CN207191392U - Horn component, frame and unmanned vehicle - Google Patents

Horn component, frame and unmanned vehicle Download PDF

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Publication number
CN207191392U
CN207191392U CN201721085699.1U CN201721085699U CN207191392U CN 207191392 U CN207191392 U CN 207191392U CN 201721085699 U CN201721085699 U CN 201721085699U CN 207191392 U CN207191392 U CN 207191392U
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China
Prior art keywords
main body
horn
component
frame
foot stool
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CN201721085699.1U
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Chinese (zh)
Inventor
郭超凡
冯建刚
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Shenzhen Dajiang Innovations Technology Co Ltd
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Shenzhen Dajiang Innovations Technology Co Ltd
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Priority to CN201721085699.1U priority Critical patent/CN207191392U/en
Priority to CN201780086814.3A priority patent/CN110382350A/en
Priority to PCT/CN2017/108103 priority patent/WO2019037242A1/en
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Publication of CN207191392U publication Critical patent/CN207191392U/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/293Foldable or collapsible rotors or rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00Constructional aspects of UAVs
    • B64U20/80Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B64U20/83Electronic components structurally integrated with aircraft elements, e.g. circuit boards carrying loads

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Details Of Aerials (AREA)
  • Toys (AREA)

Abstract

A kind of horn component, frame and unmanned vehicle, horn component are assemblied in frame main body, and the horn component includes horn main body, the Power Component in horn main body and the control board in horn main body;Horn main body includes auxiliary section, to be connected with the connection component in the frame main body, and by coordinating horn main body frame main body can deploy or fold relatively with connection component, control board is electrically connected at Power Component, to control Power Component to run.The utility model devises a kind of foldable horn component, frame and unmanned vehicle, the horn component frame main body expansion or can fold relatively, so that horn component is not take up space, realize the compact and portable of unmanned vehicle, control board, which is located in horn main body, causes horn to realize modularized design, is easy to dismount.

Description

机臂组件、机架及无人飞行器Arm assemblies, racks and unmanned aerial vehicles

技术领域technical field

本实用新型涉及无人飞行器技术领域,尤其涉及一种机臂组件、机架及无人飞行器。The utility model relates to the technical field of unmanned aerial vehicles, in particular to an arm assembly, a frame and an unmanned aerial vehicle.

背景技术Background technique

近年来,随着无人飞行器领域的快速发展,无人飞行器已然成为大众追捧的产品。目前,无人飞行器在设计方面越来越注重体积小巧,以便于用户存放及携带。然而,机臂及螺旋桨仍然需要占用一定的空间;另外,为了保护机臂及螺旋桨,在无人飞行器存放时,需要设计匹配形状的盒体来容纳该无人飞行器,如此并不能满足用户易于存放及便携的需求。In recent years, with the rapid development of the field of unmanned aerial vehicles, unmanned aerial vehicles have become popular products. At present, the design of unmanned aerial vehicles pays more and more attention to small size, so that users can store and carry them easily. However, the arms and propellers still need to occupy a certain amount of space; in addition, in order to protect the arms and propellers, when the UAV is stored, it is necessary to design a box with a matching shape to accommodate the UAV, which does not satisfy the user for easy storage. and portability requirements.

实用新型内容Utility model content

本实用新型提出一种可折叠式的机臂组件、机架及无人飞行器以解决上述技术问题。The utility model proposes a foldable arm assembly, a frame and an unmanned aerial vehicle to solve the above technical problems.

根据本实用新型实施例的第一方面,提供了一种机臂组件,装配于机架主体,其特征在于,所述机臂组件包括机臂主体、设于所述机臂主体上的动力组件、以及设于所述机臂主体内的控制电路板;其中,所述机臂主体包括配合部,用以与所述机架主体上的连接组件配合连接,并通过与所述连接组件配合使得所述机臂组件可相对所述机架主体展开或者折叠,所述控制电路板电性连接于所述动力组件,用以控制所述动力组件运行。According to the first aspect of the embodiment of the present invention, there is provided a machine arm assembly, which is assembled on the frame main body, wherein the machine arm assembly includes a machine arm main body and a power assembly provided on the machine arm main body , and a control circuit board located in the main body of the machine arm; wherein, the main body of the machine arm includes a matching portion for mating connection with the connection assembly on the frame main body, and by cooperating with the connection assembly, the The arm assembly can be unfolded or folded relative to the frame main body, and the control circuit board is electrically connected to the power assembly to control the operation of the power assembly.

进一步地,所述机臂主体上设有容纳部,用以容纳所述控制电路板。Further, a housing portion is provided on the main body of the arm to accommodate the control circuit board.

进一步地,所述机臂组件还包括机臂盖,所述机臂盖装配于所述机臂主体上,用以将所述控制电路板封装于所述容纳部内。Further, the arm assembly further includes an arm cover, and the arm cover is assembled on the main body of the arm to encapsulate the control circuit board in the accommodating portion.

进一步地,所述机臂主体还包括用于装配所述动力组件的连接部,所述连接部与所述配合部分设于所述机臂主体的两端。Further, the main body of the machine arm further includes a connection part for assembling the power assembly, and the connection part and the matching part are provided at both ends of the main body of the machine arm.

进一步地,所述动力组件包括安装于所述连接部上的驱动件、以及连接于所述驱动件上的螺旋桨,所述驱动件电性连接于所述控制电路板,以在所述控制电路板的控制信号下驱动所述螺旋桨转动。Further, the power assembly includes a driving part installed on the connecting part, and a propeller connected to the driving part, and the driving part is electrically connected to the control circuit board, so that the control circuit The propeller is driven to rotate under the control signal of the board.

进一步地,所述螺旋桨的桨叶可折叠设置。Further, the blades of the propeller are foldable.

进一步地,所述机臂组件还包括设于所述连接部下方的脚架组件,至少用于支撑所述机臂组件。Further, the arm assembly further includes a stand assembly disposed under the connecting portion, at least for supporting the arm assembly.

进一步地,所述机臂组件还包括天线组件,所述脚架组件内设有收容空间,用以收容所述天线组件。Further, the arm assembly further includes an antenna assembly, and a receiving space is provided in the tripod assembly for accommodating the antenna assembly.

进一步地,所述脚架组件包括脚架主体,所述脚架主体包括脚架壳体和天线盖,所述收容空间位于所述脚架壳体内,所述天线盖装配于所述脚架壳体以将所述天线组件封装于所述脚架壳体的收容空间内。Further, the tripod assembly includes a tripod main body, the tripod main body includes a tripod housing and an antenna cover, the accommodating space is located in the tripod housing, and the antenna cover is assembled on the tripod housing body to package the antenna assembly in the accommodation space of the tripod housing.

进一步地,所述脚架主体还包括衔接于所述连接部与所述脚架主体之间的脚架连接件,其中,所述脚架主体相对所述脚架连接件可折叠设置。Further, the tripod main body further includes a tripod connecting piece connected between the connecting portion and the tripod main body, wherein the tripod main body is foldable relative to the tripod connecting piece.

进一步地,所述天线组件包括天线面板、以及连接于所述天线面板的馈线,所述馈线于所述脚架壳体内引出并贯穿所述机臂主体而连接至所述机架主体。Further, the antenna assembly includes an antenna panel and a feeder connected to the antenna panel, the feeder is led out from the tripod housing and passes through the arm body to be connected to the frame body.

根据本实用新型实施例的第二方面,提供了一种机架,包括机架主体以及如上述中任一项所述的机臂组件,所述机架主体上设有连接组件,所述机臂组件通过配合部与连接组件配合转动连接于所述机架主体。According to the second aspect of the embodiment of the present invention, there is provided a frame, including a frame body and the arm assembly as described in any one of the above, the frame body is provided with a connecting assembly, and the frame body The arm assembly is rotatably connected to the frame main body through the matching portion and the connecting assembly.

进一步地,所述机架主体上设有收容部,用以容置所述机臂组件;其中,所述机臂组件在相对所述机架主体折叠时,所述机臂组件位于所述收容部内。Further, the main body of the frame is provided with a receiving portion for accommodating the arm assembly; wherein, when the arm assembly is folded relative to the main body of the frame, the arm assembly is located in the receiving portion. Ministry.

根据本实用新型实施例的第三方面,提供了一种无人飞行器,包括机架以及如上述中任一项所述的机臂组件,所述机臂组件转动连接于所述机架的机架主体,以相对所述机架主体处于展开状态或者折叠状态。According to a third aspect of the embodiment of the present invention, there is provided an unmanned aerial vehicle, including a frame and the arm assembly as described in any one of the above, the arm assembly is rotatably connected to the frame of the frame The frame body is in an expanded state or a folded state relative to the frame body.

本实用新型的实施例提供的技术方案可以包括以下有益效果:The technical solutions provided by the embodiments of the present invention may include the following beneficial effects:

本实用新型设计了一种可折叠式的机臂组件、机架及具有其的无人飞行器,该机臂组件在机臂主体上设有配合部,该配合部用以与机架主体上的连接组件配合连接且通过该连接组件可相对所述机架主体展开或者折叠,如此以使机臂组件可以折叠地放置于机架主体内,从而使机臂组件不占用空间,实现无人飞行器的小巧及便携。The utility model designs a foldable machine arm assembly, a frame and an unmanned aerial vehicle with the same. The arm assembly is provided with a matching part on the main body of the machine arm, and the matching part is used to cooperate with the main body of the frame. The connecting assembly is mated and connected and can be unfolded or folded relative to the main body of the frame through the connecting assembly, so that the arm assembly can be folded and placed in the main body of the frame, so that the arm assembly does not take up space, and the unmanned aerial vehicle is realized. Small and portable.

应当理解的是,以上的一般描述和后文的细节描述仅是示例性和解释性的,并不能限制本实用新型。It should be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the present invention.

附图说明Description of drawings

为了更清楚地说明本实用新型实施例中的技术方案,下面将对实施例描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本实用新型的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动性的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the accompanying drawings that need to be used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings in the following description are only some implementations of the present invention. For example, those skilled in the art can also obtain other drawings based on these drawings without paying creative labor.

图1是本实用新型一示例性实施例示出的一种机臂组件的结构示意图;Fig. 1 is a schematic structural view of an arm assembly shown in an exemplary embodiment of the present invention;

图2是本实用新型一示例性实施例示出的一种机臂组件的分解结构示意图;Fig. 2 is a schematic diagram of an exploded structure of an arm assembly shown in an exemplary embodiment of the present invention;

图3是本实用新型又一示例性实施例示出的一种机臂组件的分解结构示意图;Fig. 3 is a schematic diagram of an exploded structure of an arm assembly shown in another exemplary embodiment of the present invention;

图4是本实用新型一示例性实施例示出的一种机架配合有机臂组件的结构示意图;Fig. 4 is a schematic structural view of a rack-mounted arm assembly shown in an exemplary embodiment of the present invention;

图5是本实用新型一示例性实施例示出的一种无人飞行器的部分分解示意图;Fig. 5 is a partially exploded schematic view of an unmanned aerial vehicle shown in an exemplary embodiment of the present invention;

图6是本实用新型一示例性实施例示出的一种无人飞行器的部分结构示意图。Fig. 6 is a partial structural schematic diagram of an unmanned aerial vehicle shown in an exemplary embodiment of the present invention.

具体实施方式Detailed ways

下面将结合本实用新型实施例中的附图,对本实用新型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实用新型一部分实施例,而不是全部的实施例。基于本实用新型中的实施例,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,都属于本实用新型保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. example. Based on the embodiments of the present utility model, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of the present utility model.

下面结合附图,对本实用新型的一些实施方式作详细说明,在不冲突的情况下,下述的实施例及实施例中的特征可以相互组合。Some implementations of the present utility model will be described in detail below with reference to the accompanying drawings. The following embodiments and the features in the embodiments can be combined with each other if there is no conflict.

如图1至图4所示,本实用新型实施例的机臂组件10装配于机架主体101,当无人飞行器处于使用状态时,以使机臂组件10可以相对机架主体101展开;当无人飞行器未处于使用时,以使机臂组件10相对机架主体101折叠。本实施例通过该机臂组件10可以相对机架主体101可折叠设计,不仅可以起到保护机臂组件10的作用,而且可以减小无人飞行器的体积且便于携带。As shown in Figures 1 to 4, the arm assembly 10 of the embodiment of the present invention is assembled on the frame body 101, so that the arm assembly 10 can be expanded relative to the frame body 101 when the unmanned aerial vehicle is in use; When the UAV is not in use, the arm assembly 10 is folded relative to the frame body 101 . In this embodiment, the arm assembly 10 can be folded relative to the frame body 101 , which can not only protect the arm assembly 10 , but also reduce the volume of the UAV and make it easy to carry.

该机臂组件10包括机臂主体11、以及设于机臂主体11上的动力组件12。其中,机臂主体11包括配合部111,该配合部111用以与机架主体101上的连接组件配合连接,并通过与连接组件配合使得机臂组件10可相对机架主体101展开或者折叠。本实用新型中,该配合部111与连接组件可拆卸连接,如此可以使机臂组件10便于组装、更换及维修,操作简便,将机臂组件10实现模块化设计。The arm assembly 10 includes an arm body 11 and a power assembly 12 disposed on the arm body 11 . Wherein, the arm body 11 includes a matching portion 111 , which is used for mating connection with the connecting component on the frame body 101 , and by cooperating with the connecting component, the arm component 10 can be unfolded or folded relative to the frame body 101 . In the present invention, the matching portion 111 is detachably connected to the connection assembly, so that the arm assembly 10 can be easily assembled, replaced and maintained, and the operation is simple, and the arm assembly 10 can be modularized.

在一可选实施例中,该配合部111为一轴臂,机架主体101上的连接组件包括设于机架主体101上的连接件103、与所述连接件103连接的转轴(未示出),所述转轴可拆卸地固定于所述配合部111上,即可拆卸地固定于所述轴臂上,配合部111通过转轴与连接件103转动连接,从而使机臂组件10相对机架主体101展开或折叠。可选地,该轴臂上设有连接轴孔,该连接件103上设有连接孔并通过螺钉配合连接轴孔而固定在轴臂上,如此可以实现机臂组件10快速组装及拆卸。当然,在其他实施例在该连接件103还可以通过锁扣、卡配、焊接等方式固定于轴臂内。In an optional embodiment, the matching part 111 is a shaft arm, and the connecting assembly on the frame body 101 includes a connecting piece 103 arranged on the frame main body 101, a rotating shaft (not shown) connected with the connecting piece 103 out), the rotating shaft is detachably fixed on the matching portion 111, that is, detachably fixed on the shaft arm, and the matching portion 111 is rotationally connected with the connecting piece 103 through the rotating shaft, so that the machine arm assembly 10 is relatively machine The stand main body 101 is unfolded or folded. Optionally, the shaft arm is provided with a connecting shaft hole, and the connecting piece 103 is provided with a connecting hole and is fixed on the shaft arm by fitting the connecting shaft hole with a screw, so that the machine arm assembly 10 can be quickly assembled and disassembled. Of course, in other embodiments, the connecting member 103 can also be fixed in the shaft arm by means of locking, clamping, welding and the like.

在又一可选实施例中,该配合部111为一轴臂,轴臂通过转轴(未图示)连接于机架主体101上,本实用新型的机臂组件10通过该转轴可以转动连接于机架主体101上,该转轴处于竖直方向,以使机臂组件10在水平方向上转动,从而实现机臂组件10相对机架主体101展开以供使用,或者相对机架主体101折叠以将该机臂组件10收起。In yet another optional embodiment, the matching portion 111 is a shaft arm, and the shaft arm is connected to the frame main body 101 through a rotating shaft (not shown), and the machine arm assembly 10 of the present utility model can be rotatably connected to the frame body through the rotating shaft. On the frame main body 101, the rotating shaft is in the vertical direction, so that the machine arm assembly 10 can rotate in the horizontal direction, so that the machine arm assembly 10 can be unfolded relative to the frame main body 101 for use, or can be folded relative to the frame main body 101 to The machine arm assembly 10 is retracted.

该机臂组件10还包括设于机臂主体11内的控制电路板14,该控制电路板14电性连接于动力组件12,用以控制动力组件12运行。进一步地,该控制电路板还用以与机架主体101内的控制模块(未图示)电性连接。具体地,该控制电路板14的连接线路可以通过轴臂与连接组件的连接处引导向机架主体101内,从而与机架主体101内的控制模块电性连接。无人飞行器可以通过与控制电路板14连接的连接线路用以为机臂组件10供电,具体地为控制电路板14和动力组件12供电,并且控制模块还可以通过该连接线路发送控制指令给控制电路板14,以使控制电路板14控制动力组件12的运行模式,在某些情况下,控制电路板14还可以将动力组件12的工作状态发送给控制模块。当然,在本实用新型的其他实施例中,该控制模块还可以通过无线通信的方式与控制电路板14通信连接。The arm assembly 10 also includes a control circuit board 14 disposed in the arm body 11 , the control circuit board 14 is electrically connected to the power assembly 12 for controlling the operation of the power assembly 12 . Further, the control circuit board is also used to electrically connect with the control module (not shown) in the rack body 101 . Specifically, the connection lines of the control circuit board 14 can be guided into the frame body 101 through the connection between the shaft arm and the connection assembly, so as to be electrically connected with the control module in the frame body 101 . The unmanned aerial vehicle can be used to supply power to the arm assembly 10 through the connection line connected to the control circuit board 14, specifically to supply power to the control circuit board 14 and the power assembly 12, and the control module can also send control commands to the control circuit through the connection line Board 14, so that the control circuit board 14 controls the operation mode of the power assembly 12, and in some cases, the control circuit board 14 can also send the working status of the power assembly 12 to the control module. Of course, in other embodiments of the present invention, the control module can also be connected to the control circuit board 14 through wireless communication.

进一步地,该机臂主体11上设有容纳部15,用以容纳控制电路板14。该机臂组件10还包括机臂盖16,机臂盖16装配于机臂主体11上,用以将控制电路板14封装于容纳部15内。Further, the arm main body 11 is provided with a receiving portion 15 for receiving the control circuit board 14 . The arm assembly 10 further includes an arm cover 16 assembled on the main body 11 of the arm to encapsulate the control circuit board 14 in the accommodating portion 15 .

该机臂主体11还包括用于装配动力组件12的连接部112,连接部112与配合部111分设于机臂主体11的两端。其中,动力组件12包括安装于连接部112上的驱动件121、以及连接于驱动件121上的螺旋桨122,驱动件121电性连接于控制电路板14,以在控制电路板14的控制信号下驱动螺旋桨122转动。可选地,该驱动件121为电机,控制电路板14通过电信号控制电机转动,从而控制螺旋桨122具有不同的转速,进而使无人飞行器具有多个飞行状态切换。The arm body 11 also includes a connecting portion 112 for assembling the power assembly 12 , and the connecting portion 112 and the mating portion 111 are separately disposed at two ends of the arm body 11 . Wherein, the power assembly 12 includes a driving member 121 installed on the connecting portion 112, and a propeller 122 connected to the driving member 121, the driving member 121 is electrically connected to the control circuit board 14, so that under the control signal of the control circuit board 14 The propeller 122 is driven to rotate. Optionally, the drive member 121 is a motor, and the control circuit board 14 controls the rotation of the motor through electrical signals, thereby controlling the propeller 122 to have different rotational speeds, thereby allowing the unmanned aerial vehicle to switch between multiple flight states.

其中,该螺旋桨122包括桨毂1221以及至少一个桨叶1222,桨毂1221连接于驱动件121的转动轴上。在一可选实施例中,螺旋桨122为折叠桨,桨叶1222的数量至少为两个,每个桨叶1222可转动地连接于桨毂1221。该实施例中,螺旋桨122为折叠桨可以使机臂组件10相对机架主体101折叠后,将螺旋桨122也折叠收起,可以减小机臂组件10所占用的空间,满足无人飞行器体积减小、便于携带的需求。Wherein, the propeller 122 includes a propeller hub 1221 and at least one blade 1222 , and the propeller hub 1221 is connected to the rotating shaft of the driving member 121 . In an optional embodiment, the propeller 122 is a folding paddle, the number of blades 1222 is at least two, and each blade 1222 is rotatably connected to the hub 1221 . In this embodiment, the propeller 122 is a folding propeller, so that after the arm assembly 10 is folded relative to the frame body 101, the propeller 122 is also folded away, which can reduce the space occupied by the arm assembly 10 and meet the requirements of reducing the volume of the unmanned aerial vehicle. Small, easy to carry needs.

进一步地,机臂组件10还包括设于连接部下方的脚架组件17,至少用以支撑机臂组件10。在无人飞行器起飞或者着落时,可以通过多个机臂组件10上的脚架组件17配合起到支撑该无人飞行器的机架主体101。Further, the arm assembly 10 further includes a stand assembly 17 disposed under the connecting portion, at least for supporting the arm assembly 10 . When the unmanned aerial vehicle takes off or lands, the frame main body 101 of the unmanned aerial vehicle can be supported by the cooperation of the leg assemblies 17 on the plurality of arm assemblies 10 .

本实用新型机臂组件10还包括天线组件18,脚架组件17内设有收容空间,用以收容天线组件18。进一步地,该脚架组件17包括脚架主体171,脚架主体171包括脚架壳体1711和天线盖1712,收容空间位于脚架壳体1711内,天线盖1712装配于脚架壳体1711以将天线组件18封装于脚架壳体1711内的天线盖1712。The arm assembly 10 of the present invention further includes an antenna assembly 18 , and the tripod assembly 17 is provided with a receiving space for accommodating the antenna assembly 18 . Further, the tripod assembly 17 includes a tripod main body 171, the tripod main body 171 includes a tripod housing 1711 and an antenna cover 1712, the accommodation space is located in the tripod housing 1711, and the antenna cover 1712 is assembled on the tripod housing 1711 Antenna cover 1712 encloses antenna assembly 18 in tripod housing 1711 .

脚架组件17还包括衔接于连接部112与脚架主体171之间的脚架连接件172、以及设于脚架主体底端的脚垫175。其中,脚架主体171通过该脚架连接件172固定于连接部112从而固定于机臂主体11上,脚垫175用以保护该脚架组件17。The stand assembly 17 further includes a stand connecting member 172 connected between the connecting portion 112 and the stand body 171 , and a foot pad 175 disposed at the bottom of the stand body. Wherein, the stand main body 171 is fixed to the connecting portion 112 through the stand connecting member 172 so as to be fixed on the arm main body 11 , and the foot pad 175 is used to protect the stand assembly 17 .

如图2所示,在一可选实施例中,该脚架连接件172位于脚架主体171的顶端,与脚架主体171一体成型设置,该脚架连接件172包括锁钩1722,连接部112内设有与锁钩1722配合的锁配部(未图示)。在脚架组件17装配于连接部112时,通过脚架连接件172的锁钩1722装配于连接部112的锁配部内,并通过脚架连接件172相对连接部112旋转锁定,从而使脚架组件17固定在机臂主体11上。为了进一步确保脚架组件17与连接部112的固定,还可以通过螺钉配合于脚架组件17及连接部112上,从而实现加固。As shown in FIG. 2 , in an optional embodiment, the tripod connecting member 172 is located at the top of the tripod main body 171 and integrally formed with the tripod main body 171. The tripod connecting member 172 includes a locking hook 1722, the connecting portion 112 is provided with a locking part (not shown) that cooperates with the locking hook 1722 . When the tripod assembly 17 is assembled on the connecting part 112, the hook 1722 of the tripod connecting part 172 is assembled in the locking part of the connecting part 112, and the tripod connecting part 172 is rotated and locked relative to the connecting part 112, so that the tripod The assembly 17 is fixed on the arm main body 11 . In order to further ensure the fixing of the foot frame assembly 17 and the connecting portion 112 , screws can also be fitted to the foot frame assembly 17 and the connecting portion 112 to achieve reinforcement.

如图3所示,在又一可选实施例中,该脚架连接件172可拆卸地装配于脚架主体171的顶端,该脚架连接件172上设有卡配部1723,连接部112内设有与卡配部1723配合的锁配部(未图示)。在脚架组件17装配于连接部112时,可以预先将脚架主体171与脚架连接件172配合固定装配,而后通过脚架连接件172的卡配部1723装配于连接部112的锁配部内,并通过脚架连接件172相对连接部112旋转锁定,从而使脚架组件17固定在机臂主体11上。As shown in FIG. 3 , in yet another optional embodiment, the tripod connecting member 172 is detachably assembled on the top of the tripod main body 171 , and the tripod connecting member 172 is provided with a snap-fitting portion 1723 , and the connecting portion 112 A locking part (not shown) that cooperates with the engaging part 1723 is provided inside. When the tripod assembly 17 is assembled on the connecting part 112, the tripod main body 171 and the tripod connecting part 172 can be fixedly assembled in advance, and then assembled into the locking part of the connecting part 112 through the clamping part 1723 of the tripod connecting part 172 , and rotate and lock relative to the connecting portion 112 through the stand connecting member 172 , so that the stand assembly 17 is fixed on the arm main body 11 .

本实施例中,脚架连接件172上还可以设有与脚架主体171配合的脚架连接槽位1721,脚架主体171卡配于该脚架连接件172的连接槽位1721内,并通过销轴173限定于该连接槽位1721内。本实施例中,脚架主体171可以以销轴173为轴进行转动,以使该脚架主体171可以相对机臂主体171折叠或者展开,如此在无需使用该机臂组件10时,通过将脚架主体171折叠,可以进一步地减小机臂组件10的占用空间。In this embodiment, the tripod connecting part 172 can also be provided with a tripod connecting slot 1721 that matches with the tripod main body 171, and the tripod main body 171 is snapped into the connecting slot 1721 of the tripod connecting part 172, and The connecting slot 1721 is defined by the pin shaft 173 . In this embodiment, the tripod main body 171 can be rotated around the pin shaft 173, so that the tripod main body 171 can be folded or unfolded relative to the arm main body 171. The frame main body 171 is folded, which can further reduce the occupied space of the arm assembly 10 .

进一步地,该天线组件18包括天线面板181、以及连接于天线面板181的馈线182。相对应地,脚架壳体1711内设有供容纳所述馈线182的引线槽1713,脚架壳体1711上还设有供穿线的穿线孔(未标示)。本实施例中,馈线182于脚架壳体1711内引出并贯穿机臂主体11而连接至机架主体101,即该馈线182从穿线孔引出并从机臂主体11内穿过,最终通过配合部111与连接组件的连接处引至机架主体101上,可以电性连接于机架主体101内的控制模块,从而实现信号传输。本实施例中,将天线组件18装配在脚架主体171内,可以充分地利用机臂组件10内的空间,满足无人飞行器体积小巧、便携的设计思路。Further, the antenna assembly 18 includes an antenna panel 181 and a feeder 182 connected to the antenna panel 181 . Correspondingly, a lead groove 1713 for accommodating the feeder wire 182 is provided inside the stand housing 1711 , and a threading hole (not shown) for threading is also provided on the stand housing 1711 . In this embodiment, the feeder 182 is drawn out from the tripod housing 1711 and passes through the arm body 11 to be connected to the frame body 101, that is, the feeder 182 is drawn out from the threading hole and passes through the arm body 11, and finally passes through the arm body 11 The connection between the part 111 and the connection assembly leads to the frame body 101, and can be electrically connected to the control module in the frame body 101, so as to realize signal transmission. In this embodiment, the antenna assembly 18 is assembled in the tripod main body 171 , which can make full use of the space in the arm assembly 10 and meet the design idea of small size and portability of the unmanned aerial vehicle.

本实用新型设计了一种可折叠式的机臂组件,该机臂组件在机臂主体上设有配合部,该配合部用以与机架主体上的连接组件配合连接且通过该连接组件可相对所述机架主体展开或者折叠,如此以使机臂组件可以折叠地放置于机架主体内,从而使机臂组件不占用空间,实现无人飞行器的小巧及便携。The utility model designs a foldable machine arm assembly. The machine arm assembly is provided with a matching part on the main body of the machine arm. Expanding or folding relative to the frame main body, so that the arm assembly can be folded and placed in the frame main body, so that the arm assembly does not take up space, and realizes the compactness and portability of the unmanned aerial vehicle.

如图4所示,根据本实用新型实施例的又一方面,提供了一种机架1,该机架1包括机架主体101以及如上述实施例中所述的机臂组件10,机架主体101上可以布局多个本实用新型的机臂组件10,从而使无人飞行器具有较大的动力源,飞行也更为稳定。一可选实施例中,机架主体101上对称地设有四个本实用新型的机臂组件10。相对应地,该机架主体101上设有连接组件,机臂组件10通过配合部111与连接组件配合转动连接于机架主体101。As shown in Figure 4, according to another aspect of the embodiment of the present utility model, a frame 1 is provided, which includes a frame body 101 and the arm assembly 10 as described in the above-mentioned embodiments, the frame Multiple arm assemblies 10 of the present invention can be arranged on the main body 101, so that the unmanned aerial vehicle has a larger power source and the flight is more stable. In an optional embodiment, four machine arm assemblies 10 of the present invention are symmetrically arranged on the frame main body 101 . Correspondingly, the frame body 101 is provided with a connection assembly, and the machine arm assembly 10 is rotatably connected to the frame body 101 through the matching portion 111 and the connection assembly.

在一可选实施例中,该配合部111为一轴臂,机架主体101上的连接组件包括设于机架主体101上的连接件103、与所述连接件103连接的转轴(未示出),所述转轴可拆卸地固定于所述配合部111上,即可拆卸地固定于所述轴臂上,配合部111通过转轴与连接件103转动连接,从而使机臂组件10相对机架主体101展开或折叠。可选地,该轴臂上设有连接轴孔,该连接件103上设有连接孔并通过螺钉配合连接轴孔而固定在轴臂上。当然,在其他实施例在该连接件103还可以通过锁扣、卡配、焊接等方式固定于轴臂内。In an optional embodiment, the matching part 111 is a shaft arm, and the connecting assembly on the frame body 101 includes a connecting piece 103 arranged on the frame main body 101, a rotating shaft (not shown) connected with the connecting piece 103 out), the rotating shaft is detachably fixed on the matching portion 111, that is, detachably fixed on the shaft arm, and the matching portion 111 is rotationally connected with the connecting piece 103 through the rotating shaft, so that the machine arm assembly 10 is relatively machine The stand main body 101 is unfolded or folded. Optionally, the shaft arm is provided with a connecting shaft hole, and the connecting piece 103 is provided with a connecting hole and is fixed on the shaft arm by fitting the connecting shaft hole with a screw. Of course, in other embodiments, the connecting member 103 can also be fixed in the shaft arm by means of locking, clamping, welding and the like.

在又一可选实施例中,该配合部111为一轴臂,轴臂通过转轴(未图示)连接于机架主体101上,本实用新型的机臂组件10通过该转轴可以转动连接于机架主体101上,该转轴处于竖直方向,以使机臂组件10在水平方向上转动,从而实现机臂组件10相对机架主体101展开以供使用,或者相对机架主体101折叠以将该机臂组件10收起。In yet another optional embodiment, the matching portion 111 is a shaft arm, and the shaft arm is connected to the frame main body 101 through a rotating shaft (not shown), and the machine arm assembly 10 of the present utility model can be rotatably connected to the frame body through the rotating shaft. On the frame main body 101, the rotating shaft is in the vertical direction, so that the machine arm assembly 10 can rotate in the horizontal direction, so that the machine arm assembly 10 can be unfolded relative to the frame main body 101 for use, or can be folded relative to the frame main body 101 to The machine arm assembly 10 is retracted.

进一步地,机架主体101上设有收容部1011,用以容置机臂组件10。其中,机臂组件10在相对机架主体101折叠时,机臂组件10位于收容部1011内,该收容部1011为在机架101上凹陷结构。优选地,在机臂组件10折叠于收容部1011时,该机臂组件10的外表面与机架101的外表面对齐以构成一体结构,如此不仅有利于无人飞行器折叠后的美观,而且通过外表面的壳体可以起到保护内部元器件的效果。Further, the frame main body 101 is provided with a receiving portion 1011 for receiving the arm assembly 10 . Wherein, when the arm assembly 10 is folded relative to the frame main body 101 , the arm assembly 10 is located in the receiving portion 1011 , and the receiving portion 1011 is a recessed structure on the frame 101 . Preferably, when the arm assembly 10 is folded in the receiving portion 1011, the outer surface of the arm assembly 10 is aligned with the outer surface of the frame 101 to form an integrated structure, which is not only beneficial to the beauty of the folded unmanned aerial vehicle, but also through The shell on the outer surface can protect the internal components.

如图5、图6配合图4所示,根据本实用新型实施例的又一方面,还提供了一种无人飞行器100,该无人飞行器100包括机架1以及机臂组件10。该机臂组件10转动连接于机架1的机架主体101,以相对机架主体101处于展开状态或者折叠状态。其中,该机臂组件10具体结构特征与机架主体101的配合固定方式请参照上述机臂组件10的实施例及机架1的实施例,在此就不在重复赘述。通过该机臂组件10及配合的机架主体101,以使无人飞行器折叠后更加美观,而且折叠后的机臂组件10不占用空间,可以实现无人飞行器的小巧及便携的设计需求。As shown in FIG. 5 and FIG. 6 together with FIG. 4 , according to yet another aspect of the embodiment of the present utility model, an unmanned aerial vehicle 100 is provided, and the unmanned aerial vehicle 100 includes a frame 1 and an arm assembly 10 . The arm assembly 10 is rotatably connected to the frame body 101 of the frame 1 so as to be in an unfolded state or a folded state relative to the frame body 101 . Wherein, for the specific structural features of the arm assembly 10 and the cooperating and fixing manner of the frame main body 101, please refer to the embodiment of the above-mentioned arm assembly 10 and the embodiment of the frame 1, and will not be repeated here. Through the arm assembly 10 and the matched frame main body 101, the unmanned aerial vehicle is more beautiful after being folded, and the folded arm assembly 10 does not take up space, and the design requirement of compactness and portability of the unmanned aerial vehicle can be realized.

本实用新型设计了一种可折叠式的机臂组件、机架及具有其的无人飞行器,该机臂组件在机臂主体上设有配合部,该配合部用以与机架主体上的连接组件配合连接且通过该连接组件使得机臂组件可相对所述机架主体展开或者折叠,如此以使机臂组件可以折叠地放置于机架主体内,从而使机臂组件不占用空间,实现无人飞行器的小巧及便携。The utility model designs a foldable machine arm assembly, a frame and an unmanned aerial vehicle with the same. The arm assembly is provided with a matching part on the main body of the machine arm, and the matching part is used to cooperate with the main body of the frame. The connecting assembly is mated and connected and the arm assembly can be unfolded or folded relative to the frame main body through the connecting assembly, so that the arm assembly can be folded and placed in the frame main body, so that the arm assembly does not take up space, realizing Small and portable UAV.

本领域技术人员在考虑说明书及实践这里公开的实用新型后,将容易想到本实用新型的其它实施方案。本申请旨在涵盖本实用新型的任何变型、用途或者适应性变化,这些变型、用途或者适应性变化遵循本实用新型的一般性原理并包括本实用新型未公开的本技术领域中的公知常识或惯用技术手段。说明书和实施例仅被视为示例性的,本实用新型的真正范围和精神由本申请的权利要求指出。Other embodiments of the invention will be readily apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any modification, use or adaptation of the utility model, which follows the general principles of the utility model and includes common knowledge or common knowledge in the technical field not disclosed by the utility model. conventional technical means. It is intended that the specification and examples be considered exemplary only, with a true scope and spirit of the invention indicated by the appended claims.

应当理解的是,本实用新型并不局限于上面已经描述并在附图中示出的精确结构,并且可以在不脱离其范围进行各种修改和改变。本实用新型的范围仅由所附的权利要求来限制。It should be understood that the present invention is not limited to the precise structure which has been described above and shown in the accompanying drawings, and various modifications and changes can be made without departing from the scope thereof. The scope of the invention is limited only by the appended claims.

Claims (14)

1. a kind of horn component, is assemblied in frame main body, it is characterised in that the horn component includes horn main body, located at institute State the Power Component in horn main body and the control board in the horn main body;Wherein, the horn main body bag Auxiliary section is included, to be connected with the connection component in the frame main body, and by coordinating with the connection component The horn component frame main body expansion or can fold relatively, and the control board is electrically connected at the power packages Part, to control the Power Component to run.
2. horn component according to claim 1, it is characterised in that the horn main body is provided with receiving portion, to hold Receive the control board.
3. horn component according to claim 2, it is characterised in that the horn component also includes horn lid, the machine Arm lid is assemblied in the horn main body, the control board is packaged in described accommodation section.
4. horn component according to claim 1, it is characterised in that the horn main body also includes being used to assemble described move The connecting portion of power component, the connecting portion are located at the both ends of the horn main body with the mating part.
5. horn component according to claim 4, it is characterised in that the Power Component includes being installed on the connecting portion On actuator and the propeller that is connected on the actuator, the actuator be electrically connected at the control board, To drive the propeller rotational under the control signal of the control board.
6. horn component according to claim 5, it is characterised in that the foldable setting of blade of the propeller.
7. horn component according to claim 4, it is characterised in that the horn component also includes being located at the connecting portion The foot stool component of lower section, at least it is used to support the horn component.
8. horn component according to claim 7, it is characterised in that the horn component also includes antenna module, described Receiving space is provided with foot stool component, to house the antenna module.
9. horn component according to claim 8, it is characterised in that the foot stool component includes foot stool main body, the pin Frame body includes foot stool housing and antenna cover, and the receiving space is located in the foot stool housing, and the antenna cover is assemblied in institute Foot stool housing is stated so that the antenna module is packaged in the receiving space of the foot stool housing.
10. horn component according to claim 9, it is characterised in that the foot stool component also includes being connected in the company Foot stool connector between socket part and the foot stool main body, wherein, the relatively described foot stool connector of the foot stool main body is foldable Set.
11. horn component according to claim 8, it is characterised in that the antenna module includes aerial panel, Yi Jilian The feeder line of the aerial panel is connected to, the feeder line is connected in being drawn in the foot stool housing and running through the horn main body The frame main body.
A kind of 12. frame, it is characterised in that the horn including frame main body and as any one of claim 1 to 11 Component, the frame main body are provided with connection component, and the horn component is coordinated by auxiliary section and connection component to be rotatablely connected In the frame main body.
13. frame according to claim 12, it is characterised in that the frame main body is provided with resettlement section, to accommodating The horn component;Wherein, for the horn component when relatively described frame main body folds, the horn component is located at the receipts In appearance portion.
A kind of 14. unmanned vehicle, it is characterised in that the machine including frame and as any one of claim 1 to 11 Arm component, the horn component are rotationally connected with the frame main body of the frame, and expansion shape is in relatively described frame main body State or folded state.
CN201721085699.1U 2017-08-25 2017-08-25 Horn component, frame and unmanned vehicle Expired - Fee Related CN207191392U (en)

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CN201721085699.1U CN207191392U (en) 2017-08-25 2017-08-25 Horn component, frame and unmanned vehicle
CN201780086814.3A CN110382350A (en) 2017-08-25 2017-10-27 Horn component, rack and unmanned vehicle
PCT/CN2017/108103 WO2019037242A1 (en) 2017-08-25 2017-10-27 Arm assembly, frame, and unmanned aerial vehicle

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110382350A (en) * 2017-08-25 2019-10-25 深圳市大疆创新科技有限公司 Horn component, rack and unmanned vehicle
WO2020000658A1 (en) * 2018-06-26 2020-01-02 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and arm thereof
WO2020232645A1 (en) * 2019-05-21 2020-11-26 深圳市大疆创新科技有限公司 Unmanned aerial vehicle

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112278230A (en) * 2019-07-24 2021-01-29 广州极飞科技有限公司 Airframe of unmanned aerial vehicle and unmanned aerial vehicle having the same

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2904575C (en) * 2013-03-14 2022-02-01 Aeryon Labs Inc. Folding propellers system
CN204979215U (en) * 2015-07-23 2016-01-20 致导科技(北京)有限公司 Foldable unmanned aerial vehicle
CN205186518U (en) * 2015-10-27 2016-04-27 杭州海康威视数字技术股份有限公司 Unmanned aerial vehicle
CN105197228B (en) * 2015-10-30 2017-09-29 深圳市大疆创新科技有限公司 Foot stool and unmanned vehicle
EP3419894B1 (en) * 2016-02-22 2021-11-10 SZ DJI Technology Co., Ltd. Foldable multi-rotor aerial vehicle
CN207191392U (en) * 2017-08-25 2018-04-06 深圳市大疆创新科技有限公司 Horn component, frame and unmanned vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110382350A (en) * 2017-08-25 2019-10-25 深圳市大疆创新科技有限公司 Horn component, rack and unmanned vehicle
WO2020000658A1 (en) * 2018-06-26 2020-01-02 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and arm thereof
CN110896621A (en) * 2018-06-26 2020-03-20 深圳市大疆创新科技有限公司 Unmanned vehicles and horn thereof
WO2020232645A1 (en) * 2019-05-21 2020-11-26 深圳市大疆创新科技有限公司 Unmanned aerial vehicle

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