CN212018254U - A paint spraying device for aviation accessories - Google Patents

A paint spraying device for aviation accessories Download PDF

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Publication number
CN212018254U
CN212018254U CN201922311279.6U CN201922311279U CN212018254U CN 212018254 U CN212018254 U CN 212018254U CN 201922311279 U CN201922311279 U CN 201922311279U CN 212018254 U CN212018254 U CN 212018254U
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paint
sleeved
inlet pipe
fixedly installed
paint spraying
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CN201922311279.6U
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Chinese (zh)
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林苑
叶凯
程帅鹏
朱睿迪
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Jiangxi Normal University
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Jiangxi Normal University
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Abstract

The utility model relates to an aviation accessory production facility technical field just discloses a paint spraying apparatus for aviation accessory, the on-line screen storage device comprises a base, the both sides difference fixed mounting at base top is on the bottom of curb plate, the top fixed mounting of curb plate is on the bottom of roof, the top fixed mounting of roof is on the bottom of paint spraying case, one side fixed mounting of paint spraying case has main motor. This paint spraying apparatus for aviation accessory, the top through the curb plate has set up first advance lacquer pipe and second respectively and has advanced the lacquer pipe, the rethread first advance lacquer pipe and second advance all set up threaded rod and plectane on the lacquer pipe, it is rotatory to drive the plectane through rotating the threaded rod, be convenient for adjust the proportion between the paint vehicle and the volume of the paint vehicle of can freely controlling simultaneously at any time according to the needs of paint vehicle in-process, it is too much not also can not appear the paint vehicle to have avoided taking place the problem that the paint vehicle is not enough, the paint vehicle is with incomplete problem, the practicality of this device has been improved greatly.

Description

一种航空配件用喷漆装置A paint spraying device for aviation accessories

技术领域technical field

本实用新型涉及航空配件生产设备技术领域,具体为一种航空配件用喷漆装置。The utility model relates to the technical field of aviation parts production equipment, in particular to a paint spraying device for aviation parts.

背景技术Background technique

喷涂通过喷枪或碟式雾化器,借助于压力或离心力,分散成均匀而微细的雾滴,施涂于被涂物表面的涂装方法,可分为空气喷涂、无空气喷涂、静电喷涂以及上述基本喷涂形式的各种派生的方式,如大流量低压力雾化喷涂、热喷涂、自动喷涂、多组喷涂等。Spraying through a spray gun or disc atomizer, with the help of pressure or centrifugal force, is dispersed into uniform and fine droplets, and the coating methods applied to the surface of the object to be coated can be divided into air spraying, airless spraying, electrostatic spraying and Various derivatives of the above-mentioned basic spraying forms, such as high-flow and low-pressure atomizing spraying, thermal spraying, automatic spraying, multi-group spraying, etc.

在对航空配件进行喷漆制程的时候,之前是工人将航空配件放置在流水线上,航空配件流入到喷漆房中,由工人在喷漆房中将航空配件取出,放置在喷漆治具上,喷漆机械手开始喷漆,喷完漆,工人再将航空配件从喷漆治具上取出放到烘烤治具上,航空配件经烘烤后,流出喷漆房,采用该方式进行喷漆之间,需要提前将混好的漆料灌装到喷漆桶内,若混合的漆料过多,在喷漆完后剩余的漆料就会被丢弃,造成漆料的浪费,同时部分的自动化喷漆设备由于定位不准也容易产生喷漆不全面引起航空配件返工的现象。In the spray painting process of aviation parts, workers placed the aviation parts on the assembly line before, and the aviation parts flowed into the spray booth. The workers took out the aviation parts in the spray booth and placed them on the painting jig. The painting manipulator started After spraying the paint, the workers take out the aviation parts from the spraying jig and put them on the baking jig. After the aviation parts are baked, they flow out of the spray booth. Between spraying in this way, the mixed parts need to be mixed in advance. The paint is filled into the spray bucket. If there is too much mixed paint, the remaining paint will be discarded after painting, resulting in a waste of paint. At the same time, some automatic painting equipment is prone to spray paint due to inaccurate positioning. The phenomenon of not comprehensively causing the rework of aviation parts.

实用新型内容Utility model content

针对现有技术的不足,本实用新型提供了一种航空配件用喷漆装置,具备便于定量的使用漆料和定位更加准确的优点,解决了上述背景技术中所提到的问题。In view of the deficiencies of the prior art, the utility model provides a paint spraying device for aviation accessories, which has the advantages of convenient quantitative use of paint and more accurate positioning, and solves the problems mentioned in the above background art.

本实用新型提供如下技术方案:一种航空配件用喷漆装置,包括底座,所述底座顶部的两侧分别固定安装在侧板的底部上,所述侧板的顶部固定安装在顶板的底部上,所述顶板的顶部固定安装在喷漆箱的底部上,所述喷漆箱的一侧固定安装有主电机,所述主电机的输出轴固定套接在位于喷漆箱内腔的螺旋杆的一端上,所述螺旋杆的另一端活动套接在喷漆箱内腔的另一侧上,所述喷漆箱顶部的两侧分别固定套接有第一进漆管和第二进漆管,所述第一进漆管和第二进漆管一侧的中部分别活动套接有两个螺纹杆,两个所述螺纹杆的一端分别固定安装在位于第一进漆管和第二进漆管内腔的圆板的一侧上,所述顶板底部的一侧固定安装有抽漆泵,所述抽漆泵的两端分别固定套接在软管和导管的一端上,所述软管和导管的另一端分别固定套接在喷漆箱的另一侧上和横管的顶部上,所述横管的底部固定套接有喷头,所述底座顶部的一侧固定安装有副电机,所述底座顶部的中心处通过轴活动套接在喷漆台的底部上,所述喷漆台的底部固定安装在伸缩杆的顶部上,所述伸缩杆的外侧分别通过轴活动套接在转杆的一端上,所述转杆的中上部通过轴活动套接在喷漆台的外侧上,所述转杆的顶部固定安装有压板,所述喷漆台的外侧通过固定杆固定安装在第一齿轮的内腔里,所述副电机的输出轴固定套接在第二齿轮上,所述第一齿轮和第二齿轮的外齿相互啮合,所述底座底部的四角分别固定安装有支撑腿。The utility model provides the following technical solutions: a paint spraying device for aviation accessories, comprising a base, two sides of the top of the base are respectively fixed on the bottom of the side plate, and the top of the side plate is fixed on the bottom of the top plate, The top of the top plate is fixedly installed on the bottom of the paint spraying box, the main motor is fixedly installed on one side of the spraying box, and the output shaft of the main motor is fixedly sleeved on one end of the screw rod located in the inner cavity of the paint spraying box, The other end of the screw rod is movably sleeved on the other side of the inner cavity of the paint spray box, and the two sides of the top of the paint spray box are respectively fixed and sleeved with a first paint inlet pipe and a second paint inlet pipe. The middle parts of one side of the paint inlet pipe and the second paint inlet pipe are respectively movably sleeved with two threaded rods, and one end of the two threaded rods is respectively fixed and installed on the circle located in the inner cavity of the first paint inlet pipe and the second paint inlet pipe. On one side of the board, a paint pump is fixedly installed on one side of the bottom of the top plate, and the two ends of the paint pump are respectively fixed and sleeved on one end of the hose and the conduit, and the other end of the hose and the conduit is fixed. They are respectively fixed and sleeved on the other side of the paint spray box and on the top of the horizontal pipe, the bottom of the horizontal pipe is fixedly sleeved with a spray head, one side of the top of the base is fixedly installed with an auxiliary motor, and the center of the top of the base is fixedly installed. The bottom of the paint spraying table is fixedly installed on the top of the telescopic rod, and the outer side of the telescopic rod is respectively sleeved on one end of the rotating rod through the shaft. The middle and upper part of the rod is movably sleeved on the outer side of the paint spraying table through the shaft, a pressure plate is fixedly installed on the top of the rotating rod, and the outer side of the painting table is fixedly installed in the inner cavity of the first gear through the fixing rod. The output shaft of the motor is fixedly sleeved on the second gear, the external teeth of the first gear and the second gear are meshed with each other, and the four corners of the bottom of the base are respectively fixed with supporting legs.

精选的,所述螺旋杆的最低端到喷漆箱内腔的底部之间的距离为两毫米。Selectively, the distance between the lowest end of the screw rod and the bottom of the inner cavity of the paint spraying box is two millimeters.

精选的,所述圆板的外侧固定套接有密封圈,且密封圈分别活动套接在第一进漆管和第二进漆管的内腔里。Optionally, a sealing ring is fixedly sleeved on the outer side of the circular plate, and the sealing ring is respectively movably sleeved in the inner cavity of the first paint inlet pipe and the second paint inlet pipe.

精选的,所述喷头的数量为七个,且七个喷头均匀的分布在横管的底部上。Selectively, the number of the spray heads is seven, and the seven spray heads are evenly distributed on the bottom of the horizontal pipe.

精选的,所述转杆和压板的数量均为三个,且三个转杆和压板均匀的分布在喷漆台的外侧上。Selectively, the number of the rotating rods and the pressing plates is three, and the three rotating rods and the pressing plates are evenly distributed on the outside of the paint spraying table.

与现有技术对比,本实用新型具备以下有益效果:Compared with the prior art, the utility model has the following beneficial effects:

1、该航空配件用喷漆装置,通过侧板的顶部分别设置了第一进漆管和第二进漆管,再通过第一进漆管和第二进漆管上均都设置了螺纹杆和圆板,通过转动螺纹杆带动圆板旋转,便于根据漆料过程中的需要随时调节漆料之间的比例且同时可自由控制漆料的量,避免了发生漆料不足的问题也不会出现漆料过多、漆料用不完的问题,大大提高了此装置的实用性。1. The paint spraying device for aviation accessories is provided with a first paint inlet pipe and a second paint inlet pipe respectively through the top of the side plate, and then threaded rods and threaded rods are set on both the first paint inlet pipe and the second paint inlet pipe. The circular plate rotates the circular plate by rotating the threaded rod, which is convenient to adjust the ratio between the paints at any time according to the needs of the paint process, and at the same time, the amount of paint can be freely controlled, avoiding the problem of insufficient paint. The problem of too much paint and inexhaustible paint greatly improves the practicability of this device.

2、该航空配件用喷漆装置,通过在喷漆台的外侧设置了三个转杆和压板,在再通过转杆的底部与伸缩杆连接,便于将该航空配件三侧的位置进行定位在喷漆台上,使得喷漆时航空配件不会发生位置偏移,通过副电机的运行利用第二齿轮可带动喷漆台上的航空配件旋转,增大了对航空配件喷漆的面积,使航空配件喷漆更全面彻底,提高了喷漆的效率。2. The paint spraying device for aviation parts is equipped with three rotating rods and pressure plates on the outside of the spraying table, and then connects with the telescopic rod through the bottom of the rotating rod, so that the position of the three sides of the aviation accessories can be positioned on the spraying table. The second gear can drive the aviation parts on the painting table to rotate through the operation of the auxiliary motor, which increases the painting area of the aviation parts and makes the aviation parts painting more comprehensive and thorough. , to improve the efficiency of painting.

附图说明Description of drawings

图1为本实用新型结构示意图;Fig. 1 is the structural representation of the utility model;

图2为本实用新型喷头结构示意图;Fig. 2 is the structural representation of the nozzle of the present utility model;

图3为本实用新型转杆结构示意图;Fig. 3 is the structural schematic diagram of the rotating rod of the present invention;

图4为本实用新型转杆第一齿轮结构示意图。FIG. 4 is a schematic structural diagram of the first gear of the rotating rod of the present invention.

图中:1、底座;2、侧板;3、顶板;4、喷漆箱;5、主电机;6、螺旋杆;7、第一进漆管;8、第二进漆管;9、螺纹杆;10、圆板;11、抽漆泵;12、软管;13、导管;14、横管;15、喷头;16、副电机;17、喷漆台;18、伸缩杆;19、转杆;20、压板;21、第一齿轮;22、第二齿轮;23、支撑腿。In the picture: 1. Base; 2. Side plate; 3. Top plate; 4. Paint spray box; 5. Main motor; 6. Screw rod; 7. The first paint inlet pipe; 8. The second paint inlet pipe; Rod; 10, circular plate; 11, paint pump; 12, hose; 13, conduit; 14, horizontal pipe; 15, spray head; 16, auxiliary motor; 17, spray booth; 18, telescopic rod; 19, rotating rod ; 20, the pressure plate; 21, the first gear; 22, the second gear; 23, the support legs.

具体实施方式Detailed ways

下面将结合本实用新型实施例中的附图,对本实用新型实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本实用新型一部分实施例,而不是全部的实施例。基于本实用新型中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本实用新型保护的范围。The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the implementations. example. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

请参阅图1-4,一种航空配件用喷漆装置,包括底座1,底座1顶部的两侧分别固定安装在侧板2的底部上,侧板2的顶部固定安装在顶板3的底部上,顶板3的顶部固定安装在喷漆箱4的底部上,喷漆箱4的一侧固定安装有主电机5,主电机5的输出轴固定套接在位于喷漆箱4内腔的螺旋杆6的一端上,螺旋杆6的最低端到喷漆箱4内腔的底部之间的距离为两毫米,通过螺旋杆6的最低端到喷漆箱4内腔的底部之间的距离为两毫米,便于将位于喷漆箱4的漆料进行搅拌,使得漆料之间混合的更加彻底,螺旋杆6的另一端活动套接在喷漆箱4内腔的另一侧上,喷漆箱4顶部的两侧分别固定套接有第一进漆管7和第二进漆管8,第一进漆管7和第二进漆管8一侧的中部分别活动套接有两个螺纹杆9,两个螺纹杆9的一端分别固定安装在位于第一进漆管7和第二进漆管8内腔的圆板10的一侧上,圆板10的外侧固定套接有密封圈,且密封圈分别活动套接在第一进漆管7和第二进漆管8的内腔里,通过侧板2的顶部分别设置了第一进漆管7和第二进漆管8,再通过第一进漆管7和第二进漆管8上均都设置了螺纹杆9和圆板10,通过转动螺纹杆9带动圆板10旋转,便于根据漆料过程中的需要随时调节漆料之间的比例且同时可自由控制漆料的量,避免了发生漆料不足的问题也不会出现漆料过多、漆料用不完的问题,大大提高了此装置的实用性,顶板3底部的一侧固定安装有抽漆泵11,抽漆泵11的两端分别固定套接在软管12和导管13的一端上,软管12和导管13的另一端分别固定套接在喷漆箱4的另一侧上和横管14的顶部上,横管14的底部固定套接有喷头15,喷头15的数量为七个,且七个喷头15均匀的分布在横管14的底部上,通过七个喷头15同时对航空配件进行喷漆,提高了航空配件喷漆的效率,底座1顶部的一侧固定安装有副电机16,底座1顶部的中心处通过轴活动套接在喷漆台17的底部上,喷漆台17的底部固定安装在伸缩杆18的顶部上,伸缩杆18的外侧分别通过轴活动套接在转杆19的一端上,转杆19的中上部通过轴活动套接在喷漆台17的外侧上,转杆19的顶部固定安装有压板20,转杆19和压板20的数量均为三个,且三个转杆19和压板20均匀的分布在喷漆台17的外侧上,通过在喷漆台17的外侧设置了三个转杆19和压板20,在再通过转杆19的底部与伸缩杆18连接,便于将该航空配件三侧的位置进行定位在喷漆台17上,使得喷漆时航空配件不会发生位置偏移,喷漆台17的外侧通过固定杆固定安装在第一齿轮21的内腔里,副电机16的输出轴固定套接在第二齿轮22上,第一齿轮21和第二齿轮22的外齿相互啮合,通过副电机16的运行利用第二齿轮22可带动喷漆台17上的航空配件旋转,增大了对航空配件喷漆的面积,使航空配件喷漆更全面彻底,提高了喷漆的效率,底座1底部的四角分别固定安装有支撑腿23。Please refer to Figure 1-4, a paint spraying device for aviation accessories, including a base 1, the two sides of the top of the base 1 are respectively fixed on the bottom of the side plate 2, the top of the side plate 2 is fixed on the bottom of the top plate 3, The top of the top plate 3 is fixedly installed on the bottom of the paint spraying box 4, the main motor 5 is fixedly installed on one side of the paint spraying box 4, and the output shaft of the main motor 5 is fixedly sleeved on one end of the screw rod 6 located in the inner cavity of the paint spraying box 4. , the distance between the lowest end of the screw rod 6 and the bottom of the inner cavity of the paint spraying box 4 is two millimeters, and the distance between the lowest end of the screw rod 6 and the bottom of the inner cavity of the paint spraying box 4 is two millimeters, which is convenient for the The paint in the box 4 is stirred, so that the paint is mixed more thoroughly, the other end of the screw rod 6 is movably sleeved on the other side of the inner cavity of the paint spray box 4, and the two sides of the top of the paint spray box 4 are respectively fixed and sleeved. There are a first paint inlet pipe 7 and a second paint inlet pipe 8. The middle part of one side of the first paint inlet pipe 7 and the second paint inlet pipe 8 is respectively movably sleeved with two threaded rods 9. One end of the two threaded rods 9 They are respectively fixed and installed on one side of the circular plate 10 located in the inner cavity of the first paint inlet pipe 7 and the second paint inlet pipe 8, the outer side of the circular plate 10 is fixedly sleeved with a sealing ring, and the sealing ring is respectively movably sleeved on the first paint inlet pipe 8. In the inner cavity of the first paint inlet pipe 7 and the second paint inlet pipe 8, the first paint inlet pipe 7 and the second paint inlet pipe 8 are respectively arranged through the top of the side plate 2, and then pass through the first paint inlet pipe 7 and the second paint inlet pipe 8 respectively. Both the threaded rods 9 and the circular plate 10 are provided on the two-inlet paint pipes 8, and the circular plate 10 is driven to rotate by rotating the threaded rod 9, so that the ratio between the paints can be adjusted at any time according to the needs of the paint process and can be freely controlled at the same time. The amount of paint avoids the problem of insufficient paint and does not cause the problem of too much paint and endless paint, which greatly improves the practicability of the device. One side of the bottom of the top plate 3 is fixedly installed with paint extraction The two ends of the pump 11 and the paint pump 11 are respectively fixed and sleeved on one end of the hose 12 and the conduit 13, and the other ends of the hose 12 and the conduit 13 are respectively fixed and sleeved on the other side of the paint spray box 4 and the horizontal pipe. On the top of 14, the bottom of the horizontal pipe 14 is fixedly sleeved with nozzles 15, the number of nozzles 15 is seven, and the seven nozzles 15 are evenly distributed on the bottom of the horizontal pipe 14. The painting is carried out to improve the painting efficiency of aviation parts. The auxiliary motor 16 is fixedly installed on one side of the top of the base 1. The center of the top of the base 1 is movably sleeved on the bottom of the painting table 17 through the shaft, and the bottom of the painting table 17 is fixedly installed. On the top of the telescopic rod 18, the outer side of the telescopic rod 18 is respectively sleeved on one end of the rotating rod 19 through the shaft, and the middle and upper part of the rotating rod 19 is sleeved on the outer side of the paint spraying table 17 through the shaft. A pressure plate 20 is fixedly installed on the top, and the number of rotating rods 19 and pressure plates 20 is three, and the three rotating rods 19 and pressure plates 20 are evenly distributed on the outside of the paint spraying table 17. A rotating rod 19 and a pressure plate 20 are connected to the telescopic rod 18 through the bottom of the rotating rod 19, so that the positions of the three sides of the aviation accessories can be positioned on the painting table 17, so that the aviation accessories will not be offset during painting. ,spray The outer side of the paint table 17 is fixedly installed in the inner cavity of the first gear 21 through the fixing rod, the output shaft of the auxiliary motor 16 is fixedly sleeved on the second gear 22, and the external teeth of the first gear 21 and the second gear 22 are meshed with each other. , through the operation of the auxiliary motor 16, the second gear 22 can drive the aviation accessories on the painting table 17 to rotate, which increases the area for painting the aviation accessories, makes the painting of the aviation accessories more comprehensive and thorough, and improves the painting efficiency. The bottom of the base 1 The four corners are respectively fixed with supporting legs 23 installed.

工作原理:使用时,根据所需要的漆料之间的比例和量转动螺纹杆9上圆板10,当圆板10旋转到一定角度时,此时不同漆料会分别从第一进漆管7和第二进漆管8进入到喷漆箱4内,然后启动主电机5的运行带动螺旋杆6的旋转将漆料之间进行混合,然后将航空配件放置在喷漆台17上,然后利用伸缩杆18将转杆19和压板20向内旋转,将航空配件固定在喷漆台17上,然后分别启动抽漆泵11和副电机16的运行,通过抽漆泵11的运行将喷漆箱4内的漆料从喷头15喷在航空配件上,通过副电机16的运行带动了喷漆台17上的航空配件进行旋转喷漆,即可。Working principle: When in use, rotate the circular plate 10 on the threaded rod 9 according to the required ratio and amount of paints. When the circular plate 10 rotates to a certain angle, different paints will be fed from the first paint pipe respectively. 7 and the second paint inlet pipe 8 enter the paint spraying box 4, then start the operation of the main motor 5 to drive the rotation of the screw rod 6 to mix the paints, and then place the aviation accessories on the paint spraying table 17, and then use the telescopic The rod 18 rotates the rotating rod 19 and the pressure plate 20 inwards to fix the aviation accessories on the paint spraying table 17, and then starts the operation of the paint pump 11 and the auxiliary motor 16 respectively, and the paint pump 11 operates to remove the paint in the paint spray box 4. The paint is sprayed on the aviation accessories from the spray head 15 , and the aviation accessories on the paint spraying table 17 are driven to rotate and paint by the operation of the auxiliary motor 16 .

需要说明的是,在本文中,诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来,而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且,术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含,从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素,而且还包括没有明确列出的其他要素,或者是还包括为这种过程、方法、物品或者设备所固有的要素。同时在本实用新型的附图中,填充图案只是为了区别图层,不做其他任何限定。It should be noted that, in this document, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any relationship between these entities or operations. any such actual relationship or sequence exists. Moreover, the terms "comprising", "comprising" or any other variation thereof are intended to encompass a non-exclusive inclusion such that a process, method, article or device that includes a list of elements includes not only those elements, but also includes not explicitly listed or other elements inherent to such a process, method, article or apparatus. Meanwhile, in the drawings of the present invention, the filling pattern is only for distinguishing the layers, and does not make any other limitation.

尽管已经示出和描述了本实用新型的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本实用新型的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本实用新型的范围由所附权利要求及其等同物限定。Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes and modifications can be made to these embodiments without departing from the principles and spirit of the present invention , alternatives and modifications, the scope of the present invention is defined by the appended claims and their equivalents.

Claims (5)

1.一种航空配件用喷漆装置,包括底座(1),其特征在于:所述底座(1)顶部的两侧分别固定安装在侧板(2)的底部上,所述侧板(2)的顶部固定安装在顶板(3)的底部上,所述顶板(3)的顶部固定安装在喷漆箱(4)的底部上,所述喷漆箱(4)的一侧固定安装有主电机(5),所述主电机(5)的输出轴固定套接在位于喷漆箱(4)内腔的螺旋杆(6)的一端上,所述螺旋杆(6)的另一端活动套接在喷漆箱(4)内腔的另一侧上,所述喷漆箱(4)顶部的两侧分别固定套接有第一进漆管(7)和第二进漆管(8),所述第一进漆管(7)和第二进漆管(8)一侧的中部分别活动套接有两个螺纹杆(9),两个所述螺纹杆(9)的一端分别固定安装在位于第一进漆管(7)和第二进漆管(8)内腔的圆板(10)的一侧上,所述顶板(3)底部的一侧固定安装有抽漆泵(11),所述抽漆泵(11)的两端分别固定套接在软管(12)和导管(13)的一端上,所述软管(12)和导管(13)的另一端分别固定套接在喷漆箱(4)的另一侧上和横管(14)的顶部上,所述横管(14)的底部固定套接有喷头(15),所述底座(1)顶部的一侧固定安装有副电机(16),所述底座(1)顶部的中心处通过轴活动套接在喷漆台(17)的底部上,所述喷漆台(17)的底部固定安装在伸缩杆(18)的顶部上,所述伸缩杆(18)的外侧分别通过轴活动套接在转杆(19)的一端上,所述转杆(19)的中上部通过轴活动套接在喷漆台(17)的外侧上,所述转杆(19)的顶部固定安装有压板(20),所述喷漆台(17)的外侧通过固定杆固定安装在第一齿轮(21)的内腔里,所述副电机(16)的输出轴固定套接在第二齿轮(22)上,所述第一齿轮(21)和第二齿轮(22)的外齿相互啮合,所述底座(1)底部的四角分别固定安装有支撑腿(23)。1. A paint spraying device for aviation accessories, comprising a base (1), characterized in that: the two sides of the top of the base (1) are respectively fixed and installed on the bottom of a side plate (2), and the side plate (2) The top of the top plate (3) is fixedly installed on the bottom of the top plate (3), the top of the top plate (3) is fixedly installed on the bottom of the paint spray box (4), and the main motor (5) is fixedly installed on one side of the paint spray box (4). ), the output shaft of the main motor (5) is fixedly sleeved on one end of the screw rod (6) located in the inner cavity of the paint spray box (4), and the other end of the screw rod (6) is movably sleeved on the paint spray box (4) On the other side of the inner cavity, the two sides of the top of the paint spray box (4) are respectively fixed and sleeved with a first paint inlet pipe (7) and a second paint inlet pipe (8). The middle of one side of the paint pipe (7) and the second paint inlet pipe (8) are respectively movably sleeved with two threaded rods (9), and one end of the two threaded rods (9) is respectively fixed and installed at the first inlet. On one side of the circular plate (10) of the inner cavity of the paint pipe (7) and the second paint inlet pipe (8), a paint pump (11) is fixedly installed on one side of the bottom of the top plate (3). Both ends of the paint pump (11) are respectively fixed and sleeved on one end of the hose (12) and the conduit (13), and the other ends of the hose (12) and the conduit (13) are respectively fixed and sleeved on the paint spray box ( 4) On the other side and on the top of the horizontal pipe (14), the bottom of the horizontal pipe (14) is fixedly sleeved with the nozzle (15), and the side of the top of the base (1) is fixedly installed with the auxiliary motor (16), the center of the top of the base (1) is movably sleeved on the bottom of the painting table (17) through the shaft, and the bottom of the painting table (17) is fixedly installed on the top of the telescopic rod (18), The outer side of the telescopic rod (18) is respectively sleeved on one end of the rotating rod (19) through the shaft, and the middle and upper part of the rotating rod (19) is movably sleeved on the outer side of the paint spraying table (17) through the shaft, A pressure plate (20) is fixedly installed on the top of the rotating rod (19), the outer side of the paint spraying table (17) is fixedly installed in the inner cavity of the first gear (21) through a fixing rod, and the auxiliary motor (16) The output shaft is fixedly sleeved on the second gear (22), the external teeth of the first gear (21) and the second gear (22) are meshed with each other, and the four corners of the bottom of the base (1) are respectively fixed and installed with supports Legs (23). 2.根据权利要求1所述的一种航空配件用喷漆装置,其特征在于:所述螺旋杆(6)的最低端到喷漆箱(4)内腔的底部之间的距离为两毫米。2 . The paint spraying device for aviation parts according to claim 1 , wherein the distance between the lowest end of the screw rod ( 6 ) and the bottom of the inner cavity of the paint spray box ( 4 ) is two millimeters. 3 . 3.根据权利要求1所述的一种航空配件用喷漆装置,其特征在于:所述圆板(10)的外侧固定套接有密封圈,且密封圈分别活动套接在第一进漆管(7)和第二进漆管(8)的内腔里。3. A paint spraying device for aviation accessories according to claim 1, characterized in that: the outer side of the circular plate (10) is fixedly sleeved with a sealing ring, and the sealing ring is respectively movably sleeved on the first paint inlet pipe (7) and the inner cavity of the second paint inlet pipe (8). 4.根据权利要求1所述的一种航空配件用喷漆装置,其特征在于:所述喷头(15)的数量为七个,且七个喷头(15)均匀的分布在横管(14)的底部上。4 . The paint spraying device for aviation parts according to claim 1 , wherein the number of the spray heads ( 15 ) is seven, and the seven spray heads ( 15 ) are evenly distributed on the side of the horizontal pipe ( 14 ). 5 . on the bottom. 5.根据权利要求1所述的一种航空配件用喷漆装置,其特征在于:所述转杆(19)和压板(20)的数量均为三个,且三个转杆(19)和压板(20)均匀的分布在喷漆台(17)的外侧上。5. A paint spraying device for aviation parts according to claim 1, characterized in that: the number of the rotating rods (19) and the pressure plates (20) is three, and the three rotating rods (19) and the pressure plates are three in number. (20) are evenly distributed on the outside of the spray booth (17).
CN201922311279.6U 2019-12-20 2019-12-20 A paint spraying device for aviation accessories Expired - Fee Related CN212018254U (en)

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CN201922311279.6U CN212018254U (en) 2019-12-20 2019-12-20 A paint spraying device for aviation accessories

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Application Number Priority Date Filing Date Title
CN201922311279.6U CN212018254U (en) 2019-12-20 2019-12-20 A paint spraying device for aviation accessories

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113441331A (en) * 2021-05-21 2021-09-28 南通远大精密机械有限公司 Vertical machining center is used in new energy automobile frame processing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113441331A (en) * 2021-05-21 2021-09-28 南通远大精密机械有限公司 Vertical machining center is used in new energy automobile frame processing

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