In actual production, the rotary file does not crack after welding, but stress cracking occurs after tooth cutting, but relevant literature reports are few. This paper uses Cu-Ag-based multi-interlayer flux to weld cemented carbide/steel rotary files, analyzes the stress state of the rotary files after welding and the causes of cracking after tooth cutting. Starting from the principle, the process is optimized, and more economical and convenient measures to reduce welding and tooth cutting cracking are proposed.
(a)Original sample after induction welding; (b) Enlarged view of the polished rotary file after welding; (c) Sample after tooth cutting and surface finishing.
Fig.1 ?Macroscopic morphology of rotary file samples after welding, polishing, and tooth-cutting processes
Although the thermal conductivity of tungsten carbide is more than twice that of alloy steel, there is a significant difference in the coefficient of thermal expansion between alloy steel and cemented carbide. For example, the linear expansion coefficient of commonly used YG-grade cemented carbide is approximately 5×10??–7×10??/K, while that of commonly used 45 steel is approximately 11×10??–14×10??/K.
Zhang J et al. studied and found that during the cooling process of induction welding, steel shrinks faster, forming tensile stress in the steel shank of the rotary file and compressive stress in the cemented carbide end. Meanwhile, the distribution of residual stress in the above two parts does not change with the decrease in temperature, and the residual stress value reaches the maximum at room temperature. Amelzadeh M et al. found that the residual stress distribution on the welding surface after induction welding is uneven, and the residual stress near the boundary of the welding surface is higher than that inside the weld.
Bang H S et al. further confirmed that the distribution of brazing residual stress has directionality, which can be specifically divided into two directions: parallel to the welding surface and perpendicular to the welding surface. Among them, the peak value of longitudinal residual stress at the welding site is the highest, even reaching the yield strength of the material. The welding failure of cemented carbide/brazing layer/alloy steel mainly occurs near the boundary between cemented carbide and brazing filler metal.
In order to reduce the residual thermal stress in brazed joints, many researchers at home and abroad have carried out a large number of studies, which can be mainly divided into three aspects: pretreatment before welding, treatment during the welding process, and post-weld treatment, to alleviate the residual thermal stress of brazed joints.
(a)Macroscopic photo of the interface; (b) Schematic diagram of residual stress area testing.
Fig.2? ?Macroscopic image of tooth-cutting-induced cracking at the interface and schematic diagram of residual stress zone testing in post-weld rotary files
Research Methods
This paper uses XRD tester, infrared thermometer, metallographic microscope, scanning electron microscope and other equipment to test the micro morphology and residual stress distribution of the welding interface of cemented carbide rotary files, and analyzes the tooth cutting cracking problem of welded parts after induction welding. The results show that the Cu-Ag-based brazing multi-layer structure can release the residual thermal stress at the cemented carbide end near the weld, but the cemented carbide end far away from the weld maintains a high residual stress value, and the rotary file forms a high residual stress gradient along the direction perpendicular to the welding surface. At the same time, the fast heating and cooling rates and short holding time will also cause a large thermal stress gradient from the outside to the inside of the welding surface of the rotary file. When the tooth cutting process introduces processing stress, which destroys the stress balance state of the cemented carbide surface, the compressive stress value on the surface of the cemented carbide near the weld will rapidly increase, easily leading to crack generation. Optimizing the welding temperature, welding time, preheating of welded parts and cooling pressure treatment can all improve the residual stress of the rotary file along the welding surface and vertical direction to a certain extent, optimize the stress gradient distribution, and further reduce the cracking phenomenon of the sample during tooth cutting after welding.
Zhang Y et al. achieved the transformation of tensile stress to compressive stress at the interface by carving micron-scale periodic grooves on the ceramic surface, inhibiting crack propagation and enhancing joint bonding strength. Compared with the joint strength of untreated ceramics (24 MPa), the post-welding strength of grooved ceramics reached 66 MPa, increasing by 275%. In addition, the design of special brazing layer structures can also optimize the residual thermal stress in brazed joints. Directly using high-strength brazing filler metal to fill the welding surface is extremely likely to cause stress cracking in the brittle cemented carbide end of the rotary file. Composite solders such as copper-based, silver-based, or nickel-based materials with low yield points, easy deformation, and the ability to reduce shear stress are suitable brazing materials for cemented carbide rotary files. However, pure copper flux has problems such as high melting point and poor performance, while silver-based flux has a high cost. The Cu-Ag-based composite interlayer structure combines the plasticity and low melting point of silver-based solders with the low cost and good compatibility with other metals of copper-based solders, effectively reducing residual stress at the welding site. Such interlayers are mainly composed of an external soft porous metal fiber mesh buffer layer and a middle rigid interlayer. The soft buffer layer can alleviate residual stress through yielding, plastic deformation, and creep, while the internal rigid interlayer transfers the concentrated area of residual thermal stress from the weld side of the cemented carbide to the interlayer, effectively preventing the generation of initial cracks in the cemented carbide. Shirzadi A A et al. used Ag-Cu-based multi-layer brazing for alumina/stainless steel materials, and the bonding strength of the welded parts reached 33 MPa, which can withstand more than 60 cycles of thermal shock in air at 200–600°C.
(a)Thermal imaging diagram;(b) Schematic diagram of thermal diffusion
Fig.3 Thermal image of rotary files 2 seconds after welding during cooling and demolding and schematic of heat diffusion at the welding surface
Process control during brazing can also optimize the residual stress of joints to a certain extent. Kar A et al. studied the effects of different welding temperatures on Ag-Cu-Ti-based flux brazing of alumina and stainless steel. During the temperature rise from 900°C to 1100°C, alumina and the brazing layer underwent different diffusion reactions, resulting in significant differences in the composition and structure of the brazing layer. The phase types, micro morphology, and element arrangement in the brazing layer all affect the joint strength and residual stress distribution.
In addition to the brazing layer structure and welding process control, post-weld treatment is also the key to reducing welding cracking of rotary files. Various post-weld heat treatment measures, including cryogenic treatment, tempering, low-temperature and high-temperature pressurization, can reduce the residual stress value of alloy welding components to a certain extent.
Mishra S et al. adopted thermal cycling treatment after welding (200–500°C for 5–10 cycles, followed by cooling to room temperature), and the results showed that post-weld thermal cycling can reduce residual thermal stress caused by the difference in the coefficient of thermal expansion. It was also found that the lower the residual thermal stress value at the joint, the better the relief effect. After cryogenic and tempering treatments on YG8 cemented carbide/A3 steel welded parts, Lu Hangang found that the maximum compressive stress of the cemented carbide was 304 MPa, which was 40% lower than the maximum stress value of conventional welding. Cui Chen et al. found that after cryogenic treatment, the surface residual stress of austenitic stainless steel matrix/ferrite welded parts decreased by 36.8% and 16.3% in the X and Y directions, respectively, while ageing treatment reduced the surface residual stress by 61.2% and 58.8% in the X and Y directions, respectively.
Fig.4? Interface morphology of large-sized (D>30mm) rotary files fabricated via induction welding
Fig.5? DSC-TG curves of Ag-Cu-based filler metal
Induction heating is characterized by short heating time, high temperature, and convenient operation, making it one of the main methods for large-scale industrial and automated welding of rotary files. However, excessively high heating temperature or too short heating time can easily cause high residual stress gradients in the rotary file along the welding surface and the direction perpendicular to the welding surface. Although these high residual stresses do not generate cracks immediately after welding, they often lead to cracking during the tooth cutting process of the rotary file. Based on DSC-TG analysis, combined with thermal imaging, metallographic, and electron microscopy analyses of the macro-micro structure of materials, appropriate welding temperature, moderate welding time, preheating of components (to increase the initial welding temperature of larger-sized rotary files), and cooling pressure treatment can all improve the residual stress gradient distribution of the rotary file in the directions of the welding surface and perpendicular to the welding surface to a certain extent, thereby reducing the occurrence of welding cracking in rotary files.
]]>They cut materials with high precision. Be it metal, non-metal, or non-ferrous materials, they can transform them easily into the shapes you desire. But laser cutting is not limited to a single type. Instead, you can see varieties suitable for different materials and applications.
The question is, which suits your business or industry? We are here to answer your question with a guide to the different types of laser cutting ideal for your tasks.?
With so many types of laser cutting, it can be difficult to identify the right one for your task. Each laser cutting method is suitable for different materials and applications. Understanding how each method works will give you deeper insight and help you choose the right one for your needs.
You might have noticed engraved serial numbers or logos in cars. Have you ever wondered how it is done precisely? The pro behind the job is fiber laser cutting. Not only just those serial numbers, but also from cutting engine components in automobiles, marking turbine blades in aeroplanes, customizing electronics, etching circuit boards, to creating jewelry, and more, fiber laser cutting has always played a major role.
How does it work? It uses optical fibers and generates a highly concentrated laser beam that works with computer numerical control (CNC). The laser beam is directed at a material to slice through it with high accuracy to convert it into desired shapes.?
You can either cut metallic or non-metallic materials like stainless steel, copper, aluminum, titanium, mild steel, and various alloys using these fiber lasers.
Pros?
Cons
CO2 laser cutting, also known as carbon dioxide laser, is a popular laser cutting type. This is not similar to other types because it generates and directs in a way that’s completely different from the others.
It uses both electricity and a gas mixture of carbon dioxide and generates high-intensity infrared light. With many lenses and mirrors, it directs and focuses on the material, changing it into desired shapes.
Although it can be used for either metal or non-metal surfaces, it is best for cutting non-metallic materials like wood, leather, fabric, paper, plastic, rubber, and more.?
Pros?
Cons
This is also known as a laser diode. It transforms electrical energy into coherent light energy, with a focused and monochromatic beam of light. This compact device uses semiconductor materials to generate laser light. It relies on it as an active medium and so known as energy efficient and cost-effective.
They cut non-metallic materials like plywood, MDF sheets, Bamboo, Oak, laser board, and more. Moreover, this is best for personal use, more than for complex work.
Pros
Cons
Nd:YAG is Neodymium-doped Yttrium Aluminum Garnet, and Nd:YVO is Neodymium-doped Yttrium Orthovanadate. The Nd:YAG, a synthetic crystal, produces a laser beam with a wavelength of 1.06 micrometers, approximately.? And Nd:YVO works similarly but uses a slightly different crystal composition.
It has high cutting power and can be used for a wide range of applications. It can be used to work on metals (coated and non-coated) as well as non-metallic materials like plastics. They are better at handling reflective materials.
Pros
Cons
People use laser cutting to cut materials easily in precise shapes and designs. But which one suits you is more important to consider. These lasers can be of many types; among them, you need to consider a few things before purchasing. There are a few factors, like precision, quality, thickness, speed, and cost, to analyze so that you can make your decision on purchasing the right type.?
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In the actual machining process, selecting an appropriate cutting-in method for end mills requires comprehensive consideration of multiple factors. First, the characteristics of the workpiece material, such as hardness and toughness, are crucial. For materials with low hardness, vertical cutting-in can be appropriately considered; for materials with high hardness and great toughness, gentle cutting-in methods such as oblique cutting-in or spiral cutting-in should be prioritized.
Pre-drilling a hole in the workpiece (5 – 10% larger than the diameter of the end mill) is the safest way to insert the milling cutter. This method can prevent premature wear of the tool. Chip evacuation is smoother, thus reducing the risk of chip accumulation and tool breakage. This method is usually employed when machining materials prone to built-up edges, ensuring consistent machinability.
Vertical cutting-in is the most basic and common cutting-in method for end mills. This method refers to the end mill directly cutting in perpendicular to the workpiece surface. It is simple to operate and convenient for programming, and is widely used in rough machining with low requirements for machining accuracy and low material hardness. For example, when performing preliminary contour machining on aluminum workpieces, vertical cutting-in can quickly remove a large amount of material. However, vertical cutting-in also has obvious disadvantages. Since the cutting edge of the end mill is subjected to a large impact load at the moment of vertical cutting-in, it is prone to aggravate tool wear and even cause edge chipping. In addition, the large cutting force generated during vertical cutting-in may cause vibration of the workpiece, affecting the quality of the machined surface. Therefore, vertical cutting-in is not suitable for machining materials with high hardness or in cases where high requirements are placed on machining accuracy and surface quality.
Oblique cutting-in is a relatively gentle cutting-in method. The end mill cuts into the workpiece along an oblique line at a certain inclination angle (typically between 3° and 15°). Compared with vertical cutting-in, this cutting-in method can effectively reduce the impact at the moment of tool cutting-in, lower the peak value of cutting force, and reduce tool wear. Meanwhile, oblique cutting-in can make the cutting process more stable, which is conducive to improving the quality of the machined surface.
Recommended Angles: For hard/ferromagnetic materials: 1°-3°
For plastic/non-ferromagnetic materials: 3°-10°
When machining high-hardness materials such as cast iron, the oblique cutting-in method demonstrates obvious advantages. By gradually cutting into the workpiece, the cutting edge of the end mill comes into contact with the material step by step, avoiding the severe impact of vertical cutting-in and extending the service life of the tool. In mold machining, for some complex cavities, oblique cutting-in is also commonly used in the roughing stage to improve machining efficiency and tool durability.
Spiral cutting-in is a more advanced and efficient cutting-in method. When the end mill cuts into the workpiece, it gradually penetrates along a spiral trajectory, similar to the drilling principle of a drill bit. The advantages of spiral cutting-in are remarkable: it enables the tool to maintain a continuous cutting state during the cutting-in process, with uniform distribution of cutting force, which greatly reduces the impact and vibration on the tool.
Spiral cutting-in is widely used in machining high-hardness alloy materials such as titanium alloys and nickel-based alloys. Due to the poor cutting performance of these materials, traditional cutting-in methods easily cause rapid tool wear and damage. In contrast, spiral cutting-in can effectively reduce the cutting temperature, minimize friction between the tool and the workpiece, and thus improve machining efficiency and quality.
Programming Note: When using this method, the programmed diameter should be 110-120% larger than the diameter of the cutting insert. Additionally, spiral feed has advantages in achieving precise surface finish, making it the preferred choice for high-precision and high-surface-quality machining in industries like aerospace and medical device manufacturing.
Arc cutting-in is a method where the end mill cuts into the workpiece along an arc trajectory. This cutting-in approach is mainly used for machining contours or surfaces with special requirements, enabling the tool to maintain a stable cutting state during both cutting-in and cutting-out. It reduces tool engagement marks on the machined surface and improves surface finish. When machining complex curved parts such as cams and blades, the arc cutting-in method can precisely control the tool’s movement trajectory to ensure machining accuracy. Additionally, during contour milling, arc cutting-in avoids over-cutting or under-cutting caused by sudden changes in cutting force at corners, making the machined contour smoother and more accurate.
Rolling entry into the cut ensures that the tool can fully penetrate and naturally achieve an appropriate chip thickness. In this case, the feed rate should be reduced by 50%. Rolling tool engagement is particularly advantageous in slotting and contour machining, where maintaining consistent chip thickness is crucial for surface finish and dimensional accuracy. Machinists often use this method in high-speed cutting operations to maximize material removal rate while minimizing tool wear and heat generation.
Second, machining accuracy and surface quality requirements are also important reference factors. If high requirements are placed on the surface finish and accuracy of the machined part, vertical cutting-in should be avoided, and methods ensuring stable cutting such as arc cutting-in or spiral cutting-in should be chosen. Additionally, factors such as the performance of machining equipment, the type and size of tools, and machining costs need to be incorporated into the consideration.
Climb milling?refers to the scenario where the rotation direction of the milling cutter is the same as the feed direction of the workpiece, and the cutting thickness gradually decreases from maximum to zero. During climb milling, the cutting edge first contacts the machined surface of the workpiece, then cuts into the material, and the chip thickness continues to decrease as cutting proceeds.
Conventional milling?is when the rotation direction of the milling cutter is opposite to the feed direction of the workpiece, and the cutting thickness gradually increases from zero. During conventional milling, the cutting edge slides on the workpiece surface for a certain distance before cutting into the material, with the chip thickness increasing from thin to thick.
Selecting between climb milling and conventional milling requires comprehensive consideration of factors such as workpiece material, machining accuracy requirements, and machine tool performance. For materials with low hardness and good plasticity such as aluminum and copper, as well as for finishing with high surface quality requirements, climb milling is often the better choice; for steels with high hardness, or when the machine tool rigidity is poor and there is no clearance elimination device, conventional milling is more appropriate. Additionally, when machining castings with hard skins, conventional milling can avoid the cutting edge directly contacting the hard skin and accelerating wear.
There are various cutting-in methods for frezes, each with its unique characteristics and application scenarios. Mechanical machining practitioners need to deeply understand the principles, advantages, and disadvantages of various cutting-in methods, as well as climb milling and conventional milling. According to actual machining needs, they should comprehensively consider multiple factors to reasonably select the cutting-in method and milling method for end mills, so as to achieve efficient and precise machining and improve product quality and production efficiency. With the continuous development of machining technology, the cutting-in methods and milling methods for end mills will also continue to innovate and optimize, bringing more possibilities to the mechanical machining industry.
]]>Kareem, S. J., Wurood Asaad, M., & Al-Ethari, H. ?Enhancement of tribological properties of carbide cutting tools by ceramic coating deposition.?Heat Treatment and Surface Engineering,(2024).?6(1). https://doi.org/10.1080/25787616.2024.2331865
Coating by sol–gel deposition to modify the tribological properties of K10 carbide cutting insert was performed. The study examines the thermal and tribological characteristics of uncoated cutting inserts and the cutting inserts coated with TiO2/8YSZ and TiO2/15YSZ layers respectively. The TiO2/8YSZ and TiO2/15YSZ coatings had a hardness of 1151.6 and 1678.9 HV, respectively, and the TiO2/8YSZ and TiO2/15YSZ coated inserts had scratch hardness of 2.73 and 22.98 GPa respectively. Among the uncoated and coated inserts, the TiO2/15YSZ coated inserts had the lowest coefficient of friction and rate of wear. The TiO2/8YSZ coated insert had a lower thermal conductivity when compared to TiO2/15YSZ coated insert and uncoated carbide cutting insert (10.3 vs. 14.1, and 41.8 W/m.K). The thermal expansion coefficients of the 8YSZ layers, 15YSZ layers, and carbide cutting tool were 3.66*10?6, 3.546*10?6 and 14*10?6 K?1, respectively. The reasons for the enhancement of the tribological properties of the carbide cutting tools by the ceramic coatings are discussed.
Research Team: The team from the Department of Materials Engineering, University of Babylon, Iraq
Technical Approach: The research team deposited TiO?/yttria-stabilized zirconia (YSZ) multilayer ceramic coatings on K10 tungsten carbide inserts via the sol-gel method, systematically analyzing the effects of 8% and 15% yttrium contents (8YSZ vs. 15YSZ) on performance.
Microhardness: The 15YSZ-coated insert achieved 1,679 HV (uncoated insert: only 866 HV), a nearly 2-fold increase!
Scratch Hardness: The 15YSZ coating reached 22.98 GPa, significantly enhancing interfacial bonding strength.
Friction Coefficient: The 15YSZ coating showed a coefficient of only 0.17, a 76% reduction compared to the uncoated insert (0.71) (Figure 12).The key data from the experiments are remarkable. In terms of hardness and scratch resistance, microhardness tests show that the 15YSZ-coated insert achieves an impressive 1,679 HV—nearly double the 866 HV of the uncoated insert. This means the coated insert can more effectively withstand high-intensity cutting, reducing tool wear. Scratch hardness tests further confirm the coating’s excellence: the 15YSZ coating’s 22.98 GPa value directly reflects a significant enhancement in interfacial bonding between the coating and substrate, akin to armoring the tool with a robust, well-adhered layer.
In the realm of friction and wear resistance, the experimental data are equally striking. The friction coefficient test chart (Figure 12) clearly shows that the 15YSZ coating has a coefficient of only 0.17—76% lower than the uncoated insert’s 0.71. This dramatic reduction enables smoother tool operation during cutting, minimizing energy loss from friction. Even more impressive, wear rate tests (Figure 14) reveal that the 15YSZ coating has a wear rate as low as 0.24×10?3 g/m—85% lower than the uncoated insert—significantly extending tool service life.
Figure 10. The micro hardness of uncoated insert and different coatings, and the images of indents produced on the surface of uncoated inserts and different coatings.
Figure 12. Coefficient of friction versus time of uncoated insert and the inserts coated by TiO2/8YSZ and TiO2/15YSZ coatings respectively.
Figure 14. Wear rate of the uncoated and coated inserts.
The sol-gel method completes coating deposition at a low temperature of 700°C, avoiding thermal damage to the substrate caused by traditional high-temperature processes while achieving high purity and uniformity (Figure 4).
Grain Refinement: Increasing yttrium content from 8% to 15% inhibits grain growth and refines the coating structure (XRD shows stable cubic phase, Figure 3).
Performance Balance: High yttrium content enhances hardness and wear resistance but requires trade-offs with thermal conductivity (15YSZ has slightly higher thermal conductivity than 8YSZ).
In terms of thermal performance optimization, the 8YSZ coating exhibits unique advantages. With a thermal conductivity of only 10.3 W/m·K, it effectively blocks heat conduction generated during cutting, preventing tool performance degradation due to overheating. Meanwhile, the YSZ coating (3.5–3.6×10?? K?1) has a smaller difference in thermal expansion coefficient from the tungsten carbide substrate (14×10?? K?1), a feature that significantly reduces the risk of coating spalling caused by thermal stress and further enhances tool stability and reliability.
The technological breakthrough of this study is of milestone significance. First, the sol-gel method can complete coating deposition at a low temperature of 700°C. Compared with traditional high-temperature processes, this low-temperature process successfully avoids thermal damage to the substrate. As clearly shown in the FESEM images (Figure 4), the coating prepared by the sol-gel method features high purity and uniformity, with a dense and homogeneous structure, laying a solid foundation for improving tool performance. Second, the research on the yttrium content regulation mechanism has also achieved important results. As the yttrium content increases from 8% to 15%, the XRD pattern (Figure 3) shows that the cubic phase remains stable, and grain growth is effectively inhibited, achieving refinement of the coating structure. However, the research team also points out that although high yttrium content can improve hardness and wear resistance, it needs to be balanced with thermal conductivity, as reflected in the slightly higher thermal conductivity of 15YSZ than that of 8YSZ.
Figure 4. FESEM image of a multilayer coating (YSZ) on carbide insert: (a) 8YSZ 100000 Mag., (b) 8YSZ 25000 Mag.
Figure 3. XRD Pattern of (a) carbide cutting tool, (b) 8YSZcoating
In terms of industrial application prospects, the research findings offer broad market space and significant economic value. In high-wear scenarios such as automotive manufacturing and mining drilling, experimental data show that the service life of coated tools is increased by over 50%. This means enterprises can reduce tool replacement frequency and downtime, thus significantly improving production efficiency. Meanwhile, the 85% reduction in wear rate directly translates to substantial machining cost savings, effectively controlling both tool procurement and maintenance costs. Additionally, the low friction coefficient reduces energy consumption during tool operation, aligning with the global trend of green manufacturing and yielding non-negligible environmental benefits. The research conducted by the team from the Department of Materials Engineering, University of Babylon, Iraq, not only paves a new path for tungsten karbür alet coating technology but also demonstrates the immense potential of sol-gel processes in high-temperature industrial components. Looking ahead, with further optimization of yttrium content and multi-layer structure design, the performance of tungsten carbide tools is expected to achieve new breakthroughs, bringing more surprises and transformations to the industrial processing field.
This study not only provides a novel solution for tungsten carbide tool coating technology but also reveals the huge potential of sol-gel processes in high-temperature industrial components. In the future, optimizing yttrium content and multi-layer structure design may further break through performance limits!
]]>In high-temperature, high-wear industrial processing scenarios, the lifespan and performance of tungsten carbide (WC-Co) inserts directly determine production costs and efficiency. While traditional coating technologies (such as CVD/PVD) can enhance performance, their high-temperature processes often lead to a reduction in substrate hardness. How can we achieve low-temperature, high-efficiency coatings while maintaining high hardness, low friction, and thermal shock resistance? A recent study published in Heat Treatment and Surface Engineering (HTSE) provides an innovative solution!
Kareem, S. J., Wurood Asaad, M., & Al-Ethari, H. ?Enhancement of tribological properties of carbide cutting inserts by ceramic coating deposition. Heat Treatment and Surface Engineering,(2024).?6(1).
https://doi.org/10.1080/25787616.2024.2331865
Coating by sol–gel deposition to modify the tribological properties of K10 carbide cutting tool was performed. The study examines the thermal and tribological characteristics of uncoated cutting inserts and the cutting inserts coated with TiO2/8YSZ and TiO2/15YSZ layers respectively. The TiO2/8YSZ and TiO2/15YSZ coatings had a hardness of 1151.6 and 1678.9 HV, respectively, and the TiO2/8YSZ and TiO2/15YSZ coated inserts had scratch hardness of 2.73 and 22.98 GPa respectively. Among the uncoated and coated tools, the TiO2/15YSZ coated inserts had the lowest coefficient of friction and rate of wear. The TiO2/8YSZ coated insert had a lower thermal conductivity when compared to TiO2/15YSZ coated insert and uncoated carbide cutting insert (10.3 vs. 14.1, and 41.8 W/m.K). The thermal expansion coefficients of the 8YSZ layers, 15YSZ layers, and carbide cutting insert were 3.66*10?6, 3.546*10?6?and 14*10?6?K?1, respectively. The reasons for the enhancement of the tribological properties of the carbide cutting inserts by the ceramic coatings are discussed.
Materials Engineering Department, University of Babylon, Iraq
Deposited TiO?/Yttria-Stabilized Zirconia (YSZ) multilayer ceramic coatings on K10 tungsten carbide (WC) inserts via sol-gel method, systematically analyzing the effects of 8% vs. 15% yttria content (8YSZ vs. 15YSZ) on performance.
Microhardness:
15YSZ-coated insert: 1679 HV (vs. 866 HV for uncoated tool) → ~2× improvement
Scratch hardness: 15YSZ coating reached 22.98 GPa, indicating significantly enhanced interfacial adhesion.
Coefficient of friction (CoF):
15YSZ coating: 0.17 (vs. 0.71 for uncoated tool) → 76% reduction! (See Figure 2)
Figure 1. The micro hardness of uncoated tool and different coatings, and the images of indents produced on the surface of uncoated inserts and different coatings.
Figure 2. Coefficient of friction versus time of uncoated insert and the tools coated by TiO2/8YSZ and TiO2/15YSZ coatings respectively.
Figure 3. Wear rate of the uncoated and coated inserts.
15YSZ coating:
Wear rate: 0.24×10?3 g/m (85% reduction compared to uncoated tools, see Figure 3)
Thermal conductivity:
8YSZ coating: 10.3 W/m·K (effectively blocks cutting heat transfer)
YSZ coating (3.5-3.6×10?? K?1) vs. WC substrate (14×10?? K?1)
Minimal mismatch significantly reduces thermal stress-induced delamination risks
1Low-Temperature Processing Advantage
2Sol-gel coating deposition achieved at 700°C (low-temperature)
3Avoids thermal damage to substrate caused by conventional high-temperature processes
4Achieves high purity and excellent uniformity (see Figure 4)
Increasing yttria content from 8% to 15% effectively inhibits grain growth and refines coating structure (XRD confirms stabilized cubic phase, see Figure 5)
Higher yttria content (15YSZ) enhances hardness and wear resistance
Requires trade-off with slightly increased thermal conductivity compared to 8YSZ
Figure 4. FESEM image of a multilayer coating (YSZ) on carbide tool: (a) 8YSZ 100000 Mag., (b) 8YSZ 25000 Mag.,
Figure 5. XRD Pattern of (a) carbide cutting insert, (b) 8YSZcoating, (c) 15 YZS coating.
Extended Insert Lifespan:
Experimental results demonstrate over 50% longer tool life for coated inserts, making them ideal for high-wear applications like automotive manufacturing and mining drilling.
Cost Reduction:
An 85% reduction in wear rate translates to fewer tool replacements, significantly lowering machining costs.
Environmental Benefits:
The low friction coefficient reduces energy consumption, aligning with green manufacturing trends.
This study not only provides an innovative solution for tungsten carbide tool coatings but also highlights the immense potential of sol-gel technology in high-temperature industrial components. Future optimization of yttria content and multilayer structure design could push performance boundaries even further!
]]>In the PCB manufacturing industry, thick copper boards have become the core substrate for power modules, high-power electronic devices, and industrial control systems due to their exceptional conductivity and thermal dissipation properties. As copper thickness increases from the conventional 1-3 ounces to 6 ounces or even higher, their processing technology faces unprecedented challenges.
Drilling, as a critical process in PCB production, presents unique physical phenomena and process contradictions when working with thick copper boards:
The high thermal conductivity significantly reduces cutting temperatures
The plastic deformation characteristics of copper cause secondary issues like copper wrapping and material adhesion
Behind these contradictions lies a complex interplay of materials science, mechanical processing, and thermodynamics.
With a thermal conductivity of 401 W/(m·K) – approximately 1.8 times that of aluminum and 5 times that of iron – copper exhibits unique thermal behavior during drilling operations. The rapid heat dissipation through the copper substrate theoretically suppresses temperature rise between tool and workpiece, yielding dual benefits:
? Tool wear rate reduction by ~30%
? Over 50% decrease in positional accuracy deviation caused by thermal deformation
These characteristics make it particularly suitable for high-precision multilayer board processing.
However, this seemingly ideal thermal property conceals a paradox:
During initial drill penetration, copper’s instantaneous plastic flow creates a high-pressure zone ahead of the cutting edge. While bulk temperatures remain low, frictional heat at microscopic contact points can momentarily reach copper’s recrystallization temperature (~200°C).
This phenomenon causes dynamic softening of the copper surface layer, forming a viscous metal flow. When drill speed exceeds 80,000 RPM, the contact time between chips and the tool’s rake face shortens to microsecond levels. However, the ductility of copper chips makes them difficult to break effectively, instead forming long spiral chips under centrifugal force. These copper wires entangle between the drill shank and chip flutes, not only hindering coolant penetration but also generating secondary frictional heat. Experimental data shows that when copper thickness exceeds 4 ounces, the localized temperature rise caused by chip entanglement can reach 40% of the base cutting temperature, creating a “low-temperature cutting with localized high-temperature” paradox effect.
Pure copper has an elongation rate as high as 45%, and this excellent plasticity manifests as three-stage deformation characteristics during drilling: lattice slip during initial shear, dislocation multiplication during plastic flow, and necking before fracture. When drilling thick copper boards, increased axial cutting depth makes the material removal process closer to an orthogonal cutting model, reducing the shear plane angle to 15°-25° and increasing chip thickness by 30%-50%. These thick, continuous chips intermittently contact the hole wall during ejection, forming a periodic stick-slip dynamic process.
The essence of copper adhesion is interfacial metallurgical bonding. When cutting temperature reaches copper’s recrystallization temperature, fresh copper surfaces undergo atomic diffusion with the tool surface under high pressure. Even with relatively low bulk temperatures, instantaneous temperatures at microscopic asperities can exceed 500°C, sufficient to cause micro-welding. When using tungsten carbide drills, cobalt binder phase precipitation accelerates this adhesion. EDX analysis shows adhesion layers can contain up to 8.3wt% cobalt, forming Co-Cu intermetallic compounds. These metallurgical bonding layers have shear strength up to 350MPa – three times copper’s own strength – causing negative offset of the tool’s effective rake angle and increasing cutting force by over 25%.
Addressing thick copper board drilling challenges requires establishing a multi-dimensional process control system. For cutting parameters, the “high speed-low feed” strategy presents contradictions: increasing speed to 90,000 RPM can reduce feed per tooth to 0.01mm, helping thin chips, but greater centrifugal force increases entanglement risk. Recent research shows that variable-frequency oscillatory feed technology, superimposing 10-50Hz axial vibration, can reduce chip length by 70%. Combined with pulsed coolant systems injecting high-pressure coolant (7MPa) during vibration retraction effectively clears chip flute accumulation.
Innovative tool geometry design is more critical. Reducing drill point rake angle from conventional 30° to 15° increases cutting force but enhances edge strength, suppressing plastic flow. Adjusting helix angle from 40° to 35° maintains chip removal capability while reducing chip spiral curvature radius to promote breakage. A German tool manufacturer’s “dual-wave edge” technology creates periodic corrugations on cutting edges (0.8mm wavelength, 0.05mm amplitude), inducing mandatory bending strain that increases chip breakage probability to 92%.
In coating technology, multilayer composite coatings demonstrate unique advantages. The base layer uses 1μm-thick CrN to improve bonding strength, the intermediate layer is a 0.5μm MoS? solid lubricant layer, and the surface layer deposits 2μm diamond-like carbon (DLC) film. This structure reduces the friction coefficient from 0.6 to 0.15 and decreases adhesion by 80%. A Taiwanese PCB manufacturer using this coated drill for 6-ounce thick copper boards increased tool life from 1,200 to 4,500 holes while maintaining hole wall roughness Ra below 1.6μm.
Material engineers are seeking breakthroughs in copper foil itself. Adding 0.3%-0.5% tellurium forms Cu-Te alloy, maintaining conductivity (≥85% IACS) while increasing tensile strength to 350MPa and controlling elongation at about 15%. This moderate plasticity reduction shortens chip fracture length by 40%. Another innovative approach develops anisotropic copper foil through rolling processes that align grains along the drilling direction, utilizing crystallographic texture effects to reduce transverse plasticity. Tests show this copper foil reduces chip entanglement by 65% when processing 0.3mm diameter holes.
Laser-textured microdimple arrays (20μm diameter, 5μm depth, 50μm spacing) on copper foil surfaces provide new solutions for adhesion challenges. These microstructures act as lubricant reservoirs, continuously releasing nano-MoS? particles. During drilling, these solid lubricants form transfer films at the tool-workpiece interface, reducing interfacial shear strength to 1/3 of pure copper systems. Japanese research data shows this method decreases drilling axial force by 28% and reduces adhesive wear by 90%.
Under Industry 4.0 framework, thick copper board drilling is evolving toward digital closed-loop control. Integrated multi-physics sensors monitor spindle current (±0.1A sensitivity), acoustic emission signals (50-500kHz range), and infrared thermal imaging (0.1mm resolution). Deep learning algorithms establish cutting state recognition models that automatically adjust spindle torque output and trigger 0.8MPa high-pressure air knives for online chip removal when detecting entanglement frequencies (typically 120-180kHz).
More advanced adaptive systems include intelligent drills developed by a U.S. equipment manufacturer that dynamically adjust processing strategies based on copper thickness: constant-force feed mode (120-150N cutting force) for 4-6oz copper, and step drilling (0.8× pilot hole + stepped feed) for >6oz copper. This strategy reduces tool load fluctuation by 40% and improves hole position accuracy to ±25μm.
Laser drilling breaks traditional machining limits. Picosecond lasers (10ps pulse width) with annular beam technology achieve <2° taper microholes in 100μm copper with <5μm heat-affected zones. Though currently 3-5× more expensive than mechanical drilling, it’s replacing conventional processes in high-density interconnects. Hybrid processing shows greater potential: laser-drilled 0.05mm pilot holes followed by micro-drill finishing improves efficiency by 70% and reduces tool wear by 90%.
Ultrasonic-assisted Drilling Technology Enters Practical Application Stage
By integrating a 40kHz ultrasonic vibration device into the spindle, the drill bit generates high-frequency vibrations with 5μm axial amplitude. This vibration creates an “intermittent cutting” characteristic in the machining process, effectively releasing cutting stress periodically. When processing 8-ounce thick copper boards, the axial force is reduced by 35%, and chip thickness is decreased to 1/3 of conventional processes.
A more revolutionary breakthrough comes from cryogenic cutting technology. Using liquid nitrogen (-196°C) jets to locally freeze the cutting zone induces brittle transformation in copper, achieving brittle fracture mode. Preliminary tests show this method can completely eliminate chip entanglement, though it requires solutions for dimensional shrinkage compensation caused by low temperatures.
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As PCB technology continues advancing toward high-power and high-density applications, solving thick copper board machining challenges has evolved beyond simple process improvements into a multidisciplinary innovation arena. From interfacial behavior research at the molecular dynamics level to intelligent control of macro manufacturing systems, each technological breakthrough redefines the limits of electronics manufacturing.
In the future, with the maturation of new material technologies like superconducting copper alloys and quantum dot lubricants, along with developments in atomic-scale manufacturing processes, thick copper board drilling will transition from the “problem-solving” stage to the “performance-design” stage, opening new frontiers for miniaturization and efficiency in electronic devices. This ongoing contest between copper and drill bits will ultimately propel the entire electronics manufacturing industry to higher dimensions of evolution.
The capillary tip is a critical tool in the wire bonding process, with high value and being a perishable item. The selection and performance of the capillary tip determine the flexibility, reliability, and cost-effectiveness of the bonding.
capillary tips include those used in ball bonding (capillary tip type) and those used in wedge bonding (wedge type). The two types are fundamentally different.
The main body of a wedge capillary tip is typically cylindrical, with a wedge-shaped head. The back of the capillary tip has a hole for threading the bonding wire, and the hole diameter corresponds to the wire size. The tip face of the wedge capillary tip comes in various structures depending on application requirements, and it determines the size and morphology of the bond.
During use, the wire is threaded through the capillary tip hole, forming a 30°–60° angle with the bonding surface. When the capillary tip descends onto the bonding area, it presses the wire against the surface, forming a shovel-shaped or crescent-shaped bond. Some examples of wedge capillary tips are shown in Figure 1.
During operation, the bonding wire passing through the capillary tip generates pressure and friction between the capillary tip tip and the pad metal. Therefore, capillary tips are typically made from materials with high hardness and toughness.
Considering both manufacturing requirements and bonding methods, capillary tip materials must exhibit high density, high flexural strength, and the ability to be processed into a smooth surface. Common capillary tip materials include:
Tungsten carbide exhibits strong resistance to breakage and was widely used in early capillary tip manufacturing. However, machining tungsten carbide is challenging, making it difficult to achieve a dense, pore-free surface. Due to its high thermal conductivity, tungsten carbide capillary tips must be heated during bonding to prevent heat dissipation from the pad.
Titanium carbide has a lower material density than tungsten carbide and is more flexible. Reports indicate that under the same ultrasonic transducer and capillary tip structure, titanium carbide capillary tips produce 20% greater tip vibration amplitude than tungsten carbide capillary tips.
High-purity alumina offers excellent wear resistance, chemical stability, and low thermal conductivity, eliminating the need for capillary tip heating. When used in automated bonding equipment, alumina capillary tips can achieve up to 1 million bonding cycles.
In recent years, ceramics have been widely adopted for capillary tip manufacturing due to their smooth, dense, pore-free structure, and stable chemical properties. Ceramic capillary tips provide superior machining precision for tip faces and wire holes compared to tungsten carbide.
When selecting a capillary tip, the primary considerations include: material, hole diameter, and structural design.
The hole diameter is determined by the bonding wire diameter. An improper selection can lead to wire damage or even breakage.
For ball bonding capillary tips, the inner diameter is typically 1.3–1.4 times the gold wire diameter.
For wedge bonding capillary tips, the inner diameter is generally about 2 times the gold wire diameter.
Capillary Tip Structure
The capillary tip?features a precise and complex structure, with key parameters including length, profile, and tip geometry, all of which are closely related to the workpiece design and significantly influence bond strength. For example
The front and rear radii of the capillary tip?should be sufficiently large to avoid stress concentration and maximize bond strength.
When bonding in cavity or recessed areas, the capillary tip?shape must be carefully selected to prevent bond interference (shadowing).
The tip diameter depends on pad pitch—a larger tip diameter increases the risk of short circuits between adjacent pads but also enhances second-bond strength.
After multiple welding processes, the capillary tip will adhere to pollutant particles and be partially damaged, resulting in the aging of the capillary tip. This is mainly manifested in the deterioration of the solder joint morphology, the reduction of lead pulling force, and in severe cases, wire breakage or curling may occur. Figure 4 shows the weld morphology of a wedge-shaped titanium carbide alloy after repeated gold wire welding on the same substrate under the same welding parameters using a new cutting tip and after 3000, 6000, 9000, 12000, 14000, and 16000 welding cycles. It can be seen that the solder joint morphology of the new capillary tip is good. The solder joint morphology deteriorated after 9000 welding cycles, and after 16000 welding cycles, the solder joint morphology no longer meets the inspection requirements.
During the wire bonding process, hot press welding applies pressure from the end face of the cutting tip, causing a certain degree of mutual plastic deformation and close contact between the wire and the pad metal under pressure, and their molecules diffuse and firmly bond with each other.
Ultrasonic welding generates ultrasonic power from the transducer to vibrate the capillary tip, creating friction at ultrasonic frequencies between the lead and the pad metal, removing the oxide layer at the interface, and causing elastic deformation.
Both of these bonding principles will cause force on the end face of the cutting edge, resulting in wear and tear of the cutting edge after multiple welding, leading to severe deformation of the welding point.
The wear of the tip?end face is also affected by the operating method. When using manual bonding equipment for bonding operations, the operating technique has a significant impact on the end face of the cutting tip. For example, if the operator shakes their hand or applies excessive force during welding, it will accelerate the wear of the end face of the cutting tip. This phenomenon often occurs when novice operators operate.
During actual wire bonding operations, it was found that some capillary tips?had a service life significantly shorter than expected. Microscopic examination revealed no obvious wear on the capillary tip?tip surface, but a thin film was observed adhering to the surface.
Figure 5 shows optical and SEM micrographs of a capillary tip?tip after 9,000 bonding cycles. The images clearly show a thin film attached to the tip surface, which affected the surface flatness and caused severe deformation of the bond points.
EDX spectrum analysis indicated that the film on the capillary tip?tip contained high levels of silicon and oxygen, as shown in Figure 6. Preliminary analysis suggests that the silicon likely originated from the chip, bonding wire, or substrate. During the bonding process, silicon gradually diffused (or migrated) to the capillary tip?and accumulated on the tip surface over time, ultimately affecting the bonding performance.
The silicon and oxide compounds accumulated on the capillary tip tip surface can be effectively removed using a NaOH solution, restoring the original tip morphology. Figure 7 presents a comparative view of a capillary tip tip before and after cleaning. As evident from Figure 7, the surface deposits are completely eliminated, allowing the capillary tip to resume normal operation.
The capillary tip is a critical tool in microassembly wire bonding. This paper has examined the materials, structural design, and selection methodology for commonly used wedge capillary tips, providing engineers with guidance to choose the most suitable capillary tip for optimal bonding quality and cost efficiency.
Additionally, the study addresses capillary tip aging phenomena, identifying two primary causes:
Wear on the capillary tip tip face (irreversible degradation).
Accumulation of silicon/oxide compounds on the tip surface (removable via cleaning).
By implementing periodic cleaning to remove surface contaminants, capillary tips can remain operational until reaching their wear-induced service limit. This approach maximizes tool lifespan while maintaining process reliability.
]]>Natural or artificial aging, as well as vibration treatment, can partially eliminate residual stresses in blanks. Pre-machining is also an effective method. For bulky blanks with excessive stock allowance, post-machining deformation tends to be significant. By pre-machining to remove excess material and balance stock allowance, subsequent machining deformation can be reduced. Additionally, allowing the pre-machined blank to rest helps release residual stresses.
Tool material and geometric parameters significantly influence cutting forces and heat generation. Proper tool selection is crucial for minimizing part deformation.
A larger rake angle (while maintaining edge strength) enhances cutting sharpness, reduces chip deformation, improves chip evacuation, and lowers cutting forces and temperatures. Negative rake angles should be avoided.
The clearance angle directly affects flank wear and surface finish. For rough milling with heavy loads and high heat, a smaller clearance angle improves heat dissipation. For finish milling, a larger clearance angle reduces friction and elastic deformation.
A higher helix angle ensures smoother milling and reduces cutting resistance.
A smaller lead angle improves heat dissipation and lowers average cutting zone temperatures.
Aluminum’s high plasticity demands larger chip pockets. Tools with fewer teeth and wider gullets are preferred.
The cutting edge roughness should be below Ra = 0.4 μm. Lightly honing new tools with a fine stone removes burrs and micro-serrations, reducing heat and deformation.
Tool wear increases surface roughness, cutting temperature, and part deformation. Wear limits should not exceed 0.2 mm to prevent built-up edge. Workpiece temperature should stay below 100°C to avoid distortion.
For thin-walled aluminum parts with low rigidity:
Axial Clamping for Bushings
Radial clamping (e.g., 3-jaw chucks) causes post-machining deformation. Instead, use a threaded mandrel inserted into the part’s bore, secured axially with a endplate and nut to maintain precision during OD machining.
Uniform clamping force distribution paired with light cuts minimizes distortion.
Fill hollow parts with a low-melting filler (e.g., urea-potassium nitrate melt) to enhance rigidity during machining. Dissolve the filler post-process in water/alcohol.
High-speed machining with large stock or interrupted cuts may induce vibration. A typical CNC process flow:
Roughing → Semi-finishing → Corner Cleaning → Finishing
For high-precision parts, repeat semi-finishing before final passes. Post-roughing natural cooling relieves stresses. Leave 1–2 mm stock after roughing; maintain 0.2–0.5 mm uniform allowance in finishing to ensure stability, reduce deformation, and achieve high surface quality.
In addition to the aforementioned causes, operational methods play a crucial role in controlling deformation during aluminum part machining.
For better heat dissipation, use alternating symmetrical machining. Example: A 90mm plate machined to 60mm achieves 0.3mm flatness when processed in alternating passes versus 5mm with consecutive machining.
Machine all cavities layer-by-layer simultaneously to ensure uniform stress distribution, preventing deformation from uneven forces.
Adjust depth of cut (ap) with corresponding feed rate and spindle speed increases in CNC high-speed milling to balance productivity and reduced cutting forces.
Use conventional milling for roughing (maximum removal rate) and climb milling for finishing (better surface quality with progressive chip thickness reduction).
Before final passes, briefly release and reapply minimal clamping force to allow natural recovery, applying force along the part’s most rigid direction.
Cavity Machining Method
Avoid direct plunging; pre-drill or use helical entry paths to prevent chip packing and tool breakage.
Aluminum part deformation stems from material properties, geometry, and processing conditions, primarily involving?blank residual stresses,cutting forces/heat,and clamping stresses.The integrated application of these process optimizations and operational techniques significantly reduces deformation, enhances precision and surface quality, providing reliable technical support for production.
]]>A positive rake angle tool refers to a turning tool where the front face is inclined toward the interior of the workpiece relative to the cutting point, resulting in a positive rake angle (typically +5° to +15°). Its structural characteristic is a relatively sharp cutting edge, with a smaller contact area between the front face and the chip.
A negative rake angle tool, on the other hand, has a front face inclined outward from the workpiece relative to the cutting point, resulting in a negative rake angle (typically -5° to -10°). Its structural feature is a blunter cutting edge, with a thicker and more robust tooltip.
Advantages:
Lower Cutting Forces: A positive rake angle allows smoother chip flow and reduces deformation, decreasing main cutting forces by 15–25%.
Better Chip Evacuation: Shorter chip-tool contact length reduces built-up edge formation.
Suitable for Finishing: Minimizes vibration, enabling better surface finish (Ra < 1.6 μm).
Dezavantajlar?:
Lower Tooltip Strength: The positive geometry reduces material support, making the tool prone to chipping in interrupted cuts or hard materials.
Poor Heat Dissipation: Smaller chip-tool contact area limits heat transfer, accelerating crater wear at high speeds.
Shorter Tool Life: Typically 60–70% of negative rake tools under the same conditions.
Advantages:
High Tooltip Strength: The negative angle creates a “support wedge,” improving impact resistance by >50%.
Superior Heat Dissipation: Larger chip-tool contact area enhances heat conduction, reducing cutting temperatures by 15–30°C.
Multi-Sided Usability: Often designed with double-negative angles, allowing flipping for extended use.
Limitations:
Higher Cutting Forces: Negative rake increases chip deformation, raising main cutting forces by 20–30%.
Greater Power Demand: Requires 15–20% more motor power from the machine tool.
Vibration Risk: Prone to chatter in long overhang machining due to increased cutting forces.
The following systematic experiment compares the performance of carbide positive and negative rake tools under different machining conditions, providing practical insights for tool selection.
1.Materials & Equipment:
Positive rake tool (+8° rake angle)
Negative rake tool (-6° rake angle)
Both use YG8 karbit substrate with TiAlN coating and 0.4 mm nose radius.
2.Workpiece:45# steel (Φ50×200 mm), quenched and tempered to HRC 28–32.
3.Machine:CA6140 lathe with 3-jaw chuck and tailstock center.
4.Measurement Instruments:
Surface roughness tester (Mitutoyo SJ-210)
Electron microscope (OLYMPUS DSX510)
Cutting force dynamometer (Kistler 9257B)
Infrared thermometer (Fluke Ti400)
5.Parameters
Fixed: Depth of cut (ap = 1 mm), feed rate (f = 0.15 mm/rev).
Variable: Cutting speed (v = 60–180 m/min).
Three repetitions per condition for reliability.
Using flank wear VB = 0.3 mm as the failure criterion:
Negative rake angle tools demonstrate significantly longer service life, exceeding positive rake tools by an average of 50-70%. Analysis of wear patterns reveals that positive rake tools primarily fail through crater wear on the rake face and tooltip chipping, whereas negative rake tools exhibit more uniform flank wear, demonstrating superior fracture resistance.
The data shows that under all tested cutting speeds, negative rake tools generate significantly higher principal cutting forces than positive rake tools, with an average increase of approximately 17%. This is attributed to the negative rake design’s larger contact area between the tool’s rake face and chips, as well as intensified cutting deformation. Notably, while cutting forces for both tool types decrease with increasing cutting speed, the difference ratio remains essentially stable.
Results indicate that negative rake tools maintain consistently lower cutting temperatures than positive rake tools, typically by 15-25°C. This thermal advantage primarily stems from the negative rake design’s enhanced tooltip strength and improved heat dissipation capacity. The temperature difference becomes particularly pronounced during high-speed cutting (v>120m/min), reaching approximately 30°C.
Surface roughness serves as a critical indicator of machining quality. At a feed rate of f=0.15mm/rev, measurements show:
Positive rake tool surface roughness (Ra): 1.6-2.0μm
Negative rake tool surface roughness (Ra): 1.2-1.5μm
Electron microscope observations reveal that surfaces machined with negative rake tools exhibit more uniform texture patterns with fewer burrs and vibration marks. This improvement results from the negative rake design’s enhanced system rigidity that reduces cutting vibrations. Furthermore, negative rake tools maintain more stable tooltip geometry during machining, avoiding the surface quality degradation caused by micro-chipping that often occurs with positive rake tools.
1.While carbide negative rake tools show slightly inferior performance in cutting force, they demonstrate clear advantages in cutting temperature control, surface quality, and tool life.
2.The performance advantages of negative rake tools become more pronounced at higher cutting speeds, making them particularly suitable for modern high-speed machining requirements.
3.Positive rake tools excel in reducing cutting forces and are better suited for machining systems with limited rigidity.
4.Optimal tool angle selection should comprehensively consider multiple factors including workpiece material, machine tool conditions, and specific machining stages.
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The physical essence of coating technology lies in modifying interfacial properties of the substrate via surface engineering. For rotating tools like drills, coatings must simultaneously reduce friction, enhance surface hardness, and inhibit thermal conduction. When coating thickness ranges from nanometers to micrometers, significant size effects emerge in mechanical properties. Experimental data shows that TiN coatings reach peak microhardness (≈2300HV) at 2-3μm thickness; further increases reduce hardness due to accumulated residual stress. This stress heterogeneity creates preferential paths for microcrack propagation during drilling, especially under interrupted cutting conditions, where excessively thick coatings are prone to delamination.
Thermal barrier effects are vital, but thermal conductivity does not scale linearly with thickness. Finite element simulations reveal that beyond 5μm, AlCrN coatings show diminishing thermal resistance gains. Excessive thickness may impede heat dissipation, intensifying thermal stress concentration in high-speed machining.
Drill edge sharpness directly affects chip evacuation and force distribution. The “rounding effect” during deposition causes exponential growth in edge radius with thickness. For DLC coatings increasing from 1μm to 3μm, edge radius swells from 3.2μm to 8.7μm, raising cutting resistance by 23%. This geometric dulling is pronounced in ductile materials—aluminum alloy tests show a 15% rise in chip buildup probability per micrometer increase in edge radius. Paradoxically, moderate dulling suppresses edge chipping in brittle materials, highlighting the need for material-specific thickness optimization.
Coating thickness impacts flute hydrodynamics, often overlooked. 3D flow simulations show that when coating exceeds 12% of flute depth, secondary chip flow intensifies, causing blockages. In deep-hole drilling, this exacerbates radial vibration, increasing borehole deviation. A German toolmaker reduced straightness errors by 40% by decreasing TiAlSiN thickness from 4μm to 2.5μm.
Coating-substrate bond strength does not monotonically change with thickness. Interface energy tests reveal a 30% strength drop when CrN exceeds ~4μm, due to lattice mismatch stress accumulation. This weakening is perilous under cyclic loading, with failures originating at nanoscale voids. Gradient transition layers enhance critical thickness—inserting a 50nm Ti interlayer between WC-Co and TiCN boosts critical thickness from 3.2μm to 5.1μm.
Cyclic loading reveals time-dependent failure. Accelerated life tests show 3μm AlTiN coatings reduce crack growth by 67% after 10? impacts, benefiting from crack closure effects. Beyond 2×10? cycles, thicker coatings exhibit larger spalling areas, indicating an optimal thickness for fatigue life. This non-monotonic relationship demands precise service life predictions.
Coating thickness has dual impacts on precision. In micro-hole drilling, a 2μm thickness deviation causes 0.8-1.2% diameter variation. A Japanese firm’s adaptive coating technology deposits 1.5μm at the tip and 2.2μm at margins, controlling diameter?floating?to 0.3%. Such differential designs surpass conventional uniform coatings.
Residual stress in workpieces couples with coating thickness. XRD analysis shows a drop from -450MPa to -280MPa when thickness increases from 1μm to 3μm, potentially reducing dimensional stability. However, thicker coatings reduce heat-affected zones by 35%, critical for aerospace aluminum.
Coating cost scales with thickness squared, but lifespan gains have inflection points. An automotive plant found that increasing TiAlN from 2μm to 3μm raised costs by 18% while only improving life by 12%, resulting in negative ROI. However, nano-multilayered 2.5μm coatings outperformed 3μm by 25%, indicating that thickness alone is suboptimal.
Future coatings will feature intelligent thickness control. Digital twin-based optimization systems are operational, adjusting parameters via real-time force/temperature feedback. A German AI system predicts optimal thickness in 48 hours, enhancing performance by >30%. Dynamic adaptation may revolutionize traditional thickness determination.
Coating thickness orchestrates a precision symphony in drill performance, where each parameter adjustment triggers cascading effects. Modern engineers must transcend empirical selection, establishing multi-physics digital design paradigms. Future breakthroughs may lie in self-sensing smart coatings with dynamic thickness adjustment, potentially sparking a new revolution. In this era of precision and intelligence, mastering coating thickness will benchmark a nation’s advanced manufacturing prowess.
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