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.
Wniosek
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 fracture and separation of materials during metal cutting constitute a complex dynamic process involving multiple physical mechanisms. Research indicates that this process primarily consists of three key stages:
Plastic deformation occurs first. Crack initiation and propagation follow. Finally, material separation is achieved.
Based on extensive experimental data and theoretical analysis, this phenomenon can be systematically explained as follows:
According to material response and processing conditions, fracture can be divided into the following categories:
Dominant type, where shear bands form at the tool-workpiece contact surface, and material separates along slip planes. For example, pure shear fracture is common in highly plastic materials (such as low-carbon steel), with fracture surfaces appearing wedge-shaped; microvoid coalescence fracture achieves separation through microvoid nucleation and aggregation.
At the tool’s leading edge or chip’s free surface, material forms tear ridges due to tensile stress, mostly occurring in brittle materials or under high cutting speed conditions.
Under low temperature or impact loading, cracks rapidly propagate along specific crystal planes (cleavage planes), producing flat and shiny fracture surfaces, commonly seen in body-centered cubic metals (such as ferritic steel).
The fracture in metal cutting can be divided into three stages:
Crack initiation: When the tool contacts the workpiece, localized stress concentration leads to the formation of microcracks inside or on the surface of the material. For example, in the first deformation zone (chip formation zone) during cutting, the material undergoes slip deformation due to shear stress, thereby initiating cracks.
As the tool advances, the crack extends along specific paths. The propagation direction is influenced by stress state and material properties, potentially manifesting as shear fracture (along the direction of maximum shear stress) or tensile fracture (along the direction of maximum normal stress).
The crack penetrates through the material to form chips, and the resulting fracture surface may exhibit either ductile (fibrous) or brittle (crystalline) characteristics.
Taking the cutting card theory illustrated in the following diagram as an example, the cutting process is divided into four stages: initial contact, crack initiation, material uplift, and cyclic phase. The crack initiation stage represents the critical point for fracture formation, while the cyclic phase involves periodic crack nucleation, resulting in saw-tooth shaped chips.
Primary Deformation Zone (A-H region): Material undergoes intense shear deformation, forming initial cracks.
Secondary Deformation Zone (G-E region): Friction between chip and tool causes additional plastic deformation, potentially accompanied by localized fracture.
Tertiary Deformation Zone (E-D region): Workpiece surface material fractures due to tool flank face compression, forming the machined surface.
Tool Parameters: The tool’s rake angle, clearance angle, and major cutting edge angle affect stress distribution. For example, increasing the major cutting edge angle reduces cutting forces but may alter crack propagation paths.
Low speed → Ductile fracture; High speed → Brittle fracture (thermal softening effect reduces material strength).
Large feed increases cutting thickness, promoting fracture (as utilized in chip breaker design).
Negative rake angle increases compressive stress, suppressing fracture; Positive rake angle intensifies tensile stress.
Dull cutting edges enhance extrusion, easily inducing microcracks in brittle materials.
In shearing operations, the clearance between upper and lower blades (typically 5-10% of material thickness) controls crack meeting position. Improper clearance leads to increased burrs or rough fracture surfaces.
High ductility materials (e.g., aluminum) tend toward ductile fracture, forming fibrous fracture surfaces; Brittle materials (e.g., cast iron) readily exhibit cleavage or intergranular fracture.
High-speed cutting may induce adiabatic shear bands, causing periodic cracks and saw-toothed chips; Low temperature or alternating loads promote brittle fracture.
material type | fracture tendency | Reason |
low carbon steel | niski | High plasticity, easy to form continuous chips |
gray pig iron | wysoki | Graphite sheets weaken the matrix and promote cracking |
titanium alloy | ?redni | The local shear band leads to adiabatic shear fracture |
Chip morphology: Continuous cutting produces ribbon-like chips, while periodic fracture leads to saw-toothed chips.
Surface quality: Incomplete fracture generates burrs, whose height is positively correlated with clearance and material ductility. For example, excessive clearance significantly increases burr height.
Energy consumption: The fracture process requires overcoming material shear strength and plastic deformation energy; optimizing tool angles can reduce energy consumption.
Case 1: Crumbling Control in Cast Iron Cylinder Metal Cutting
Problem: Edge chipping occurs when cutting gray cast iron, and surface roughness exceeds standards.
Solution:
Switch to CBN tools (high hardness reduces compressive stress);
Use small feed rate (f = 0.1 mm/rev) and negative rake angle (?5°).
Case 2: Adiabatic Shear Fracture in Titanium Alloy Aerospace Components
Problem: Localized melting and adhesion of chips to the tool during cutting.
Solution:
High-pressure coolant to suppress temperature rise;
Optimize cutting speed to vc = 50 m/min.
Fracture in metal cutting results from the combined effects of mechanical response and metal cutting parameters. By controlling tool design (e.g., rake angle, clearance), optimizing cutting parameters (e.g., speed, feed rate), and considering material properties (e.g., ductility, fracture toughness), efficient and low-damage material separation can be achieved. Understanding fracture mechanisms is crucial for improving metal cutting quality, reducing burrs, and extending tool life.
]]>When applied correctly, surface treatments can improve both the physical properties and functionality of machined parts. Since different types of CNC machining surface finishes involve distinct procedures and outcomes, understanding the fundamentals of these treatments is essential to determine the best option that meets the requirements of your intended application.
CNC machining processes (including milling and turning) often leave visible cutting marks, which can compromise the surface quality of machined parts. Although CNC machining delivers precision components, these parts frequently require surface finishing for various reasons.
Why Surface Finishing Is Crucial for CNC-Machined Metal Parts:
Surface treatments such as sanding, polishing, electroplating, or painting help conceal sharp edges and machining marks left during CNC processing. As a result, these finishes enhance the visual appeal of CNC-machined parts.
Most CNC-machined materials are susceptible to corrosive substances. To protect the surface of machined components and extend their service life, product designers often employ surface treatments like anodizing, polishing, and passivation.
Manufacturers apply various surface finishes to CNC-machined parts to ensure they are easy to clean and maintain. This is particularly critical in applications where hygiene is paramount, such as food processing equipment and medical devices.
Different CNC surface treatments are used to enhance material properties (e.g., conductivity), reduce friction, and add other desirable characteristics—improving overall functional performance.
By selecting the appropriate surface finish for your machined parts, you can customize them to meet specific preferences and requirements. A variety of finishes can be achieved to deliver desired surface properties, textures, or colors.
Different surface treatments are suitable for various CNC machining materials, each with distinct surface roughness values. However, it is crucial to select the surface finish that best ensures optimal performance, functionality, durability, and visual appeal of the machined parts.
Below are the commonly used surface finishes for metal CNC-machined parts:
Polishing is a classic mechanical finishing process that uses chemical agents or abrasives to create a highly glossy, mirror-like surface on metal parts. This finishing technique enhances the physical properties of machined metal components, improves corrosion resistance, ensures better cleanliness, and reduces friction.
Polishing is particularly suitable for metals such as aluminum, stainless steel, and brass. It is widely adopted by product designers and manufacturers in the food processing, medical, and luxury goods industries due to its functional and aesthetic benefits.
Although polishing can produce a smooth, reflective surface that enhances visual appeal, the process can be time-consuming and labor-intensive. This is especially true for machined parts requiring extremely high finishes or those with complex geometries.
Electroplating is a finishing process that involves depositing a layer of metal coating onto machined parts to increase their thickness. Applying this surface treatment to CNC-machined components protects them from corrosion, impact, high temperatures, and rust, ensuring long-term durability. This process is most suitable for metals such as chromium, cadmium, tin, copper, nickel, and gold. Electroplating enhances adhesion between the substrate and its external coating while also enabling machined parts to acquire magnetic or conductive properties depending on the plated metal.
Unlike other CNC surface treatments, electroplating is not environmentally friendly due to its generation of hazardous waste. Improper handling can lead to significant pollution. Additionally, electroplating is time-consuming and relatively expensive, requiring specialized equipment, metals, and chemicals—especially when multiple layers are needed on metal components.
Passivation protects ferrous materials like steel and stainless steel from corrosion and rust, improving appearance, performance, and cleanliness. This chemical treatment involves immersing machined metal parts in acidic solutions such as nitric or citric acid to remove surface iron, resulting in a smooth, polished finish.
Since passivation is not a coating, it does not require masking or add thickness to the machined part. The acid bath eliminates traces of iron and rust from the surface, forming a protective layer composed of chromium or nickel. While nitric acid is the traditional choice for passivation, citric acid baths have gained widespread acceptance due to their shorter processing times.
Passivated parts exhibit excellent rust resistance, making them ideal for outdoor applications. Moreover, passivation is widely used across industries—from aerospace (requiring high-quality steel and tight tolerances) to medical sectors (where sterilization and longevity are critical).
However, passivation may extend production lead times because machined metal parts must undergo pretreatment, such as cleaning to remove debris, grease, or other contaminants. While immersion is the most common passivation technique (offering faster cycles and better consistency), acid spraying serves as a viable alternative.
Anodizing creates a protective oxide layer on the surface of machined metal parts. This coating shields the metal from corrosion and wear while being compatible with various colors. It is non-conductive and highly durable (Type III). Anodizing is ideal for forming corrosion-resistant coatings on aluminum and titanium components.
To anodize a CNC-machined metal part, it is immersed in a diluted sulfuric acid solution, and an electrical current is applied between the part (anode) and a cathode. This triggers an electrochemical reaction, converting the exposed surface into hard titanium or aluminum oxide. However, critical features like threaded holes—which must remain conductive—should be masked before anodizing.
Anodized parts can be dyed in colors such as gold, red, black, or blue before sealing. The coating’s thickness and density can be adjusted by varying the anodizing time, consistency, and duration. There are three primary anodizing variants, each with distinct processes, coating thicknesses, and properties:
Type I (Chromic Acid Anodizing)
Produces the thinnest layer, preserving part dimensions.
Results in a grayish finish that cannot be dyed.
Type II (Boric-Sulfuric Acid Anodizing)
A safer option with better paint adhesion, allowing for color customization.
Known as “decorative” or standard anodizing, with coatings up to 25 μm thick.
Type III (Hardcoat Sulfuric Acid Anodizing)
The most common type, especially for aluminum and titanium alloys.
Provides the clearest surface, enabling the widest color compatibility.
Coating thickness ranges from 0.001 to 0.004 inches (25–100 μm).
Combined with PTFE/Teflon, it forms a dry lubricated surface.
Alodine or chem film is the brand name for chromate conversion coating. This chemical surface treatment requires immersing machined components in a proprietary chemical solution primarily composed of chromium. When selecting Alodine treatment for metal CNC machined parts, please ensure the process complies with the MIL-DTL-5541F standard. This standard specifies the technical requirements for chemical conversion coatings on aluminum and aluminum alloys in U.S. military specifications.
The Alodine protective coating effectively inhibits corrosion. More importantly, it can be used in conjunction with decorative surface treatments as it significantly improves the adhesion of paints and adhesives. Unlike other surface treatments that reduce the thermal and electrical conductivity of aluminum parts, Alodine actually enhances the electrical conductivity of aluminum components. This surface treatment method is relatively low-cost, but its coating is more prone to scratches and surface damage.
Powder coating is an electrostatic process that applies dry powder to form a thin, uniform protective layer on the surface of CNC-machined parts. This technique is compatible with all metals and enhances the strength, corrosion resistance, and wear resistance of the components.
Unlike anodized metal parts, powder-coated metal parts exhibit superior impact resistance and are available in a wide range of colors. The process can be combined with sandblasting to produce machined parts with smooth, uniform surfaces and exceptional corrosion resistance. The powders used can be either thermosetting or thermoplastic polymers.
Although similar to painting, powder coating involves applying dry powder to the metal part surface and curing it in an oven. For optimal corrosion protection, machined parts may first require a primer treatment, such as chromate conversion or phosphating. The parts are then coated with dry powder using an electrostatic spray gun and cured in an oven at 200°C (392°F). Multiple layers can be applied to achieve the desired coating thickness, typically ranging from 18 μm to 72 μm.
Electroplating is a finishing process that deposits a metallic coating onto machined metal parts to increase their thickness. This surface treatment enhances CNC-machined components by protecting them against corrosion, impact, high temperatures, and rust, significantly extending their service life. The process is most suitable for metals such as chromium, cadmium, tin, copper, nickel, and gold. Electroplating improves adhesion between the substrate and external coatings while also enabling customized properties—magnetic or conductive—depending on the plated metal.
Unlike other CNC surface treatments, electroplating is not environmentally friendly due to its generation of hazardous waste. Improper disposal can lead to severe pollution. Additionally, the process is time-consuming and relatively costly, requiring specialized equipment, metals, and chemicals—especially for multi-layer plating.
Passivation protects ferrous materials (e.g., steel, stainless steel) from corrosion and rust, improving appearance, performance, and cleanliness. This chemical treatment involves immersing machined parts in acidic solutions (nitric or citric acid) to remove surface iron, resulting in a smooth, polished finish.
As passivation is not a coating, it requires no masking and adds no thickness to the part. The acid bath eliminates iron and rust residues, forming a protective chromium/nickel oxide layer. While nitric acid is the traditional choice, citric acid baths are now widely adopted for their shorter cycle times.
Passivated parts excel in rust resistance, making them ideal for outdoor applications. The process is critical across industries—from aerospace (demanding high-grade steel and tight tolerances) to medical (requiring sterilization-compatible surfaces).
However, passivation may extend lead times due to mandatory pre-treatment (e.g., cleaning to remove debris or oils). Immersion remains the most common method for its consistency, though acid spraying offers an efficient alternative for complex geometries.
The electroless nickel plating process involves forming a nickel alloy protective layer on CNC machined parts to enhance their corrosion resistance. It uses a nickel bath and chemical reducing agents (such as sodium hypophosphite) to deposit a nickel alloy coating (typically nickel-phosphorus) on metal components. This process uniformly applies the nickel alloy coating to complex parts with features like holes and grooves.
There are several types of electroless nickel plating, each with different phosphorus contents. These include low-phosphorus, medium-phosphorus, and high-phosphorus nickel.
Parts treated with nickel plating typically exhibit excellent hardness and wear resistance. Additionally, they can be made harder through heat treatment. The electroless nickel plating process is suitable for various metals, including stainless steel, aluminum, and steel.
Despite its significant advantages, this method has certain limitations, including:
Subsequent reduction in plating rate
Accumulation of contaminants in the nickel bath
Increasing phosphorus content
Furthermore, electroless nickel plating is less suitable for rough, uneven, or poorly machined surfaces.
Wniosek
Metal CNC machined parts can undergo any surface treatment to ensure they meet your project requirements. In this article, we have discussed the most common surface treatments for metal CNC parts, each with its unique advantages and disadvantages. We hope this helps you understand how these surface treatments work and their outcomes, enabling you to determine the most suitable surface treatment for your specific application.
]]>Globally, approximately 30,000 to 50,000 metric tons of waste tungsten carbides are generated annually, with China accounting for over 40% of this volume, indicating tremendous recycling potential. Specifically, waste tungsten carbides primarily originate from the following sources:
Residual materials from worn cutting tools, such as lathe tools, milling cutters, and drill bits;
Large tungsten carbide components, including mining drill bits, molds, and rolling mill rolls;
Certain wear-resistant electronic components (e.g., semiconductor packaging materials) that contain tungsten carbides.
Currently, mainstream recycling technologies include mechanical, chemical, and zinc melting processes, each with its own advantages and limitations:
The mechanical crushing method is one of the simplest approaches for recycling waste tungsten carbides. It does not alter the chemical composition of the waste material and does not require separation of tungsten and cobalt. After surface cleaning, the waste tungsten carbide undergoes mechanical crushing and ball milling to produce a mixed powder with a chemical composition nearly identical to the original waste (except for a slight increase in iron content and decrease in carbon content).
For tungsten carbides with low cobalt content (which tend to have relatively lower strength), the material can be manually or mechanically crushed to a certain fineness before being ground in a wet mill to achieve the desired particle size for reuse in tungsten carbide production.
Advantages:
Simple process, short workflow
Low energy consumption
Environmentally friendly (no chemical pollution)
Limitations:
Risk of contamination from metal tool debris during manual crushing
Ineffective for high-cobalt tungsten carbides due to their resistance to crushing
Difficulty in ensuring consistent quality for recycled products made from complex carbide mixtures
Russian researchers have developed an innovative tungsten carbide?recycling process utilizing a simple mechanical crushing approach. This method employs a novel high-power crusher—the conical inertial crusher—enabling high-quality recovery of waste tungsten carbides through crushing and fine grinding alone, without requiring any chemical treatment.
For instance, when processing waste YG6 anvils (used in synthetic diamond production), the waste anvils are first crushed in the conical inertial crusher to produce raw material for tungsten carbide?manufacturing. To enhance the performance of the crushed powder mixture, it is recommended to add 1%–2% cobalt powder, which improves compaction and sintering densification.
Currently, the crushing method continues to evolve, with the adoption of more advanced, cleaner, and efficient crushing equipment for processing waste tungsten carbides.
The mechanism of the zinc melting process for tungsten carbides is based on the formation of?low-melting-point carbides?between zinc and the binder-phase metals (cobalt or nickel) in tungsten carbides at?900°C. At?896°C, the solubility of cobalt in zinc reaches?27%, allowing the binder metal to separate from the tungsten carbide?and form a?zinc-cobalt solid-solution carbide?liquid. This disrupts the tungsten carbide’s structure, leaving behind a loosely bound?hard-phase skeleton.
Since zinc does not chemically react with refractory metal carbides, and given that zinc’s vapor pressure is significantly higher than cobalt’s at specific temperatures, zinc can be?evaporated and recovered (at 925°C)?for reuse. As a result, the carbide powder obtained through the zinc melting process retains most of its original properties. After the process, cobalt or nickel is extracted into the zinc melt, while the carbides remain. The zinc is then distilled off and recycled for subsequent reuse.
Traditional zinc melting furnaces?are?vertical vacuum furnaces. The system operates under conditions ranging from?vacuum to partial-pressure atmospheres, up to just below atmospheric pressure. The components of zinc melting equipment are illustrated in?Figure 2, while the furnace’s main structure is shown in?Figure 3.
The zinc melting process was invented by the British in the 1950s. Subsequently, the United States improved this process and enhanced the equipment. After the 1970s, it became widely adopted in many countries. In China, many manufacturers engaged in recycling waste tungsten carbides have mastered this method. Its main advantages are simple process, short flow, simple equipment, small investment, and low cost, making it particularly suitable for processing waste tungsten carbides with cobalt content below 10% and applicable for small enterprises to reuse waste tungsten carbides for carbide reproduction.
However, this process also has some disadvantages. First, the residual zinc content in the mixed material is relatively high. During the zinc melting and zinc recovery processes, whether the equipment is reasonable or not affects the zinc recovery efficiency. Second, the entire process consumes a large amount of electricity, with power consumption for each ton of tungsten carbide reaching approximately 6,000~12,000 kW·h. Additionally, there are environmental protection issues, as zinc emissions may have certain impacts on operators.
Currently, China’s WC-Co carbides have three tungsten carbide grain structures: coarse, medium, and fine. P-type carbides can be roughly divided into three categories based on titanium content: low-titanium, medium-titanium, and high-titanium. During recycling, it is best to strictly separate them to avoid mixing different sizes of tungsten carbide grains or zinc-melted mixed materials with different titanium contents.
Electrochemical methods mainly include the electrolysis method, as well as the electrolytic electrodeposition method and the electrodialysis electrolysis method developed from the electrolysis method.
Each method offers unique capabilities for metal recovery and purification from tungsten carbide waste streams.
The electrolysis method involves directly placing waste tungsten carbides into an electrolytic cell with acids (hydrochloric acid, sulfuric acid, nitric acid, etc.) as the electrolyte. During electrolysis, the Co in the carbide transforms into Co2? and enters the solution, while the WC, having lost its binder metal cobalt, becomes a porous carbide. The cobalt-containing solution is precipitated with ammonium oxalate, and cobalt powder is obtained after calcination and reduction. The WC can be directly used in tungsten carbide production after ball milling and crushing or appropriate treatment (such as post-crushing carbon supplementation and re-carburization).
The electrolytic electrodeposition method takes advantage of the fact that hydrogen’s deposition potential is more positive than that of cobalt, causing hydrogen gas to preferentially deposit at the cathode. As the Co2? concentration increases and H? decreases, metallic cobalt is simultaneously deposited alongside hydrogen at the cathode. Thus, the electrolytic system becomes an electrolytic refining process where waste carbide serves as the anode, CoCl? as the electrolyte, and pure cobalt is deposited at the cathode.
The electrodialysis electrolysis method introduces a cation-exchange membrane into the electrolytic cell, dividing it into anode and cathode compartments. The cation-exchange membrane, a functional polymer film selectively permeable to ions, allows only cations to pass while blocking anions. Consequently, Co2? migrates through the membrane into the cathode compartment during electrolysis, while OH? accumulates in the cathode compartment due to the membrane’s barrier effect, raising the pH and resulting in Co(OH)? precipitation. Compared to conventional electrolysis, both the electrolytic electrodeposition and electrodialysis electrolysis methods shorten the cobalt recovery process and improve recovery rates.
The high-temperature treatment process is a novel recycling technology for tungsten carbides. This method involves re-sintering tungsten carbides at high temperatures to loosen their structure and promote grain growth. Subsequent mechanical crushing yields high-quality powder suitable for producing coarse-grained tungsten carbides. tungsten carbides manufactured from this powder exhibit performance metrics that meet or exceed those of standard carbide products. The high-temperature treatment process provides a new approach for recycling waste tungsten carbides and producing coarse-grained tungsten carbides.
The high-temperature treatment of tungsten carbides is conducted in specially designed high-temperature furnaces. Under a protective atmosphere at temperatures exceeding 1800°C, the waste carbide undergoes treatment where binder metals like cobalt liquefy and boil, causing carbide deformation and significant volume expansion. The carbide structure transforms into a porous, honeycomb-like formation, making the hardened carbide extremely easy to crush and process. During this high-temperature treatment:
A substantial liquid phase forms in the carbide
Atomic diffusion intensifies→
WC dissolution-precipitation effects strengthen→
WC grains grow rapidly from 1-2μm to several dozen or even hundreds of micrometers→
Defects in WC crystal structures are eliminated during recrystallization→
WC crystal structures become more complete→
Trace metal/non-metal impurities and harmful contaminants are removed
This regenerated mixed material is particularly suitable for producing coarse-grained, high-cobalt-content tungsten carbides. For fine-grained, low-cobalt carbides:
Processing steps:
Initial crushing of treated w?glik
Ball milling to -180 mesh (80μm) for regeneration suitability
The recycled carbide powder is ideal for coarse-grained tungsten carbide production. Test results show:
Advantages:
Limitations:
Currently used by manufacturers in industrialized nations like Japan and Sweden.
Waste tungsten carbide recycling represents not just economic resource reuse but a crucial component of green manufacturing. With advancing technology and policy support, the recycling industry will become more efficient and environmentally friendly, contributing to global sustainable development.
What’s more, industrial enterprises should establish classified recycling systems.Individual users should properly dispose of used tools/drill bits through professional recyclers
“Waste is just resources in the wrong place” – tungsten carbide recycling perfectly embodies this philosophy!
]]>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.
]]>Figure 1 shows the vertical section of the W-Co-C ternary phase diagram along the Co-WC line. Taking a WC-60%Co alloy as an example:
Before liquid phase formation, the solubility of WC in Co increases with temperature.
At the eutectic temperature (~1340°C), a liquid phase with eutectic composition begins to form in the sintered body.
During sintering at 1400°C and subsequent holding, the sintered body consists of a liquid phase and residual WC solid phase.
Upon cooling, WC first precipitates from the liquid phase. Below the eutectic temperature, the WC-based carbides forms a two-phase structure of WC + γ.
Figure 1: Vertical Section of the W-Co-C Ternary Phase Diagram Along the Co-WC Line
In actual production, the composition of sintered bodies often deviates from the vertical section of the Co-WC line. Consequently, the alloy is not simply composed of γ+WC two phases. As shown in Figure 2 , the carbon-rich side of the γ+WC two-phase region borders the γ+WC+C three-phase region and the γ+C two-phase region, while the carbon-deficient side borders the γ+WC+η three-phase region. Only when the carbon content of the sintered body varies strictly within the γ+WC two-phase region can the WC-based carbide avoid the formation of a third phase. Otherwise, it may lead to carbon inclusions or the formation of carbon-deficient η phase.
Since the strength of the alloy is closely related to the structure and composition of the γ phase, while the presence of η phase may degrade toughness, extensive research has been conducted on the γ and η phases, as well as phase transformation processes, in an effort to control the phase composition of WC-Co alloys and improve their overall performance.
As shown in Figure 2, the composition of the γ phase depends on the carbon content of the alloy, while its tungsten content increases with decreasing carbon content. When the alloy’s carbon content lies at the boundary between the γ+WC two-phase region and the γ+WC+η three-phase region, the γ phase exhibits the highest tungsten concentration. Conversely, when free carbon is present and the carbon content aligns precisely with the Co-WC cross-section (i.e., the theoretical carbon content of 6–12 wt.%), the γ phase contains the lowest tungsten concentration.
The tungsten concentration in the γ phase is also influenced by the cooling rate: slower cooling results in lower tungsten content, while rapid cooling leads to higher tungsten retention. This occurs because faster cooling suppresses the diffusion-driven precipitation of tungsten from the γ phase, locking in a non-equilibrium concentration. Additionally, higher sintering temperatures increase the tungsten solubility in the liquid phase, thereby raising the tungsten content in the γ phase at a given cooling rate. However, under sufficiently slow cooling, thermodynamic equilibrium dictates that the γ phase composition becomes independent of the sintering temperature.
In WC-Co cemented carbides, the γ phase is a cobalt-based solid solution of W and C. It exists either as discrete γ grains separated by grain boundaries or as isolated γ domains unevenly distributed within the matrix. Both γ grains and domains typically exhibit equiaxed or near-equiaxed morphologies. Notably, the volume fraction of γ domains increases with higher cobalt content in the WC-based carbide.
The mismatch in thermal expansion coefficients between WC phase (384×10??/°C) and γ phase (1.25×10??/°C) generates microstructural stresses during cooling (tensile in γ phase, compressive in WC phase).
Increased cooling rate or quenching suppresses W diffusion precipitation in γ phase, elevating W concentration in room-temperature γ phase while reducing hcp γ phase content.
Cryogenic treatment (below Ms point) induces W supersaturation in γ phase, enlarging the free energy difference between fcc and hcp γ phases. Concurrently, enhanced internal stresses promote Ms transformation, markedly increasing hcp γ phase fraction—particularly pronounced in low-Co alloys.
In low-Co alloys (e.g., WC-8Co), thin γ phase layers (<0.3 μm) facilitate W diffusion to WC grains, lowering W concentration in γ phase. This raises the Ms point, favoring hcp γ phase formation during cooling and yielding higher room-temperature hcp γ phase content.
Due to the narrow carbon content range in the WC-γ two-phase region (Fig. 2), carbon deficiency in raw materials or sintering decarburization often leads to η phase formation (e.g., M?C-type Co?W?C, Co?W?C, and M??C-type Co?W?C). Among these, Co?W?C is most common.
Heterogeneous nucleation: γ phase nucleates along WC-γ interfaces using WC grain surfaces as nucleation sites, facilitated by slow W diffusion from WC to γ phase and high W concentration at phase boundaries. γ phase tends to fill surface defects (high-energy sites) of WC grains.
Rapid C diffusion in γ phase causes C depletion when WC dissolves, resulting in W/C ratio imbalance (room temperature [W]/[C]≈284).
During sintering (1350-1500°C), excessive C loss leads to W-rich γ phase, precipitating carbon-deficient η phase (intermediate phases like Co?W and Co?W?C form first, transforming to η phase at high temperatures).
η phase growth consumes W and C, driving WC dissolution until equilibrium is reached.
η phase morphology is influenced by γ liquid phase flow (e.g., cross-shaped single crystals).
Key point: Carbon imbalance is the primary cause of η phase formation, with γ phase nucleation dependent on WC interfaces and high-temperature C loss driving η phase precipitation.
Carbon content is critically important for η phase formation. In the WC+γ+η three-phase region:
Higher carbon content maintains W and C concentrations in γ phase closer to equilibrium, hindering η phase nucleation.
Mild carbon deficiency: η phase growth relies on dissolution of WC microcrystals in γ interlayers, resulting in η phases enveloping undissolved WC grains with regular geometries.
Severe carbon deficiency: Significant deviation from equilibrium W/C ratio in γ phase promotes extensive WC dissolution, leading to dispersed particulate η phase distribution.
High-Co alloys contain more γ phase with better fluidity, facilitating W and C diffusion. While η phase nucleation is difficult, growth is easier, forming coarse, clustered grains.
Coarser WC grains promote η phase nucleation but slow growth, resulting in dispersed particulate phases.
Faster cooling reduces dwell time at η phase critical temperature, suppressing η phase formation.
Higher sintering temperatures increase γ liquid phase quantity, favoring coarse η phase grains, but excessive temperatures may keep γ liquid away from η phase boundaries, inhibiting η phase growth.
A comprehensive understanding of the phase transformation processes during the sintering of WC-based carbides is crucial for optimizing production processes, controlling phase composition and microstructure in the alloys, thereby creating favorable conditions for manufacturing high-performance WC cemented carbides.
]]>The grain growth inhibitors primarily influence WC grain growth through the following approaches:
Principle:grain growth Inhibitor elements (e.g., V, Cr) dissolve into the WC or Co phase, adsorb at WC/Co phase boundaries or WC/WC grain boundaries, hindering atomic diffusion and grain boundary migration.
Inhibitors such as VC and Cr?C? decompose during sintering, with V and Cr atoms dissolving into the WC lattice or Co binder phase.
Example: V substitutes W sites in WC (forming (V,W)C solid solution), while Cr dissolves into the Co phase (forming (Co,Cr) solid solution).
Solute atoms (e.g., V, Cr) enrich at WC grain boundaries or WC/Co interfaces, forming a “solute atmosphere.”
These segregated atoms pin grain boundaries, increasing the energy barrier for migration.
When grain boundaries attempt to migrate, solute atoms must move along, but their slower diffusion rate impedes boundary motion.
Analogous to “viscous drag,” this suppresses WC grain coalescence and growth.
Applicable grain growth Inhibitors: VC, Cr?C? (primarily rely on solute drag).
Principle: grain growth inhibitors form nanoscale carbide particles (e.g., (V,W)C, (Cr,W)C) that physically obstruct WC grain growth at boundaries.
During sintering, decomposed VC or Cr?C? reprecipitate as nanoscale carbides (e.g., 5–50 nm (V,W)C particles), typically located at WC/WC or WC/Co interfaces.
Migrating boundaries must overcome the restraint of these nanoparticles, requiring additional energy.
According to the Zener equation, pinning force (F?) correlates with particle volume fraction (f) and size (r). Finer, denser particles yield stronger inhibition.
Nanoparticles hinder WC dissolution in liquid Co and redeposition, reducing Ostwald ripening (“large grains consuming small ones”).
Applicable grain growth Inhibitors: VC (strongest pinning), Cr?C? (moderate), TaC/NbC (weaker).
Mechanism | Primary Inhibitors | Key Characteristics |
Solute Drag | VC, Cr?C? | Hinders grain boundary migration through solute atom segregation |
Second-Phase Pinning | VC, Cr?C? | Physically blocks grain boundaries via nanoparticle dispersion (Zener pinning) |
Dissolution-Reprecipitation Control | VC, Cr?C? | Reduces WC dissolution in Co binder and slows atomic diffusion |
Grain Boundary Energy Modification | TaC, NbC | Lowers grain boundary energy, enhancing high-temperature stability |
VC > Cr?C? > TaC ≈ NbC
Sintering Temperature and Time:
High temperatures or prolonged sintering may weaken inhibitor effectiveness (e.g., VC particle coarsening).
Alloys with higher Co require greater grain growth inhibitor content (due to enhanced WC dissolution in liquid Co).
Inhibitors may consume free carbon, necessitating carbon potential adjustment to avoid η-phase formation (e.g., Co?W?C).
Grain growth inhibitors (e.g., VC, Cr?C?, TaC) are widely used in the cemented carbide industry, primarily in cutting tools, mining tools, and wear-resistant components. The selection of different inhibitors directly affects the alloy’s hardness, toughness, wear resistance, and high-temperature stability. Below is an in-depth analysis of several typical application cases.
Requirement: High-speed cutting and precision machining (e.g., automotive engine blocks, aerospace titanium alloys) demand tools with both high hardness (>90 HRA) and chipping resistance.
Conventional WC-Co alloys have coarse grains (1–3 μm), exhibiting high hardness but low toughness, leading to edge chipping.
Ultra-fine grain cemented carbide (grain size 0.2–0.5 μm) achieved through VC (0.3–0.5 wt%) + Cr?C? (0.5–1.0 wt%) composite addition.
VC: Nano-sized (V,W)C particles pin WC grain boundaries (Zener pinning), suppressing grain coalescence.
Cr?C?: Cr dissolves into the Co phase, reducing WC dissolution rate (solute drag) while enhancing oxidation resistance.
Sandvik GC4325: For titanium alloy machining, using VC+Cr?C? inhibition (0.3 μm grains).
Kennametal KCS10B: For stainless steel finishing, incorporating nano-VC.
Requirement: Oil drill bits and tunnel boring machine cutters operate under high temperatures (>800°C) and impact loads, requiring thermal fatigue resistance and wear resistance.
Conventional WC-Co alloys experience rapid grain growth at high temperatures, reducing strength.
TaC (1–3 wt%) or NbC (1–2 wt%) addition to leverage their high-temperature stability for grain growth suppression.
TaC/NbC: Form (Ta,W)C or (Nb,W)C solid solutions at high temperatures, pinning grain boundaries (Zener effect) and reducing boundary mobility.
Synergy with Co binder: Ta/Nb dissolution into Co increases liquid Co viscosity, slowing WC dissolution-reprecipitation.
Atlas Copco Button Bits: TaC-containing drill bits for granite drilling.
Sumitomo Electric DX Series: Oil drilling alloys with NbC for thermal stability.
Requirement: Mechanical seals and bearing sleeves require high wear resistance + corrosion resistance (e.g., chemical pumps, seawater environments).
WC-Co suffers from selective corrosion of the Co phase in corrosive media, causing WC grain detachment.
Cr?C? (1.0–1.5 wt%) + rare earth oxides (Y?O? 0.1–0.3 wt%) composite addition.
Cr?C?: Forms (Cr,W)C particles to refine grains while improving corrosion resistance via Cr dissolution in Co.
Y?O?: Rare earth elements segregate at grain boundaries, purifying interfaces and strengthening boundary cohesion.
Mitsubishi Materials EX Series: Chemical pump seals with Cr?C? + rare earth modification.
Oerlikon Durit CR: Corrosion-resistant alloys with Cr?C?.
Requirement: PCB micro-drills (diameter 0.1–0.3 mm) demand ultra-high precision (roundness <1 μm) and fatigue resistance.
Grain coarsening causes drill edge blunting and fracture during drilling.
Ultra-fine VC (0.2–0.4 wt%) + low-temperature sintering (1350°C, vs. conventional 1450°C).
Nano-VC: Prepared via high-energy ball milling (<50 nm particles) for enhanced pinning.
Low-temperature sintering: Reduces Ostwald ripening time, preserving inhibitor efficacy.
Toshiba Tungaloy DLC-Coated Micro-Drills: Nano-VC inhibition technology.
TaeguTec PCB Drill: Optimized for high-layer PCBs.
Grain growth inhibitors in cemented carbides control grain size through solute drag and second-phase pinning mechanisms. Their selection must be optimized based on material composition, sintering processes, and performance requirements. Future trends favor nano-composite inhibitors and multi-component synergistic regulation to further enhance comprehensive material properties.
]]>The core task of oil drilling is to penetrate complex formations, including hard rock layers such as sandstone, shale, and even granite. During this process, friction between the drill bit and rock generates significant heat, while abrasive particles like quartz sand and metal debris in the formation accelerate surface wear on equipment.
Oil drilling operations can reach depths of several thousand meters, where downhole temperatures may exceed 200°C and pressures can surpass 100 MPa. Conventional steel is prone to thermal expansion deformation or oxidation embrittlement under such conditions. Valve seals may soften and fail under high temperatures, leading to drilling fluid leaks and causing substantial economic losses. Additionally, frequent thermal cycling (e.g., in Arctic operations) can induce material fatigue cracking, jeopardizing equipment safety.
The direct consequences of equipment wear are increased maintenance costs and extended downtime. According to API standards (API Spec 7-1), traditional PDC drill bits achieve an average footage of only about 380–520 meters in formations with >40% quartz content, while each replacement operation takes 8–12 hours, severely hindering extraction progress. Moreover, component failures can trigger blowouts, oil spills, and other safety incidents, further amplifying.
Cemented carbide is a composite material with tungsten carbide (WC) as the matrix and cobalt (Co) as the binder phase. Its performance advantages stem from its unique microstructure:
Tungsten carbide boasts a Vickers hardness of 1,600–2,400 HV, second only to diamond, enabling effective resistance to rock cutting and abrasive wear.
Tungsten carbide has an extremely high melting point (2,870°C) and maintains high strength even at elevated temperatures. The ductility provided by the cobalt binder phase further enhances the material’s impact resistance.
Cemented carbide exhibits strong resistance to acidic media (pH 2–12) and salt spray environments.
Performance Metric | Traditional Material (e.g., Steel) | Cemented Carbide | Improvement Effect |
Hardness (HRC) | 50–55 | 60–90+ | — |
Odporno?? na zu?ycie | — | — | 2–5x improvement |
Corrosion Resistance | Susceptible to acidic corrosion | Acid/alkali/oxidation resistant | 3x+ lifespan extension |
Compressive Strength (MPa) | 800–1,200 | 3,000–6,000 | — |
Deformation Resistance | — | — | 2–3x improvement |
High-Temperature Stability | ≤300°C | ≤800°C | Suitable for deep wells & high-temperature oil/gas environments |
Cemented carbide bearings are widely used in extreme-condition equipment within the petroleum industry. Their tungsten carbide-cobalt composite structure (HRA 85-93) combines high hardness with impact resistance. These bearings are primarily employed in critical components such as rotary steerable systems, mud pump plungers, and downhole motors. They can withstand temperatures exceeding 200°C and pressures up to 100 MPa in drilling fluids containing abrasive particles, offering a service life 3-5 times longer than traditional steel bearings.
Through gradient structure design, these bearings achieve an optimal balance between surface wear resistance and core toughness, significantly reducing unplanned tripping frequency for downhole tools. This enhancement ensures both operational safety and cost-effectiveness in ultra-deep well drilling.
Cemented carbide bushings are extensively utilized in high-wear components of petroleum equipment such as downhole drilling tools, mud pumps, and valves. Composed of tungsten carbide or chromium carbide matrix (HRA 88-92) and densified through hot isostatic pressing (HIP) technology, these bushings demonstrate exceptional wear and corrosion resistance against sand-laden, saline drilling fluid erosion while withstanding temperatures of 150-300°C and acidic environments.
The surface-gradient alloying design enhances galling resistance while maintaining core toughness, extending bushing service life by 2-4 times in directional drilling tools. This innovation effectively reduces stuck pipe risks and minimizes maintenance downtime, ensuring continuous operation under complex deep-well conditions.
In petroleum extraction, the valve balls and seats of oil well pumps serve as critical sealing elements. Conventional materials are prone to failure due to wear, corrosion, or high-pressure impact, necessitating frequent shutdowns for replacement.
Cemented carbide valve seats (e.g., YG series) overcome these limitations with:
1.Superior hardness (HRC 90+), delivering 3× greater wear resistance
2.Extended service life (2-3× longer than standard materials) when paired with carbide valve cores
3.Significant reduction in downtime-related costs
This engineered solution ensures reliable performance in demanding pumping applications while optimizing operational efficiency.
Hardened carbide nozzles for high-pressure abrasive jet technology significantly enhance formation cutting efficiency, making them ideal for deep reservoir extraction with wear resistance far exceeding conventional materials.
The innovative spiral-flow-channel nozzles feature gradient structure design with:
1.Surface WC content up to 94wt% for extreme wear resistance
2.Core cobalt content of 8-10wt% for optimal toughness
This balanced composition achieves both superior surface durability and bulk material integrity.
1.The advanced fluid dynamics optimization:
2.Increases drilling fluid velocity by 30%
3.Effectively removes downhole cuttings
4.Maintains stable performance in extreme downhole conditions
Cemented carbide centralizers are used for casing cementing. The spiral rib design improves displacement efficiency, making them suitable for deviated and horizontal wells, with strong impact resistance and low friction coefficient.
The centralizers support the casing through rigid or elastic structures, reducing eccentricity caused by wall friction, significantly improving casing centralization—especially in deviated and horizontal wells. For example, the spiral rib design reduces casing running resistance through its streamlined structure and uses rotational action to condition the wellbore, ensuring gauge protection.
The development of ultra-fine grain cemented carbide (grain size <0.5μm) and novel binder phases (such as nickel-based alloys) will elevate material performance to new heights. Furthermore, the application of intelligent monitoring systems (e.g., embedded wear sensors) enables real-time prediction of component lifespan, driving the petroleum industry toward its goal of “zero unplanned downtime.” Cemented carbide wear-resistant components are not merely vessels of technology, but cornerstones for the sustainable development of the petroleum industry.
From penetrating ten-thousand-meter rock formations to resisting deep-sea corrosion, cemented carbide wear-resistant components have written a revolutionary chapter in the petroleum industry with their unique combination of “strength and resilience.” They are not only powerful tools for extending equipment lifespan but also critical enablers for reducing carbon emissions and achieving green extraction. Looking ahead, with growing global energy demands and technological advancements, cemented carbide is destined to shine even brighter in the petroleum sector.
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In the powder metallurgy of cemented carbides, binders (also called forming agents) play critical roles, including:
Reduces interparticle friction, enabling homogeneous mold filling and uniform compaction.
Prevents powder segregation (e.g., separation of WC and Co).
Provides sufficient “green strength” to prevent cracking or edge chipping during handling or demolding.
Minimizes elastic aftereffects (post-compaction expansion).
Reduces friction between powder and die walls, lowering compaction pressure and extending mold life.
Improves surface finish and minimizes defects (e.g., delamination, cracks).
Must be fully removable (via thermal decomposition or dissolution) before sintering to avoid carbon residue or impurities that degrade alloy properties.
Uniformly mixes with WC-Co powders without agglomeration or sedimentation.
Chemically inert to powders (e.g., no oxidation of cobalt).
Melting point must align with compaction temperatures (typically room temperature to 100°C) to ensure:
Liquid-phase homogeneity during mixing.
Solid-phase strength during pressing.
Too high moderate viscosity leads to impedes powder flow.
Too low moderate viscosity leads to insufficient binding force.
Binding capacity: Ensures green strength (flexural strength typically ≥5 MPa).
Lubricity: Reduces compaction pressure (e.g., from 600 MPa to 400 MPa).
Broad debinding temperature range (e.g., 150–500°C) to prevent cracking from rapid volatilization.
Low carbon residue after debinding (<0.1%) to avoid disrupting alloy carbon balance.
Non-toxic, low volatility (e.g., water-soluble PEG outperforms solvent-based rubber binders).
Meets industrial emission standards (e.g., sulfur- and chlorine-free).
Low-cost and readily available (e.g., paraffin wax is more economical than rubber).
Recyclable or easy to dispose of (e.g., PEG can be water-washed and recovered).
When manufacturing cemented carbide products, selecting the right binder is crucial for quality and efficiency. Here’s a detailed comparison of the three most common binder types to help you make the best choice for your application.
Characteristics:Composition: Hydrocarbon-based, solid at room temperature with low melting point (50-70°C)
Best for: Small, simple-shaped carbide products
Advantages:
Excellent lubricity reduces die friction
Low debinding temperature (200-400°C) simplifies processing
Cost-effective and readily available
Limitations:
Lower green strength (prone to cracking)
Potential carbon residue during high-temperature debinding
Temperature-sensitive – requires dry storage
Pro Tip: Ideal for mass production of standard inserts where cost is key.
Characteristics:Composition: Water-soluble polymer with adjustable molecular weight (PEG-2000/4000)
Best for: Complex-shaped tools and precision molds
Advantages:
Higher green strength for intricate shapes
Water-soluble – enables aqueous pre-debinding
Minimal carbon residue
Limitations:
Hygroscopic – requires humidity control
Narrow debinding window (200-300°C)
More expensive than paraffin
Pro Tip: The go-to choice for premium cutting tools requiring precision.
Characteristics:Composition: Polymer elastomer requiring organic solvents (e.g., acetone)
Best for: Large, high-density components like rolls and mining tools
Advantages:
Highest green strength
Excellent elasticity prevents cracking
Limitations:
Challenging debinding (500°C+)
Potential sulfur contamination
Environmental concerns with solvents
Highest cost
Pro Tip: Reserved for specialized applications where extreme strength is critical.
Recommended Medium: Ethanol + 10-20% acetone (enhances solubility)
Recommended Medium: Deionized water + 0.5% antioxidant (e.g., oxalic acid)
Recommended Medium: Pure acetone (requires sealed system to prevent evaporation)
Rubber binders provide the highest strength due to their polymer chain structure, making them suitable for large compacts. PEG offers moderate strength ideal for complex geometries, while paraffin wax has the lowest binding strength as it relies solely on physical bonding.
Paraffin wax can be removed at relatively low temperatures between 200 to 400°C, though carbon balance must be carefully controlled. PEG requires aqueous pre-debinding followed by thermal cycling, but is sensitive to moisture. Rubber binders demand high-temperature pyrolysis above 500°C and carry risks of sulfur contamination.
Paraffin may leave carbon residues that affect the WC/Co ratio, requiring adjustment of carbon potential during sintering. PEG leaves virtually no residue, making it excellent for high-purity alloys. Rubber can leave sulfur residues that reduce the alloy’s corrosion resistance.
Paraffin wax has the lowest initial cost but may incur additional expenses for carbon management. PEG provides the best value for precision components and mass production. Rubber is the most expensive option and is only justified for specialized heavy-duty applications.
For cost-sensitive production where simple processes are preferred, paraffin wax is suitable but requires careful control of dimensional stability during debinding. When high precision and environmental considerations are priorities, PEG is the optimal choice though it needs humidity-controlled storage. Rubber binders are reserved for applications requiring maximum strength and large components, provided that high-temperature debinding equipment is available.
Modern developments are creating hybrid binder systems that combine the advantages of these materials, such as PEG’s performance with paraffin’s cost benefits through advanced formulation techniques.
]]>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.
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