1. Introduction
Injection moulds are used in the manufacturing process of a wide variety of products, and these can be made from different materials with unique properties for given applications. Injection moulding requires a substantial amount of material to fabricate them, resulting in expensive mould costs and the installation of supplementary equipment. It is a vital process in polymer processing [1] that produces rework-free moulded parts from raw materials. The high flexibility associated with injection moulding elevates the process across various industries [2]. Quality criteria such as dimensional accuracy, surface impression, and the minimum achievable cycle time are essential considerations [3,4]. Numerous examples of injection mould products include short-glass-fibre composites, thermoplastic and thermosetting polymers, and standard plastic [5]. The high-pressure injection moulding (HPIM) industry is rapidly expanding due to the extensive use of these products. Fe alloys are more commonly used to produce injection moulds since mechanical strength, corrosion resistance, hardness, wear resistance, and fatigue resistance are guaranteed at lower costs [6,7,8]. The present review will focus on three primary alloys used in HPIM. CuBe or AMPCO® alloys are popular for plastic injection moulds due to their excellent thermal conductivity (k), allowing for fast and efficient mould cooling. Additionally, this alloy is highly resistant to corrosion and wear, making it an ideal material for high-T and high-pressure moulding applications; Fe-Ni36 or INVAR-36® is commonly used in injection moulds. These materials are known for their low thermal expansion coefficient (α), meaning they maintain their dimensional stability even when exposed to T changes, and heat-treated (HT) steels are ideal for high-volume moulding applications where durability is critical [9,10].
1.1. Copper–Beryllium Alloys (AMPCO®)
The incorporation of Cu [11,12] in the HPIM process, especially in Polymer Injection Moulding (PIM), enhances (1) elevated k, (2) corrosion and wear resistance, (3) dimensional stability, (4) electrical resistivity (ρR), and (5) substantial mechanical strength [13]. Cu alloys are extensively utilized across diverse industries due to their exceptional properties. Nonetheless, the surface quality of these materials holds paramount importance in ensuring optimal performance in moulds. Consequently, various cleaning processes enhance surface quality, including mechanical, chemical, chemical–mechanical, and electrochemical polishing [14]. During manufacturing, lubricating oils, drawing compounds, dirt, oxides, and metallic particles can accumulate, and these impurities must be eliminated to ensure quality. Chemical and chemical–mechanical polishing methods can yield finishes closely resembling those achieved through electropolishing, a technique known for creating smoother and brighter surfaces.
Moreover, electropolishing offers a more straightforward process that can effectively be applied to larger surface areas [15,16]. On the contrary, Be [17] is acknowledged for its inherent hardness and granular state, requiring powder metallurgy technology. Additionally, Be and its compounds are toxic, which can incur high costs and complexity in manufacturing and repair/service [18,19,20,21]. This inherent characteristic poses challenges in attaining polished and flawless surfaces due to the abrasive nature of the hard particles, thereby exacerbating tool wear during the machining of an injection moulding insert of a Cu-Be [22] alloy by amplifying the costs and intricacy associated with manufacturing and repair/service procedures [19]. Figure 1 depicts a binary phase diagram of CuBe alloys.
CuBe alloys, such as those found in AMPCO® alloys, are often employed for PIM [24]. Zhong et al. [25] compared a rapidly solidified Al alloy, CuBe C17200 alloy, according to the ASTM B 194-15 [26] standard, and Al-6061 alloy regarding their wear rates, hardness, and suitability as materials for mould inserts. Among the materials examined for mould inserts, the CuBe alloy exhibited the highest hardness and the lowest wear rate, whereas the Al-6061 alloy was the worst material. Cu alloying with Be enhances its mechanical properties while significantly decreasing k [27,28]. AMPCO® variants’ incorporation into PIM tools can enhance the efficiency and quality of the moulding process [29]. It merges the characteristics of Cu [11,12] and Be [17] to create a sturdy alloy with improved resistance to wear due to high hardness and excellent seizing and galling resistance. These characteristics make this alloy an excellent option for bearing and bushing applications [30,31] and from aerospace to automotive and nuclear sectors, as presented in Table 1 [32].
As a result, several investigations have been carried out into processing these alloys for injection moulding applications, focusing on the electrical discharge machining of Cu-based alloys. This method has proven highly effective in producing mould cavities. High-reliability engineered materials, specifically CuBe alloys, have gained widespread utilization in numerous engineering domains. Due to the high hardness of Be particles and T fatigue strength, machining challenges, such as tool wear (TW), built-up edge (BUE), where material adhesion to tool surfaces can cause rapid tool deterioration [14,34], and the micro-tearing of the grain lattice may arise, when creating smooth surfaces on AMPCO® alloys using CM methods [35,36]. Research has focused on overcoming these challenges, including electrical discharge machining (EDM) [37] and diamond-like-coated tools. Table 2 presents some AMPCO® alloys’ chemical compositions, which can differ from the contents established by the ASTM B 194-15 [26] standard since it is heavily commercial branded material. Enterprises tend to compete with their counterparts who have specific know-how, thus adding more wt% of certain elements to enhance performance. Table 3 presents some critical physical, mechanical, and thermodynamical properties of AMPCO® and CuBe C17200 alloys.
1.2. Iron–Nickel (INVAR-36®)
INVAR-36® is a ferromagnetic Ni alloy classified in the Fe-Ni [40] and Fe-based superalloy series. Shallow α values characterize it over a wide range of T of 20 < T < 200 °C [41], known as INVAR behaviour. Ruled by the ASTM F 1684-06 (2016) [42] standard, this alloy has emerged as a crucial material in advancing science and technology, particularly for precision measurements [43,44]. Due to the unique properties of Fe-Ni alloys with a Face-Centred Cubic (FCC) structure and a Ni concentration of approximately wt% = 36% (Figure 2), these materials exhibit the most excellent INVAR behaviour [44,45], excellent for dimensional stability applications such as (1) the Aerospace industry, (2) Appliance and heater thermostats, (3) Automotive control devices, (4) Bimetals for circuit breakers, (5) Composite layup moulds, (6) Gauge tubes, (7) Heating and air conditioning, (8) Metrology devices, (9) Motor controls, (10) Optical mounting and components, (11) Orbiting satellites, (12) Precision measuring instruments/tools, (13) Ring laser gyroscopes, (14) Shadow masks to produce Organic Light-Emitting Diodes (OLEDs), and (15) Time-keeping devices.
However, its low hardness limits its use in tribological applications, such as manufacturing bulky composite tooling for the aerospace [46] and automotive industries. The production of structural components from Fe-Ni alloys maintains its popularity due to their excellent resistance to chemical and environmental corrosion [47,48], fatigue resistance, mechanical properties in low T environments, reasonable ductility, and toughness. The hot ductility of the base metal Fe-Ni36 can be improved by increasing the strain rate (), in the range of 0.001 < < 1 Hz or by the influence of dynamic recrystallization at high T [49,50]. Table 4 and Table 5 present some important physical, mechanical, and thermodynamical properties of INVAR-36® and the typical chemical composition according to some authors, respectively.
High-quality nanometric finish surfacing is one of the significant challenges when machining INVAR-36® since it has low hardness and high chemical activity [44,57]. Hauschwitz et al. [58] suggest that optimizing the rolling torque, polishing speed, and reducing the polishing depth can improve the process’s efficiency and quality while lowering subsurface damage [59,60]. Moreover, some authors have been overcoming these issues thanks to the brisk development of the selective laser melting (SLM) process [61,62,63] allied to a post-machining process.
1.3. HT Steels
HT steels are designed to improve hardness, toughness, and wear resistance through controlled heating and cooling, which is ideal for PIM purposes because they can maintain shape and structural integrity [64,65]. Suitable steels for this purpose, namely AISI H11 (DIN 1.2343), AISI H13 (DIN 1.2344), and AISI L6 (DIN 1.2714) [66], will be addressed in this paper. AISI H11 (DIN 1.2343) in tooling applications [67] for PIM is especially advantageous as it is a vital material for producing tools and dies. It is classified as air-hardening, high Cr, and premium C-steel and is sturdy and abrasive in wear [68]. AISI H13 (DIN 1.2344) is a highly sought-after hot work tool steel with remarkable strength at high T. This alloy also has excellent resistance to abrasion at low and high T, a high level of toughness, a high level of machinability and polishability, and optimal resistance to thermal fatigue [69]. Typically, H13 is utilized in a quenched and tempered state, featuring a microstructure comprising a lath martensitic matrix and secondary-hardening carbide precipitates. This situation brings up challenges when machining, as shown by Figure 3.
In order to enhance machinability, authors have concluded that the microstructure of H13 produced via AM significantly differs from that of its conventional counterparts. The material’s k was improved by heat treatment; however, its value depends on the specific parameters of the selective laser melting and post heat treatment process [70,71]. AISI L6 [72] die steel is prominently featured in hot forging manufacturing processes [73], having enhanced properties compared to the H11 and H13 [72] steels. This alloy can also be found in extrusion dies, bolts, casting inserts, forging dies, drop forges, embossing dies, pressure pads, and dies [74]. Table 6 presents the physical, mechanical, and thermodynamical properties of the different HT steels that will be addressed in this work.
Figure 4 illustrates a Typical Time–Temperature-Transformation (TTT) diagram for AISI H11 (DIN 1.2343) steel. Table 7 has some chemical compositions of the AISI H11 (DIN 1.2343), AISI H13 (DIN 1.2344), and AISI L6 (DIN 1.2714) steels, according to the literature, and Table 8 completes the information by presenting each element’s contribution.
While some chemical elements enhance the final product, others may induce disadvantages. Table 9 summarizes numerous pros and cons of some of the addressed elements from Table 8.
The noteworthy study by Twardowski et al. [87] pertains to the analysis of diverse factors impacting Surface Roughness (SR) after the end milling of hardened steel under High-Speed Milling (HSM) circumstances. It encompasses investigations into milling parameters such as the cutting speed (Vc) and axial depth of cut (ap, or ADOC), along with exploring process dynamics influencing the SR of machined surfaces. Additionally, an SR model incorporating cutter displacements was developed. The research also examined surface profile charts, focusing on vibrations, and cutting force (Fcut) components. The investigation revealed that actual SR parameters exhibit values 16 to 25× greater than the theoretical values derived from the kinematic–geometric projection of the cutter onto the workpiece. As the theoretical model postulates, the primary determinant of the surface micro-irregularity height and configuration is the feed rate (f) rather than the feed-per-tooth (fz). This deviation is ascribed to the milling process dynamics, which are intricately linked to the spindle speed (s) frequency. Ensuring the surface quality of injection moulding materials is paramount for achieving optimal performance. Conventional Manufacturing (CM) remains the predominant method for fabricating injection moulds among the three materials addressed. Since they are older and more established machining processes, milling, turning, drilling, and many more are widely employed for shaping and finishing moulds.
Nonetheless, Non-Conventional Machining (NCM), like EDM, can be applied to injection mould manufacturing and enhance the machinability of HPIM. The inquiry originates from its paramount significance within the injection moulding industry, regarding the most common and used materials’ machinability. This paper also does not intend to give a broad vision on HPIM to every academic and practitioner but to deliver a structured review able to contribute to fast knowledge acquisition in the field of HPIM, rendering research in this field invaluable for industry optimization. Following the presentation of the theoretical framework in Section 1, Section 2 delineates the methodology employed in this study, which is based on the Systematic Literature Review (SLR) approach [88] aimed at identifying pertinent papers. In Section 3, these identified papers undergo analysis to present the newer prospects within the research fields of CM and non-traditional machining methods applied to AMPCO®, INVAR-36®, and HT steels, all injection mould materials. Section 4 discusses findings derived from content analysis, providing an overview of emerging research areas and challenges when machining these types of materials. Section 5 succinctly summarizes the findings and offers a brief outlook.
2. Materials and Methods
The conceptual map (Figure 5) depicts the methodology for conducting research and gathering information and provides an easily understandable visual representation of all the steps involved in creating this review.
The research and information-compiling phases were carried out through SLR since it is based on a systematic, method-driven, and replicable approach [89,90]. The platform used for SLR was Dimensions.ai, which is connected to all data from Scopus. The method employed for research and data compilation was assessed for quality by considering factors such as citation score and journal impact, and it was systematized. The information sources utilized for this review included ScienceDirect, Springer, MDPI, and ResearchGate platforms, all renowned for their reliability and expertise. To collect data on these subjects, relevant keywords and their combinations were employed, for example, manufacturing processes, machining, conventional, non-conventional, injection moulds, INVAR-36®, Fe-Ni36, CuBe, and HT steels. While collecting articles, all critical information was systematized in a table, including processes, names, sources, respective journals, and an indication that it had been used.
3. Literature Review
3.1. Conventional Manufacturing (CM)
This section addresses CM processes that allow for the removal of considerable material from the workpiece. The upcoming literature review will focus on the milling, turning, drilling, and boring processes applied to AMPCO®, INVAR-36®, and HT steels.
3.1.1. Milling
Milling is a crucial manufacturing process that has evolved significantly in recent years [91]. Milling tools come in various forms, including coated and/or uncoated. Coated tools improve the overall process productivity by enhancing the tool life (TL) and production quality of machined components [92]. Nonetheless, for specific applications, uncoated tools have the upper hand, as seen in Lakner et al.’s [93] work, where the cutting performance of uncoated milling tools was superior, producing the highest quality hole surface, the lowest Fcut values, and experiencing the least amount of TW [94,95]. Delamination damage is still a challenge when machining with coated tools. Four techniques were devised by Zou et al. [18] during the helical milling of CFRP/Ti-6Al-4V stacks with coated tools. Based on experimental data, it was discovered that the extent of delamination damage is linked to the axial cutting load and can be curtailed by altering the sequence of the stacks [96]. It is important to note that a milling process with a high f can result in surface deterioration caused by the phenomenon known as built-up edge (BUE) [19]. Table 10 addresses some of the most recent state-of-the-art works regarding milling AMPCO®, INVAR-36®, and HT steels.
Figure 6 and Figure 7 from Nogueira et al.’s [34] and Sousa et al.’s [14] works, respectively, depict the associated wear mechanisms in the tools used when milling AMPCO®.
3.1.2. Turning
Turning is a machining technique that has become increasingly popular in industrial manufacturing. The process presents challenges, such as the TW and tear of the coated inserts over time, affecting the surface and subsurface properties of the workpiece [114,115]. The tool–workpiece interaction is a critical aspect to consider in hard turning [116,117]. While hard turning offers benefits in terms of productivity, it is essential to consider the resulting properties of the workpiece: SR, dimensional and geometric tolerances, residual stress, surface and bulk hardness, and the microstructure of the surface layers. According to Meyer et al. [118], the effective contact dimensions at the primary cutting edge are essential to characterize the complex turning process. Adjustments in finishing, nominal process parameters, ap, and f are imperative to obtain the best results [118,119,120].
Although orthogonal cutting is not the most used process when manufacturing injection moulds, it is intended to provide in Table 11 some of the most recent state-of-the-art works regarding the challenges other researchers felt, which can be extrapolated to milling situations.
3.1.3. Drilling
Drilling is crucial in manufacturing and assembling parts used in various industries, including PIM [128]. Reduced hole quality and degraded drills due to the significant Fcut and Tcut during the process are still great challenges due to the tear of drill bits. According to Ortner and Kromoser [129], the effect of the drill diameter on Fcut is not significant at a low Vc, but for a higher f, an apparent increase in the influence can be observed [129,130]. Newer technologies like Ultrasonic Vibration Drilling (UVD) offer high efficiency, good stratum adaptability, and a fast drilling speed. Ma et al. [131] investigated four different types of drilling in a Ti6Al4V alloy: Direct Drilling (DD), Peck Drilling (PD), UVD, and Ultrasonic Vibration Peck Drilling (UVPD). UVD could still obtain a smaller axial force (Fa) than DD, and Fa continued to decline with the increased vibration amplitude. When the amplitude was increased from 0 to 5.5 μm, the mean thrust force decreased by 41.8 N, about 18.6%. The major drawback is that mathematical models and Finite Element Analysis (FEA) are needed to study the longitudinal vibration characteristics of the drill when machining in overburden layers. Based on the mechanical vibration theory, a model considering the stratum coupling boundary and vibration head is paramount to be established, according to Li et al. [132]. Table 12 addresses two state-of-the-art works regarding drilling INVAR-36® and HT steels. It is noteworthy that there is a gap in the literature around HT steels’ drilling and the most about AMPCO® is conducted by Electro-Discharge Drilling (EDD).
3.1.4. Surface Polishing
Traditional methods like lapping, polishing, and honing are prevalent in the industry, yet they present limitations such as subsurface damage, residual stress, and challenges in finishing complex and free-form surfaces. However, various advanced finishing techniques have been explored in pursuit of attaining damage-free, nano-level, or angstrom-level surface finishes on challenging materials. These include Abrasive Flow Finishing (AFF), Chemical Mechanical Polishing (CMP), Elastic Emission Machining (EEM), Magnetic Abrasive Finishing (MAF), Magnetorheological Finishing (MRF), and Plasma-Assisted Polishing (PAP) [135]. Electrolytic polishing is exclusively viable for metals. It is influenced by the preceding mechanical background of the surface, shedding light on the mechanisms involved in the mechanical abrasion processes [136]. Table 13 addresses some of the most recent state-of-the-art works regarding surface polishing AMPCO®, INVAR-36®, and HT steels.
3.2. Non-Conventional Manufacturing (NCM)
3.2.1. Electrical Discharge Machining (EDM)
EDM is an unconventional machining process that uses the induced thermal energy leading to material ablation. Electrical discharges remove material from a wrought stock that develops high-energy plasma at T between 8000 °C and 20,000 °C, melting material and vaporizing cavities from an electrode [141]. The main advantage of this NCM process is the ability to machine materials with high hardness without needing contact between the tool and the workpiece [142]. The main drawbacks are the relatively slow material removal and energy intensity [143]. Micro-EDM is particularly useful to machine CuBe alloys, which are known for their toxicity and high mechanical strength [144]. These alloys have a higher k, which can enhance the thermal removal of unwanted material [145,146]. Table 14 addresses some of the most recent state-of-the-art works regarding EDM AMPCO®, INVAR-36®, and HT steels.
3.2.2. Laser Beam Drilling (LBD)
LBD, a non-contact drilling process derived from Laser Beam Machining (LBM) [154], shares similar operational principles but offers distinct advantages. It enables the precise and accurate drilling of holes at high speeds and efficiency across various materials such as metals, ceramics, plastics, and composites. Additionally, it can create holes with high aspect ratios, increased tapers [155], and intricate geometries while minimizing thermal damage and surface defects. Furthermore, LDM boasts a higher MRR than electroerosion techniques in manufacturing applications [141]. Table 15 addresses some of the most recent state-of-the-art works regarding LDM, INVAR-36®, and HT steels.
4. Discussion
Given all the information presented in this document, a SWOT analysis was performed to discuss the perceptions of the AMPCO®, INVAR-36®, and HT steels’ machinability among the various manufacturing processes addressed. The AMPCO®, INVAR-36®, and HT steels’ machinability analysis is divided into milling (Table 16), turning (Table 17), drilling (Table 18), surface polishing (Table 19), EDM (Table 20), and LDM (Table 21).
5. Conclusions
The main objective of this review was to provide a concise and comprehensive review of the most recent investigations of these alloys’ manufacturing processes. The machinability of AMPCO®, INVAR-36®, and HT steel challenges from other authors were presented, remarks were highlighted, and their objectives and conclusions were discussed. In the context of milling, turning, drilling, surface polishing, EDM, and LBD, the following conclusions can be drawn:
Both AMPCO® and HT steels exhibit good machinability characteristics in milling and turning processes, allowing for an efficient MRR and dimensional accuracy,
INVAR-36® presents challenges due to its low k and tendency to generate heat during machining, requiring the careful selection of cutting parameters to avoid TW and surface defects,
The drillability of AMPCO® is generally favourable, with optimal cutting parameters leading to efficient hole production and minimal TW,
INVAR-36® poses challenges in drilling due to its high plasticity and toughness, leading to increased thrust forces and Tcut,
The surface polishing of AMPCO® and INVAR-36® can be effectively achieved using techniques such as electropolishing and nano-polishing, enhancing surface quality and corrosion resistance,
HT steels may require additional post-machining processes to achieve the desired surface finishes, depending on the specific material characteristics and machining parameters,
EDM proves to be a versatile machining technique for all three addressed alloys, offering high precision and complex shape capabilities,
Challenges include the formation of surface defects and recast layers, particularly in HT steels, requiring careful process optimization and control,
LBD demonstrates high efficiency and precision in drilling micro-holes in materials like INVAR-36®, with techniques such as burst mode and ultrashort pulsed lasers yielding promising results,
The optimization of laser parameters is crucial for achieving the desired drilling quality while minimizing heat-affected zones and surface defects.
As for limitations, it was difficult to obtain information, particularly regarding the conventional drilling and LBD of AMPCO® alloys and AISI L6 (DIN 1.2714). This hiatus of the literature highlights the need for further research and development in these areas. On the other hand, a trend in EDM drilling was seen for CuBe alloys compared to traditional drilling. Regarding prospects, there is a clear need for more research and development on the CuBe alloys, as this topic remains relatively underdeveloped. Moreover, there is a scarcity of information regarding the composition and research of the alloy, emphasizing that it is a heavily commercial branded material and the importance of further exploration in this field. Overall, this review article sheds light on the current state of CM and NCM processes applied to the HPIM moulding industry. Each machining technique offers unique advantages and challenges, and it is intended to bring significant contributions to the endeavours of the HPIM industry, particularly concerning the milling of AMPCO®, INVAR-36®, and HT steels. Continued research and innovation in machining technologies will further enhance the capabilities of these techniques for manufacturing injection moulding materials.
Conceptualization: F.R.N., A.F.V.P., F.J.G.S. and R.D.S.G.C.; methodology: F.R.N., A.F.V.P., F.J.G.S. and R.D.S.G.C.; validation: N.P.V.S., R.D.F.S.C., M.L.S.B. and R.C.M.S.-C.; formal analysis: N.P.V.S., R.D.F.S.C., M.L.S.B. and R.C.M.S.-C.; investigation: F.R.N. and A.F.V.P.; data curation: N.P.V.S., R.D.F.S.C., M.L.S.B. and R.C.M.S.-C.; writing—original draft preparation: A.F.V.P.; writing—review and editing: F.J.G.S., R.D.S.G.C. and R.C.M.S.-C.; visualization: N.P.V.S., R.D.F.S.C., M.L.S.B. and R.C.M.S.-C.; supervision: F.J.G.S. and R.D.S.G.C.; project administration: F.J.G.S.; funding acquisition: F.J.G.S. All authors have read and agreed to the published version of the manuscript.
No new data were created or analyzed in this study. Data sharing is not applicable to this article.
The authors thank ISEP, INEGI, and CIDEM for their institutional support.
The authors declare no conflicts of interest.
Footnotes
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Figure 1. The binary CuBe phase diagram. The composition range of interest typically contains approximately 1.8 weight percentage (wt%) of Be, denoted by the vertical dashed line [23].
Figure 2. Fe-Ni phase diagram where stable phase equilibria are demonstrated (adapted from [40]).
Figure 3. Surface residual stresses were investigated during the turning process of H13 (DIN 1.2344) tool steel, employing coated cemented carbide and PcBN cutting tools across 56 distinct cutting conditions [69].
Figure 4. Typical Time–Temperature-Transformation (TTT) diagrams (alongside Continuous Cooling Transformation (CCT) diagrams) delineate the onset of phase precipitation in AISI H11 (DIN 1.2343) hot work tool steel. The symbols represent austenite (A), cementite (C), martensite (M), bainite (B), martensite start temperature (MS), ferrite (F), and the initiation (Ac1e) and conclusion (Ac1b) temperatures of austenite transformation [78].
Figure 6. SEM images of a TiAlTaN-coated tool during testing at Lcut = 53.6 m and f = 750 mm/min. Magnifications of 100× and 220× of the following: (a) Tooth 1 of the cutting tool with CF, (b) Tooth 2 of the cutting tool with CF, (c) Tooth 2 of the cutting tool with RF, and (d) the top surface [34].
Figure 7. (a) Wear mechanisms observed on the RF of an uncoated tool during testing at Lcut = 48 m and f = 750 mm/min. (b) Wear mechanisms detected on the top surface (TOP) of tools employed by an uncoated tool during testing at Lcut = 48 m and f = 1500 mm/min [14].
Figure 8. The progression of the (a) thrust force and (b) Tcut signals as the tool advances during single-pass drilling; (c) the evolution of thrust forces with various processing parameters in the INVAR-36® layer [133].
Industry applications and characteristics of AMPCO® alloys.
Alloy | Industry Applications | Characteristics |
---|---|---|
AMPCO® 83 [ | Construction of chill plates, | High levels of hardness, |
AMPCO® 88 | Flash welding dies, | Good machinability, |
AMPCO® 89 | Welding wheels, | Good machinability, |
AMPCO® 91 | Spot welding electrodes, | Extremely resistant to wear and corrosion, |
Chemical composition of some AMPCO® alloys.
wt% | ||||||||
---|---|---|---|---|---|---|---|---|
Cu | Be | Co + Ni | Co | Ni | Si | Al | Others | |
AMPCO® 83 [ | Bal. | 2.0 | 0.5 | - | - | - | - | ≤0.5 |
AMPCO®88 [ | Bal. | 0.5 | 2.5 | - | - | - | - | ≤0.5 |
AMPCO®89 [ | Bal. | 0.4 | - | 0.3 max. | 2.8 | - | - | ≤0.4 |
AMPCO®91 [ | Bal. | 0.5 | - | 2.4 | - | - | - | ≤0.5 |
CuBe C17200 [ | Bal. | 1.9 | - | 0.2 | - | - | - | - |
CuBe C17200 [ | Bal. | 1.8–2.0 | ≥0.2 | - | - | ≤0.2 | ≤0.2 | - |
Bal.—balance.
Physical, mechanical, and thermodynamic properties of some AMPCO® alloys.
Property | AMPCO® Alloys | Units | ||||
---|---|---|---|---|---|---|
83 [ | 88 | 89 | 91 | |||
Ø ≤ 35 mm | Ø ≥ 35 mm | |||||
E | 128 | 130 | 135 | 130 | 130 | GPa |
ν | - | - | - | - | - | [-] |
σu | 1140 | 890 | 740 | 900 | 723 | MPa |
σy | 1000 | 680 | 680 | 550 | 517 | MPa |
HV | 376 | 277 | 235 | 262 | 255 | HV |
εu | 5 | 14 | 12 | 10 | 17 | % |
ρ | 8260 | 8750 | 8800 | 8750 | kg/m3 | |
α | 17.5 | 17.0 | 17.2 | 17.0 | 10−6/K | |
k (@100 °C) | 130 | 230 | 300 | 208 | W/m·K |
E—Young’s Modulus, HV—Vickers’ hardness, εu—strain at fracture, ρ—volumetric mass density, σu—tensile strength, σy—yield strength.
Physical, mechanical, and thermodynamic properties of INVAR-36®, according to the literature.
Property | Value | Units | ||||
---|---|---|---|---|---|---|
[ | [ | [ | [ | [ | ||
E | 141 | 146 | 140 | 145 | 141 | GPa |
ν | 0.29 | 0.28 | - | - | 0.29 | [-] |
σu | - | 583 | 448 | 717 | 448 | MPa |
σy | - | - | 276 | 679 | 276 | MPa |
HV | - | - | - | - | - | HV |
εu | - | - | 35 | 5.5 | - | % |
ρ | 8100 | - | - | - | 8050 | kg/m3 |
α | 1.8 | 1.7 | - | - | 1.3 | 10−6/K |
k | 11 | 11.9 | - | - | - | W/m-K |
CR—Cold-Rolled, ν—Poisson’s coefficient.
The chemical composition of INVAR-36®, according to the literature.
INVAR-36® | wt% | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|
Fe | Ni | C | P | Cr | Mn | Mo | S | Si | Co | Nb | Ti | |
[ | Bal. | 35–37 | ≤0.5 | 0.020 | 0.500 | 0.600 | 0.500 | 0.025 | 0.300 | - | - | - |
[ | 63.4 | 36.1 | 0.04 | - | 0.04 | 0.16 | - | - | 0.12 | 0.06 | - | - |
[ | Bal. | 35–37 | ≤0.05 | ≤0.02 | - | 0.2–0.6 | - | ≤0.02 | ≤0.2 | - | - | - |
[ | 61.6 | 35.66 | 0.22 | - | 0.01 | 0.43 | - | - | - | - | 1.38 | 0.53 |
Bal.—balance.
Mechanical properties of HT steels.
Property | Value | Units | |||||
---|---|---|---|---|---|---|---|
DIN 1.2343 (AISI H11) | DIN 1.2344 | DIN 1.2714 | |||||
[ | [ | [ | |||||
E | 207 | 208 | 210 | 211 | 211 | 205 | GPa |
ν | 0.27–0.30 | [-] | |||||
σu | 1450–2130 | 1497 | 1469 | 1464 | 1469 | - | MPa |
σy | 1200–1850 | 1303 | 1265 | 1255 | 1253 | - | MPa |
HV | 448–505 | ≥649 | HV | ||||
εu | - | 16.8 | 14.2 | 12.1 | 18.0 | - | % |
The typical chemical composition of HT steels, according to the literature.
AISI | H11 | H13 | L6 | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
[ | [ | [ | [ | [ | [ | [ | [ | [ | [ | [ | [ | ||
wt% | Fe | Bal. | Bal. | Bal. | Bal. | Bal. | Bal. | Bal. | Bal. | Bal. | Bal. | 94.2–97.0 | 94.19–97.15 |
C | 0.37 | 0.379 | 0.36 | 0.38 | 0.32–0.40 | 0.39 | 0.37 ± 0 | 0.33–0.41 | 0.38 | 0.55 | 0.65–0.75 | 0.65–0.75 | |
Cr | 5.16 | 4.64 | 5.05 | 5.00 | 5.13–5.25 | 5.00 | 4.95 ± 0.05 | 4.80–5.50 | 5.00 | 0.75 | 0.6–1.2 | 0.60–1.20 | |
Mn | 0.27 | 0.373 | 0.54 | 0.40 | - | 0.32 | 0.43 ± 0 | 0.25–0.50 | 0.40 | 0.70 | 0.25–0.8 | 0.25–0.80 | |
Mo | 1.28 | 1.23 | 1.22 | 1.30 | 1.33–1.40 | 1.27 | 1.22 ± 0 | 1.10–1.50 | 1.30 | 0.50 | ≤0.50 | ≤0.50 | |
Si | ≤1.0 | 1.04 | 0.97 | 1.10 | 1.00 | 0.88 | 1.16 ± 0.01 | 0.8–1.20 | 1.10 | 0.25 | 0.25 | 0.10–0.15 | |
V | 0.41 | 0.364 | 0.38 | 0.40 | 1.00 | 0.93 | 0.4 ± 0 | 0.30–0.50 | 0.90 | 0.10 | 0.20–0.31 | - | |
P | - | 0.027 | 0.015 | - | 0.018 | - | - | - | - | ≤0.03 | |||
S | - | 0.005 | 0.002 | - | 0.007 | - | - | - | - | ≤0.03 | |||
Co | - | 0.017 | - | - | 0.01 | - | - | - | - | - | |||
Ni | - | 0.248 | - | - | - | 0.26 ± 0 | - | - | 1.25–2.00 | 1.25–2.00 | |||
W | - | - | - | - | 0.18 | - | - | - | - | - |
Bal.—balance.
The characteristics of the main elements of the addressed HT steels [
Element | Characteristics |
---|---|
Cu | Increase the γ phase domain, |
Be | Energetic deoxidizer, |
Ni | It does not form carbides but is dissolved in the matrix (both in annealed and quenched states), |
Co | It does not form carbides, |
C | It improves the hardness and mechanical resistance (annealed) because the reaction of Fe and C forms hard carbides that are resistant to wear, |
Cr | A part is dissolved in the matrix, and the other part is combined with C to form carbides, |
Mn | Deoxidizer, |
Mo | Strong carbide former, usually combined with Cr, Mn, Ni, and Co, |
Si | Deoxidizer or alloying element, |
Advantages and disadvantages of the main elements of the alloys mentioned above [
Co | Cr | Cu | Mn | Mo | Ni | S | Si | |
---|---|---|---|---|---|---|---|---|
Advantages | ||||||||
Improve machinability | X | |||||||
Improve wear resistance | X | X | X | |||||
Improve tempering resistance | X | X | ||||||
Improve T resistance | X | X | X | |||||
Improve hot wear resistance | X | X | ||||||
Improve corrosion resistance | X | X | X | X | X | |||
Disadvantages | ||||||||
Improve corrosion | X | X | X | X | X | X | X | |
Improve fatigue failure | X | X | ||||||
Brittle at high T | X | X | ||||||
Low ductility | X | X | ||||||
High melting point | X | |||||||
High thermal expansion | X | |||||||
Improve brittleness | X | X | X | X | X | X | ||
Difficulty in machining | X | X | X |
Milling processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
AMPCO® | Ramesh et al. [ | The authors assessed the CuBe C17200 [ | (1) A higher MRR is achieved at a higher s, f, and lower ap. A lower Ra is achieved at a medium s, lower f, and higher ap. A lower MRR will lead to a higher surface finish. |
Zuo et al. [ | Several investigations were carried out to examine the impact of s on the TW characteristics of uncoated and TiAlN-coated [ | (1) Abrasion decreases the TL and negatively affects the surface finish because of the adhesive TW. | |
Sousa et al. [ | Evaluated TW after machining a CuBe alloy AMPCOLOY® 83, employing solid-carbide uncoated end mills and DLC/CrN multi-layered coated tools, possessing identical geometries. The experimental setups were conducted using an L9 array with Vc = 126 m/min; f = 350, 750, and 1500 mm/min; Lcut = 18, 36, and 48 m; ap = 0.5 mm, and the radial depth of cut (ae or RDOC) was 2.5 mm. | The SR was significantly influenced by f, resulting in a fourfold increase in Ra values when transitioning from f = 750 mm/min to 1500 mm/min. This trend was observed for uncoated and coated tools. The last referred exhibited superior performance for cutting lengths (Lcut) up to 36 m. Conversely, uncoated tools consistently provided better surface quality for Lcut = 48 m. The wear behaviour of the tools was similar, VB = 80.71 µm and VB = 102.3 µm for uncoated and coated tools at Lcut = 48 m, respectively, exhibiting increased and pronounced VB at f = 1500 mm/min. At Lcut = 18 and 36 m, the coated tools revealed less VB than uncoated ones. | |
Nogueira et al. [ | Conducted an assessment, identification, and quantification of TW mechanisms during the machining of AMPCO® using WC-Co uncoated tools and TiAlTaN-coated tools by Physical Vapour Deposition (PVD) [ | For WC-Co uncoated tools, f and Lcut parameters noticeably influence the Ra values. The lowest Ra values were observed under f = 750 mm/min and Lcut = 26.8 m, while the highest Ra values were noted for f = 1500 mm/min and Lcut = 73.7 m, both longitudinally and transversely. This suggests that the superior Ra, the total height of the profile (Rt), and the maximum height of the profile (Rz) values were achieved at lower f and Lcut values, indicating that a poorer machined surface quality was obtained for higher f and Lcut values. Concerning VB, the primary wear mechanisms identified were the abrasion and adhesion of the machined material. | |
INVAR-36® | Zheng et al. [ | A trialled face milling experiment was conducted on INVAR-36® using a coated carbide. The microhardness was assessed, and the metallographic structure was observed to identify work-hardening mechanisms. | Work-hardening occurred during the face milling of INVAR-36®, ranging from 120 to 150% at a 30 μm depth. Parameters such as ap and fz significantly influenced the degree and depth of work-hardening. As these parameters increased, the depth and degree of work-hardening also increased. Upon metallographic observation, the work-hardening layer comprised two distinct regions: the thermal-force-influenced and force-influenced. |
Cornelius et al. [ | These authors elucidated the definition and transfer of the coordinate system for the five-axis machining of additively manufactured preforms. The practical application of this method was demonstrated through the precision machining of a mould for a Carbon Fibre-Reinforced Polymer (CFRP) layup fabricated from an additively manufactured INVAR-36® preform. | The utilization of this technique holds the potential to enhance accuracy, minimize material wastage, and reduce the overall machining cycle time. However, the final machined component proved unsuitable when applied to the Wire Arc Additive Manufactured (WAAMed) INVAR-36® preform examined in this study. This outcome was attributed to several inherent challenges associated with additively manufactured parts, including warping, internal stresses, and porosities. | |
Gil Del Val et al. [ | A study characterizing the machinability of INVAR-36® samples produced through Wire Arc Additive Manufacturing (WAAM) technology was proposed, employing Minimum Quantity Lubrication (MQL) during the finishing milling process. | The SR values of WAAM samples are minimal under all cutting conditions, despite a 9% increase in average Fcut compared to wrought samples, attributed to the higher hardness level of WAAM samples (20%). Furthermore, the statistical analysis not only underscores the negligible influence of Vc on machinability but also identifies the optimal roughness value (0.8 µm) achieved at Vc = 50 m/min and fz = 0.06 mm/tooth. Ultimately, the predominant wear mechanism observed during the finishing milling of WAAM INVAR-36® samples is adhesion on the rake and clearance faces (RF and CF). | |
HT Steels | Arruda et al. [ | This work aimed to optimize Ra on AISI H13 (DIN 1.2344) steel, using a ball nose end mill, during finishing milling. Ra was evaluated in two cutting directions. | The ball nose end mills can effectively produce suitable Ra values for manufacturing moulds and dies when used for the finishing milling of AISI H13 hardened steel. The outcomes of this investigation can be applied in the finishing milling process of AISI H13 hardened steel using ball nose end mills to obtain consistent Ra values that are robust against noise factors. |
Singh et al. [ | The impact of machining parameters during the milling of AISI H11 (DIN 1.2343) was assessed by evaluating SR and MRR. TGRA with a standard L27 orthogonal array was conducted to determine the optimal milling setup. Data analysis was conducted using Microsoft® Excel™ software, and the significance of the model was assessed using the ANOVA method. | (1) Vc emerges as the sole significant machining parameter affecting SR. Increasing Vc leads to enhanced SR. | |
Şahinoğlu [ | This author investigated the vibration, energy consumption, power consumption (Pin), and SR values during the machining of AISI H11 (DIN 1.2343) tool steel under cryogenic CO2 (l), coolant, and dry cutting lubricating environments. | Vibration values increase with extreme cutting parameters, with the highest vibration occurring during CO2 (l) cutting. The coolant environment exhibits the slightest vibration. f is determined to be the most influential parameter on SR. The optimal cutting conditions for reduced vibration and SR values were identified as ap = 0.2 mm, Vc = 175 m/min, and f = 0.119 mm/rev with coolant lubrication. Under these conditions, vibration, SR, and Pin were reduced by 5.18%, 37.12%, and 36.19%, respectively, and machine efficiency increased by 7.16%. It is noteworthy that other authors have also studied the subject of machining vibrations [ | |
Platt et al. [ | These authors conducted a study on the High-Feed Milling (HFM) of surface structures in components made of AISI H11 (DIN 1.2343) hot work tool steel (HWS). The process’s performance was assessed through Fcut measurements and TL tests. The resulting surface topography was measured and assessed based on the quality of the structure and roughness parameters. | Vc = 200 m/min resulted in reduced Fcut and TW development compared to Vc = 100 m/min. Higher values for the lead angle (βf) also contribute to decreased Fcut while altering the resulting structure geometry. Increasing ap reinforces these trends. Significant differences are observed in the achievable Rz and their qualitative geometry, along with anisotropies in the structure formation, concerning the surface topography. Additional investigations are required to assess burr formation associated with VB in HFM. | |
Wojciechowski et al. [ | During the precise ball-end milling of AISI L6 (DIN 1.2714) alloy steel, the ploughing phenomenon was assessed by analysing Fcut at the interface between the tool flank face and the workpiece. A novel ploughing Fcut model was developed for ball-end milling, accounting for the influence of the minimum uncut chip thickness (hmin) and the ploughing volume. | The ploughing Fcut was significantly higher when milling with a worn tool, due to the irregular non-circular profile of the cutting edge below the stagnant point and the presence of attrition and micro-grooves on the tool flank face. The angle that represents the slope of the machined surface was found to have a non-linear impact on the estimated values of hmin and k. When using a worn tool, VB = 150 μm [ | |
Abu Bakar et al. [ | These authors conducted an experimental study to investigate TW mechanisms during the dry and cryogenic N2(l) milling of AISI H13 (DIN 1.2344) steel, employing different cutting-edge radii. The objective was to examine how the cutting-edge radius influences the TW mechanism of uncoated carbide-cutting tools with rounded edges. | The milling setup is determined by Vc = 200 m/min, fz = 0.03 mm/tooth, and ap = 0.1 mm for dry and cryogenic N2(l) cooling environments. Milling using N2(l) with a tool that has a cutting-edge radius of Rn = 0.03 mm enhances the performance of an uncoated carbide tool during the milling of AISI H13 (DIN 1.2344) steel. This reduces TW rates and extends TL compared to dry machining with a commercial tool of Rn = 0.018 mm. N2(l) dissipating heat efficiency delays the development of TW. A larger cutting-edge radius significantly impacts the TL, attributed to the higher VB generated at a sharper cutting edge. Analysis using Field-Emission Scanning Electron Microscopy (FESEM) revealed that abrasive and adhesive wear were the predominant wear mechanisms observed under dry and cryogenic N2(l) milling, being more pronounced in dry machining due to high T. |
Turning processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
AMPCO® | Sharma et al. [ | These authors employed a molecular dynamics simulation to investigate the interaction between the tool and hard particles during the nano-orthogonal cutting of CuBe. They observed that including hard particles within the workpiece materials influences the cutting process, impacting surface formation, material deformation, and TW mechanisms. | The position and dimensions of a hard particle are determining factors in surface formation and subsurface damage. Fcut experienced sudden increases, leading to surface deterioration. Subsequently, the particle rebounds after the tool passage, causing protrusions on the surface. |
Sharma et al. [ | These authors examined the mechanisms involved in machining Cu and CuBe alloys by analysing imprints on the tools and machined surfaces. In addition, the authors investigated factors such as TL, wear patterns, changes in the diamond tool’s phase, and the interactions between the tool and workpiece materials during the machining process. | (1) CuBe has a high VB rate, which means that the roughness increase is also high as a reflection of the rate affecting the surface. | |
INVAR-36® | Zhao et al. [ | These authors focused on the cutting performance of ceramic cutting tools in wet turning the INVAR-36® alloy, including TL, Ra, and failure mechanisms. The optimal cutting parameters were determined using an orthogonal test and range analysis. | Parameter ap significantly impacted the metal MRR amount, while f significantly affected Ra. The observed wear mechanisms included abrasive, diffusion, and oxidation wear. |
Mahir [ | The performance of three distinct tools was compared: a two-layered TiCN-Al2O3-coated tool, a single-layered TiAlN-coated tool, and one uncoated tool when machining INVAR-36®. The TW is about 30% and 60% better using the TiCN-Al2O3-coated insert than the single-layer TiAlN-coated and uncoated inserts, respectively. | (1) VB and BUE were the predominant wear mechanisms observed for all cutting tools. | |
HT Steels | Suresh and Basavarajappa [ | This work is focused on formulating a response surface methodology to represent the relationship between cutting parameters and the turning process of hardened AISI H13 (DIN 1.2344) steel (55 HRc) using TiCN-coated ceramic tools under dry cutting conditions. Mathematical models were developed to correlate machining parameters with TW and SR. | The central composite design utilized in this study has demonstrated its effectiveness in modelling TW and SR. Vc is the most significant parameter affecting TW, accounting for 47.4% of the variance, followed by f at 28.15% and ap at 15.8%. Abrasion is identified as the primary wear mechanism observed under extreme cutting conditions, while adhesion predominates at softer cutting conditions. Regarding SR, f emerges as the most influential factor, explaining 49.55% of the variance, followed by Vc at 40.3% and ap at 8.8%. SR improves with increasing Vc but deteriorates with higher f. |
Benlahmidi et al. [ | The impacts of Vc, f, ap, and workpiece hardness on SR, cutting pressure, and cutting power were investigated during hard turning hardened AISI H11 (DIN 1.2343) utilizing cBN7020 tools. | Factors and performance relationship measures are expressed through quadratic regression equations, enabling the estimation of the expected performance. The mathematical models demonstrate a good fit with experimental values within a 95% confidence interval. The hardness of the machined material predominantly influences the variations in output factors. This insight has facilitated the precise delineation of the hard turning domain for the proposed cBN tool and workpiece. The presented results indicate a significant improvement in SR with increasing Vc and workpiece hardness while displaying adverse effects with a higher f, although ap has a negligible influence. The optimal setup is Vc = 178.32 m/min, f = 0.08 mm/rev, ap = 0.43 mm, and a workpiece hardness of 41.73 HRc. Additionally, it was determined that TL is primarily influenced by Vc, with a 91.68% contribution and to a lesser extent by f, with a 3.83% contribution. | |
Liu et al. [ | TiCN-based cermets and cemented carbide tools were manufactured with a multi-layer TiN/Al2O3/TiCN/TiN CVD coating to evaluate their performance in the orthogonal cutting machining of hardened AISI H13 (DIN 1.2344) steel. | (1) An increase in Vc, ap, and f accelerates VB. Coated cermets exhibit a longer TL than uncoated ones. However, with increasing ap and f, Fcut significantly rises. Due to poor toughness, cracks are more prone to initiate and propagate in coated cermets, resulting in a shorter TL. | |
Özbek [ | This author explored how cryogenic treatment affects the performance of cutting tools when turning AISI H11 (DIN 1.2343) steel. This treatment resulted in an increased hardness of the cutting tools. | The cutting tools that underwent deep cryogenic treatment experienced the most substantial increase in hardness, with a rise of 10.87%. The wear resistance of tungsten carbide cutting tools coated with TiCN-Al2O3-TiN was enhanced through cryogenic treatment. Tools subjected to deep cryogenic treatment demonstrated a superior wear resistance and Ra compared to those treated with shallow cryogenic treatment for six hours. As Vc increased, the cutting tools exhibited an increased VB. The abrasive TW mechanism resulted in VB on all tools, while the adhesive wear mechanism caused a built-up edge on the tools. Cryogenically treated tools induced superior Ra values on the workpieces compared to untreated tools. Tools that underwent deep cryogenic treatment for 24 h achieved the most optimal Ra. The experimental findings indicated that cryogenic treatment enhanced the cutting tool’s resistance to abrasion. |
Drilling processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
INVAR-36® | Zhang et al. [ | These authors endeavoured to elucidate the progression of crucial cutting phenomena, such as thrust forces, Tcut, and surface quality while drilling holes in INVAR-36®/CFRP T700 multi-material stacks, focusing on the influence of cutting parameters. Additionally, the mechanism governing the control of the interfacial drilling response was examined. PVD TiAlN-coated drills were used, and the machining levels were defined by s = 2000, 4000, 6000, and 8000 rpm/min, and f = 0.005 mm/rev, 0.01 mm/rev, 0.015 mm/rev, and 0.02 mm/rev. Only the findings about INVAR-36® will be addressed. | (1) The thrust forces and Tcut encountered during the drilling of the INVAR-36® phase surpass those observed in both the upper and lower CFRP phases ( |
HT Steels | Sorgato et al. [ | The TW and surface quality in drilling operations of multi-layered cladding were investigated, which is particularly challenging and requires further investigation. The laser cladding of AISI H13 (DIN 1.2344) tool steel layers using varying powder sizes and laser power was performed. Later, drilling tests at constant cutting parameters were conducted to evaluate drill bit wear. Additionally, the study investigated the quality of the drilled holes by analysing the internal Ra and edge contour and their relationship with TW. | The accuracy of the drilled holes’ diameter and their internal surface finish quality were evaluated. The primary wear mechanisms identified were adhesion, the coating peeling off, and laser cladding samples at the slowest scanning speed experienced BUE on the tool’s cutting edges. The improved mechanical properties obtained at lower scanning speeds generate more heat in the cutting zone, increasing BUE formation. The results indicate that the microstructural features induced by the deposition process significantly impacted the TW and the quality of the drilled hole when using laser cladding AISI H13 tool steel. The parameters used for laser cladding significantly impact TW and, consequently, the quality of the drilled hole. |
Surface polishing processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
AMPCO® | Kityk et al. [ | Research on electropolishing bronze using an electrolyte composed of a deep eutectic solvent known as Ethaline was conducted. This solvent comprises a eutectic blend of choline chloride and ethylene glycol in a 1:2 mass ratio. Two types of bronze alloys, namely AMPCO® 22 and AMPCO® 712, were employed in the study. | Electropolishing AMPCO® 22 and AMPCO® 712 can be carried out in Ethaline at an electrode potential of +2.5 V and T = 25 °C for 20 min. The SR was reduced by 80% and 60% compared to its initial values for AMPCO® 22 and AMPCO® 712, respectively. Additionally, the electropolished surfaces of AMPCO® 22 and AMPCO® 712 showed improved corrosion resistance by nearly 30% and 10% for AMPCO® 22 bronze and AMPCO® 712 bronze, respectively. |
INVAR-36® | Wang et al. [ | A numerical investigation was performed to ascertain the primary factors influencing the nano-polishing characteristics of INVAR-36®. Given its low hardness and pronounced chemical reactivity, achieving superior surface quality with nanometric precision presents a formidable challenge. FEA was employed via a molecular dynamics simulation, complemented by an experimental validation of the simulation outcomes. | (1) Within the molecular dynamics simulations, elevating the polishing velocity yielded an increased MRR and mitigated subsurface damage. However, this also led to a coarser groove surface and encouraged the formation of amorphous regions. As the speed escalated further, the polishing efficiency reached a critical threshold. |
HT Steels | Temmler et al. [ | The impact of multi-step laser polishing on the microstructural characteristics of the remelted surface layer of AISI H11 (DIN 1.2343) tool steel was examined. Four distinct sets of process parameters were chosen for the laser polishing initially annealed samples composed of H11 tool steel. | Electron Backscatter Diffraction (EBSD) analysis demonstrated a refinement in grain structure, with an average size ranging from 1.1 to 1.5 μm after remelting using the laser. Surface hardness significantly increased the hardness of the initially soft annealed base material, attributed to grain refinement and the formation of martensite. SR measurements revealed Ra = 0.11 μm achieved within an Ar atmosphere. Introducing 6 vol% CO2 into the process gas atmosphere further reduced Ra = 0.05 μm. |
Awale et al. [ | The capability of non-destructive methods such as micromagnetic Barkhausen Noise (MBN) in evaluating grinding burn defects concerning the microstructural and mechanical characteristics of hardened AISI H13 (DIN 1.2344) die steel was discussed. The study employed an MQL lubrication grinding environment, utilizing environmentally friendly machining fluids such as Paraffin Oil (PO) and castor oil (CO) and compared their efficacy with traditional wet and dry grinding methods. | A 75% decrease in grinding T accompanied by minimal oxidation and carbonization layers, C = 3.16% and O = 1.23%, occurred at higher f = 12 m/min. This was facilitated by adequate lubrication and cooling during the wheel–work–chip interaction through the capillary penetration of castor oil-based MQL, as observed in dry grinding. The MQL-CO grinding method exhibited the lowest Ra = 0.232 μm and Rz = 1.838 μm on the surface topography. This was attributed to the superior anti-friction and anti-wear properties of CO, which mitigated ploughing and rubbing actions. Dry grinding resulted in notable alterations in the microstructure, with a thermal damage region of 55 μm and a lower microhardness, 429 HV, due to temper damage effects on the ground surface and subsurface at elevated T = 817 °C. A non-destructive assessment revealed a poor MBN signal and small envelope amplitude during MQL-CO grinding. This was attributed to the minimal impact of temper damage on the newly formed surface grains at higher work f = 12 m/min, hindering magnetic domain wall rotation. |
EDM processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
AMPCO® | Yıldız et al. [ | The thickness (t) of the white layer (WLT) that forms during the EDD of the CuBe alloy and how the WLT changes as the drilling depth increases were examined. Statistical analysis using ANOVA and significant difference methods determined that as the drilling depth, working current, and pulse duration increase, t the WLT also increases. | The working current, pulse-on time (Ton), and pulse-off time (Toff) duration primarily influence the WLT formed during the process. The depth of the drilled hole also plays a meaningful role. A second-order response surface model has been created in this study, incorporating the main and interaction effects of various influential combinations of EDD control factors and variations in hole measurements, effectively predicting the formation of the WLT’s t and optimal EDD performance with a 95% confidence interval. For thinner t achievement, using lower working currents, Ton and Toff are recommended during EDD. The authors address that future attempts should address the variations in Ra that arise due to the EDD machining depth. |
Dong et al. [ | In this investigation, auxiliary electrodes were employed to mitigate the impacts of stray-current corrosion on the terminal surfaces of holes in the C17200 [ | The micro-EDM drilling of micro-holes on the C17200 CuBe alloy in deionized H2O reveals electrochemical dissolution and anodic oxidation occurring at the end surface of the micro-hole, directly impacting the performance and lifespan of components. The effectiveness of micro-EDM with an auxiliary electrode in mitigating stray-current corrosion on the C17200 CuBe alloy was confirmed across various pulse currents and pulse widths. Fine micro-hole end surfaces were achieved with the auxiliary electrode under 0.34 A pulse current conditions and a 20 μs pulse width. Minimal impact on electrode wear was verified with the auxiliary electrode. However, the machining time slightly increased when the pulse current was below 0.55 A and the pulse width was 20 μs. Beyond this threshold, the effect of the auxiliary electrode on machining time was less apparent. | |
Rebelo et al. [ | This work presented an experiment that examines how various processing parameters for the rough, finishing, and micro-finishing or polishing of EDM impact the MRR and surface quality when machining high-strength CuBe alloys. | (1) The average recrystallization rates observed in the CuBe alloy are approximately 0.1 of those in steels. | |
Mouralova et al. [ | This work aimed to optimize AMPCOLOY® 35 EDM parameters such as Vc, surface topography, and complex surface. A mathematical model was developed to determine the optimal Vc, and an optimization process was carried out using this model. The optimization aimed to achieve the maximum Vc while minimizing Ra. Equal importance was given to both objectives during the optimization procedure. | All the machined samples exhibited a similar surface morphology, regardless of the specific machine parameters used. The samples were relatively smooth and did not contain any large craters. While there were some small cracks on the surface of all samples, these were found to be purely superficial and did not extend into the cross-section of the samples. This evidence suggested that the cracks did not compromise the functionality or service life of the machined parts. The machined specimens’ surfaces display segregated lead crystals in various regions. The subsurface region of all samples was entirely free of defects, and the recast layer was thin, measuring no more than t = 15 μm and only present in localized areas. Using TEM, a lamella analysis identified an elevated concentration of alloying elements in the recast layer. The analysis also revealed a shift in crystal orientation resulting from Wire EDM (WEDM) | |
Mouralova et al. [ | These authors developed mathematical models to optimize the machining process of AMPCOLOY® 35 across a varying t, ranging from 5 mm to 160 mm in increments of 5 mm, employing WEDM to enhance the surface characteristics of mould parts. The Box–Behnken-type experiment design generated 448 samples. | (1) The highest Ra = 4 µm at the centre of the samples was reported, while a slightly lower value of Ra = 3.6 µm was observed at the margins. The lowest Ra = 1.6 µm was recorded in the sample machined with Ton = 6 µs, Toff = 40 µs, and a peak current (Ip) of 25 A. | |
Dong et al. [ | The mill micro-ball socket technique in the C17200 [ | The most favourable outcomes were obtained when k = 0.98 and the initial layer was t = 0.024 mm (innovative approach for manufacturing micro-ball sockets in C17200 [ | |
INVAR-36® | Mohanty et al. [ | These authors systematically refined multiple input parameters for the wire EDM machining of INVAR-36®, employing TGRA for optimization. Key control parameters, including Ton, pulse-off time (Toff), servo voltage (SV), and WF, were selected to assess their impact on the MRR and SR of the INVAR-36® alloy. To achieve the optimization of the MRR and SR, a total of nine experiments were conducted using the L9 orthogonal array design. | The MRR increases with a higher WF and Ton, with SV demonstrating the most negligible impact on the MRR, contributing only 16.22%. The optimal combination of process parameters for achieving the maximum MRR comprises Ton = 25 µs, Toff = 46 µs, WF = 5 mm/min, and SV = 30 V. The SR escalates with elevations in WF and Toff, while SV exhibits minimal influence on SR, contributing only 17.97%. The ideal set of process parameters for attaining the lowest SR involves Ton = 25 µs, Toff = 19 µs, WF = 3 mm/min, and SV = 20 V. WF emerges as the most influential parameter affecting the MRR and SR, whereas SV is the least influential factor in both aspects. |
HT Steels | Gill and Kumar [ | The surface alloying phenomenon induced by the EDM process employing tool electrodes fabricated via powder metallurgy (PM) was explored. The study employed a TGRA with an L18 orthogonal array to determine the optimal setup for achieving the minimum SR. Experiments were conducted on the AISI H11 (DIN 1.2343) hot die steel utilizing WCu electrodes produced via the PM process. Tool polarity (P), the percentage of the alloying element in the tool (%W), Ip, Ton, duty factor (τ), and SV input parameters were considered, and their significance was analysed through ANOVA. Scanning Electron Microscopy (SEM), Energy-Dispersive Spectroscopy (EDS), and X-ray diffraction (XRD) were utilized to examine the characteristics of the machined surface. | The presence of W3C on the surface suggests a reaction between W migrated from the PM tool and C in the high-T discharge zone. A portion of Cu from the PM electrode is also transferred to the machined surface. As Cu forms a solid solution with the α-Fe phase, this phenomenon further enhances the machined surface quality and the hardness by up to 83%. This improves the surface to abrasion, extending the lifespan of press tools and dies for hot working applications. No microcracks are observed on surfaces machined with the PM tool, indicating that the alloying process does not compromise SR, which is Ra ≈ 4 μm and aligns with typical values obtained in conventional EDM processes. |
Hess et al. [ | During the process of the AISI H11 (DIN 1.2343) EDM, the application of thermal energy leads to the formation of microstructural changes and modifications in the material of the machined component. Although a T near or above the evaporation point is generated during the discharge at the surface, the actual T decreases as the depth within the component increases. | Ablation occurs when the material is exposed to thermal loads caused by an electrical discharge, which results in the heating of the material to T, exceeding the melting and evaporation points. As a result of the structural changes occurring within the component during EDM, the material properties are modified, leading to significant impacts on the functionality and potential applications of the resulting manufactured part. The degree of austenitization became progressively less advanced, further moving deeper inside the workpiece. At the top of the material, the carbides wholly dissolved during the heating process, but as they moved towards the bottom of the heat-affected zone (HAZ), some carbides remained even after the heating process. When the T gradients and maximum temperature (Tmax) are increased, the areas of retained austenite become larger. | |
Le [ | The impact of various main process parameters, such as peak current (Ip) and pulse-on time (Ton) during fine finishing, as well as powder concentration (Cp), on the machined performance (MP) and recast layer properties (RLPs) of AISI H13 (DIN 1.2344) steel samples was studied in this work. The goal was to investigate how these parameters affect the quality of the finished product. | As the main process parameters are incrementally changed, both the MRR and TWR show an upward trend. There is a decrease in the percentage of the Fe element on the surface of the recast layer compared to the substrate of AISI H13 steel. While the percentage of C increases compared to the substrate layer, it remains lower than the percentage found on the surface of the recast layer in the EDM process. |
LDM processes: addressed challenges and remarks.
Material | Author | Challenges | Remarks |
---|---|---|---|
INVAR-36® | Butkus et al. [ | A burst mode laser was used to perform micromachining on 20–250 µm thick INVAR-36® foils to determine the best micromachining parameters for percussion drilling. The method used for drilling holes involved firing multiple laser pulses transversely onto the sample, known as percussion drilling, without moving the beam. The study examined the rate at which holes were drilled and how the quality of the holes was affected by the number of laser pulses per burst and the laser’s average power. | The micromachining efficiency significantly improved using the burst mode laser. The micromachining throughput was up to 10× higher when using the burst mode. Using a specific laser mode of repetition rate burst can enhance the efficiency of micromachining through holes. The efficiency of ablation decreases as the t of the sample increases. The efficiency of ablation decreases for thick samples. In general, generating burst pulses for micromachining appears to be a promising approach to achieve faster and more efficient results while maintaining a similar level of quality. |
Hauschwitz et al. [ | Choose INVAR-36® for high-quality micrometre-scale patterns within metal shadow masks, like OLED displays, because of its exceptional characteristics, precisely its low k. | The optical module’s attributes enable the rapid alignment of the setup to achieve a consistent intensity distribution throughout the entire pattern and facilitate focus adjustments. | |
Chung et al. [ | An ultrashort pulsed laser system was highly recommended for micro-hole drilling in INVAR-36®, as it minimized the adverse effects of heat and produced high-quality edges. | An Nd:YAG laser is the preferred method to create a hole in INVAR-36®. Although it has the drawback of producing burrs at the edges that necessitate further processing, the study decided to employ an ultrashort pulsed laser instead. | |
Choi et al. [ | The impact of focal plane adjustments, achieved through vibration, on the quality of the INVAR-36® alloy’s fabrication during femtosecond laser hole drilling was examined. This process is used to create high-quality metal masks. The ability to control the taper angles during femtosecond laser hole drilling makes it a promising technique for the accurate micromachining of various intelligent devices. | The processing efficiency and productivity were maximized when the initial laser pulse was directed towards the sample’s upper surface, resulting in the most profound processed depth. Therefore, synchronizing the laser and vibrator in the hole processing system can significantly impact overall productivity. Decreasing the vibrator amplitude during femtosecond laser hole machining increased the taper angle of the processed hole. These findings indicate that the hole’s taper angle can be effectively managed by adjusting the amplitude of the continuously operating vibrator. | |
HT Steels | Rubaiee [ | The authors LDMed a 0.44 mm thick AISI H13 (DIN 1.2344) using 100 m fibre laser beams. The Complex Proportional Assessment (COPRAS) method optimizes the fibre laser settings for drilling holes. ANOVA was conducted to validate the model, and ANN was utilized to forecast the experimental outcomes. | Laser power emerges as the most critical factor influencing the quality of drilled holes. Under the optimal setup, the drilled holes exhibit Ra = 4.27 µm, a heat-affected zone of 89.89 µm, and an overcut of 139.60 µm. The experimental results indicate a close match between the observed and predicted values, and the optimal conditions yield a superior surface precision compared to the initial trials. |
SWOT analysis on machinability of injection mould materials’ milling.
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SWOT analysis on machinability of injection mould materials’ turning.
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SWOT analysis on machinability of injection mould materials’ drilling.
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SWOT analysis on machinability of injection mould materials’ surface polishing.
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SWOT analysis on machinability of injection mould materials’ EDM.
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SWOT analysis on machinability of injection mould materials’ LBD.
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Abstract
Injection moulds are crucial to produce plastic and lightweight metal components. One primary associated challenge is that these may suffer from different types of failures, such as wear and/or cracking, due to the extreme temperatures (T), thermal cycles, and pressures involved in the production process. According to the intended geometry and respective needs, mould manufacturing can be performed with conventional or non-conventional processes. This work focuses on three foremost alloys: AMPCO® (CuBe alloy), INVAR-36® (Fe-Ni alloys, Fe-Ni36), and heat-treated (HT) steels. An insight into the manufacturing processes’ limitations of these kinds of materials will be made, and solutions for more effective machining will be presented by reviewing other published works from the last decade. The main objective is to provide a concise and comprehensive review of the most recent investigations of these alloys’ manufacturing processes and present the machinability challenges from other authors, discovering the prospects for future work and contributing to the endeavours of the injection mould industry. This review highlighted the imperative for more extensive research and development in targeted domains.
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1 CIDEM, ISEP, Polytechnic of Porto, Rua Dr. António Bernardino de Almeida, 4249-015 Porto, Portugal;
2 CIDEM, ISEP, Polytechnic of Porto, Rua Dr. António Bernardino de Almeida, 4249-015 Porto, Portugal;
3 CIDEM, ISEP, Polytechnic of Porto, Rua Dr. António Bernardino de Almeida, 4249-015 Porto, Portugal;
4 LAETA-INEGI, Associate Laboratory for Energy, Transports and Aerospace, Rua Dr. Roberto Frias 400, 4200-465 Porto, Portugal;
5 Department of Mechanical Engineering, Faculty of Engineering, University of Porto, Rua Dr. Roberto Frias 400, 4200-465 Porto, Portugal;