Abstract:In this paper, a state-of-the-art review on cutting tool technology in machining of Ni-based superalloys is presented to better understand the current status and to identify future directions of research and development of cutting tool technologies. First, past review articles related to the machining of Ni-based superalloys are summarized. Then machinability of superalloys is introduced, together with the reported methods used in cutting tool design. The current researches on cutting tools in the machining of… Show more
“…Here, as the nickel content, which is the main element of nickel-based superalloys, the cutting temperature rises and the notch wear increases as the hardness increases, as shown in Figure 6. The chemical structure of superalloys should be related to hardness while deciding machining conditions [41], [42]. The hardness of Ni and Ti alloys rises considerably with heat treatment, so they are also called age hardening.…”
Section: Machinability Of Titanium Alloys and Nickel Based Superalloys (Ti̇tanyum Alaşimlari Ve Ni̇kel Esasli Süperalaşimlarin İşlenebi̇mentioning
confidence: 99%
“…Figure 6. Machinability of superalloys (Süperalaşımların işlenebilirliği) [42] Titanium alloys cover 30% of engine mass in the field of commercial and 40% in military [46]. The use of this material will increase with processing techniques that reduce faults that are harmful to the effective operation of the engine by early collapse of the relevant parts.…”
Section: Machinability Of Titanium Alloys and Nickel Based Superalloys (Ti̇tanyum Alaşimlari Ve Ni̇kel Esasli Süperalaşimlarin İşlenebi̇mentioning
Superalloys are a group of materials that are commonly used in aerospace applications and are also called high temperature materials, as they have superior wear and corrosion resistance. Ni-based superalloys are used more often than Ti alloys in the aerospace industry as they have mechanical and physical properties such as superior temperature resistance and toughness, high corrosion resistance, excellent fatigue and creep resistance. Ti alloys, on the other hand, have the highest strength / weight ratio among metals, increasing their preference in these industries continuously. Casting, forging, powder metallurgy and machining methods are used in the process of shaping machine parts used in the aviation industry from superalloys. However, many components are mostly manufactured using machining methods due to the part geometry, desired size and surface quality requirements. In this context, in the production of parts from Ti alloys and Ni-based superalloys, which are difficult to process, the correct selection or optimization of processing parameters is very important in terms of minimization of processing costs and therefore sustainable manufacturing. In this study, factors such as cutting tool quality and cooling/lubrication technology were evaluated for criteria such as tool life, surface integrity and cutting forces, which have an important place in the machinability of titanium and nickel-based superalloys.
“…Here, as the nickel content, which is the main element of nickel-based superalloys, the cutting temperature rises and the notch wear increases as the hardness increases, as shown in Figure 6. The chemical structure of superalloys should be related to hardness while deciding machining conditions [41], [42]. The hardness of Ni and Ti alloys rises considerably with heat treatment, so they are also called age hardening.…”
Section: Machinability Of Titanium Alloys and Nickel Based Superalloys (Ti̇tanyum Alaşimlari Ve Ni̇kel Esasli Süperalaşimlarin İşlenebi̇mentioning
confidence: 99%
“…Figure 6. Machinability of superalloys (Süperalaşımların işlenebilirliği) [42] Titanium alloys cover 30% of engine mass in the field of commercial and 40% in military [46]. The use of this material will increase with processing techniques that reduce faults that are harmful to the effective operation of the engine by early collapse of the relevant parts.…”
Section: Machinability Of Titanium Alloys and Nickel Based Superalloys (Ti̇tanyum Alaşimlari Ve Ni̇kel Esasli Süperalaşimlarin İşlenebi̇mentioning
Superalloys are a group of materials that are commonly used in aerospace applications and are also called high temperature materials, as they have superior wear and corrosion resistance. Ni-based superalloys are used more often than Ti alloys in the aerospace industry as they have mechanical and physical properties such as superior temperature resistance and toughness, high corrosion resistance, excellent fatigue and creep resistance. Ti alloys, on the other hand, have the highest strength / weight ratio among metals, increasing their preference in these industries continuously. Casting, forging, powder metallurgy and machining methods are used in the process of shaping machine parts used in the aviation industry from superalloys. However, many components are mostly manufactured using machining methods due to the part geometry, desired size and surface quality requirements. In this context, in the production of parts from Ti alloys and Ni-based superalloys, which are difficult to process, the correct selection or optimization of processing parameters is very important in terms of minimization of processing costs and therefore sustainable manufacturing. In this study, factors such as cutting tool quality and cooling/lubrication technology were evaluated for criteria such as tool life, surface integrity and cutting forces, which have an important place in the machinability of titanium and nickel-based superalloys.
“…Zagadnienia te są przedmiotem zainteresowania światowej nauki i poświęcono im wiele świetnych przeglądów literatury, np. [1][2][3][4][5][6]. Tu zostaną omówione jedynie najnowsze osiągnięcia w technikach chłodzenia przy obróbce superstopów -z lat 2018-2020.…”
The paper presents an update of the recent literature on advances in cooling techniques for machining of difficult to machine materials such as nickel and titanium-based alloys used in aero-engine and aerostructure applications. The review covers: cryogenic machining, minimum quantity lubrication, the combination of MQL and cryogenic cooling, and high-pressure lubricoolant supply. Examples of applications in industrial processes are also given.
“…Y i =1*a 0 + x i a 1 + u i a 2 + w i a 3 +e i (2) where 1 is the error, a 0 is the constant for temperature; , , represent speed, feed, depth of cut, and a1, a2, and a3 are the coefficients for speed, feed, and depth of cut, respectively. Further, Eq.…”
Section: Y= a 0 + A 1 X+a 2 U+a 3 Wmentioning
confidence: 99%
“…The parameter is based on the ease with which material can be machined with an acceptable surface finish [1]. Machinability can be estimated in terms of characteristics like tool wear, chip formation, and surface finish [2] (see Figure 1). Nickel alloys are known for hard-to-machine materials, have tremendous applications in the areas of aerospace, marine, and biomedical parts because of their favourable properties such as corrosion resistance, good strength, along with superior thermal fatigue.…”
Machinability of any material is defined as how easily it can be machined (cut) and the factors that govern this machinability comprise machining temperature, tool wear, surface roughness, and the shape of the chip. To enhance the machinability of materials, the improvement of these governing factors is a must. In this regards machinability of Nickel alloys is of great concern as they are associated with problems of high heat generation causing tool wear and poor surface finishing, which adds to the product cost. Therefore, this research aims to improve the machinability of Inconel 625 with the use of MQL assisted with h-BN nano cutting fluid. A comparative study of machining performance of h-BN NMQL with dry and MQL conventional conditions is performed. The outcomes of this study establish the superiority of h-BN over dry machining and MQL conventional machining on various machining parameters by reducing both machining temperature and tool wear. The experimental results revealed that the machining with nano h-BN MQL technique reduces the machining tool tip temperature by 25% and 12%, along with the reduction in tool wear by 67% and 47% in comparison with dry and MQL machining. Additionally, this paper also proposes a numerical model for predicting machining tool temperature using machining parameters (speed, feed and depth of cut) during turning of Inconel 625 under nano h-BN MQL technique.
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