WO2021258682A1 - 一种无人机机体柔性装配工装 - Google Patents

一种无人机机体柔性装配工装 Download PDF

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Publication number
WO2021258682A1
WO2021258682A1 PCT/CN2020/137458 CN2020137458W WO2021258682A1 WO 2021258682 A1 WO2021258682 A1 WO 2021258682A1 CN 2020137458 W CN2020137458 W CN 2020137458W WO 2021258682 A1 WO2021258682 A1 WO 2021258682A1
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Prior art keywords
assembly
lifting
aerial vehicle
unmanned aerial
hand wheel
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PCT/CN2020/137458
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English (en)
French (fr)
Inventor
李俊
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江苏新扬新材料股份有限公司
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Publication of WO2021258682A1 publication Critical patent/WO2021258682A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P21/00—Machines for assembling a multiplicity of different parts to compose units, with or without preceding or subsequent working of such parts, e.g. with programme control
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06—Work-clamping means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
    • B25B11/02—Assembly jigs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H1/00—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
    • B25H1/08—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby with provision for attachment of work holders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H1/00—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
    • B25H1/10—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby with provision for adjusting holders for tool or work
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H1/00—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
    • B25H1/14—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby with provision for adjusting the bench top
    • B25H1/16—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby with provision for adjusting the bench top in height
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor

Definitions

  • the invention relates to an auxiliary equipment for the production of an unmanned aerial vehicle, in particular to a flexible assembly tooling for an unmanned aerial vehicle body.
  • Frame is a very important part of UAV assembly.
  • the quality of the UAV assembly is mainly determined by the accuracy of the manufacturing and installation of the frame. Due to the large number of assembly jigs used in aircraft manufacturing and the long production cycle, the manufacturing and installation of assembly jigs occupies a large proportion in the preparation of aircraft production. Prototypes or functional verification machines in the conceptual design stage or pre-research stage have variable structural design, which has a greater impact on the design and manufacturing of the frame, and may even lead to the repair or scrapping of the frame. In some cases, it is necessary to redesign and manufacture the frame. Greatly affect the development cost, cycle, etc.
  • the purpose of the present invention is to provide a flexible assembly tooling for the body of the unmanned aerial vehicle, which makes the assembly of the unmanned aerial vehicle more convenient and improves the reliability of the assembly.
  • a flexible assembly tooling for the body of an unmanned aerial vehicle including an assembly platform, a plurality of columns, a plurality of beams, a plurality of pallets, and a plurality of pallets.
  • the beam is provided with a number of connection through holes, the column is installed on the assembly platform through the connection pin and the connection through hole, the beam is installed on a part of the column through the connection pin and the connection through hole, and the top of the other part of the column is installed
  • a pallet the pallet is connected with a clamping plate; the connected and assembled column and the beam form a mounting frame, and the mounting frame is provided with a lifting assembly, the lifting assembly includes a lifting cylinder fixed on the beam, so The lifting cylinder is provided with a lifting screw, a hand wheel is installed on the top of the lifting cylinder, the hand wheel is threadedly connected to the outer circumference of the screw, and the hand wheel and the screw form a ball screw pair.
  • the mounting frame includes four uprights and four crossbeams.
  • the four crossbeams are installed on the top of the four uprights to form a box-shaped frame body, and the top of the two crossbeams is also provided with one for mounting and lifting.
  • the beam of the component is also provided with one for mounting and lifting.
  • each surface of the assembly platform except for the bottom surface is provided with connection through holes.
  • the pallet is installed on the column through the connecting plate.
  • the invention uses the assembly platform, column and beam as the reference to design the positioning structure of each pallet support plate, and uses the connecting pin to quickly and efficiently connect the column with the assembly platform and the beam; different types of frames and different parts of the frame are assembled At this time, you only need to adjust the shape of the card board and the pallet or adjust the connection position with the column.
  • the present invention has the beneficial effects: the present invention shortens the design and manufacturing cycle of the profile frame and saves the cost of the profile frame manufacturing; in addition, the present invention can also be used for the assembly of the whole body of the drone, and can also be used For the assembly of various parts of the fuselage or wings.
  • Figure 1 is a schematic diagram of the first three-dimensional structure of the present invention.
  • Figure 2 is a second schematic diagram of the three-dimensional structure of the present invention.
  • Figure 3 is a schematic diagram of the structure of the lifting assembly of the present invention.
  • Figure 4 is a diagram of the state of use of the present invention.
  • 1 assembly platform 21, 22 columns, 3 beams, 4 pallets, 5 clamping plates, 6 connecting pins, 7 lifting components, 71 lifting cylinders, 72 screws, 73 hand wheels, 8 connecting plates.
  • An unmanned aerial vehicle body flexible assembly tooling as shown in Figure 1-4 including an assembly platform 1, a plurality of columns 21, 22, a plurality of beams 3, a plurality of pallets 4 and a plurality of pallets 5, the assembly platform 1
  • a number of connecting through holes are provided on the top surface, the columns 21, 22, and the beam 3, the columns 21, 22 are installed on the assembly platform 1 through the connecting pins 6 and the connecting holes, and the beam 3 is installed through the connecting pins 6 and the connecting holes.
  • a supporting plate 4 is installed on one part of the upright 22 and the top of the other part of the upright 21, and a clamping plate 5 is connected to the supporting plate 4; the assembled upright column 22 and the beam 3 are connected to form a mounting frame, and a lifting assembly 7 is provided on the mounting frame.
  • the mounting frame includes four uprights 21, 22 and four cross beams 3.
  • the four cross beams 3 are installed on the tops of the four uprights 21, 22 to form a box-shaped frame body, and the top of the two cross beams 3 is also provided with one for installation and lifting
  • the wheel 73 and the hand wheel 73 are threadedly connected to the outer circumference of the screw 72.
  • the hand wheel 73 and the screw 72 form a ball screw pair.
  • the screw 72 can be raised and lowered by rotating the hand wheel 73.
  • the assembly platform 1 is provided on all sides except the bottom surface. Connecting through holes, the support plate 4 is installed on the uprights 21 and 22 through the connecting plate 8.
  • the pallet 5 is first retracted to the highest point through the lifting assembly 7, the aircraft parts are positioned and assembled on the pallet 4, and finally the pallet 5 is put down to align with the pallet 4 to install the upper and lower skins of the aircraft
  • the present invention is not limited to the above-mentioned embodiments.
  • those skilled in the art can make some substitutions and replacements for some of the technical features without creative work according to the disclosed technical content. Deformations, these replacements and deformations are all within the protection scope of the present invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

一种无人机机体柔性装配工装，包括装配平台（1）、多个立柱（21,22）、多个横梁（3）、多个托板（4）以及多个卡板（5），装配平台（1）顶面、立柱（21,22）上、横梁（3）上均开设有若干连接通孔，立柱（21,22）通过连接销（6）配合连接通孔安装在装配平台（1）上，横梁（3）通过连接销（6）配合连接通孔安装在一部分立柱（21,22）上，另一部分立柱（21,22）的顶部安装有托板（4），托板（4）上连接有卡板（5）；连接装配好的立柱（21,22）与横梁（3）组成安装架，安装架上设置有升降组件（7），升降组件（7）包括固定在横梁（3）上的升降筒（71），升降筒（71）内设置有可升降的螺杆（72），升降筒（71）的顶部安装有手轮（73），手轮（73）螺纹连接在螺杆（72）外周，手轮（73）与螺杆（72）形成滚珠丝杠副，上述工装使得无人机的装配更加方便，提高了装配的可靠性。

Description

一种无人机机体柔性装配工装 技术领域
本发明涉及一种无人机生产辅助设备，特别涉及一种无人机机体柔性装配工装。
背景技术
型架是无人机装配中一个非常重要的环节。无人机装配的质量主要决定于型架的制造和安装准确。由于飞机制造中使用的装配型架数量多，生产周期长，装配型架的制造和安装工作在飞机生产准备工作中占有很大的比重。处于方案设计阶段或预研阶段的样机或功能验证机，结构设计多变，对型架的设计、制造影响更大，甚至会导致型架返修或报废，个别情况需要重新设计制造型架，会较大的影响研制成本、周期等。
发明内容
本发明的目的是提供一种无人机机体柔性装配工装，使得无人机的装配更加方便，提高装配的可靠性。
本发明的目的是这样实现的：一种无人机机体柔性装配工装，包括装配平台、多个立柱、多个横梁、多个托板以及多个卡板，所述装配平台顶面、立柱上、横梁上均开设有若干连接通孔，所述立柱通过连接销配合连接通孔安装在装配平台上，所述横梁通过连接销配合连接通孔安装在一部分立柱上，另一部分立柱的顶部安装有托板，所述托板上连接有卡板；所述连接装配好的立柱与横梁组成安装架，所述安装架上设置有升降组件，所述升降组件包括固定在横梁上的升降筒，所述升降筒内设置有可升降的螺杆，所述升降筒的顶部安装有手轮，所述手轮螺纹连接在螺杆外周，所述手轮与螺杆形成滚 珠丝杠副。
作为本发明的进一步限定，所述安装架包括四根立柱和四根横梁，四根横梁安装在四根立柱的顶部，形成方框形架体，其中两横梁顶部还设置有一根用以安装升降组件的横梁。
作为本发明的进一步限定，所述装配平台上除底面外其余各面均开设有连接通孔。
作为本发明的进一步限定，所述托板通过连接板安装在立柱上。
本发明以装配平台、立柱、横梁为基准设计各卡板托板等定位结构，利用连接销快速进行高效率的连接立柱与装配平台、横梁；在进行不同型号的型架以及型架不同部位装配时，只需调整卡板和托板的形状或调整与立柱的连接位置即可。与现有技术相比，本发明的有益效果在于：本发明缩短了型架设计制造周期，节省了型架制造费用；此外，本发明还能用于无人机整机机体的装配，还可用于机身或机翼各部件的装配。
附图说明
图1为本发明立体结构示意图一。
图2为本发明立体结构示意图二。
图3为本发明中升降组件结构示意图。
图4为本发明使用状态图。
其中，1装配平台，21、22立柱，3横梁，4托板，5卡板，6连接销，7升降组件，71升降筒，72螺杆，73手轮，8连接板。
具体实施方式
如图1-4所示的一种无人机机体柔性装配工装，包括装配平台1、多个立柱21、22、多个横梁3、多个托板4以及多个卡板5，装配平台1顶面、 立柱21、22上、横梁3上均开设有若干连接通孔，立柱21、22通过连接销6配合连接通孔安装在装配平台1上，横梁3通过连接销6配合连接通孔安装在一部分立柱22上，另一部分立柱21的顶部安装有托板4，托板4上连接有卡板5；连接装配好的立柱22与横梁3组成安装架，安装架上设置有升降组件7，安装架包括四根立柱21、22和四根横梁3，四根横梁3安装在四根立柱21、22的顶部，形成方框形架体，其中两横梁3顶部还设置有一根用以安装升降组件7的横梁3，升降组件7包括固定在横梁3上的升降筒71，升降筒71内设置有可升降的螺杆72，螺杆72的底部连接有卡板5，升降筒71的顶部安装有手轮73，手轮73螺纹连接在螺杆72外周，手轮73与螺杆72形成滚珠丝杠副，通过旋转手轮73可实现螺杆72的升降，装配平台1上除底面外其余各面均开设有连接通孔，托板4通过连接板8安装在立柱21、22上。
本发明使用时，首先将卡板5通过升降组件7收至最高处，将飞机零件在托板4上定位组装在一起，最后将卡板5放下与托板4相合对飞机上下蒙皮进行安装
本发明并不局限于上述实施例，在本发明公开的技术方案的基础上，本领域的技术人员根据所公开的技术内容，不需要创造性的劳动就可以对其中的一些技术特征作出一些替换和变形，这些替换和变形均在本发明的保护范围内。

Claims (4)

  1. 一种无人机机体柔性装配工装，其特征在于，包括装配平台、多个立柱、多个横梁、多个托板以及多个卡板，所述装配平台顶面、立柱上、横梁上均开设有若干连接通孔，所述立柱通过连接销配合连接通孔安装在装配平台上，所述横梁通过连接销配合连接通孔安装在一部分立柱上，另一部分立柱的顶部安装有托板，所述托板上连接有卡板；所述连接装配好的立柱与横梁组成安装架，所述安装架上设置有升降组件，所述升降组件包括固定在横梁上的升降筒，所述升降筒内设置有可升降的螺杆，所述升降筒的顶部安装有手轮，所述手轮螺纹连接在螺杆外周，所述手轮与螺杆形成滚珠丝杠副。
  2. 根据权利要求1所述的一种无人机机体柔性装配工装，其特征在于，所述安装架包括四根立柱和四根横梁，四根横梁安装在四根立柱的顶部，形成方框形架体，其中两横梁顶部还设置有一根用以安装升降组件的横梁。
  3. 根据权利要求1或2所述的一种无人机机体柔性装配工装，其特征在于，所述装配平台上除底面外其余各面均开设有连接通孔。
  4. 根据权利要求1或2所述的一种无人机机体柔性装配工装，其特征在于，所述托板通过连接板安装在立柱上。
PCT/CN2020/137458 2020-06-22 2020-12-18 一种无人机机体柔性装配工装 WO2021258682A1 (zh)

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CN101813550A (zh) * 2009-11-05 2010-08-25 吉林大学 一体式铁路车辆转向架参数动态测试台
CN102825413A (zh) * 2012-09-10 2012-12-19 北京二七轨道交通装备有限责任公司 转向架构架的组焊工装
CN106218810A (zh) * 2016-08-31 2016-12-14 中船黄埔文冲船舶有限公司 一种多用途船舶建造用的装配平台
CN107335948A (zh) * 2017-05-17 2017-11-10 沪东中华造船(集团)有限公司 一种t型材快速组装工装
CN207255721U (zh) * 2017-08-08 2018-04-20 沈阳东友航空技术有限公司 圆柱形材料打孔用夹具
CN108725693A (zh) * 2018-07-10 2018-11-02 大连壹海科技有限公司 船舶立体分段生产流水线

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040093731A1 (en) * 2002-11-14 2004-05-20 The Boeing Company Adjustable system and method for supporting and joining structural members
CN101813550A (zh) * 2009-11-05 2010-08-25 吉林大学 一体式铁路车辆转向架参数动态测试台
CN102825413A (zh) * 2012-09-10 2012-12-19 北京二七轨道交通装备有限责任公司 转向架构架的组焊工装
CN106218810A (zh) * 2016-08-31 2016-12-14 中船黄埔文冲船舶有限公司 一种多用途船舶建造用的装配平台
CN107335948A (zh) * 2017-05-17 2017-11-10 沪东中华造船(集团)有限公司 一种t型材快速组装工装
CN207255721U (zh) * 2017-08-08 2018-04-20 沈阳东友航空技术有限公司 圆柱形材料打孔用夹具
CN108725693A (zh) * 2018-07-10 2018-11-02 大连壹海科技有限公司 船舶立体分段生产流水线

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