WO2020253621A1 - Support frame fitting structure - Google Patents

Support frame fitting structure Download PDF

Info

Publication number
WO2020253621A1
WO2020253621A1 PCT/CN2020/095691 CN2020095691W WO2020253621A1 WO 2020253621 A1 WO2020253621 A1 WO 2020253621A1 CN 2020095691 W CN2020095691 W CN 2020095691W WO 2020253621 A1 WO2020253621 A1 WO 2020253621A1
Authority
WO
WIPO (PCT)
Prior art keywords
support frame
mounting
bottom plate
block
assembly structure
Prior art date
Application number
PCT/CN2020/095691
Other languages
French (fr)
Chinese (zh)
Inventor
李坤煌
和瑞江
周理嘉
陈泽楠
Original Assignee
深圳高度创新技术有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 深圳高度创新技术有限公司 filed Critical 深圳高度创新技术有限公司
Publication of WO2020253621A1 publication Critical patent/WO2020253621A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts

Definitions

  • the invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a support frame assembly structure.
  • UAVs Due to its many advantages such as vertical lifting, hovering gaze, and strong maneuverability, UAVs have become effective means for image collection, intelligence collection and reconnaissance requirements, and their applications are becoming more and more extensive, such as the application of rescue activities and fire fighting.
  • the existing support frame is more complicated to assemble with the drone, and the disassembly and assembly operations are more complicated, and there are many operations. inconvenient.
  • the purpose of the present invention is to provide a support frame assembly structure, which aims to solve the technical problems of complex support frame assembly structure and complicated disassembly and assembly operations in the prior art.
  • a support frame assembly structure including:
  • the cabinet has a fixed block at the bottom;
  • the support frame has a mounting portion at the top end that cooperates with the fixing block, the fixing block is adapted to be inserted into the mounting portion, and corresponding positions of the mounting portion and the fixing block are respectively provided with insertion holes;
  • the quick plug is inserted in the insertion hole, the fixing block is connected and fixed to the mounting part by the quick plug, the quick plug is provided with a button, and the quick plug can be removed from the button when the button is pressed.
  • the insertion hole is disengaged, so that the mounting part can be disengaged from the fixing block.
  • the support frame includes a horizontally arranged bottom plate, a mounting block, and a connecting piece connected between the bottom plate and the mounting block, the top of the mounting block is formed with the mounting portion;
  • the fixing block has A positioning protrusion protruding downward, the mounting portion is recessed with a positioning groove adapted to the positioning protrusion, the positioning protrusion is adapted to be inserted into the positioning groove, and the positioning protrusion
  • the insertion holes are respectively opened at the corresponding positions of the upper and the mounting portion.
  • a fixed block is respectively provided at the bottom of the casing near the front and rear ends, the supporting frame is provided with four connecting pieces and two mounting blocks, and the top surface of each mounting block Two mounting parts are respectively formed, two connecting pieces are connected between each mounting block and the bottom plate, and the space enclosed by the four connecting pieces is approximately rectangular.
  • a front side or a rear side of the mounting block is provided with an assembly notch communicating with the positioning groove.
  • the two mounting blocks close to the front end of the cabinet and the two mounting blocks close to the rear end of the cabinet are provided with the assembly notches on the opposite sides.
  • the connecting piece is perpendicular to the bottom plate.
  • the connecting piece is a hexagon socket screw
  • the hexagon socket screw includes a head and a rod part provided with an external thread
  • the rod part is threadedly connected with the bottom plate and the mounting block, and the head conflict with the bottom surface of the bottom plate.
  • a clamping plate is fixed at the bottom of the mounting block, and the hexagon socket screw passes through the clamping plate and is screwed to the mounting block.
  • the bottom plate is provided with a plurality of through holes.
  • the plurality of through holes includes a plurality of first through holes symmetrically arranged along the length direction of the bottom plate and a plurality of second through holes symmetrically arranged along the width direction of the bottom plate.
  • the beneficial effects of the present invention in the support frame assembly structure of the present invention, since the mounting part of the support frame and the fixed block at the bottom of the cabinet are connected by quick bolts, when the support frame needs to be installed, the fixing block is assembled behind the mounting part to make The insertion holes of the two are aligned, insert the quick plug into the insertion hole, the mounting part is fixed with the fixing block, so that the support frame is installed at the bottom of the casing, and the quick plug is equipped with a button, which can be pressed after the button is pressed Pull out from the plug hole to make the support frame detach from the casing, and the disassembly and assembly operation of the support frame is very convenient.
  • FIG. 1 is a schematic structural diagram of a drone provided by an embodiment of the present invention
  • Figure 2 is a schematic side view of the structure of the UAV shown in Figure 1;
  • Fig. 3 is a partial three-dimensional structure diagram of the UAV shown in Fig. 2;
  • Fig. 4 is an enlarged schematic diagram of part A in Fig. 3;
  • Figure 5 is a schematic side view of the structure of the support frame assembly structure in the UAV shown in Figure 1;
  • Fig. 6 is a three-dimensional structural diagram of the supporting frame assembly structure shown in Fig. 5;
  • Fig. 7 is an enlarged schematic diagram of part B in Fig. 6;
  • Figure 8 is a partial exploded schematic diagram of the UAV shown in Figure 1;
  • Fig. 9 is an enlarged schematic diagram of part C in Fig. 8.
  • FIG. 10 is a schematic side view of the structure of the casing in the support frame assembly structure shown in FIG. 5;
  • Fig. 11 is a partial exploded schematic diagram of the assembly structure of the support frame shown in Fig. 5.
  • first and second are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of indicated technical features. Thus, the features defined with “first” and “second” may explicitly or implicitly include one or more of these features. In the description of the present invention, “plurality” means two or more than two, unless specifically defined otherwise.
  • the terms “installed”, “connected”, “connected”, “fixed” and other terms should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection. , Or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the internal communication of two components or the interaction relationship between two components.
  • installed can be a fixed connection or a detachable connection. , Or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the internal communication of two components or the interaction relationship between two components.
  • the support frame 20 assembly structure provided by the embodiment of the present invention is applied to an unmanned aerial vehicle 10, such as an unmanned aerial vehicle 10 with a fire fighting function.
  • the assembly structure of the support frame 20 includes a casing 11, a support frame 20 and a quick plug 300.
  • the bottom surface of the casing 11 is provided with a fixed block 100, and the casing 11 is provided with a controller and a battery.
  • the top end of the support frame 20 is provided with a mounting part.
  • the mounting block 220 is used in conjunction with the fixing block 100.
  • the corresponding positions of the mounting part and the fixing block 100 are respectively provided with insertion holes 221.
  • the axis of the insertion holes 221 can be set parallel to the horizontal direction. .
  • the quick plug 300 is inserted into the insertion hole 221, and the fixing block 100 is connected and fixed with the installation part through the quick plug 300.
  • the support frame 20 is fixed to the casing 11 by the quick plug 300, and the installation of the support frame 20 is completed;
  • the latch 300 is provided with a button. After the button is pressed, the quick latch 300 can be disengaged from the insertion hole 221, thereby disengaging the mounting portion from the fixing block 100, so that the support frame 20 can be removed from the bottom of the casing 11, and the support frame 20
  • the disassembly and assembly operations are very convenient.
  • the fixing block 100 is assembled to the mounting portion After that, the insertion holes 221 of the two are aligned, the quick plug 300 is inserted into the insertion hole 221, the mounting part is fixed to the fixing block 100, so that the support frame 20 is installed on the bottom of the casing 11, and the quick plug 300 is provided with a button After pressing the button, the quick-release pin 300 can be pulled out from the insertion hole 221, so that the support frame 20 can be separated from the casing 11, and the disassembly and assembly operation of the support frame 20 is very convenient.
  • the quick bolt 300 is a standard part.
  • the quick bolt 300 includes a mandrel, a bolt shaft, a bushing, a return spring and a button.
  • the mandrel is slidably embedded in the bolt shaft, and the bolt shaft is provided with a receiving hole near the front end.
  • a steel ball is contained inside, and the front end of the mandrel is provided with a beveled groove.
  • the quick plug 300 When using the quick plug 300, insert the pin shaft into the plug hole 221, and the steel ball abuts against the wall of the plug hole 221, so that the quick plug 300 is fixed relative to the wall of the plug hole 221, and the quick plug 300 needs to be pulled out
  • the button When the button is pressed out, the core shaft moves forward a certain distance, the steel ball falls into the inclined groove, and the steel ball is contained in the receiving hole and the inclined groove. At this time, the steel ball does not contact the wall of the insertion hole 221 or only a small amount exists.
  • the contact area can easily pull out the quick plug 300 from the plug hole 221.
  • the outer wall of the shaft sleeve may be provided with a handle to facilitate the force application of the quick plug 300 plugging operation.
  • the top of the fixed block 100 has a connecting portion 120, and the fixed block 100 and the connecting portion 120 are integrally formed.
  • the bottom of the casing 11 can be fixed with a connecting portion 120 by screws;
  • the bottom surface is recessed to form a groove 101 with a width adapted to the connecting portion 120, so that the space under the casing 11 occupied by the fixing block 100 is reduced, and thereby the assembly space between the support frame 20 and the casing 11 is larger.
  • the fixing block 100 may be provided with a hollow structure or a through hole.
  • the fixing block 100 is provided with a through hole passing through the front and rear, so that the weight of the fixing block 100 can be reduced.
  • the support frame 20 includes a bottom plate 210, a mounting block 220, and a connecting piece.
  • the bottom plate 210 may be a carbon fiber board
  • the bottom plate 210 may be horizontally arranged
  • the bottom plate 210 may be a rectangular plate
  • the connecting pieces may be arranged perpendicular to the bottom plate 210, that is, the connecting pieces are arranged vertically.
  • the mounting block 220 is formed with a mounting portion, and the connecting piece is connected between the bottom plate 210 and the mounting block 220, so that there is a bearing space between the bottom surface of the casing 11 and the bottom plate 210 for installing and bearing external components;
  • the fixing block 100 has a downwardly protruding Positioning protrusion 110, the mounting portion is recessed to form a positioning groove 222 adapted to the positioning protrusion 110, the positioning protrusion 110 is adapted to be inserted into the positioning groove 222, the positioning protrusion 110 and the groove wall of the positioning groove 222 Inserting holes 221 are respectively opened at corresponding positions of, and when the quick plug 300 is inserted into the plug hole 221, the quick plug 300 passes through the setting groove 222.
  • the support frame 20 is provided with two mounting blocks 220, and the top surface of each mounting block 220 is formed with two mounting parts, a total of four mounting parts, and the connecting parts are correspondingly arranged There are four.
  • Two connecting pieces are connected between each mounting block 220 and the bottom plate 210. The space enclosed by the four connecting pieces is roughly rectangular.
  • the supporting frame 20 is frame-shaped as a whole and has four sides and top openings.
  • the fixing block 100 There are two, two fixed blocks 100 are respectively arranged at the bottom of the casing 11 near the front and rear ends, and the bottom surface of each fixed block 100 is protrudingly formed with two positioning protrusions 110, namely the front end and the rear end of the support frame 20.
  • each mounting part is recessed to form a positioning groove 222.
  • the longitudinal section of the positioning groove 222 is trapezoidal, and the longitudinal section of the corresponding positioning protrusion 110 is trapezoidal. It is understandable that the longitudinal section of the positioning protrusion 110 may also be formed in other shapes, such as a rectangle.
  • the front or rear side of the mounting block 220 is provided with an assembly notch communicating with the positioning groove 222. That is to say, the top surface and one side surface of the positioning groove 222 are respectively opened, and the assembly notch on the side facilitates the positioning protrusion 110 of the fixing block 100 to fit into the positioning groove 222, which facilitates the connection between the fixing block 100 and the mounting block 220. Assembly operation.
  • the two mounting blocks 220 close to the front end of the casing 11 and the two mounting blocks 220 close to the rear end of the casing 11 are provided with assembly notches on the opposite sides, that is, the two mounting blocks 220 at the front end are assembled
  • the opening direction of the notch is opposite to the opening direction of the assembly notch of the two mounting blocks 220 at the rear end.
  • the longitudinal section of the positioning groove 222 is trapezoidal.
  • the groove wall of the positioning groove 222 opposite to the assembly notch can be set as an inclined groove wall.
  • an assembly inclined surface 223 adapted to the groove wall is formed on the corresponding side of the fixing block 100.
  • the three groove walls of the positioning groove 222 all form assembling slopes 223, and the three corresponding sides of the fixing block 100 form mating slopes 111.
  • Each of the assembling slopes 223 fits with the corresponding mating slope 111.
  • the fixing block 100 is installed The slopes can be used to generate sliding movement to fit the mounting block 220 to achieve the purpose of quickly and accurately aligning the insertion holes of the two.
  • the bottom plate 210 is arranged horizontally, the drone 10 is a drone for fire fighting, and both sides of the drone 10 are equipped with fire extinguishing bombs.
  • the bottom of the UAV 10 is provided with a landing gear 12.
  • the bottoms of the two sides of the landing gear 12 are respectively connected with horizontal support rods.
  • Two parallel support rods are connected with two cross rods.
  • the support frame is formed with two cross rods. Card bit.
  • the bottom of the mounting block 220 is fixed with a clamping plate 240.
  • the hexagon socket screw 230 passes through the clamping plate 240 and is screwed to the mounting block 220.
  • An adapter is formed between the clamping plate 240 and the bottom plate 210.
  • the clamping position of the cross beam of the landing gear 12, that is, the cross beam of the landing gear 12 is clamped between the splint 240 and the bottom plate 210.
  • the splint 240 is substantially a rectangular plate, and the splint 240 is provided with threaded holes corresponding to the threaded holes of the mounting block 220.
  • the splint 240 can be a carbon fiber board to reduce the overall weight.
  • the connecting member adopts a hexagon socket screw 230.
  • the hexagon socket screw 230 includes a head with a hexagon socket and a rod with an external thread on the outer peripheral wall.
  • the bottom plate 210 and the mounting The corresponding positions of the block 220 are respectively provided with threaded holes, the rods pass through the threaded holes of both, that is, the rods are screwed and fixed to the bottom plate 210 and the mounting block 220 respectively, and the head abuts against the bottom surface of the bottom plate 210.
  • the four hexagon socket screws 230 penetrate through the four corners of the bottom plate 210 respectively.
  • the bottom plate 210 is provided with a plurality of through holes 212, and the through holes 212 can reduce the weight of the bottom plate 210, thereby reducing the weight of the support frame 20.
  • the plurality of through holes 212 include a plurality of first through holes symmetrically arranged along the length direction of the bottom plate 210 and a plurality of second through holes symmetrically arranged along the width direction of the bottom plate 210, for example, the bottom plate 210 is rectangular as a whole.
  • the bottom plate 210 is provided with six through holes, and the six through holes form a m-shaped hollow structure in the middle of the bottom plate 210.

Abstract

The present invention relates to the technical field of unmanned aerial vehicles, and particularly relates to a support frame fitting structure, comprising: a housing provided with a fastening block at a base thereof; a support frame, wherein a mounting portion engageable with the fastening block is provided at a top end of the support frame, and insertion connection holes are provided at corresponding positions of the mounting portion and the fastening block, respectively; and a quick release pin capable of being inserted into the insertion connection holes, wherein the fastening block is connected and fastened to the mounting portion via the quick release pin, the quick release pin is provided with a button, and the quick release pin is released from the insertion connection holes when the button is pressed, such that the mounting portion is released from the fastening block. The support frame fitting structure provided by the present application enables the following operations when the support frame needs to be mounted: first fitting the fastening block at the mounting portion, aligning the insertion connection holes of the two, and inserting the quick release pin into the insertion connection holes, such that the mounting portion is fastened to the fastening block. In addition, the quick release pin is provided with the button, and a press on the button enables removal of the quick release pin from the insertion connection holes , such that the support frame is released from the housing, thereby achieving quick and easy mounting and disassembly of the support frame.

Description

支撑架装配结构Support frame assembly structure 技术领域Technical field
本发明属于无人机技术领域,尤其涉及一种支撑架装配结构。The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a support frame assembly structure.
背景技术Background technique
无人机因具有垂直升降、悬停凝视、机动性强等诸多优点,已成为图像采集、情报收集和侦察需求的有效手段,其应用也越来越广泛,例如应用救援活动和灭火等,在诸多应用中,常需要在机身下方设有支撑架,用来承载或安装其它增加的部件,现有的支撑架,其与无人机的装配较为复杂,拆装操作较为繁琐,操作多有不便。Due to its many advantages such as vertical lifting, hovering gaze, and strong maneuverability, UAVs have become effective means for image collection, intelligence collection and reconnaissance requirements, and their applications are becoming more and more extensive, such as the application of rescue activities and fire fighting. In many applications, it is often necessary to have a support frame under the fuselage to carry or install other additional components. The existing support frame is more complicated to assemble with the drone, and the disassembly and assembly operations are more complicated, and there are many operations. inconvenient.
技术问题technical problem
本发明的目的在于提供一种支撑架装配结构,旨在解决现有技术中的支撑架装配结构复杂、拆装操作繁琐的技术问题。The purpose of the present invention is to provide a support frame assembly structure, which aims to solve the technical problems of complex support frame assembly structure and complicated disassembly and assembly operations in the prior art.
技术解决方案Technical solutions
为实现上述目的,本发明采用的技术方案是:一种支撑架装配结构,包括:In order to achieve the above objective, the technical solution adopted by the present invention is: a support frame assembly structure, including:
机壳,底部设有固定块;The cabinet has a fixed block at the bottom;
支撑架,顶端设有与所述固定块配合的安装部,所述固定块适配插设于所述安装部,所述安装部和所述固定块的对应位置分别开设有插接孔;The support frame has a mounting portion at the top end that cooperates with the fixing block, the fixing block is adapted to be inserted into the mounting portion, and corresponding positions of the mounting portion and the fixing block are respectively provided with insertion holes;
快速插销,插设于所述插接孔内,所述固定块通过所述快速插销与所述安装部连接固定,所述快速插销设有按钮,所述按钮被按压时所述快速插销能从所述插接孔脱离,进而使所述安装部能从所述固定块脱离。The quick plug is inserted in the insertion hole, the fixing block is connected and fixed to the mounting part by the quick plug, the quick plug is provided with a button, and the quick plug can be removed from the button when the button is pressed. The insertion hole is disengaged, so that the mounting part can be disengaged from the fixing block.
进一步地,所述支撑架包括水平设置的底板、安装块和连接于所述底板及所述安装块之间的连接件,所述安装块的顶部形成有所述安装部;所述固定块具有向下凸伸的定位凸起,所述安装部凹陷形成有适配于所述定位凸起的定位凹槽,所述定位凸起适配插设于所述定位凹槽内,所述定位凸起和所述安装部的对应位置分别开设有所述插接孔。Further, the support frame includes a horizontally arranged bottom plate, a mounting block, and a connecting piece connected between the bottom plate and the mounting block, the top of the mounting block is formed with the mounting portion; the fixing block has A positioning protrusion protruding downward, the mounting portion is recessed with a positioning groove adapted to the positioning protrusion, the positioning protrusion is adapted to be inserted into the positioning groove, and the positioning protrusion The insertion holes are respectively opened at the corresponding positions of the upper and the mounting portion.
进一步地,所述机壳底部靠近前后端处分别设有一个所述固定块,所述支撑架设置有四个所述连接件和两个所述安装块,每个所述安装块的顶面分别形成有两个所述安装部,每个所述安装块与所述底板之间连接有两个所述连接件,四个所述连接件围成的空间大致呈长方形。Further, a fixed block is respectively provided at the bottom of the casing near the front and rear ends, the supporting frame is provided with four connecting pieces and two mounting blocks, and the top surface of each mounting block Two mounting parts are respectively formed, two connecting pieces are connected between each mounting block and the bottom plate, and the space enclosed by the four connecting pieces is approximately rectangular.
进一步地,所述安装块的前侧或后侧开设有与所述定位凹槽连通的装配缺口。Further, a front side or a rear side of the mounting block is provided with an assembly notch communicating with the positioning groove.
进一步地,靠近所述机壳前端的两个所述安装块与靠近所述机壳后端的两个所述安装块上相背离的一侧开设有所述装配缺口。Further, the two mounting blocks close to the front end of the cabinet and the two mounting blocks close to the rear end of the cabinet are provided with the assembly notches on the opposite sides.
进一步地,所述连接件与所述底板垂直。Further, the connecting piece is perpendicular to the bottom plate.
进一步地,所述连接件为内六角螺钉,所述内六角螺钉包括头部和设有外螺纹的杆部,所述杆部分别与所述底板和所述安装块螺纹连接,所述头部与所述底板的底面相抵。Further, the connecting piece is a hexagon socket screw, the hexagon socket screw includes a head and a rod part provided with an external thread, the rod part is threadedly connected with the bottom plate and the mounting block, and the head Conflict with the bottom surface of the bottom plate.
进一步地,所述安装块的底部固定有夹板,所述内六角螺钉的穿过所述夹板与所述安装块螺接。Further, a clamping plate is fixed at the bottom of the mounting block, and the hexagon socket screw passes through the clamping plate and is screwed to the mounting block.
进一步地,所述底板开设有多个通孔。Further, the bottom plate is provided with a plurality of through holes.
进一步地,多个所述通孔包括沿所述底板的长度方向对称布设的多个第一通孔和沿所述底板的宽度方向对称布设的多个第二通孔。Further, the plurality of through holes includes a plurality of first through holes symmetrically arranged along the length direction of the bottom plate and a plurality of second through holes symmetrically arranged along the width direction of the bottom plate.
有益效果Beneficial effect
本发明的有益效果:本发明的支撑架装配结构,由于支撑架的安装部与机壳底部的固定块之间通过快速插销连接,需要安装支撑架时,将固定块装配于安装部后,使两者的插接孔对齐,将快速插销插入插接孔中,安装部与固定块固定,从而将支撑架安装于机壳的底部,并且快速插销设有按钮,按下按钮后可将快速插销从插接孔拔出,使支撑架从机壳上脱离,支撑架的拆装操作非常便捷。The beneficial effects of the present invention: in the support frame assembly structure of the present invention, since the mounting part of the support frame and the fixed block at the bottom of the cabinet are connected by quick bolts, when the support frame needs to be installed, the fixing block is assembled behind the mounting part to make The insertion holes of the two are aligned, insert the quick plug into the insertion hole, the mounting part is fixed with the fixing block, so that the support frame is installed at the bottom of the casing, and the quick plug is equipped with a button, which can be pressed after the button is pressed Pull out from the plug hole to make the support frame detach from the casing, and the disassembly and assembly operation of the support frame is very convenient.
附图说明Description of the drawings
为了更清楚地说明本发明实施例中的技术方案,下面将对实施例或现有技术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发明的一些实施例,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 explain the technical solutions in the embodiments of the present invention more clearly, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the drawings in the following description are only of the present invention. For some embodiments, for those of ordinary skill in the art, other drawings can be obtained from these drawings without creative labor.
图1为本发明实施例提供的无人机的结构示意图;FIG. 1 is a schematic structural diagram of a drone provided by an embodiment of the present invention;
图2为图1所示无人机的侧视结构示意图;Figure 2 is a schematic side view of the structure of the UAV shown in Figure 1;
图3为图2所示无人机的部分立体结构示意图;Fig. 3 is a partial three-dimensional structure diagram of the UAV shown in Fig. 2;
图4为图3中A部的放大示意图;Fig. 4 is an enlarged schematic diagram of part A in Fig. 3;
图5为图1所示无人机中支撑架装配结构的侧视结构示意图;Figure 5 is a schematic side view of the structure of the support frame assembly structure in the UAV shown in Figure 1;
图6为图5所示支撑架装配结构的立体结构示意图;Fig. 6 is a three-dimensional structural diagram of the supporting frame assembly structure shown in Fig. 5;
图7为图6中B部的放大示意图;Fig. 7 is an enlarged schematic diagram of part B in Fig. 6;
图8为图1所示无人机的部分爆炸示意图;Figure 8 is a partial exploded schematic diagram of the UAV shown in Figure 1;
图9为图8中C部的放大示意图;Fig. 9 is an enlarged schematic diagram of part C in Fig. 8;
图10为图5所示支撑架装配结构中机壳的侧视结构示意图;10 is a schematic side view of the structure of the casing in the support frame assembly structure shown in FIG. 5;
图11为图5所示支撑架装配结构的部分爆炸示意图。Fig. 11 is a partial exploded schematic diagram of the assembly structure of the support frame shown in Fig. 5.
其中,图中各附图标记:Among them, the reference signs in the figure:
10—无人机         11—机壳         12—起落架10—UAV 11—Chassis 12—Landing gear
101—凹槽          100—固定块     110—定位凸起101-groove 100-fixed block 110—Locating bump
111—配合斜面    112—贯穿孔     120—连接部     111-Cooperate with slope 112-Through hole 120-Connecting Department
20—支撑架        210—底板         212—通孔       20-Support frame 210-Bottom plate 212-Through hole
220—安装块      221—插接孔      222—定位凹槽   220—mounting block 221—plug hole 222—positioning groove
223—装配斜面   230—内六角螺钉 240—夹板       223—Assembly inclined surface 230—Hexagon socket screw 240—Plywood
300—快速插销。300—Quick latch.
本发明的最佳实施方式The best mode of the invention
在此处键入本发明的最佳实施方式描述段落。Type here a paragraph describing the best mode of the invention.
本发明的实施方式Embodiments of the invention
下面详细描述本发明的实施例,所述实施例的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。The embodiments of the present invention are described in detail below. Examples of the embodiments are shown in the accompanying drawings, in which the same or similar reference numerals indicate the same or similar elements or elements with the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention, but should not be construed as limiting the present invention.
在本发明的描述中,需要理解的是,术语“长度”、“宽度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”“内”、“外”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 the description of the present invention, it should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", The orientation or positional relationship indicated by "horizontal", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, not It indicates or implies that the pointed device or element must have a specific orientation, be configured and operated in a specific orientation, and therefore cannot be understood as a limitation of the present invention.
此外,术语“第一”、“第二”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”的特征可以明示或者隐含地包括一个或者更多个该特征。在本发明的描述中,“多个”的含义是两个或两个以上,除非另有明确具体的限定。In addition, the terms "first" and "second" are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include one or more of these features. In the description of the present invention, "plurality" means two or more than two, unless specifically defined otherwise.
在本发明中,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”、“固定”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。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, unless otherwise clearly defined and defined, the terms "installed", "connected", "connected", "fixed" and other terms should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection. , Or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the internal communication of two components or the interaction relationship between two components. For those of ordinary skill in the art, the specific meaning of the above-mentioned terms in the present invention can be understood according to specific circumstances.
如图1~2所示,本发明实施例提供的支撑架20装配结构,应用于无人机10,例如具有灭火功能的无人机10。如图2~4所示,支撑架20装配结构包括机壳11、支撑架20和快速插销300。机壳11的底面设有固定块100,机壳11内设有控制器和电池等。支撑架20的顶端设有安装部,安装块220与固定块100配合使用,安装部和固定块100的对应位置分别开设有插接孔221,插接孔221的轴线可设置为与水平方向平行。快速插销300插接于插接孔221,固定块100通过快速插销300与安装部连接固定,如此,通过快速插销300将支撑架20固定在机壳11上,即完成支撑架20的安装;快速插销300设有按钮,该按钮被按压后快速插销300能从插接孔221脱离,进而使安装部从固定块100上脱离,如此支撑架20可从机壳11的底部取下,支撑架20的拆装操作都非常便捷。As shown in FIGS. 1 to 2, the support frame 20 assembly structure provided by the embodiment of the present invention is applied to an unmanned aerial vehicle 10, such as an unmanned aerial vehicle 10 with a fire fighting function. As shown in FIGS. 2 to 4, the assembly structure of the support frame 20 includes a casing 11, a support frame 20 and a quick plug 300. The bottom surface of the casing 11 is provided with a fixed block 100, and the casing 11 is provided with a controller and a battery. The top end of the support frame 20 is provided with a mounting part. The mounting block 220 is used in conjunction with the fixing block 100. The corresponding positions of the mounting part and the fixing block 100 are respectively provided with insertion holes 221. The axis of the insertion holes 221 can be set parallel to the horizontal direction. . The quick plug 300 is inserted into the insertion hole 221, and the fixing block 100 is connected and fixed with the installation part through the quick plug 300. In this way, the support frame 20 is fixed to the casing 11 by the quick plug 300, and the installation of the support frame 20 is completed; The latch 300 is provided with a button. After the button is pressed, the quick latch 300 can be disengaged from the insertion hole 221, thereby disengaging the mounting portion from the fixing block 100, so that the support frame 20 can be removed from the bottom of the casing 11, and the support frame 20 The disassembly and assembly operations are very convenient.
本实施例提供的支撑架20装配结构,由于支撑架20的安装部与机壳11底部的固定块100之间通过快速插销300连接,需要安装支撑架20时,将固定块100装配于安装部后,两者的插接孔221对齐,将快速插销300插入插接孔221中,安装部与固定块100固定,从而将支撑架20安装于机壳11的底部,并且快速插销300设有按钮,按下按钮后可将快速插销300从插接孔221拔出,使支撑架20从机壳11上脱离,支撑架20的拆装操作非常便捷。In the assembling structure of the support frame 20 provided in this embodiment, since the mounting portion of the support frame 20 is connected to the fixing block 100 at the bottom of the casing 11 through a quick-release pin 300, when the support frame 20 needs to be installed, the fixing block 100 is assembled to the mounting portion After that, the insertion holes 221 of the two are aligned, the quick plug 300 is inserted into the insertion hole 221, the mounting part is fixed to the fixing block 100, so that the support frame 20 is installed on the bottom of the casing 11, and the quick plug 300 is provided with a button After pressing the button, the quick-release pin 300 can be pulled out from the insertion hole 221, so that the support frame 20 can be separated from the casing 11, and the disassembly and assembly operation of the support frame 20 is very convenient.
快速插销300为标准件,快速插销300包括芯轴、插销轴、轴套、回位弹簧和按钮,芯轴滑动嵌设于插销轴内,插销轴靠近前端处开设有容置孔,容置孔内收容有钢珠,芯轴的前端设有斜面槽,在自然状态下,钢珠的一部分伸出于插销轴,轴套固定于插销轴的后端,按钮连接于芯轴的后端且伸出于轴套,芯轴和插销轴相对的两端的外周壁分别设有限位台,回位弹簧卡设于两限位台之间且收容于芯轴与插销轴之间。使用快速插销300时,将插销轴插设于插接孔221内,钢珠与插接孔221的孔壁相抵,使快速插销300相对于插接孔221的孔壁固定,需要将快速插销300拔出时,按压按钮,芯轴向前移动一段距离,钢珠落入斜面槽中,钢珠收容于容置孔和斜面槽中,此时钢珠不与插接孔221的孔壁接触或者只存在很小接触面积,可以很容易地将快速插销300从插接孔221内拔出。轴套的外壁可设有把手,以便于快速插销300插拔操作的施力。The quick bolt 300 is a standard part. The quick bolt 300 includes a mandrel, a bolt shaft, a bushing, a return spring and a button. The mandrel is slidably embedded in the bolt shaft, and the bolt shaft is provided with a receiving hole near the front end. A steel ball is contained inside, and the front end of the mandrel is provided with a beveled groove. In a natural state, a part of the steel ball extends from the bolt shaft, the sleeve is fixed to the rear end of the bolt shaft, and the button is connected to the rear end of the mandrel and extends from The outer peripheral walls of the opposite ends of the shaft sleeve, the core shaft and the bolt shaft are respectively provided with limit tables, and the return spring is clamped between the two limit tables and is accommodated between the core shaft and the bolt shaft. When using the quick plug 300, insert the pin shaft into the plug hole 221, and the steel ball abuts against the wall of the plug hole 221, so that the quick plug 300 is fixed relative to the wall of the plug hole 221, and the quick plug 300 needs to be pulled out When the button is pressed out, the core shaft moves forward a certain distance, the steel ball falls into the inclined groove, and the steel ball is contained in the receiving hole and the inclined groove. At this time, the steel ball does not contact the wall of the insertion hole 221 or only a small amount exists. The contact area can easily pull out the quick plug 300 from the plug hole 221. The outer wall of the shaft sleeve may be provided with a handle to facilitate the force application of the quick plug 300 plugging operation.
如图5、图10及图11所示,固定块100的顶部具有连接部120,固定块100和连接部120一体成型,机壳11的底部可通过螺丝固定有连接部120;机壳11的底面凹陷形成宽度适配连接部120的凹槽101,以使固定块100占用机壳11下方的空间的减小,进而使支撑架20与机壳11之间的装配空间较多。As shown in Figures 5, 10 and 11, the top of the fixed block 100 has a connecting portion 120, and the fixed block 100 and the connecting portion 120 are integrally formed. The bottom of the casing 11 can be fixed with a connecting portion 120 by screws; The bottom surface is recessed to form a groove 101 with a width adapted to the connecting portion 120, so that the space under the casing 11 occupied by the fixing block 100 is reduced, and thereby the assembly space between the support frame 20 and the casing 11 is larger.
如图6、图7所示,固定块100可设有镂空结构或者开设有贯穿孔,例如固定块100开设有贯穿前后的贯穿孔,如此可减轻固定块100的重量。As shown in FIG. 6 and FIG. 7, the fixing block 100 may be provided with a hollow structure or a through hole. For example, the fixing block 100 is provided with a through hole passing through the front and rear, so that the weight of the fixing block 100 can be reduced.
在一实施例中,如图2及图5~8所示,支撑架20包括底板210、安装块220和连接件。底板210可采用碳纤维板,底板210为水平布设,底板210可采用矩形板,连接件可设置为与底板210垂直,即连接件呈竖向布设。安装块220形成有安装部,连接件连接于底板210和安装块220之间,以使机壳11底面与底板210之间具有安装承载外部部件的承载空间;固定块100具有向下凸伸的定位凸起110,安装部凹陷形成有适配于定位凸起110的定位凹槽222,定位凸起110适配插设于定位凹槽222内,定位凸起110和定位凹槽222的槽壁的对应位置分别开设有插接孔221,快速插销300插接于插接孔221时,快速插销300穿设定位凹槽222。In one embodiment, as shown in FIGS. 2 and 5 to 8, the support frame 20 includes a bottom plate 210, a mounting block 220, and a connecting piece. The bottom plate 210 may be a carbon fiber board, the bottom plate 210 may be horizontally arranged, and the bottom plate 210 may be a rectangular plate, and the connecting pieces may be arranged perpendicular to the bottom plate 210, that is, the connecting pieces are arranged vertically. The mounting block 220 is formed with a mounting portion, and the connecting piece is connected between the bottom plate 210 and the mounting block 220, so that there is a bearing space between the bottom surface of the casing 11 and the bottom plate 210 for installing and bearing external components; the fixing block 100 has a downwardly protruding Positioning protrusion 110, the mounting portion is recessed to form a positioning groove 222 adapted to the positioning protrusion 110, the positioning protrusion 110 is adapted to be inserted into the positioning groove 222, the positioning protrusion 110 and the groove wall of the positioning groove 222 Inserting holes 221 are respectively opened at corresponding positions of, and when the quick plug 300 is inserted into the plug hole 221, the quick plug 300 passes through the setting groove 222.
在一实施例中,如图5~8所示,支撑架20设有两个安装块220,每个安装块220的顶面形成有两个安装部,共四个安装部,连接件对应设置有四个,每个安装块220与底板210之间连接有两个连接件,四个连接件围成的空间大致呈长方形,支撑架20整体呈框型且四侧和顶部开口,固定块100设有两个,两个固定块100分别设于机壳11底部靠近前后端处,每个固定块100的底面凸出形成有两个定位凸起110,即支撑架20前端和后端各两个安装部,前端的两个安装部对称布设,后端的两个安装部也对称布设,每个安装部的顶面分别凹陷形成定位凹槽222。在一实施方式中,定位凹槽222的纵截面呈梯形,对应的定位凸起110的纵截面呈梯形,可以理解的,定位凸起110的纵截面也可以是其它形成,如矩形等。In one embodiment, as shown in FIGS. 5 to 8, the support frame 20 is provided with two mounting blocks 220, and the top surface of each mounting block 220 is formed with two mounting parts, a total of four mounting parts, and the connecting parts are correspondingly arranged There are four. Two connecting pieces are connected between each mounting block 220 and the bottom plate 210. The space enclosed by the four connecting pieces is roughly rectangular. The supporting frame 20 is frame-shaped as a whole and has four sides and top openings. The fixing block 100 There are two, two fixed blocks 100 are respectively arranged at the bottom of the casing 11 near the front and rear ends, and the bottom surface of each fixed block 100 is protrudingly formed with two positioning protrusions 110, namely the front end and the rear end of the support frame 20. There are two mounting parts, the two mounting parts at the front end are arranged symmetrically, and the two mounting parts at the rear end are also arranged symmetrically. The top surface of each mounting part is recessed to form a positioning groove 222. In one embodiment, the longitudinal section of the positioning groove 222 is trapezoidal, and the longitudinal section of the corresponding positioning protrusion 110 is trapezoidal. It is understandable that the longitudinal section of the positioning protrusion 110 may also be formed in other shapes, such as a rectangle.
在一实施例中,如图6~9所示,安装块220的前侧或后侧开设有与定位凹槽222连通的装配缺口。也就是说,定位凹槽222的顶面和一侧面分别开口,侧面的装配缺口方便固定块100的定位凸起110适配插入定位凹槽222内,便于固定块100与安装块220之间的装配操作。在一实施方式中,靠近机壳11前端的两个安装块220与靠近机壳11后端的两个安装块220上相背离的一侧开设有装配缺口,即前端的两个安装块220的装配缺口的开设方向与后端的两个安装块220的装配缺口的开设方向相反,如此可便于安装时固定块100的定位,便于快速地将各定位块的定位凸起110与对应的定位凹槽222进行对位,对位时不易滑脱。In one embodiment, as shown in FIGS. 6 to 9, the front or rear side of the mounting block 220 is provided with an assembly notch communicating with the positioning groove 222. That is to say, the top surface and one side surface of the positioning groove 222 are respectively opened, and the assembly notch on the side facilitates the positioning protrusion 110 of the fixing block 100 to fit into the positioning groove 222, which facilitates the connection between the fixing block 100 and the mounting block 220. Assembly operation. In one embodiment, the two mounting blocks 220 close to the front end of the casing 11 and the two mounting blocks 220 close to the rear end of the casing 11 are provided with assembly notches on the opposite sides, that is, the two mounting blocks 220 at the front end are assembled The opening direction of the notch is opposite to the opening direction of the assembly notch of the two mounting blocks 220 at the rear end. This facilitates the positioning of the fixing block 100 during installation, and facilitates the quick connection of the positioning protrusion 110 of each positioning block to the corresponding positioning groove 222 It is not easy to slip off during alignment.
定位凹槽222的纵截面呈梯形,定位凹槽222与装配缺口相对的槽壁可设置为倾斜的槽壁,对应的,固定块100对应的一侧形成适配该槽壁的装配斜面223,如此,定位凹槽222的三个槽壁均形成装配斜面223,固定块100对应的三侧面形成配合斜面111,各装配斜面223与对应的配合斜面111相契合,如此,固定块100在安装时可借助各斜面产生滑动,从而与安装块220进行契合,达到更快速更精确地使两者的插接孔快速对齐的目的。The longitudinal section of the positioning groove 222 is trapezoidal. The groove wall of the positioning groove 222 opposite to the assembly notch can be set as an inclined groove wall. Correspondingly, an assembly inclined surface 223 adapted to the groove wall is formed on the corresponding side of the fixing block 100. In this way, the three groove walls of the positioning groove 222 all form assembling slopes 223, and the three corresponding sides of the fixing block 100 form mating slopes 111. Each of the assembling slopes 223 fits with the corresponding mating slope 111. In this way, the fixing block 100 is installed The slopes can be used to generate sliding movement to fit the mounting block 220 to achieve the purpose of quickly and accurately aligning the insertion holes of the two.
在一实施例中,如图1~4所示,底板210为水平布设,无人机10为灭火用无人机,无人机10的两侧搭载有灭火弹。无人机10底部设有起落架12,起落架12两侧的底部分别连接有水平设置的支撑杆,两平行的支持杆之间连接有两横杆,支撑架形成有用于固定两横杆的卡位。In one embodiment, as shown in FIGS. 1 to 4, the bottom plate 210 is arranged horizontally, the drone 10 is a drone for fire fighting, and both sides of the drone 10 are equipped with fire extinguishing bombs. The bottom of the UAV 10 is provided with a landing gear 12. The bottoms of the two sides of the landing gear 12 are respectively connected with horizontal support rods. Two parallel support rods are connected with two cross rods. The support frame is formed with two cross rods. Card bit.
如图4、图8及图9所示,安装块220的底部固定有夹板240,内六角螺钉230的穿过夹板240与安装块220螺接,夹板240与底板210之间形成适配卡固起落架12的横梁的卡位,即起落架12的横梁被夹紧于夹板240与底板210之间。夹板240大致为矩形板,夹板240对应安装块220的螺纹孔处对应开设有螺纹孔,夹板240可采用碳纤维板,以减轻整体重量。As shown in Figure 4, Figure 8 and Figure 9, the bottom of the mounting block 220 is fixed with a clamping plate 240. The hexagon socket screw 230 passes through the clamping plate 240 and is screwed to the mounting block 220. An adapter is formed between the clamping plate 240 and the bottom plate 210. The clamping position of the cross beam of the landing gear 12, that is, the cross beam of the landing gear 12 is clamped between the splint 240 and the bottom plate 210. The splint 240 is substantially a rectangular plate, and the splint 240 is provided with threaded holes corresponding to the threaded holes of the mounting block 220. The splint 240 can be a carbon fiber board to reduce the overall weight.
在一实施例中,如图5~7所示,连接件采用内六角螺钉230,内六角螺钉230包括具有内六角凹槽的头部和外周壁设有外螺纹的杆部,底板210和安装块220对应位置处分别开设有螺纹孔,杆部穿过两者的螺纹孔,即杆部分别与底板210和安装块220螺接固定,头部与底板210的底面相抵。四个内六角螺钉230分别穿设底板210的四个边角处。In one embodiment, as shown in FIGS. 5-7, the connecting member adopts a hexagon socket screw 230. The hexagon socket screw 230 includes a head with a hexagon socket and a rod with an external thread on the outer peripheral wall. The bottom plate 210 and the mounting The corresponding positions of the block 220 are respectively provided with threaded holes, the rods pass through the threaded holes of both, that is, the rods are screwed and fixed to the bottom plate 210 and the mounting block 220 respectively, and the head abuts against the bottom surface of the bottom plate 210. The four hexagon socket screws 230 penetrate through the four corners of the bottom plate 210 respectively.
在一实施例中,如图8所示,底板210开设有多个通孔212,开设通孔212可减轻底板210的重量,进而减轻支撑架20的重量。在一实施方式中,多个通孔212包括沿底板210的长度方向对称布设的多个第一通孔和沿底板210的宽度方向对称布设的多个第二通孔,如底板210整体呈矩形,在底板210开设有六个通孔,该六个通孔使得底板210中间形成米字型的镂空结构。In one embodiment, as shown in FIG. 8, the bottom plate 210 is provided with a plurality of through holes 212, and the through holes 212 can reduce the weight of the bottom plate 210, thereby reducing the weight of the support frame 20. In one embodiment, the plurality of through holes 212 include a plurality of first through holes symmetrically arranged along the length direction of the bottom plate 210 and a plurality of second through holes symmetrically arranged along the width direction of the bottom plate 210, for example, the bottom plate 210 is rectangular as a whole. , The bottom plate 210 is provided with six through holes, and the six through holes form a m-shaped hollow structure in the middle of the bottom plate 210.
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modification, equivalent replacement and improvement made within the spirit and principle of the present invention shall be included in the protection of the present invention. Within range.
工业实用性Industrial applicability
在此处键入工业实用性描述段落。Type a paragraph describing industrial applicability here.
序列表自由内容Sequence Listing Free Content
在此处键入序列表自由内容描述段落。Type here the free content description paragraph of the sequence listing.

Claims (10)

  1. 一种支撑架装配结构,其特征在于:包括:A supporting frame assembly structure, characterized in that it comprises:
    机壳,底部设有固定块;The cabinet has a fixed block at the bottom;
    支撑架,顶端设有与所述固定块配合的安装部,所述固定块适配插设于所述安装部,所述安装部和所述固定块的对应位置分别开设有插接孔;The support frame has a mounting portion at the top end that cooperates with the fixing block, the fixing block is adapted to be inserted into the mounting portion, and corresponding positions of the mounting portion and the fixing block are respectively provided with insertion holes;
    快速插销,插设于所述插接孔内,所述固定块通过所述快速插销与所述安装部连接固定,所述快速插销设有按钮,所述按钮被按压时所述快速插销能从所述插接孔脱离,进而使所述安装部能从所述固定块脱离。The quick plug is inserted in the insertion hole, the fixing block is connected and fixed to the mounting part by the quick plug, the quick plug is provided with a button, and the quick plug can be removed from the button when the button is pressed. The insertion hole is disengaged, so that the mounting part can be disengaged from the fixing block.
  2. 根据权利要求1所述的支撑架装配结构,其特征在于:所述支撑架包括水平设置的底板、安装块和连接于所述底板及所述安装块之间的连接件,所述安装块的顶部形成有所述安装部;所述固定块具有向下凸伸的定位凸起,所述安装部凹陷形成有适配于所述定位凸起的定位凹槽,所述定位凸起适配插设于所述定位凹槽内,所述定位凸起和所述安装部的对应位置分别开设有所述插接孔。The support frame assembly structure according to claim 1, wherein the support frame includes a horizontally arranged bottom plate, a mounting block, and a connector connected between the bottom plate and the mounting block, and the mounting block The top part is formed with the mounting part; the fixing block has a positioning protrusion protruding downward, the mounting part is recessed and formed with a positioning groove adapted to the positioning protrusion, and the positioning protrusion is adapted for insertion It is arranged in the positioning groove, and the corresponding positions of the positioning protrusion and the mounting portion are respectively provided with the insertion holes.
  3. 根据权利要求2所述的支撑架装配结构,其特征在于:所述机壳底部靠近前后端处分别设有一个所述固定块,所述支撑架设置有四个所述连接件和两个所述安装块,每个所述安装块的顶面分别形成有两个所述安装部,每个所述安装块与所述底板之间连接有两个所述连接件,四个所述连接件围成的空间大致呈长方形。The support frame assembly structure according to claim 2, characterized in that: the bottom of the casing near the front and rear ends are respectively provided with a fixed block, and the support frame is provided with four connecting members and two fixed blocks. In the mounting block, two mounting parts are respectively formed on the top surface of each mounting block, two connecting pieces are connected between each mounting block and the bottom plate, and four connecting pieces The enclosed space is roughly rectangular.
  4. 根据权利要求3所述的支撑架装配结构,其特征在于:所述安装块的前侧或后侧开设有与所述定位凹槽连通的装配缺口。The support frame assembly structure according to claim 3, wherein the front side or the rear side of the mounting block is provided with an assembly notch communicating with the positioning groove.
  5. 根据权利要求4所述的支撑架装配结构,其特征在于:靠近所述机壳前端的两个所述安装块与靠近所述机壳后端的两个所述安装块上相背离的一侧开设有所述装配缺口。The support frame assembly structure according to claim 4, wherein the two mounting blocks close to the front end of the casing and the two mounting blocks close to the rear end of the casing are opened on opposite sides. There is the assembly gap.
  6. 根据权利要求2所述的支撑架装配结构,其特征在于:所述连接件与所述底板垂直。The support frame assembly structure according to claim 2, wherein the connecting member is perpendicular to the bottom plate.
  7. 根据权利要求2所述的支撑架装配结构,其特征在于:所述连接件为内六角螺钉,所述内六角螺钉包括头部和设有外螺纹的杆部,所述杆部分别与所述底板和所述安装块螺纹连接,所述头部与所述底板的底面相抵。The support frame assembly structure according to claim 2, wherein the connecting member is a hexagon socket screw, and the hexagon socket screw includes a head and a rod part provided with an external thread, and the rod part is connected to the The bottom plate and the mounting block are threadedly connected, and the head abuts against the bottom surface of the bottom plate.
  8. 根据权利要求7所述的支撑架装配结构,其特征在于:所述安装块的底部固定有夹板,所述内六角螺钉的穿过所述夹板与所述安装块螺接。7. The support frame assembly structure according to claim 7, wherein a clamping plate is fixed at the bottom of the mounting block, and the hexagon socket screw passes through the clamping plate and is screwed to the mounting block.
  9. 根据权利要求1所述的支撑架装配结构,其特征在于:所述底板开设有多个通孔。The support frame assembly structure according to claim 1, wherein the bottom plate is provided with a plurality of through holes.
  10. 根据权利要求9所述的支撑架装配结构,其特征在于:多个所述通孔包括沿所述底板的长度方向对称布设的多个第一通孔和沿所述底板的宽度方向对称布设的多个第二通孔。The support frame assembly structure according to claim 9, wherein the plurality of through holes include a plurality of first through holes symmetrically arranged along the length direction of the bottom plate and a plurality of first through holes symmetrically arranged along the width direction of the bottom plate. A plurality of second through holes.
PCT/CN2020/095691 2019-06-18 2020-06-12 Support frame fitting structure WO2020253621A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201910538016.0 2019-06-18
CN201910538016.0A CN110271684A (en) 2019-06-18 2019-06-18 Support frame assembling structure

Publications (1)

Publication Number Publication Date
WO2020253621A1 true WO2020253621A1 (en) 2020-12-24

Family

ID=67961197

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2020/095691 WO2020253621A1 (en) 2019-06-18 2020-06-12 Support frame fitting structure

Country Status (2)

Country Link
CN (1) CN110271684A (en)
WO (1) WO2020253621A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110271684A (en) * 2019-06-18 2019-09-24 深圳高度创新技术有限公司 Support frame assembling structure

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB678132A (en) * 1951-03-14 1952-08-27 Dowty Equipment Ltd Improvements relating to push button electric switches
US7296375B2 (en) * 2003-05-08 2007-11-20 Michael Brunn Shotgun launching cup
CN205770123U (en) * 2016-05-16 2016-12-07 哈瓦国际航空技术(深圳)有限公司 A kind of unmanned plane propeller rapid dismounting apparatus
CN206984379U (en) * 2017-05-25 2018-02-09 青岛锐擎航空科技有限公司 A kind of medicine-chest retaining mechanism of plant protection unmanned plane
CN207737506U (en) * 2017-12-25 2018-08-17 广东西北航空科技股份有限公司 A kind of quick-locking device
CN108791806A (en) * 2018-06-22 2018-11-13 北京中飞东方航空科技有限公司 A kind of unmanned plane folding horn connector
CN108820188A (en) * 2018-06-20 2018-11-16 上海歌尔泰克机器人有限公司 A kind of Quick-dismantle component and unmanned plane
CN109760850A (en) * 2017-11-09 2019-05-17 成都博昱新能源有限公司 A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted
CN110271684A (en) * 2019-06-18 2019-09-24 深圳高度创新技术有限公司 Support frame assembling structure
CN305594522S (en) * 2019-06-18 2020-02-07

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206179949U (en) * 2016-11-11 2017-05-17 深圳市大疆创新科技有限公司 Unmanned aerial vehicle battery compartment and unmanned aerial vehicle
CN206437210U (en) * 2016-12-26 2017-08-25 国网辽宁省电力有限公司检修分公司 A kind of rotor Laser Radar Scanning unmanned plane
CN206782056U (en) * 2017-03-23 2017-12-22 西安天问智能科技有限公司 A kind of Portable unmanned machine landing gear structure
CN207029569U (en) * 2017-07-11 2018-02-23 广东容祺智能科技有限公司 A kind of unmanned plane load Quick Release interface arrangement
CN107572001A (en) * 2017-09-29 2018-01-12 成都鑫晨航空科技有限公司 A kind of Quick Release unmanned plane task platform interface and unmanned plane
CN207496958U (en) * 2017-11-06 2018-06-15 深圳市大智无疆科技有限公司 A kind of unmanned machine head quick-disassembly structure
CN108528739A (en) * 2018-03-09 2018-09-14 芜湖翼讯飞行智能装备有限公司 A kind of quick-disassembly structure for unmanned machine head
CN210310912U (en) * 2019-06-18 2020-04-14 深圳高度创新技术有限公司 Support frame assembly structure

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB678132A (en) * 1951-03-14 1952-08-27 Dowty Equipment Ltd Improvements relating to push button electric switches
US7296375B2 (en) * 2003-05-08 2007-11-20 Michael Brunn Shotgun launching cup
CN205770123U (en) * 2016-05-16 2016-12-07 哈瓦国际航空技术(深圳)有限公司 A kind of unmanned plane propeller rapid dismounting apparatus
CN206984379U (en) * 2017-05-25 2018-02-09 青岛锐擎航空科技有限公司 A kind of medicine-chest retaining mechanism of plant protection unmanned plane
CN109760850A (en) * 2017-11-09 2019-05-17 成都博昱新能源有限公司 A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted
CN207737506U (en) * 2017-12-25 2018-08-17 广东西北航空科技股份有限公司 A kind of quick-locking device
CN108820188A (en) * 2018-06-20 2018-11-16 上海歌尔泰克机器人有限公司 A kind of Quick-dismantle component and unmanned plane
CN108791806A (en) * 2018-06-22 2018-11-13 北京中飞东方航空科技有限公司 A kind of unmanned plane folding horn connector
CN110271684A (en) * 2019-06-18 2019-09-24 深圳高度创新技术有限公司 Support frame assembling structure
CN305594522S (en) * 2019-06-18 2020-02-07

Also Published As

Publication number Publication date
CN110271684A (en) 2019-09-24

Similar Documents

Publication Publication Date Title
US20230366503A1 (en) Quick Connection Mechanism
WO2019232941A1 (en) Wing of unmanned aerial vehicle and unmanned aerial vehicle
CN112520011A (en) Quick-release quick-lock structure and method and unmanned aerial vehicle
WO2020253621A1 (en) Support frame fitting structure
US9995992B2 (en) Telescopic limiting structure, camera body and camera
WO2020119248A1 (en) Frame for aircraft and aircraft
EP3450885A1 (en) Ice-maker/ice storage box assembly and refrigerator
CN113903272A (en) LED display device
CN210310912U (en) Support frame assembly structure
CN209767536U (en) Aircraft communication device based on mobile communication technology and aircraft with same
WO2022041468A1 (en) Inspection unmanned aerial vehicle
WO2019134406A1 (en) Unmanned aerial vehicle
CN116039981B (en) Adaptive multi-module assembled unmanned aerial vehicle
CN208915424U (en) A kind of detachable empennage bindiny mechanism
CN109643774A (en) Unmanned plane and its battery component, battery case
CN218181434U (en) Fixing structure device of communication product module assembly
CN115610685B (en) Unmanned aerial vehicle and rapid dismounting method thereof
WO2020062757A1 (en) Unmanned aerial vehicle and tilting mechanism
CN220915602U (en) LED display device
CN114296528B (en) Safe disassembly and assembly mechanism for main board and expansion board and server
CN218525271U (en) LED display device
CN217033576U (en) Visual inspection control device
CN110549621A (en) Quick detach formula nozzle structure and 3D printer
CN210284618U (en) Quick detach subassembly and unmanned aerial vehicle
CN218806726U (en) Unmanned aerial vehicle foot rest

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 20827214

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 20827214

Country of ref document: EP

Kind code of ref document: A1