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CN110666356A - Method for texturing surface of laser-etched aluminum alloy - Google Patents

Method for texturing surface of laser-etched aluminum alloy Download PDF

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CN110666356A
CN110666356A CN201910979131.1A CN201910979131A CN110666356A CN 110666356 A CN110666356 A CN 110666356A CN 201910979131 A CN201910979131 A CN 201910979131A CN 110666356 A CN110666356 A CN 110666356A
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aluminum alloy
texturing
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laser processing
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CN110666356B (en
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李绍龙
杨文锋
侯秋园
刘畅
张殊伦
李佐
钱自然
付蝉媛
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Civil Aviation Flight University of China
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/352Working by laser beam, e.g. welding, cutting or boring for surface treatment
    • B23K26/3568Modifying rugosity
    • B23K26/3584Increasing rugosity, e.g. roughening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/362Laser etching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/70Auxiliary operations or equipment
    • B23K26/702Auxiliary equipment

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  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Laser Beam Processing (AREA)

Abstract

本发明提供了一种激光刻蚀铝合金表面纹理化的方法,属于飞机铝合金蒙皮加工技术领域,所述方法包括采用激光处理装置中的振镜控制激光的扫描路径,在飞机铝合金蒙皮表面刻蚀出不同的纹理表面,扫描速度2000mm/s,频率90kHz,脉宽0.35μs,扫描次数1次,间距0.3mm,光斑直径50μm,功率24W。通过改变激光的扫描路径使铝合金表面刻蚀出纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力。

The invention provides a method for laser etching aluminum alloy surface texturing, which belongs to the technical field of aircraft aluminum alloy skin processing. Different texture surfaces are etched on the surface of the skin. The scanning speed is 2000mm/s, the frequency is 90kHz, the pulse width is 0.35μs, the number of scans is 1, the spacing is 0.3mm, the spot diameter is 50μm, and the power is 24W. By changing the scanning path of the laser, the aluminum alloy surface is etched with a textured structure to increase the surface roughness and surface wettability of the aluminum alloy skin, thereby increasing the adhesion of the aluminum alloy surface coating.

Description

一种激光刻蚀铝合金表面纹理化的方法A kind of method of laser etching aluminum alloy surface texturing

技术领域technical field

本发明涉及飞机铝合金蒙皮加工技术领域,具体是一种激光刻蚀铝合金表面纹理化的方法。The invention relates to the technical field of aircraft aluminum alloy skin processing, in particular to a method for texturing the surface of an aluminum alloy by laser etching.

背景技术Background technique

为了提高飞机铝合金蒙皮的耐候性、耐化学性、耐腐蚀性,需要在飞机铝合金蒙皮表面喷涂专用航空涂料,提高铝合金蒙皮表面涂层的附着力一直是民航领域研究的热点之一。研发新型涂料不仅成本昂贵,而且周期长,为了增加涂层附着力,对铝合金蒙皮进行表面改性成为了一种经济有效的方法。In order to improve the weather resistance, chemical resistance and corrosion resistance of aircraft aluminum alloy skins, it is necessary to spray special aviation coatings on the surface of aircraft aluminum alloy skins. Improving the adhesion of aluminum alloy skin surface coatings has always been a research hotspot in the field of civil aviation. one. The development of new coatings is not only expensive, but also takes a long time. In order to increase the adhesion of coatings, surface modification of aluminum alloy skins has become a cost-effective method.

化学法对铝合金表面处理需要经过脱脂、酸洗、清洗等过程,但化学法产生的废液对环境有极大污染。化学法增加附着力,产生废液对环境造成污染,手工打磨对工作人员的熟练程度要求较高,且对工作人员的健康造成影响。The chemical method for the surface treatment of aluminum alloy needs to go through the process of degreasing, pickling, cleaning, etc., but the waste liquid produced by the chemical method has great pollution to the environment. The chemical method increases the adhesion, produces waste liquid and pollutes the environment, and manual grinding requires higher proficiency of the staff and affects the health of the staff.

申请公布号CN109719469A公开了一种提高钛合金抗磨损性能的纹理表面加工方法,具有如下步骤:采用珩磨机对钛合金基材表面进行物理研磨;采用清洗液在超声波清洗机中对研磨好的钛合金基材进行清洗并烘干;使用激光打标机按照加工方案对钛合金基材表面进行加工处理;采用精抛光的方法对加工过的钛合金基材表面进行抛光处理;采用清洗液在超声波清洗机中对抛光过的钛合金基材进行清洗并干燥处理。该专利通过控制激光技术的加工参数获得多种表面性能不同的钛合金基材表面,钛合金基材表面的局部硬度、粗糙度和局部弹性模量等性能是不同的,用作工业设备的摩擦时能够获得较低的摩擦系数,表现出较好的抗磨损性能,并且能够承载较高的工作载荷。Application Publication No. CN109719469A discloses a textured surface processing method for improving the wear resistance of titanium alloys, comprising the following steps: using a honing machine to physically grind the surface of a titanium alloy substrate; The alloy substrate is cleaned and dried; the surface of the titanium alloy substrate is processed by a laser marking machine according to the processing plan; the surface of the processed titanium alloy substrate is polished by the method of fine polishing; The polished titanium alloy substrate is cleaned and dried in a cleaning machine. The patent obtains a variety of titanium alloy substrate surfaces with different surface properties by controlling the processing parameters of the laser technology. The local hardness, roughness and local elastic modulus of the titanium alloy substrate surface are different. It is used as friction for industrial equipment. It can obtain a lower coefficient of friction, show better anti-wear performance, and can carry a higher working load.

申请公布号CN109514174A公开激光纹理化和阳极化表面处理,其包括以下步骤:提供具有金属表面的制品;使用激光对所述表面进行纹理化处理以产生横跨所述表面的受控图案;以及对所述表面进行阳极化处理。所述受控图案可包括一系列凹坑,所述一系列凹坑是以横跨所述表面的预定重复图案(如点阵列或格栅)蚀刻的。所述受控图案还可包括以横跨所述表面的预定伪随机图案蚀刻的一系列凹坑。其用途为用于金属表面的抛光。Application Publication No. CN109514174A discloses a laser texturing and anodizing surface treatment comprising the steps of: providing an article with a metallic surface; texturing the surface using a laser to create a controlled pattern across the surface; and The surface is anodized. The controlled pattern may comprise a series of pits etched in a predetermined repeating pattern (eg, an array or grid of dots) across the surface. The controlled pattern may also include a series of pits etched in a predetermined pseudo-random pattern across the surface. Its use is for polishing metal surfaces.

目前尚未见有关通过用激光刻蚀纹理结构来增加铝合金表面涂层的附着力的报道。There are no reports on increasing the adhesion of aluminum alloy surface coatings by etching textured structures with lasers.

发明内容SUMMARY OF THE INVENTION

上述现有的要提高铝合金蒙皮表面涂层的附着力时,研发新型涂料成本昂贵,周期长;化学法对铝合金表面处理产生的废液对环境有极大污染的缺陷,本发明的目的是提供一种激光刻蚀铝合金表面纹理化的方法,通过改变激光的扫描路径使铝合金表面刻蚀出纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力。When the above-mentioned existing coating is to improve the adhesion of the aluminum alloy skin surface coating, the research and development of new coatings is expensive and the cycle is long; the waste liquid generated by the chemical method on the surface of the aluminum alloy has the defect of great pollution to the environment, and the method of the present invention is The purpose is to provide a method for laser etching aluminum alloy surface texture, by changing the scanning path of the laser to etch the texture structure on the aluminum alloy surface, to increase the surface roughness and surface wettability of the aluminum alloy skin, so as to increase the surface roughness and surface wettability of the aluminum alloy skin. Increase the adhesion of aluminum alloy surface coatings.

一种激光刻蚀铝合金表面纹理化的方法,所述方法包括采用激光处理装置中的振镜控制激光的扫描路径,在飞机铝合金蒙皮表面刻蚀出不同的纹理表面,扫描速度2000mm/s,频率90kHz,脉宽0.35μs,扫描次数1次,间距0.3mm,光斑直径50μm,功率24W。A method for laser etching aluminum alloy surface texturing, the method comprises using a galvanometer in a laser processing device to control a laser scanning path, etching different textured surfaces on the surface of aircraft aluminum alloy skin, and the scanning speed is 2000mm/ s, frequency 90kHz, pulse width 0.35μs, scan times 1, spacing 0.3mm, spot diameter 50μm, power 24W.

本申请的技术方案中,通过振镜控制激光的扫描路径,扫描速度2000mm/s,频率90kHz,脉宽0.35μs,扫描次数1次,间距0.3mm,光斑直径50μm,功率24W,在飞机铝合金蒙皮表面刻蚀出不同的纹理表面,通过改变激光的扫描路径使铝合金表面刻蚀出纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力。In the technical solution of the present application, the scanning path of the laser is controlled by a galvanometer, the scanning speed is 2000mm/s, the frequency is 90kHz, the pulse width is 0.35μs, the number of scans is 1, the spacing is 0.3mm, the spot diameter is 50μm, and the power is 24W. The surface of the skin is etched with different textured surfaces. By changing the scanning path of the laser, the surface of the aluminum alloy is etched with a textured structure to increase the surface roughness and surface wettability of the aluminum alloy skin, so as to increase the surface coating of the aluminum alloy. layer adhesion.

优选的,激光在飞机铝合金蒙皮表面产生的凹坑直径为45-55μm,凹坑的形状近似为圆形,凹坑叠加而成形成扫描路径。Preferably, the diameter of the pits produced by the laser on the surface of the aircraft aluminum alloy skin is 45-55 μm, the shape of the pits is approximately circular, and the pits are superimposed to form a scanning path.

更为优选的,凹坑直径为50μm。凹坑的深度可以通过调节激光器的功率来调节;路径是由凹坑叠加而成的,通过控制脉冲频率和扫描移动速度可以改变光斑的搭接率,进而影响表面的粗糙度。More preferably, the diameter of the pit is 50 μm. The depth of the pit can be adjusted by adjusting the power of the laser; the path is formed by the superposition of pits, and the overlap ratio of the spot can be changed by controlling the pulse frequency and scanning speed, thereby affecting the surface roughness.

优选的,纹理表面为菱形。菱形的粗糙度和浸润性最好,对增加涂层的附着力最有利。Preferably, the textured surface is diamond-shaped. Rhombus has the best roughness and wettability and is most beneficial to increase the adhesion of the coating.

优选的,纹理表面为正方形。使用波长1064nm脉冲激光设备进行表面纹理化处理,扫描路径是由光斑的叠加形成的直线。根据预设扫描路径对飞机铝合金蒙皮表面进行处理,使铝合金表面形成正方形的交错线,正方形纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力。Preferably, the textured surface is square. Surface texturing was performed using a pulsed laser device with a wavelength of 1064 nm, and the scanning path was a straight line formed by the superposition of light spots. The surface of the aircraft aluminum alloy skin is processed according to the preset scanning path, so that the aluminum alloy surface forms a square staggered line and a square texture structure to increase the surface roughness and surface wettability of the aluminum alloy skin, thereby increasing the aluminum alloy. Adhesion of surface coatings.

优选的,所述激光处理装置包括载物台,所述载物台的上方设置有激光加工头,所述激光加工头与电脑服务器电连接,所述电脑服务器还与激光器电连接,所述激光器发射激光束进入所述激光加工头的输入端,所述激光加工头将激光束向下照射于所述载物台上部的飞机铝合金蒙皮表面,所述激光加工头由六轴机械臂控制。将需要对飞机铝合金蒙皮表面处理的图形预先输入电脑服务器,振镜来调节扫描路径,通过更换场镜与调节功率控制光斑大小,通过控制脉冲频率和扫描移动速度可以改变光斑的搭接率,通过电脑服务器可以调节激光器的功率,通过六轴机械臂控制的动态激光加工头在待处理试样上有合适的位置进行调节,电脑服务器控制激光器在需要刻蚀的部位出光,完成刻蚀。Preferably, the laser processing device includes a stage, a laser processing head is arranged above the stage, the laser processing head is electrically connected to a computer server, the computer server is also electrically connected to a laser, and the laser The laser beam is emitted into the input end of the laser processing head, and the laser processing head irradiates the laser beam downward on the surface of the aircraft aluminum alloy skin on the upper part of the stage, and the laser processing head is controlled by a six-axis mechanical arm . The graphics that need to be treated on the surface of the aircraft's aluminum alloy skin are input into the computer server in advance, the galvanometer is used to adjust the scanning path, the spot size is controlled by changing the field lens and the power is adjusted, and the overlap rate of the spot can be changed by controlling the pulse frequency and scanning speed. , The power of the laser can be adjusted through the computer server, and the dynamic laser processing head controlled by the six-axis robotic arm can be adjusted in a suitable position on the sample to be processed. The computer server controls the laser to emit light at the part that needs to be etched to complete the etching.

更为优选的,所述六轴机械臂的下部设置有固定支座。More preferably, the lower part of the six-axis robotic arm is provided with a fixed support.

更为优选的,所述激光加工头中设置有用于调节激光束扫描路径的振镜。More preferably, the laser processing head is provided with a galvanometer for adjusting the scanning path of the laser beam.

更为优选的,所述激光加工头中还设置有用于实现自动对焦的距离感应器。距离感应器可以实现自动对焦。More preferably, the laser processing head is also provided with a distance sensor for realizing automatic focusing. The distance sensor enables autofocus.

优选的,所述激光器为脉冲激光器,波长为1064nm,平均功率120W。Preferably, the laser is a pulsed laser with a wavelength of 1064 nm and an average power of 120W.

本申请的技术方案中:In the technical solution of this application:

每条扫描出的平行线之间的距离为300μm;The distance between each scanned parallel line is 300 μm;

激光器为120W红外光纤激光器;The laser is 120W infrared fiber laser;

本申请的纹理化后可不经过任何处理,直接进行喷涂。After the texturing of the present application, it can be directly sprayed without any treatment.

较于现有技术,本发明的有益效果是:Compared with the prior art, the beneficial effects of the present invention are:

(1)通过改变激光的扫描路径使铝合金表面刻蚀出纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力;(1) By changing the scanning path of the laser, the surface of the aluminum alloy is etched with a texture structure to increase the surface roughness and surface wettability of the aluminum alloy skin, thereby increasing the adhesion of the aluminum alloy surface coating;

(2)凹坑的深度可以通过调节激光器的功率来调节;路径是由凹坑叠加而成的,通过控制脉冲频率和扫描移动速度可以改变光斑的搭接率,进而影响表面的粗糙度;(2) The depth of the pit can be adjusted by adjusting the power of the laser; the path is formed by superimposing the pit, and the overlap rate of the spot can be changed by controlling the pulse frequency and the scanning speed, thereby affecting the surface roughness;

(3)使用波长1064nm脉冲激光设备进行表面纹理化处理,扫描路径是由光斑的叠加形成的直线。根据预设扫描路径对铝合金表面进行处理,使铝合金表面形成正方形的交错线,正方形纹理结构,来增加铝合金蒙皮的面粗糙度,表面浸润性,以此来增加铝合金表面涂层的附着力;(3) The surface texture treatment is carried out by using a pulsed laser device with a wavelength of 1064 nm, and the scanning path is a straight line formed by the superposition of the light spots. The surface of the aluminum alloy is processed according to the preset scanning path, so that the surface of the aluminum alloy forms square staggered lines and a square texture structure to increase the surface roughness and surface wettability of the aluminum alloy skin, thereby increasing the surface coating of the aluminum alloy adhesion;

(4)菱形的粗糙度和浸润性最好,对增加涂层的附着力最有利;(4) The roughness and wettability of the diamond shape are the best, which is most beneficial to increase the adhesion of the coating;

(5)现有激光技术对铝合金表面的处理的方式一般是尽量使铝合金表面全部处理,这样的处理会造成粗糙度过大,涂料无法渗透到激光刻蚀的凹槽内,影响涂层附着力。与现有技术相比,对铝合金表面进行纹理化处理可以根据涂料的粘稠度来选择相应的图案,通过控制扫描间距、更换场镜等方式来改变铝合金蒙皮表面的粗糙度,使涂料与基材的结合力达到最大;(5) The existing laser technology is generally used to treat the aluminum alloy surface as much as possible. Such treatment will cause excessive roughness, and the coating cannot penetrate into the grooves etched by the laser, affecting the coating. adhesion. Compared with the prior art, the texture treatment of the aluminum alloy surface can select the corresponding pattern according to the viscosity of the paint, and the roughness of the aluminum alloy skin surface can be changed by controlling the scanning distance, changing the field lens, etc. The bonding force between the coating and the substrate is maximized;

(6)将需要对飞机铝合金蒙皮表面处理的图形预先输入电脑服务器,振镜来调节扫描路径,通过更换场镜与调节功率控制光斑大小,通过控制脉冲频率和扫描移动速度可以改变光斑的搭接率,通过电脑服务器可以调节激光器的功率,通过六轴机械臂控制的动态激光加工头在待处理试样上有合适的位置进行调节,电脑服务器控制激光器在需要刻蚀的部位出光,完成刻蚀。(6) Input the graphics that need to be processed on the surface of the aircraft aluminum alloy skin into the computer server in advance, adjust the scanning path by the galvanometer, control the spot size by changing the field lens and adjusting the power, and change the spot size by controlling the pulse frequency and scanning speed. Lap rate, the power of the laser can be adjusted through the computer server, and the dynamic laser processing head controlled by the six-axis robotic arm can be adjusted in a suitable position on the sample to be processed, and the computer server controls the laser to emit light at the part that needs to be etched. etching.

附图说明Description of drawings

图1是本申请激光处理装置的结构示意图;1 is a schematic structural diagram of a laser processing device of the present application;

图2是本申请菱形的纹理表面结构示意图;Fig. 2 is the texture surface structure schematic diagram of the rhombus of the present application;

图3是本申请正方形的纹理表面结构示意图;Fig. 3 is the texture surface structure schematic diagram of the square of the present application;

图4是本申请飞机铝合金蒙皮表面的原始表面三维轮廓图;Fig. 4 is the original surface three-dimensional profile diagram of the aircraft aluminum alloy skin surface of the present application;

图5是本申请飞机铝合金蒙皮表面处理后菱形的三维轮廓图;Fig. 5 is the three-dimensional profile diagram of the rhombus after the surface treatment of the aircraft aluminum alloy skin of the present application;

图6是本申请飞机铝合金蒙皮表面处理后正方形的三维轮廓图。FIG. 6 is a three-dimensional outline view of a square after surface treatment of the aircraft aluminum alloy skin of the present application.

附图标记:1-激光器,2-六轴机械臂,3-激光加工头,4-待处理试样,5-载物台,6-固定支座,7-电脑服务器。Reference numerals: 1-laser, 2-six-axis robotic arm, 3-laser processing head, 4-sample to be processed, 5-stage, 6-fixed support, 7-computer server.

具体实施方式Detailed ways

为了使本领域的技术人员更好地理解本发明的技术方案,下面结合具体实施例对本发明作进一步的详细说明。In order to make those skilled in the art better understand the technical solutions of the present invention, the present invention will be further described in detail below with reference to specific embodiments.

实施例1Example 1

如图1和图2所示,一种激光刻蚀铝合金表面纹理化的方法,所述方法包括采用激光处理装置中的振镜控制激光的扫描路径,在飞机铝合金蒙皮表面刻蚀出不同的纹理表面,扫描速度2000mm/s,频率90kHz,脉宽0.35μs,扫描次数1次,间距0.3mm,光斑直径50μm,功率24W;激光在飞机铝合金蒙皮表面产生的凹坑直径为50μm,凹坑的形状近似为圆形,凹坑叠加而成形成扫描路径,纹理表面为菱形。As shown in Figure 1 and Figure 2, a method for laser etching aluminum alloy surface texturing, the method includes using a galvanometer in a laser processing device to control the scanning path of the laser, and etching the surface of the aircraft aluminum alloy skin. For different textured surfaces, the scanning speed is 2000mm/s, the frequency is 90kHz, the pulse width is 0.35μs, the number of scans is 1, the spacing is 0.3mm, the spot diameter is 50μm, and the power is 24W; the diameter of the pits generated by the laser on the surface of the aircraft aluminum alloy skin is 50μm , the shape of the pits is approximately circular, the pits are superimposed to form a scanning path, and the textured surface is rhombus.

实施例2Example 2

如图1和图3所示,凹坑直径为45μm,纹理表面为正方形,其余均同实施例1。As shown in Figures 1 and 3, the diameter of the pit is 45 μm, the textured surface is square, and the rest are the same as in Example 1.

实施例3Example 3

如图1和图2所示,凹坑直径为50μm,纹理表面为菱形,其余均同实施例1。As shown in Figures 1 and 2, the diameter of the pit is 50 μm, the textured surface is rhombus, and the rest are the same as in Example 1.

实施例4Example 4

如图1所示,所述激光处理装置包括载物台5,所述载物台5的上方设置有激光加工头3,所述激光加工头3与电脑服务器7电连接,所述电脑服务器7还与激光器1电连接,所述激光器1发射激光束进入所述激光加工头3的输入端,所述激光加工头3将激光束向下照射于所述载物台5上部的飞机铝合金蒙皮表面,所述激光加工头3由六轴机械臂2控制;所述六轴机械臂2的下部设置有固定支座6;所述激光加工头3中设置有用于调节激光束扫描路径的振镜;所述激光加工头3中还设置有用于实现自动对焦的距离感应器;所述激光器1为脉冲激光器1,波长为1064nm,平均功率120W。As shown in FIG. 1 , the laser processing device includes a stage 5 , a laser processing head 3 is arranged above the stage 5 , and the laser processing head 3 is electrically connected to a computer server 7 , and the computer server 7 Also electrically connected with the laser 1, the laser 1 emits a laser beam into the input end of the laser processing head 3, and the laser processing head 3 irradiates the laser beam downward on the aircraft aluminum alloy mask on the upper part of the stage 5. The laser processing head 3 is controlled by the six-axis mechanical arm 2; the lower part of the six-axis mechanical arm 2 is provided with a fixed support 6; the laser processing head 3 is provided with a vibrator for adjusting the scanning path of the laser beam The laser processing head 3 is also provided with a distance sensor for realizing automatic focusing; the laser 1 is a pulsed laser 1 with a wavelength of 1064 nm and an average power of 120W.

实施例5Example 5

对实施例1-4得到的菱形或正方形的飞机铝合金蒙皮表面先用无水乙醇进行简单擦拭去除表面杂物,选用宣伟RECOATABLE EPOXY 300型环氧双组份航空专用涂料,用喷枪均匀喷涂到试样表面,涂层厚度控制在40~50μm,喷漆环境温度控制在20-24℃,优选为22℃,相对湿度控制在53-57%,优选为55%,采用萨塔SATAjet H型喷枪,喷涂气压50MPa,喷涂过程中使用QJT-2.3M漆雾净化装置,符合油漆施工技术指标以及国标GB 14444-93《喷漆室安全技术规定》。室温下放置7d,在涂层实干之后使用美国DeFelsko PosiTest AT-A型拉脱法附着力仪,测试其附着力。根据GB/T 5210-2006《色漆和清漆拉开法附着力试验》要求,试验前试样应在温度23℃,相对湿度50%的条件下放置至少16h,使用专用胶水将试柱与涂层紧密结合,每个试样测试6组,取得的数值取平均值,如表1所示。The surface of the rhombus or square aircraft aluminum alloy skin obtained in Example 1-4 was briefly wiped with anhydrous ethanol to remove surface debris, and Xuanwei RECOATABLE EPOXY 300 type epoxy two-component aviation special paint was used, and sprayed evenly. Spray on the surface of the sample, the thickness of the coating is controlled at 40-50μm, the temperature of the painting environment is controlled at 20-24°C, preferably 22°C, and the relative humidity is controlled at 53-57%, preferably 55%, using Sata SATAjet H type Spray gun, spraying air pressure 50MPa, QJT-2.3M paint mist purification device is used in the spraying process, which conforms to the technical indicators of paint construction and the national standard GB 14444-93 "Safety Technical Regulations for Spray Paint Room". It was placed at room temperature for 7 days, and after the coating was dry, the adhesion was tested using the American DeFelsko PosiTest AT-A pull-off adhesion tester. According to the requirements of GB/T 5210-2006 "Paints and Varnishes Adhesion Test by Pull-Off Method", the samples should be placed for at least 16 hours at a temperature of 23 °C and a relative humidity of 50% before the test. The layers are closely combined, and each sample is tested for 6 groups, and the obtained values are averaged, as shown in Table 1.

表1不同处理方式的试样涂层附着力Table 1 Coating adhesion of samples with different treatments

Figure BDA0002234610120000051
Figure BDA0002234610120000051

原始试样的附着力大小为6.71MPa,正方形试样与菱形试样的附着力相较于原始试样提升了70%左右。The adhesion of the original sample is 6.71MPa, and the adhesion between the square sample and the diamond sample is about 70% higher than that of the original sample.

试验例1Test Example 1

如图4,5和6所示,使用德国奥林巴斯OLS4100型激光共聚焦扫描显微镜测试(LSCM)表面粗糙度,采用5倍物镜进行测试,其中原始表面的粗糙度为1.9μm,菱形激光处理的表面粗糙度达到了7.9μm,粗糙度的提升明显。As shown in Figures 4, 5 and 6, the surface roughness was measured using a laser scanning confocal microscope (LSCM) of Olympus OLS4100, Germany, with a 5x objective lens, where the roughness of the original surface was 1.9 μm, and a diamond-shaped laser The treated surface roughness reaches 7.9 μm, and the roughness is significantly improved.

试验例2Test Example 2

如图4,5和6所示,采用德国KRUSS的DSA100型视频接触角测量仪对试样表面的接触角进行测试,以蒸馏水为测试液,原始表面的接触角大小为53.8°,激光处理过的表面接触角大小为25.6°,可见激光处理之后的试样表面有更好的浸润性。As shown in Figures 4, 5 and 6, the contact angle of the sample surface was measured by using the DSA100 video contact angle measuring instrument from KRUSS, Germany. Using distilled water as the test liquid, the contact angle of the original surface was 53.8°. The size of the surface contact angle is 25.6°, and it can be seen that the surface of the sample after laser treatment has better wettability.

试验例3Test Example 3

如图4,5和6所示,采用美国DeFelsko PosiTest AT-A型拉脱法附着力仪测试表面涂层附着力,试样经过喷涂之后对附着力进行测试,原始试样附着力的大小为6.71MPa,经过激光处理的试样涂层附着力大小为11.53MPa,可见激光表面纹理化处理能有效提升涂层附着力。As shown in Figures 4, 5 and 6, the adhesion of the surface coating was tested by the American DeFelsko PosiTest AT-A pull-off adhesion tester. The adhesion of the sample was tested after spraying, and the adhesion of the original sample was 6.71. MPa, the coating adhesion of the laser-treated sample is 11.53MPa, and it can be seen that the laser surface texturing treatment can effectively improve the coating adhesion.

本申请中,图2和图3中的标尺(1-500μm)显示放大比例。In this application, the scale (1-500 μm) in Figures 2 and 3 shows an enlarged scale.

以上所述实施例仅表达了本申请的具体实施方式,其描述较为具体和详细,但并不能因此而理解为对本申请保护范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本申请技术方案构思的前提下,还可以做出若干变形和改进,这些都属于本申请的保护范围。The above-mentioned embodiments only represent specific implementations of the present application, and the descriptions thereof are specific and detailed, but should not be construed as limiting the protection scope of the present application. It should be pointed out that for those of ordinary skill in the art, without departing from the concept of the technical solution of the present application, several modifications and improvements can be made, which all belong to the protection scope of the present application.

Claims (10)

1.一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述方法包括采用激光处理装置中的振镜控制激光的扫描路径,在飞机铝合金蒙皮表面刻蚀出不同的纹理表面,扫描速度2000mm/s,频率90kHz,脉宽0.35μs,扫描次数1次,间距0.3mm,光斑直径50μm,功率24W。1. a method for laser etching aluminum alloy surface texturing, it is characterized in that, described method comprises the scanning path that adopts the galvanometer in the laser processing device to control the laser, etch different textures on the aircraft aluminum alloy skin surface Surface, scanning speed 2000mm/s, frequency 90kHz, pulse width 0.35μs, scanning times 1 time, spacing 0.3mm, spot diameter 50μm, power 24W. 2.根据要求1所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,激光在飞机铝合金蒙皮表面产生的凹坑直径为45-55μm,凹坑的形状近似为圆形,凹坑叠加而成形成扫描路径。2. a method for laser etching aluminum alloy surface texturing according to claim 1, is characterized in that, the diameter of the pit that laser produces on the surface of the aircraft aluminum alloy skin is 45-55 μm, and the shape of the pit is approximately a circle. shape, the pits are superimposed to form a scanning path. 3.根据要求2所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,凹坑直径为50μm。3. The method for texturing the surface of an aluminum alloy by laser etching according to claim 2, wherein the diameter of the pit is 50 μm. 4.根据要求1所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,纹理表面为菱形。4. The method for texturing the surface of an aluminum alloy by laser etching according to claim 1, wherein the textured surface is a rhombus. 5.根据要求1所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,纹理表面为正方形。5. The method for texturing the surface of an aluminum alloy by laser etching according to claim 1, wherein the textured surface is a square. 6.根据要求1所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述激光处理装置包括载物台,所述载物台的上方设置有激光加工头,所述激光加工头与电脑服务器电连接,所述电脑服务器还与激光器电连接,所述激光器发射激光束进入所述激光加工头的输入端,所述激光加工头将激光束向下照射于所述载物台上部的飞机铝合金蒙皮表面,所述激光加工头由六轴机械臂控制。6. A method for laser etching aluminum alloy surface texturing according to claim 1, wherein the laser processing device comprises a stage, and a laser processing head is arranged above the stage, and the The laser processing head is electrically connected to a computer server, and the computer server is also electrically connected to a laser, the laser emits a laser beam into the input end of the laser processing head, and the laser processing head irradiates the laser beam downward on the carrier. The aircraft aluminum alloy skin surface on the upper part of the stage, the laser processing head is controlled by a six-axis robotic arm. 7.根据要求5所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述六轴机械臂的下部设置有固定支座。7 . The method for texturing the surface of an aluminum alloy by laser etching according to claim 5 , wherein the lower part of the six-axis robotic arm is provided with a fixed support. 8 . 8.根据要求5所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述激光加工头中设置有用于调节激光束扫描路径的振镜。8 . The method for texturing the surface of an aluminum alloy by laser etching according to claim 5 , wherein the laser processing head is provided with a galvanometer for adjusting the scanning path of the laser beam. 9 . 9.根据要求8所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述激光加工头中还设置有用于实现自动对焦的距离感应器。9 . The method for texturing the surface of an aluminum alloy by laser etching according to claim 8 , wherein the laser processing head is further provided with a distance sensor for realizing automatic focusing. 10 . 10.根据要求5所述的一种激光刻蚀铝合金表面纹理化的方法,其特征在于,所述激光器为脉冲激光器,波长为1064nm,平均功率120W。10. The method for laser etching aluminum alloy surface texturing according to claim 5, wherein the laser is a pulsed laser with a wavelength of 1064 nm and an average power of 120W.
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111349930A (en) * 2020-03-23 2020-06-30 北京工业大学 A kind of aluminum alloy laser surface composite modification method
CN111590206A (en) * 2020-05-15 2020-08-28 盐城市奇镌激光科技有限公司 Laser pretreatment device and method for improving paint surface adhesion
CN112626588A (en) * 2020-12-25 2021-04-09 常州凯泽环保科技有限公司 Wear-resistant and corrosion-resistant cathode electrophoresis coating process
CN112719606A (en) * 2020-12-10 2021-04-30 苏州铁人光学技术有限公司 Layered processing technology of laser equipment
CN115430915A (en) * 2021-06-01 2022-12-06 南京莱特威特轻量化技术研究院有限公司 Aluminum alloy surface laser treatment method for improving adhesive bonding performance
CN116851908A (en) * 2023-09-01 2023-10-10 天蔚蓝电驱动科技(江苏)有限公司 Optimization method for improving coating adhesion by laser surface treatment and processing method
US11828196B2 (en) 2022-01-28 2023-11-28 Rtx Corporation Gas turbine engine article with serpentine groove for coating interlock
EP4282573A1 (en) * 2022-05-23 2023-11-29 Nio Technology (Anhui) Co., Ltd Laser surface treatment method and laser surface treatment station
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CN118342112A (en) * 2024-06-18 2024-07-16 成都飞机工业(集团)有限责任公司 Self-adaptive motion control method for whole-row motion mechanism and anti-falling connecting cloth

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014164919A (en) * 2013-02-22 2014-09-08 Furukawa Electric Co Ltd:The Manufacturing method and manufacturing apparatus of crimp terminal
CN104646833A (en) * 2014-12-25 2015-05-27 广东工业大学 Laser preparation method of gradient wetted surface of metal substrate
CN104964487A (en) * 2015-05-18 2015-10-07 广东美的制冷设备有限公司 Heat exchanger, air conditioner and machining method for metal foils
CN105798463A (en) * 2016-05-31 2016-07-27 山东大学 Pre-treatment technology used before coating of hard alloy cutter
CN206764133U (en) * 2016-10-21 2017-12-19 华中科技大学 A kind of laser accurate manufacturing equipment of laser Machining head and its composition
CN109514174A (en) * 2011-09-30 2019-03-26 苹果公司 Laser-graining and anodized surface processing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109514174A (en) * 2011-09-30 2019-03-26 苹果公司 Laser-graining and anodized surface processing
JP2014164919A (en) * 2013-02-22 2014-09-08 Furukawa Electric Co Ltd:The Manufacturing method and manufacturing apparatus of crimp terminal
CN104646833A (en) * 2014-12-25 2015-05-27 广东工业大学 Laser preparation method of gradient wetted surface of metal substrate
CN104964487A (en) * 2015-05-18 2015-10-07 广东美的制冷设备有限公司 Heat exchanger, air conditioner and machining method for metal foils
CN105798463A (en) * 2016-05-31 2016-07-27 山东大学 Pre-treatment technology used before coating of hard alloy cutter
CN206764133U (en) * 2016-10-21 2017-12-19 华中科技大学 A kind of laser accurate manufacturing equipment of laser Machining head and its composition

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111349930A (en) * 2020-03-23 2020-06-30 北京工业大学 A kind of aluminum alloy laser surface composite modification method
CN111590206A (en) * 2020-05-15 2020-08-28 盐城市奇镌激光科技有限公司 Laser pretreatment device and method for improving paint surface adhesion
CN112719606A (en) * 2020-12-10 2021-04-30 苏州铁人光学技术有限公司 Layered processing technology of laser equipment
CN112626588A (en) * 2020-12-25 2021-04-09 常州凯泽环保科技有限公司 Wear-resistant and corrosion-resistant cathode electrophoresis coating process
CN115430915A (en) * 2021-06-01 2022-12-06 南京莱特威特轻量化技术研究院有限公司 Aluminum alloy surface laser treatment method for improving adhesive bonding performance
US11828196B2 (en) 2022-01-28 2023-11-28 Rtx Corporation Gas turbine engine article with serpentine groove for coating interlock
EP4282573A1 (en) * 2022-05-23 2023-11-29 Nio Technology (Anhui) Co., Ltd Laser surface treatment method and laser surface treatment station
CN116851908A (en) * 2023-09-01 2023-10-10 天蔚蓝电驱动科技(江苏)有限公司 Optimization method for improving coating adhesion by laser surface treatment and processing method
CN116851908B (en) * 2023-09-01 2023-12-12 天蔚蓝电驱动科技(江苏)有限公司 Optimization method for improving coating adhesion by laser surface treatment and processing method
CN117928462A (en) * 2024-01-31 2024-04-26 兰州交通大学 A multifunctional concrete sample surface roughness measuring and making device and its use method
CN117928462B (en) * 2024-01-31 2024-06-04 兰州交通大学 Multifunctional concrete sample surface roughness measuring and manufacturing device and application method thereof
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Inventor before: Qian Ziran

Inventor before: Fu Chan yuan

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Granted publication date: 20210402