CN108058839A - A multi-axis freely adjustable UAV platform - Google Patents
A multi-axis freely adjustable UAV platform Download PDFInfo
- Publication number
- CN108058839A CN108058839A CN201711419832.7A CN201711419832A CN108058839A CN 108058839 A CN108058839 A CN 108058839A CN 201711419832 A CN201711419832 A CN 201711419832A CN 108058839 A CN108058839 A CN 108058839A
- Authority
- CN
- China
- Prior art keywords
- shaft
- connecting plate
- folding rod
- axis
- fixedly connected
- 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
- 230000005540 biological transmission Effects 0.000 claims abstract description 29
- 230000008878 coupling Effects 0.000 claims description 11
- 238000010168 coupling process Methods 0.000 claims description 11
- 238000005859 coupling reaction Methods 0.000 claims description 11
- 244000309464 bull Species 0.000 claims 4
- 238000009434 installation Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Description
技术领域technical field
本发明涉及无人机技术领域,具体为一种多轴自由调节无人机云台。The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-axis freely adjustable unmanned aerial vehicle platform.
背景技术Background technique
目前传统无人飞行器的云台安装方式多为固定式及快拆式,安装后云台位置不能改变,同时云台周围有多个飞行器支撑架保护云台不会接触地面造成损坏,这样装在云台上的拍摄录像装置在随云台旋转进行拍摄录像时会被飞行器支撑架甚至飞行器机体遮挡,拍摄效果及客户体验不好,现有技术中为了解决这个为了,将云台设计为伸缩式云台,在无人机飞行到空中时,云台通过伸缩支架可以展开,扩大摄像机的拍摄范围,但是这种伸缩支架靠拉绳提升,伸缩支架为折叠式支架,上下两端分别与无人机底座以及云台铰接连接,故拉伸的伸长与缩短可以控制摄像机的上升与下降,但是由于伸缩架的两端为铰接式结构,云台的移动不是很稳定,为此我们提出一种多轴自由调节无人机云台用以解决上述问题。At present, the gimbal installation methods of traditional unmanned aerial vehicles are mostly fixed and quick-release. After installation, the position of the gimbal cannot be changed. The shooting and video recording device on the gimbal will be blocked by the aircraft support frame or even the aircraft body when it rotates with the gimbal to shoot video. The shooting effect and customer experience are not good. In order to solve this problem in the prior art, the gimbal is designed as a telescopic The gimbal, when the UAV flies into the air, the gimbal can be expanded through the telescopic bracket to expand the shooting range of the camera, but this telescopic bracket is lifted by a pull rope, and the telescopic bracket is a folding bracket, and the upper and lower ends are respectively connected to the unmanned The machine base and the pan/tilt are hingedly connected, so the elongation and shortening of the stretch can control the rise and fall of the camera, but because the two ends of the telescopic frame are hinged structures, the movement of the pan/tilt is not very stable, so we propose a The multi-axis free adjustment drone platform is used to solve the above problems.
发明内容Contents of the invention
本发明的目的在于提供一种多轴自由调节无人机云台,以解决上述背景技术中提出的问题。The purpose of the present invention is to provide a multi-axis freely adjustable unmanned aerial vehicle platform to solve the problems raised in the above-mentioned background technology.
为实现上述目的,本发明提供如下技术方案:一种多轴自由调节无人机云台,包括连接板,所述连接板的下表面轴动安装有两根转动轴,两根所述转动轴的一端为锥齿轮结构,所述连接板的下表面轴动安装有传动轴,所述传动轴的两端分别与两根转动轴的锥齿轮结构啮合连接,所述连接板的下表面电性安装有传动电机,该传动电机的输出轴与主动齿轮轴动连接,所述主动齿轮与从动齿轮啮合连接,且从动齿轮固定设在传动轴的中间位置,所述传动轴的侧面固定连接折叠杆的上端,且折叠杆的下端铰接连接云台的上表面,所述云台的下表面固定连接有电机腔,该电机腔内电性安装有第一转向电机,所述第一转向电机的输出轴通过联轴器与转杆的上端轴动连接,所述转杆的下端贯穿电机腔并与转轴铰接连接,所述转轴的一端与第二转向电机的输出轴轴动连接,且第二转向电机电性安装在转杆的侧面,所述转轴的侧面与连接杆的上端固定连接,所述连接杆与安装架上表面固定连接。In order to achieve the above object, the present invention provides the following technical solutions: a multi-axis freely adjustable unmanned aerial vehicle platform, including a connecting plate, the lower surface of the connecting plate is axially equipped with two rotating shafts, and the two rotating shafts One end of the connecting plate is a bevel gear structure, and the lower surface of the connecting plate is equipped with a transmission shaft. A transmission motor is installed, the output shaft of the transmission motor is dynamically connected with the driving gear shaft, the driving gear is meshed with the driven gear, and the driven gear is fixed at the middle position of the transmission shaft, and the side of the transmission shaft is fixedly connected The upper end of the folding rod, and the lower end of the folding rod is hingedly connected to the upper surface of the cloud platform, the lower surface of the cloud platform is fixedly connected with a motor cavity, and the first steering motor is electrically installed in the motor cavity, and the first steering motor The output shaft of the rotating shaft is dynamically connected with the upper end of the rotating rod through a coupling, the lower end of the rotating rod passes through the motor cavity and is hingedly connected with the rotating shaft, one end of the rotating shaft is dynamically connected with the output shaft of the second steering motor, and the second The two steering motors are electrically installed on the side of the rotating shaft, the side of the rotating shaft is fixedly connected to the upper end of the connecting rod, and the connecting rod is fixedly connected to the upper surface of the mounting frame.
优选的,所述转动轴的数量为两根,两根所述转动轴的长度方向与连接板的长度方向垂直,且两根转动轴分别轴动安装在连接板下表面的两端。Preferably, there are two rotating shafts, the length direction of the two rotating shafts is perpendicular to the length direction of the connecting plate, and the two rotating shafts are axially mounted on both ends of the lower surface of the connecting plate respectively.
优选的,所述传动轴的长度方向与连接板的长度方向保持一致,且传动轴的两端均为锥形齿轮结构。Preferably, the length direction of the transmission shaft is consistent with the length direction of the connecting plate, and both ends of the transmission shaft are bevel gear structures.
优选的,所述转杆的长度方向垂直于水平面,所述转轴的轴线方向与水平面平行。Preferably, the length direction of the rotating rod is perpendicular to the horizontal plane, and the axial direction of the rotating shaft is parallel to the horizontal plane.
优选的,所述折叠杆包括上折叠杆与下折叠杆,且上折叠杆的下端与下折叠杆的上端铰接连接,所述折叠杆的数量为四组,四组所述折叠杆的上端与两根转动轴两端的侧面固定连接,且四组折叠杆所处平面与水平面垂直。Preferably, the folding rods include an upper folding rod and a lower folding rod, and the lower end of the upper folding rod is hingedly connected to the upper end of the lower folding rod, the number of the folding rods is four groups, and the upper ends of the four groups of the folding rods are connected to The sides at the two ends of the two rotating shafts are fixedly connected, and the planes where the four sets of folding rods are located are perpendicular to the horizontal plane.
优选的,所述电机腔包括侧壁以及底板,所述侧壁的上端与云台的下表面固定连接,且侧壁的下端与底板一体成型,所述底板上贯穿设有穿孔,所述转杆的下端贯穿该穿孔,所述穿孔的孔径小于联轴器的直径,气联轴器的下表面与底板的上表面滚动卡设有滚珠。Preferably, the motor cavity includes a side wall and a bottom plate, the upper end of the side wall is fixedly connected to the lower surface of the pan-tilt, and the lower end of the side wall is integrally formed with the bottom plate, and a perforation is formed on the bottom plate, and the rotating The lower end of the rod passes through the perforation, the diameter of the perforation is smaller than the diameter of the coupling, and the lower surface of the gas coupling and the upper surface of the bottom plate are locked with rolling balls.
与现有技术相比,本发明的有益效果是:Compared with prior art, the beneficial effect of the present invention is:
1、本发明在传动电机开启转动时可以带动主动齿轮的转动,主动齿轮的转动带动从动齿轮的转动,从动齿轮转动时带动转动轴的转动,由于折叠杆的上端与转动轴的侧面固定连接,故传动电机的正反转可以控制摄像机的升降;1. The present invention can drive the rotation of the driving gear when the transmission motor is turned on, the rotation of the driving gear drives the rotation of the driven gear, and the rotation of the rotation shaft is driven by the rotation of the driven gear. Connected, so the positive and negative rotation of the drive motor can control the camera's lifting;
2、本发明第一转向电机在转动时可以带动安装架在水平方向发生转动,第二转向电机在转动时可以带动安装架在竖直方向上转动,增大摄像机的拍摄范围。2. The first steering motor of the present invention can drive the mounting frame to rotate in the horizontal direction when rotating, and the second steering motor can drive the mounting frame to rotate in the vertical direction when rotating to increase the shooting range of the camera.
附图说明Description of drawings
图1为本发明结构示意图;Fig. 1 is a structural representation of the present invention;
图2为本发明图1中A处放大结构示意图;Fig. 2 is a schematic diagram of enlarged structure at A place in Fig. 1 of the present invention;
图3为本发明转动轴安装结构示意图。Fig. 3 is a schematic diagram of the installation structure of the rotating shaft of the present invention.
图中:1连接板、2转动轴、3传动轴、4传动电机、5主动齿轮、6从动齿轮、7折叠杆、8云台、9电机腔、10第一转向电机、11转杆、12转轴、13第二转向电机、14滚珠。In the figure: 1 connecting plate, 2 rotating shaft, 3 transmission shaft, 4 transmission motor, 5 driving gear, 6 driven gear, 7 folding lever, 8 cloud platform, 9 motor chamber, 10 first steering motor, 11 rotating rod, 12 rotating shafts, 13 second steering motors, 14 balls.
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 following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
请参阅图1-3,本发明提供一种技术方案:一种多轴自由调节无人机云台,包括连接板1,连接板1的下表面轴动安装有两根转动轴2,两根转动轴2的一端为锥齿轮结构,连接板1的下表面轴动安装有传动轴3,传动轴3的长度方向与连接板1的长度方向保持一致,且传动轴2的两端均为锥形齿轮结构,传动轴3的两端分别与两根转动轴2的端部啮合连接,传动轴3的两端分别与两根转动轴2的锥齿轮结构啮合连接,连接板1的下表面电性安装有传动电机4,该传动电机4的输出轴与主动齿轮5轴动连接,主动齿轮5与从动齿轮6啮合连接,且从动齿轮6固定设在传动轴2的中间位置,转动轴2的数量为两根,两根转动轴2的长度方向与连接板1的长度方向垂直,且两根转动轴2分别轴动安装在连接板1下表面的两端,在传动电机4开启转动时可以带动主动齿轮5的转动,主动齿轮5的转动带动从动齿轮6的转动。Please refer to Figures 1-3, the present invention provides a technical solution: a multi-axis freely adjustable unmanned aerial vehicle platform, including a connecting plate 1, the lower surface of the connecting plate 1 is axially installed with two rotating shafts 2, two One end of the rotating shaft 2 is a bevel gear structure, and the lower surface of the connecting plate 1 is axially mounted with a transmission shaft 3. The length direction of the transmission shaft 3 is consistent with the length direction of the connecting plate 1, and both ends of the transmission shaft 2 are cones. The two ends of the transmission shaft 3 are meshed with the ends of the two rotating shafts 2 respectively, and the two ends of the transmission shaft 3 are meshed with the bevel gear structures of the two rotating shafts 2 respectively. The lower surface of the connecting plate 1 is electrically connected. A transmission motor 4 is permanently installed, the output shaft of the transmission motor 4 is dynamically connected with the driving gear 5, the driving gear 5 is meshed with the driven gear 6, and the driven gear 6 is fixed at the middle position of the transmission shaft 2, and the rotating shaft The number of 2 is two, the length direction of the two rotating shafts 2 is perpendicular to the length direction of the connecting plate 1, and the two rotating shafts 2 are installed on the two ends of the lower surface of the connecting plate 1 respectively, and the driving motor 4 starts to rotate Can drive the rotation of driving gear 5, the rotation of driving gear 5 drives the rotation of driven gear 6.
如图3所示,传动轴2的侧面固定连接折叠杆7的上端,且折叠杆7的下端铰接连接云台8的上表面,折叠杆7包括上折叠杆与下折叠杆,且上折叠杆的下端与下折叠杆的上端铰接连接,折叠杆7的数量为四组,四组折叠杆7的上端与两根转动轴2两端的侧面固定连接,且四组折叠杆7所处平面与水平面垂直,折叠杆7包括两根可以折叠的上折叠杆与下折叠杆,转动轴2在转动的时候可以带动上折叠杆的转动,实现折叠杆7的折叠与展开,结构稳定。As shown in Figure 3, the side of transmission shaft 2 is fixedly connected to the upper end of folding rod 7, and the lower end of folding rod 7 is hingedly connected to the upper surface of cloud platform 8, and folding rod 7 comprises upper folding rod and lower folding rod, and upper folding rod The lower end of the lower end is hingedly connected with the upper end of the lower folding rod. The number of folding rods 7 is four groups. The upper ends of the four groups of folding rods 7 are fixedly connected with the sides of the two ends of the two rotating shafts 2, and the planes and horizontal planes of the four groups of folding rods 7 Vertically, the folding rod 7 includes two foldable upper folding rods and lower folding rods. When the rotating shaft 2 rotates, it can drive the rotation of the upper folding rod to realize the folding and unfolding of the folding rod 7, and the structure is stable.
如图2所示,云台8的下表面固定连接有电机腔9,该电机腔9内电性安装有第一转向电机10,第一转向电机10的输出轴通过联轴器与转杆11的上端轴动连接,转杆11的长度方向垂直于水平面,转杆11的下端贯穿电机腔9并与转轴12铰接连接,转轴12的轴线方向与水平面平行,转轴12的一端与第二转向电机13的输出轴轴动连接,且第二转向电机13电性安装在转杆11的侧面,转轴12的侧面与连接杆的上端固定连接,连接杆与安装架上表面固定连接,安装架的下方安装摄像机,电机腔9包括侧壁以及底板,侧壁的上端与云台8的下表面固定连接,且侧壁的下端与底板一体成型,底板上贯穿设有穿孔,转杆11的下端贯穿该穿孔,穿孔的孔径小于联轴器的直径,气联轴器的下表面与底板的上表面滚动卡设有滚珠14,底板起到支撑联轴器的作用,减轻第一转向电机10上悬挂的重量,联轴器与底板上均嵌入设有滚珠槽,滚珠14滚动卡设在滚珠槽内,第一转向电机10在转动时可以带动安装架在水平方向发生转动,第二转向电机13在转动时可以带动安装架在竖直方向上转动。As shown in Figure 2, a motor cavity 9 is fixedly connected to the lower surface of the cloud platform 8, and a first steering motor 10 is electrically installed in the motor cavity 9, and the output shaft of the first steering motor 10 is connected to the rotating rod 11 through a coupling. The upper end of the rotating shaft is dynamically connected, the length direction of the rotating rod 11 is perpendicular to the horizontal plane, the lower end of the rotating rod 11 runs through the motor chamber 9 and is hingedly connected with the rotating shaft 12, the axial direction of the rotating shaft 12 is parallel to the horizontal plane, and one end of the rotating shaft 12 is connected to the second steering motor The output shaft of 13 is dynamically connected, and the second steering motor 13 is electrically installed on the side of the rotating rod 11, the side of the rotating shaft 12 is fixedly connected to the upper end of the connecting rod, and the connecting rod is fixedly connected to the upper surface of the mounting frame. Camera is installed, and motor cavity 9 comprises side wall and base plate, and the upper end of side wall is fixedly connected with the lower surface of cloud platform 8, and the lower end of side wall is integrally formed with base plate, and perforation is provided on base plate, and the lower end of rotating rod 11 runs through this. Perforation, the hole diameter of the perforation is smaller than the diameter of the coupling, the lower surface of the gas coupling and the upper surface of the bottom plate are rollingly clamped with balls 14, and the bottom plate plays the role of supporting the coupling, reducing the suspension of the first steering motor 10. The weight, the coupling and the bottom plate are all embedded with ball grooves, and the balls 14 are rolled and locked in the ball grooves. When the first steering motor 10 rotates, it can drive the mounting frame to rotate in the horizontal direction, and the second steering motor 13 rotates It can drive the installation frame to rotate in the vertical direction.
工作原理:本发明在传动电机4开启转动时可以带动主动齿轮5的转动,主动齿轮5的转动带动从动齿轮6的转动,从动齿轮6固定套在转动轴2上,故转动轴2在转动的时候可以带动上折叠杆的转动,实现折叠杆7的折叠与展开,从而调节摄像机的上升与下降,结构稳定,第一转向电机10在转动时可以带动安装架在水平方向发生转动,第二转向电机13在转动时可以带动安装架在竖直方向上转动。Working principle: the present invention can drive the rotation of the driving gear 5 when the transmission motor 4 is turned on, the rotation of the driving gear 5 drives the rotation of the driven gear 6, and the driven gear 6 is fixedly sleeved on the rotating shaft 2, so the rotating shaft 2 is When rotating, it can drive the rotation of the upper folding rod to realize the folding and unfolding of the folding rod 7, thereby adjusting the rise and fall of the camera, and the structure is stable. The first steering motor 10 can drive the mounting frame to rotate in the horizontal direction when rotating, and the second Two steering motors 13 can drive the installation frame to rotate in the vertical direction when rotating.
在本发明的描述中,需要理解的是,术语“同轴”、“底部”、“一端”、“顶部”、“中部”、“另一端”、“上”、“一侧”、“顶部”、“内”、“前部”、“中央”、“两端”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。In describing the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "side", "top ", "inner", "front", "central", "both ends" and other indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, and It is not to indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, or operate in a particular orientation, and thus should not be construed as limiting the invention.
此外,术语“第一”、“第二”、“第三”、“第四”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量,由此,限定有“第一”、“第二”、“第三”、“第四”的特征可以明示或者隐含地包括至少一个该特征。In addition, the terms "first", "second", "third" and "fourth" are used for descriptive purposes only, and should not be understood as indicating or implying relative importance or implicitly specifying the number of indicated technical features, Thus, a feature defined as "first", "second", "third" and "fourth" may explicitly or implicitly include at least one of such features.
在本发明中,除非另有明确的规定和限定,术语“安装”、“设置”、“连接”、“固定”、“旋接”等术语应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系,除非另有明确的限定,对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, terms such as "installation", "installation", "connection", "fixation" and "rotation connection" should be interpreted in a broad sense unless otherwise clearly specified and limited, for example, it may be a fixed connection, or It can be a detachable connection or integrated; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediary; it can be the internal communication of two components or the interaction relationship between two components Unless otherwise clearly defined, those skilled in the art can understand the specific meanings of the above terms in the present invention according to specific situations.
尽管已经示出和描述了本发明的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本发明的范围由所附权利要求及其等同物限定。Although the embodiments of the present invention have been shown and described, those skilled in the art can understand that various changes, modifications and substitutions can be made to these embodiments without departing from the principle and spirit of the present invention. and modifications, the scope of the invention is defined by the appended claims and their equivalents.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711419832.7A CN108058839A (en) | 2017-12-25 | 2017-12-25 | A multi-axis freely adjustable UAV platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711419832.7A CN108058839A (en) | 2017-12-25 | 2017-12-25 | A multi-axis freely adjustable UAV platform |
Publications (1)
Publication Number | Publication Date |
---|---|
CN108058839A true CN108058839A (en) | 2018-05-22 |
Family
ID=62139968
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711419832.7A Pending CN108058839A (en) | 2017-12-25 | 2017-12-25 | A multi-axis freely adjustable UAV platform |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108058839A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110637183A (en) * | 2018-06-29 | 2019-12-31 | 深圳市大疆创新科技有限公司 | Control method and device of vertical stability augmentation device and computer readable storage medium |
CN112224429A (en) * | 2020-10-26 | 2021-01-15 | 湖南库里斯智能科技有限公司 | Camera adjustable device based on unmanned aerial vehicle and use method thereof |
CN112309731A (en) * | 2020-10-23 | 2021-02-02 | 广东电网有限责任公司梅州供电局 | Insulating rod |
CN117781241A (en) * | 2023-12-09 | 2024-03-29 | 江苏泰锐格照明有限公司 | Street lamp post structure convenient for lamp replacement and use method thereof |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102996983A (en) * | 2011-09-09 | 2013-03-27 | 深圳市大疆创新科技有限公司 | Gyro-type dynamic self-balancing pan-tilt |
CN203941453U (en) * | 2014-07-17 | 2014-11-12 | 金陵科技学院 | A kind of unmanned plane that can monitor shooting and control by intelligent glasses |
CN105173100A (en) * | 2015-08-04 | 2015-12-23 | 致导科技(北京)有限公司 | Unmanned plane cloud deck and unmanned plane |
CN204956946U (en) * | 2015-08-10 | 2016-01-13 | 普宙飞行器科技(深圳)有限公司 | Unmanned aerial vehicle with flexible cloud platform |
CN204956945U (en) * | 2015-08-10 | 2016-01-13 | 普宙飞行器科技(深圳)有限公司 | Concertina type cloud platform |
CN105329455A (en) * | 2015-12-01 | 2016-02-17 | 国家电网公司 | Carrying cloud deck for unmanned aerial vehicle high-energy ray emitter |
CN205203411U (en) * | 2015-11-20 | 2016-05-04 | 山东英特力光通信开发有限公司 | Carry on three -axis pan -tilt of camera |
CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
CN206494136U (en) * | 2016-10-27 | 2017-09-15 | 江苏云端智能科技有限公司 | A kind of UAV flight's head |
-
2017
- 2017-12-25 CN CN201711419832.7A patent/CN108058839A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102996983A (en) * | 2011-09-09 | 2013-03-27 | 深圳市大疆创新科技有限公司 | Gyro-type dynamic self-balancing pan-tilt |
CN203941453U (en) * | 2014-07-17 | 2014-11-12 | 金陵科技学院 | A kind of unmanned plane that can monitor shooting and control by intelligent glasses |
CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
CN105173100A (en) * | 2015-08-04 | 2015-12-23 | 致导科技(北京)有限公司 | Unmanned plane cloud deck and unmanned plane |
CN204956946U (en) * | 2015-08-10 | 2016-01-13 | 普宙飞行器科技(深圳)有限公司 | Unmanned aerial vehicle with flexible cloud platform |
CN204956945U (en) * | 2015-08-10 | 2016-01-13 | 普宙飞行器科技(深圳)有限公司 | Concertina type cloud platform |
CN205203411U (en) * | 2015-11-20 | 2016-05-04 | 山东英特力光通信开发有限公司 | Carry on three -axis pan -tilt of camera |
CN105329455A (en) * | 2015-12-01 | 2016-02-17 | 国家电网公司 | Carrying cloud deck for unmanned aerial vehicle high-energy ray emitter |
CN206494136U (en) * | 2016-10-27 | 2017-09-15 | 江苏云端智能科技有限公司 | A kind of UAV flight's head |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110637183A (en) * | 2018-06-29 | 2019-12-31 | 深圳市大疆创新科技有限公司 | Control method and device of vertical stability augmentation device and computer readable storage medium |
WO2020000363A1 (en) * | 2018-06-29 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Control method and device for vertical stabilizing device, and computer-readable storage medium |
CN112309731A (en) * | 2020-10-23 | 2021-02-02 | 广东电网有限责任公司梅州供电局 | Insulating rod |
CN112309731B (en) * | 2020-10-23 | 2023-02-10 | 广东电网有限责任公司梅州供电局 | Insulating rod |
CN112224429A (en) * | 2020-10-26 | 2021-01-15 | 湖南库里斯智能科技有限公司 | Camera adjustable device based on unmanned aerial vehicle and use method thereof |
CN117781241A (en) * | 2023-12-09 | 2024-03-29 | 江苏泰锐格照明有限公司 | Street lamp post structure convenient for lamp replacement and use method thereof |
CN117781241B (en) * | 2023-12-09 | 2024-07-23 | 江苏泰锐格照明有限公司 | Street lamp post structure convenient for lamp replacement and use method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108058839A (en) | A multi-axis freely adjustable UAV platform | |
US8125564B2 (en) | Stabilized camera platform system | |
CN204124373U (en) | Unmanned plane twin shaft video cradle head structure | |
WO2013191962A1 (en) | Camera head with pan, roll and tilt movement | |
KR101805837B1 (en) | Focus Stabilization supporter of Manned Aerial photo-Camera | |
JPWO2019021414A1 (en) | Rotorcraft | |
CN106005458B (en) | It is a kind of for unmanned plane high-altitude take photo by plane from steady platform | |
CN211543880U (en) | Adjustable retracting mechanism for unmanned aerial vehicle | |
WO2018095214A1 (en) | Unmanned aerial vehicle and landing gear device thereof | |
WO2019062139A1 (en) | Unmanned aerial vehicle | |
WO2019028871A1 (en) | Frame assembly and unmanned aerial vehicle | |
CN111284692A (en) | Panoramic camera unmanned aerial vehicle | |
CN211001897U (en) | Unmanned aerial vehicle movie & TV shoots cloud platform | |
CN201380965Y (en) | Aerial photography gimbal on small unmanned aircraft | |
CN207417151U (en) | A kind of unmanned vehicle | |
JP6618000B1 (en) | Electronic component and flying object with the electronic component attached | |
CN211618110U (en) | Diaxon VTOL unmanned aerial vehicle | |
CN105882992B (en) | A kind of unmanned plane fixation holder | |
CN108995820A (en) | Holder, filming apparatus and unmanned plane with the holder | |
WO2018095238A1 (en) | Unmanned aerial vehicle and undercarriage device thereof | |
CN211618058U (en) | Adjustable unmanned aerial vehicle | |
CN107878752A (en) | From steady wind resistance unmanned plane | |
CN207060404U (en) | Flapping wing structure and flapping wing for ornithopter unit | |
CN119037751B (en) | Electric power monitoring unmanned aerial vehicle based on laser radar real-time imaging | |
CN114594448A (en) | Balanced installation device for lidar, unmanned aerial vehicle, lidar system and method |
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 | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180522 |