN216424679U (en) | Convenient hatch board of ventilating that opens and shuts | |
| CN104803014B (en) | The spherical motion platform of two-freedom | |
| CN218431764U (en) | Battery replacing device and unmanned aerial vehicle | |
| CN217603460U (en) | Electric valve actuator with linkage structure | |
| CN205931264U (en) | Throw thing unmanned aerial vehicle | |
| CN216861840U (en) | Suspension mechanism for unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200825 |
|
| RJ01 | Rejection of invention patent application after publication |