WO2023159691A1 - 一种航空设备电路板焊接装置 - Google Patents

一种航空设备电路板焊接装置 Download PDF

Info

Publication number
WO2023159691A1
WO2023159691A1 PCT/CN2022/080815 CN2022080815W WO2023159691A1 WO 2023159691 A1 WO2023159691 A1 WO 2023159691A1 CN 2022080815 W CN2022080815 W CN 2022080815W WO 2023159691 A1 WO2023159691 A1 WO 2023159691A1
Authority
WO
WIPO (PCT)
Prior art keywords
circuit board
welding
telescopic cylinder
mounting
support
Prior art date
Application number
PCT/CN2022/080815
Other languages
English (en)
French (fr)
Inventor
石向阳
Original Assignee
滨州学院
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 滨州学院 filed Critical 滨州学院
Publication of WO2023159691A1 publication Critical patent/WO2023159691A1/zh

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K3/00—Tools, devices, or special appurtenances for soldering, e.g. brazing, or unsoldering, not specially adapted for particular methods
    • B23K3/08—Auxiliary devices therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K3/00—Tools, devices, or special appurtenances for soldering, e.g. brazing, or unsoldering, not specially adapted for particular methods
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K3/00—Apparatus or processes for manufacturing printed circuits
    • H05K3/30—Assembling printed circuits with electric components, e.g. with resistor
    • H05K3/32—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits
    • H05K3/34—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits by soldering

Definitions

  • the invention relates to the technical field of circuit board welding, in particular to an aviation equipment circuit board welding device.
  • the technical problem to be solved by the present invention is the low efficiency of circuit board welding in the prior art.
  • the present invention provides a kind of aviation equipment circuit board welding device, the technical scheme that it adopts is as follows:
  • An aviation equipment circuit board welding device the device includes a support platform, a jacking cylinder is arranged on the support platform, the output end of the jacking cylinder is connected to a mounting plate, and at least one welding mechanism is installed on the mounting plate,
  • the welding mechanism includes a first telescopic cylinder, a first mounting assembly, a second mounting assembly, a second telescopic cylinder and a welding head, the first telescopic cylinder is installed at the lower end of the mounting plate, and the output of the first telescopic cylinder The end is connected to the first installation assembly to drive the first installation assembly to move laterally, the second telescopic cylinder is installed on the first installation assembly, and the output end of the second telescopic cylinder is connected to the welding head.
  • the two welding mechanisms are arranged symmetrically with respect to the mounting plate.
  • the welding head is arranged obliquely, and is driven by the second telescopic cylinder to move back and forth along the inclination direction of the welding head.
  • the output end of the second telescopic cylinder is connected to a rotating motor, and the output end of the rotating motor is connected to the welding head.
  • the first mounting assembly includes a first connecting rod and a first mounting block, one end of the first connecting rod is connected to the output end of the first telescopic cylinder, and the other end of the first connecting rod is fixedly connected to
  • the first installation block has first installation holes installed on the first installation block, and several first fastening holes are arranged on the first installation block.
  • the second mounting assembly includes a second connecting rod and a second mounting block, the second connecting rod is fixedly mounted on the first mounting block through the first mounting hole, and the second connecting rod
  • the second installation block is fixedly connected, and the second telescopic cylinder is installed on the second installation block.
  • the support platform includes a support base, a reinforcement plate, a vertical support plate and a horizontal support plate, the support base supports the horizontal support plate through the vertical support plate, and the jacking plate is installed on the horizontal support plate.
  • cylinder and an opening for the jacking cylinder to protrude is opened on the support plate, the installation plate is arranged below the horizontal support plate, and at least two of the stiffeners.
  • the device further includes a circuit board support, the circuit board support at least includes a circuit board support bottom plate, and the circuit board support bottom plate is provided with a fixing groove for fixing the circuit board and a plurality of through holes.
  • the circuit board support is fixed on the conveying mechanism through the plurality of through holes.
  • the device further includes a controller, and the controller is signal-connected with the jacking cylinder, the first telescopic cylinder and the second telescopic cylinder.
  • the present invention makes the welding head move up and down in the radial direction through the driving of the jacking cylinder, and makes the welding head move back and forth in the lateral direction under the drive of the first telescopic cylinder, and drives the welding head through the second telescopic cylinder.
  • the welding head moves back and forth along the tilting direction of the welding head.
  • the present invention can automatically weld each position of the circuit board.
  • the overall device can be realized based on intelligence, which greatly improves the PCB soldering efficiency.
  • Fig. 1 is a perspective view of an aviation equipment circuit board welding device according to an embodiment of the present invention.
  • Fig. 2 is a front view of an aviation equipment circuit board welding device according to an embodiment of the present invention.
  • Fig. 3 is a side view of an aviation equipment circuit board welding device according to an embodiment of the present invention.
  • 1 is a support platform
  • 101 is a support base
  • 102 is a reinforcement plate
  • 103 is a vertical support plate
  • 104 is a horizontal support plate
  • 2 is a jacking cylinder
  • 3 is a mounting plate
  • 4 is a welding mechanism
  • 401 is the first Telescopic cylinder
  • 402 is the first mounting component
  • 4021 is the first connecting rod
  • 4022 is the first mounting block
  • 4023 is the first mounting hole
  • 4024 is the first fastening hole
  • 403 is the second mounting component
  • 4031 is the second Connecting rod
  • 4032 is the second mounting block
  • 404 is the second telescopic cylinder
  • 405 is the welding head
  • 406 is the rotating motor
  • 5 is the circuit board support
  • 501 is the support base
  • 502 is the fixing groove
  • 503 is the through hole, 6 for the motor.
  • the present invention provides a circuit board welding device for aviation equipment
  • the device includes a support platform 1, a jacking cylinder 2 is arranged on the support platform 1, and the output end of the jacking cylinder 2 Connect the mounting plate 3, and at least one welding mechanism 4 is installed on the mounting plate 3, and the welding mechanism includes a first telescopic cylinder 401, a first mounting assembly 402, a second mounting assembly 403, a second telescopic cylinder 404 and a welding head 405, the first telescopic cylinder 401 is installed at the lower end of the installation plate 3, and the output end of the first telescopic cylinder 401 is connected to the first installation assembly 402 to drive the first installation assembly 402 to move laterally.
  • the second telescopic cylinder 404 is installed on the first mounting assembly 402 , and the output end of the second telescopic cylinder 404 is connected to the welding head 405 .
  • the circuit board can be fixed by the circuit board tooling, and the movement of each cylinder is controlled to make the welding head 405 move correspondingly according to the needs of the welding point, so as to realize the welding accuracy. need.
  • the welding structure 4 can be arranged in multiples according to actual needs. As an example only, in the device shown in FIG. 1 and FIG. 2 , there are two welding mechanisms 4 , and the two welding mechanisms 4 are arranged symmetrically with respect to the installation plate 3 .
  • the vertical height of the welding head 405 is adjusted by lifting the cylinder 2, so as to be suitable for welding circuit boards of different thicknesses.
  • the jacking cylinder 2 stops working.
  • the function of the jacking cylinder 2 is mainly to adjust the position of the overall welding mechanism 4. According to the thickness of different batches of circuit boards, it can be properly adjusted on the same welding production line. Manufactured by welding suitable for each batch of circuit boards.
  • the first installation assembly 402 is driven by the first telescopic cylinder 401 to move, and then the second installation assembly 403 drives the second telescopic cylinder 402 installed to move to find the welding point.
  • the second telescopic cylinder 402 drives the welding head 405 to perform welding on the preset welding point on the circuit board. The whole process can be based on automated control.
  • the device further includes a controller, and the controller is signal-connected with the jacking cylinder 2 , the first telescopic cylinder 401 and the second telescopic cylinder 404 .
  • the controller described herein may be a PLC controller or a device with a controller that can play a controlling role. For example, PC platform, etc.
  • the embodiment of the present invention does not limit the specific type of the controller.
  • the welding head 405 can be arranged obliquely and driven by the second telescopic cylinder to move back and forth along the inclination direction of the welding head 405 .
  • the output end of the second telescopic cylinder 404 is connected to a rotating motor 406 , and the output end of the rotating motor 406 is connected to the welding head 405 .
  • the welding head 405 may be in a rotating state driven by the rotating motor 406 to improve the welding effect.
  • the first mounting assembly 402 includes a first connecting rod 4021 and a first mounting block 4022, one end of the first connecting rod 4021 is connected to the output end of the first telescopic cylinder 401, the The other end of the first connecting rod 4021 is fixedly connected to the first mounting block 4022, and the first mounting hole 4023 is installed on the first mounting block 4022, and several first fastening holes 4023 are arranged on the first mounting block 4022. Hole 4024.
  • the first installation component 402 mainly plays the role of connection and support, wherein the first connecting rod 4021 plays the role of connection, so that the driving force of the first telescopic cylinder 401 can be transmitted to the first installation block 4022 .
  • the first installation block 4022 plays a role of supporting and installing the second installation component 403 .
  • a first installation hole 4023 is provided, and several first fastening holes 4024 are provided on the first installation block 4022, so that in the process of stably installing the second installation assembly 403, it is also possible to Facilitate disassembly.
  • the first fastening hole 4024 can be fastened in the form of bolts or screws.
  • the second mounting assembly 403 includes a second connecting rod 4031 and a second mounting block 4032, and the second connecting rod 4031 is fixedly mounted on the first mounting hole 4023 through the first mounting hole.
  • the second connecting rod 4031 is fixedly connected to the second installation block 4032, and the second telescopic cylinder 404 is installed on the second installation block 4032.
  • the second installation component 403 is mainly used to install the second telescopic cylinder 404, and the second telescopic cylinder 404 is used to connect the welding head 405, so as to ensure the stable operation of the whole welding mechanism.
  • the second connecting rod 4031 may be rotatably mounted on the first mounting block 4022 , and at this time, the first fastening hole 4024 serves as a limit protection.
  • the second connecting rod 4022 is connected to the motor 6 , and during the welding process, the second connecting rod 4022 can be driven to rotate by the motor 6 to enrich the welding track of the welding head 405 .
  • the support platform 1 includes a support base 101, a reinforcing plate 102, a vertical support plate 103 and a horizontal support plate 104, and the support base 101 supports the The horizontal support plate 104, the jacking cylinder 2 is installed on the horizontal support plate 104, and an opening for the jacking cylinder to extend is provided on the support plate 104, and the mounting plate 3 is arranged on the Below the horizontal support plate 104 , at least two reinforcement plates 102 are arranged between the support base 101 and the vertical support plate 103 .
  • the device further includes a circuit board support 5, the circuit board support 5 at least includes a circuit board support bottom plate 501, and the circuit board support bottom plate 501 is provided with a The fixing groove 502 of the circuit board and a plurality of through holes 503 .
  • the circuit board supporting member 5 is fixed on the conveying mechanism through the plurality of through holes 503 .
  • the circuit board support 5 is essentially a jig tool for installing the circuit board to be soldered.
  • the embodiment of the present invention is only an example of a clamp tool, and various clamp tools in the prior art can also be used to fix the circuit board when the circuit board is soldered in the embodiment of the present invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Combinations Of Printed Boards (AREA)
  • Electric Connection Of Electric Components To Printed Circuits (AREA)

Abstract

一种航空设备电路板焊接装置，包括支撑平台（1），支撑平台上设置顶升气缸（2），顶升气缸的输出端连接安装板（3），安装板上安装有至少一个焊接机构（4），焊接机构包括第一伸缩气缸（401）、第一安装组件（402）、第二安装组件（403）、第二伸缩气缸（404）以及焊接头（405），第一伸缩气缸安装在安装板下端，第一伸缩气缸的输出端连接第一安装组件，以驱动第一安装组件横向移动，第一安装组件上安装第二伸缩气缸，第二伸缩气缸的输出端连接焊接头。该焊接装置基于智能化实现，大大提升了电路板的焊接效率。

Description

一种航空设备电路板焊接装置 技术领域
本发明涉及电路板焊接技术领域，特别涉及一种航空设备电路板焊接装置。
背景技术
航空设备中存在有大量的电路板，电路板在制备的过程中，焊接是必不可少的工艺之一。现有电路板生产过程中对电路板上的电子元件进行焊接操作时，操作人员一手拿烙铁，另一手拿锡丝，先将电子元器件插入电路板的孔洞中，再将电路板翻转过来进行焊接固定。这种方式工作效率低，不能满足航空设备所需的批量电路板的需求。
发明内容
本发明需解决的技术问题是现有技术中的电路板焊接效率低下的问题。
为了解决上述问题，本发明提供一种航空设备电路板焊接装置，其采用的技术方案如下：
一种航空设备电路板焊接装置，所述装置包括支撑平台，所述支撑平台上设置顶升气缸，所述顶升气缸的输出端连接安装板，所述安装板上安装有至少一个焊接机构，所述焊接机构包括第一伸缩气缸、第一安装组件、第二安装组件、第二伸缩气缸以及焊接头，所述第一伸缩气缸安装在所述安装板下端，所述第一伸缩气缸的输出端连接所述第一安装组件，以驱动所述第一安装组件横向移动，所述第一安装组件上安装所述第二伸缩气缸，所述第二伸缩气缸的输出端连接所述焊接头。
优选的，所述焊接机构设置为两个，两个所述焊接机构关于所述安装板对称布设。
优选的，所述焊接头倾斜布设，并由所述第二伸缩气缸驱动沿着所述焊接头的倾斜方向来回移动。
优选的，所述第二伸缩气缸的输出端连接一旋转电机，所述旋转电机的输出端连接所述焊接头。
优选的，所述第一安装组件包括第一连接杆以及第一安装块，所述第一连接杆的一端连接所述第一伸缩气缸的输出端，所述第一连接杆的另一端固定连接所述第一安装块，所述第一安装块上安装有第一安装孔，并在所述第一安装块上设置若干第一紧固孔。
优选的，所述第二安装组件包括第二连接杆以及第二安装块，所述第二连接杆通过所述第一安装孔固定安装在所述第一安装块上，所述第二连接杆固定连接所述第二安装块，并且所述第二安装块上安装所述第二伸缩气缸。
优选的，所述支撑平台包括支撑底座、加固板、垂直支撑板以及水平支撑板，所述支撑底座通过所述垂直支撑板支撑所述水平支撑板，所述水平支撑板上安装所述顶升气缸，并在所述支撑板上开设有用于所述顶升气缸伸出的开口，所述安装板设置在所述水平支撑板的下方，所述支撑底座与所述垂直支撑板之间设置至少两个所述加固板。
优选的，所述装置还包括电路板支撑件，所述电路板支撑件至少包括电路板支撑底板，所述电路板支撑底板上设置有用于固定电路板的固定槽以及多个通孔。
优选的，所述电路板支撑件通过所述多个通孔固定在输送机构上。
优选的，所述装置还包括控制器，所述控制器与所述顶升气缸、所述第一伸缩气缸以及所述第二伸缩气缸信号连接。
本发明的有益效果是：本发明通过顶升气缸的驱动以使得焊接头在径向上下移动，并通过第一伸缩气缸的驱动下使得焊接头在横向上来回移动，通过第二伸缩气缸的驱动下使得焊接头沿着所述焊接头的倾斜方向来回移 动，三个气缸的联合作用下，使得本发明可以自动化地对电路板各个位置进行焊接，整体装置可以基于智能化实现，大大提升地了电路板的焊接效率。
附图说明
图1为本发明一实施例的一种航空设备电路板焊接装置的立体图。
图2为本发明一实施例的一种航空设备电路板焊接装置的前视图；以及
图3为本发明一实施例的一种航空设备电路板焊接装置的侧视图。
图中，1为支撑平台，101为支撑底座，102为加固板，103为垂直支撑板，104为水平支撑板，2为顶升气缸，3为安装板，4为焊接机构，401为第一伸缩气缸，402为第一安装组件，4021为第一连接杆，4022为第一安装块，4023为第一安装孔，4024为第一紧固孔，403为第二安装组件，4031为第二连接杆，4032为第二安装块，404为第二伸缩气缸，405为焊接头，406为旋转电机，5为电路板支撑件，501为支撑底板，502为固定槽，503为通孔，6为电机。
具体实施方式
以下通过特定的具体实例说明本发明的实施方式，本领域技术人员可由本说明书所揭露的内容轻易地了解本发明的其他优点与功效。本发明还可以通过另外不同的具体实施方式加以实施或应用，本说明书中的各项细节也可以基于不同观点与应用，在没有背离本发明的精神下进行各种修饰或改变。需说明的是，在不冲突的情况下，以下实施例及实施例中的特征可以相互组合。
需要说明的是，以下实施例中所提供的图示仅以示意方式说明本发明的基本构想，遂图式中仅显示与本发明中有关的组件而非按照实际实施时的组件数目、形状及尺寸绘制，其实际实施时各组件的型态、数量及比例可为一种随意的改变，且其组件布局型态也可能更为复杂。
下面结合附图和实施例，对本发明的具体实施方式作进一步详细描述。
如图1和图2所示，本发明提供一种航空设备电路板焊接装置，所述装置包括支撑平台1，所述支撑平台1上设置顶升气缸2，所述顶升气缸2的输出端连接安装板3，所述安装板3上安装有至少一个焊接机构4，所述焊接机构包括第一伸缩气缸401、第一安装组件402、第二安装组件403、第二伸缩气缸404以及焊接头405，所述第一伸缩气缸401安装在所述安装板3下端，所述第一伸缩气缸401的输出端连接所述第一安装组件402，以驱动所述第一安装组件402横向移动，所述第一安装组件402上安装所述第二伸缩气缸404，所述第二伸缩气缸404的输出端连接所述焊接头405。
利用本发明实施例中的装置在对电路板进行焊接时，电路板可以通过电路板工装固定，通过控制各个气缸的运动以使得焊接头405根据焊接点的需要进行相应的移动，以实现焊接的需要。焊接结构4根据实际需要可以布设为多个。仅作为示例，如图1和图2所示的装置，所述焊接机构4设置为两个，两个所述焊接机构4关于所述安装板3对称布设。
下面本发明实施例将对焊接结构4的具体工作原理结合附图作进一步的说明。
在对电路板进行焊接时，首先通过顶升气缸2来调整焊接头405的上下高度，以适用于不同的厚度的电路板的焊接。调整好安装板3的位置后，顶升气缸2停止工作，顶升气缸2的作用主要是调整整体焊接机构4的位置，根据不同批次的电路板厚度在同一焊接生产线上可以进行合适的调整以适用于各个批次的电路板的焊接制造。焊接机构4在工作时，通过第一伸缩气缸401驱动第一安装组件402移动，进而会使得第二安装组件403带动其安装的第二伸缩气缸402进行移动，寻找焊接点位，在达到焊接点位后，通过第二伸缩气缸402驱动焊接头405在电路板上预设的焊接点位进行焊接。整个过程可以基于自动化控制。
因此，在一些实施例中，所述装置还包括控制器，所述控制器与所述顶升气缸2、所述第一伸缩气缸401以及所述第二伸缩气缸404信号连接。其中，本文中所述的控制器可以是PLC控制器或者带有控制器能够起到控制作用的设备。例如，PC平台等。本发明实施例对控制器的具体类型不作限制。
如图1所示，本发明实施例中，所述焊接头405可以倾斜布设，并由所述第二伸缩气缸驱动沿着所述焊接头405的倾斜方向来回移动。
本发明实施例中，所述第二伸缩气缸404的输出端连接一旋转电机406，所述旋转电机406的输出端连接所述焊接头405。在焊接过程中，可以通过旋转电机406的带动下使得焊接头405处于旋转状态，以提升焊接效果。
本发明实施例中，提供具体的第一安装组件402的结构。请参考图1所示，所述第一安装组件402包括第一连接杆4021以及第一安装块4022，所述第一连接杆4021的一端连接所述第一伸缩气缸401的输出端，所述第一连接杆4021的另一端固定连接所述第一安装块4022，所述第一安装块4022上安装有第一安装孔4023，并在所述第一安装块4022上设置若干第一紧固孔4024。第一安装组件402主要起到连接和支撑的作用，其中第一连接杆4021起到连接作用，使得第一伸缩气缸401的驱动力可以传递至第一安装块4022上。第一安装块4022起到支撑安装第二安装组件403的作用。并且为了提升支撑的稳定性，设置了第一安装孔4023，并在所述第一安装块4022上设置若干第一紧固孔4024，使得在稳定安装第二安装组件403的过程中，还可以利于拆卸。其中，第一紧固孔4024可以通过螺栓或者螺钉形式来实现紧固装配。
本发明实施例中，提供具体的第二安装组件403的结构。请参考图1所示，所述第二安装组件403包括第二连接杆4031以及第二安装块4032，所述第二连接杆4031通过所述第一安装孔4023固定安装在所述第一安装块4022上，所述第二连接杆4031固定连接所述第二安装块4032，并且所 述第二安装块4032上安装所述第二伸缩气缸404。第二安装组件403主要用于安装所述第二伸缩汽缸404，第二伸缩气缸404用于连接所述焊接头405，以此来保证整体焊接机构的稳定运行。
在一些实施例中，如图3所示，第二连接杆4031可以是可旋转地安装在第一安装块4022上，此时第一紧固孔4024起到限位保护作用。第二连接杆4022连接电机6，在焊接过程中，可以通过电机6驱动第二连接杆4022旋转，以丰富所述焊接头405的焊接轨迹。
本发明实施例中，如图1所示，所述支撑平台1包括支撑底座101、加固板102、垂直支撑板103以及水平支撑板104，所述支撑底座101通过所述垂直支撑板103支撑所述水平支撑板104，所述水平支撑板104上安装所述顶升气缸2，并在所述支撑板104上开设有用于所述顶升气缸伸出的开口，所述安装板3设置在所述水平支撑板104的下方，所述支撑底座101与所述垂直支撑板103之间设置至少两个所述加固板102。
本发明实施例中，如图1所示，所述装置还包括电路板支撑件5，所述电路板支撑件5至少包括电路板支撑底板501，所述电路板支撑底板501上设置有用于固定电路板的固定槽502以及多个通孔503。所述电路板支撑件5通过所述多个通孔503固定在输送机构上。电路板支撑件5实质上是一种夹具工装，用以安装待焊接的电路板。本发明实施例仅仅是对一种夹具工装的示例，本发明实施例在对电路板进行焊接时，还可以使用到现有技术中的各个夹具工装以满足电路板的固定。
以上实施方式仅用于说明本发明，而并非对本发明的限制，有关技术领域的普通技术人员，在不脱离本发明的精神和范围的情况下，还可以做出各种变化和变型，因此所有等同的技术方案也属于本发明的范畴，本发明的专利保护范围应由权利要求限定。

Claims (10)

  1. 一种航空设备电路板焊接装置，其特征在于，所述装置包括支撑平台，所述支撑平台上设置顶升气缸，所述顶升气缸的输出端连接安装板，所述安装板上安装有至少一个焊接机构，
    所述焊接机构包括第一伸缩气缸、第一安装组件、第二安装组件、第二伸缩气缸以及焊接头，所述第一伸缩气缸安装在所述安装板下端，所述第一伸缩气缸的输出端连接所述第一安装组件，以驱动所述第一安装组件横向移动，所述第一安装组件上安装所述第二伸缩气缸，所述第二伸缩气缸的输出端连接所述焊接头。
  2. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述焊接机构设置为两个，两个所述焊接机构关于所述安装板对称布设。
  3. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述焊接头倾斜布设，并由所述第二伸缩气缸驱动沿着所述焊接头的倾斜方向来回移动。
  4. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述第二伸缩气缸的输出端连接一旋转电机，所述旋转电机的输出端连接所述焊接头。
  5. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述第一安装组件包括第一连接杆以及第一安装块，所述第一连接杆的一端连接所述第一伸缩气缸的输出端，所述第一连接杆的另一端固定连接所述第一安装块，所述第一安装块上安装有第一安装孔，并在所述第一安装块上设置若干第一紧固孔。
  6. 如权利要求5所述的航空设备电路板焊接装置，其特征在于，所述第二安装组件包括第二连接杆以及第二安装块，所述第二连接杆通过所述第一安装孔固定安装在所述第一安装块上，所述第二连接杆固定连接所述第二安装块，并且所述第二安装块上安装所述第二伸缩气缸。
  7. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述 支撑平台包括支撑底座、加固板、垂直支撑板以及水平支撑板，所述支撑底座通过所述垂直支撑板支撑所述水平支撑板，所述水平支撑板上安装所述顶升气缸，并在所述支撑板上开设有用于所述顶升气缸伸出的开口，所述安装板设置在所述水平支撑板的下方，所述支撑底座与所述垂直支撑板之间设置至少两个所述加固板。
  8. 如权利要求1所述的航空设备电路板焊接装置，其特征在于，所述装置还包括电路板支撑件，所述电路板支撑件至少包括电路板支撑底板，所述电路板支撑底板上设置有用于固定电路板的固定槽以及多个通孔。
  9. 如权利要求8所述的航空设备电路板焊接装置，其特征在于，所述电路板支撑件通过所述多个通孔固定在输送机构上。
  10. 如权利要求1-9所述的航空设备电路板焊接装置，其特征在于，所述装置还包括控制器，所述控制器与所述顶升气缸、所述第一伸缩气缸以及所述第二伸缩气缸信号连接。
PCT/CN2022/080815 2022-02-25 2022-03-15 一种航空设备电路板焊接装置 WO2023159691A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202210176262.8A CN114473120A (zh) 2022-02-25 2022-02-25 一种航空设备电路板焊接装置
CN202210176262.8 2022-02-25

Publications (1)

Publication Number Publication Date
WO2023159691A1 true WO2023159691A1 (zh) 2023-08-31

Family

ID=81485197

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2022/080815 WO2023159691A1 (zh) 2022-02-25 2022-03-15 一种航空设备电路板焊接装置

Country Status (2)

Country Link
CN (1) CN114473120A (zh)
WO (1) WO2023159691A1 (zh)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117862762B (zh) * 2024-03-12 2024-06-11 潍坊鑫恒钢结构工程有限公司 一种预制钢结构用焊接装置

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3427424A (en) * 1965-10-24 1969-02-11 Globe Union Inc Welding machine
CN210157478U (zh) * 2019-03-22 2020-03-17 浙江东泰阀门有限公司 一种电路板水泥电阻焊接安装装置
CN210908666U (zh) * 2019-07-02 2020-07-03 无锡兆奕达电子科技有限公司 一种电路板生产用焊接装置
CN111761263A (zh) * 2020-06-23 2020-10-13 合肥晶浦传感科技有限公司 一种电路板电子元件安装焊接机构
CN211991336U (zh) * 2020-04-13 2020-11-24 杭州优智联科技有限公司 一种uwb接收器电路焊接装置
CN214978373U (zh) * 2021-07-30 2021-12-03 东莞市协创辉机械有限公司 Dc焊锡机手柄摇摆缓冲结构

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3363090B2 (ja) * 1998-04-02 2003-01-07 株式会社ジャパンユニックス 自動機用ハンダ付けヘッド
CN207914744U (zh) * 2017-12-29 2018-09-28 成都恒成工具股份有限公司 一种刀片焊接装置
CN212734563U (zh) * 2020-07-23 2021-03-19 无锡永华电池有限公司 一种碱性电池负极紧固装置

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3427424A (en) * 1965-10-24 1969-02-11 Globe Union Inc Welding machine
CN210157478U (zh) * 2019-03-22 2020-03-17 浙江东泰阀门有限公司 一种电路板水泥电阻焊接安装装置
CN210908666U (zh) * 2019-07-02 2020-07-03 无锡兆奕达电子科技有限公司 一种电路板生产用焊接装置
CN211991336U (zh) * 2020-04-13 2020-11-24 杭州优智联科技有限公司 一种uwb接收器电路焊接装置
CN111761263A (zh) * 2020-06-23 2020-10-13 合肥晶浦传感科技有限公司 一种电路板电子元件安装焊接机构
CN214978373U (zh) * 2021-07-30 2021-12-03 东莞市协创辉机械有限公司 Dc焊锡机手柄摇摆缓冲结构

Also Published As

Publication number Publication date
CN114473120A (zh) 2022-05-13

Similar Documents

Publication Publication Date Title
WO2018152863A1 (zh) 一种高效自动贴片设备
CN108996152A (zh) 一种四区模组机
WO2023159691A1 (zh) 一种航空设备电路板焊接装置
CN105720453A (zh) 插排组装机的第二组装机构
CN106826006A (zh) 一种门板电阻点焊自动送料系统
CN110315204A (zh) 双工位单激光镜头多段焊接设备
CN205543651U (zh) 插排组装机的第二组装机构
CN214109297U (zh) 一种旋转焊接工作站
CN116765734B (zh) 一种建筑焊接装置的转台机构
CN215747351U (zh) 一种电气工程自动化焊接机
CN209998564U (zh) 用于蜂窝铝及铝合金多工艺快速焊接装置及系统
CN113784610A (zh) 一种电子元器件高效安装装置及安装方法
CN113086555A (zh) 一种ccd视觉调幅定位机构及其调幅定位输送方法
CN220375746U (zh) 一种采用多点定位的自动抓板机
CN219669481U (zh) 一种高效率180°翻面装置
CN211280271U (zh) 一种多线路矩阵喷码设备
CN215616313U (zh) 一种模具吹气式锁付用协作机器人
CN112846454A (zh) 一种不锈钢分水器的支管自动焊接装置
CN218874392U (zh) 一种大力钳钻孔攻牙装置
CN219445249U (zh) 一种基板切割设备
CN219372991U (zh) 便于调节的smt生产上料工装
CN220409674U (zh) 一种超声波自动焊接平台
CN221164868U (zh) 一种承载鞍立式定位抓取机构
CN218534614U (zh) 一种使用灵活的焊接机械臂
CN220839261U (zh) 一种深孔活塞杆水平找正机构

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: 22927970

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE