Machinability Analysis and ANFIS modelling on Advanced Machining of Hybrid Metal Matrix Composites for Aerospace Applications

Manikandan, N.; Balasubramanian, K.; Palanisamy, D.; Gopal, P. M.; Arulkirubakaran, D.; Binoj, J. S.

doi:10.1080/10426914.2019.1689264

Cited by 54 publications

(7 citation statements)

References 25 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…For a cryogenically treated stainless steel insert with other inserts, a relationship between input parameters (feed, DoC, speed) and output parameters (roughness of surface and force of cutting) was established using the ANFIS tool. It was discovered that the predicted results are very close to the experimental data [13]. Studying the impact of various turning factors on the material removing rate and surface roughness of stainless steel 202 revealed that the ANFIS model accurately predicts the output value to within 98 percent of the actual value.…”

Section: Introductionmentioning

confidence: 52%

Optimization of Surface Roughness: Effect of Machining Parameters on EN23

Barnwal¹,

Mishra

Prasad

2022

Advances in Transdisciplinary Engineering

View full text Add to dashboard Cite

EN23 is one of the most commonly used materials to fabricate forging die in Indian industries. The dies are manufactured through machining process and the parameters of the machining process have considerable impact on the roughness value of the material’s surface. While forging, it was found that die life varies with the change in the machining parametric value and this took my interest to investigate the area. Speed in rpm, feed in mm/rev, and depth of cut in mm were chosen as the process parameters for the investigation of the machining. Design of experiment was used to know the number of specimens required for proper investigation. Specimens were prepared using a L9 orthogonal array and a full factorial design. The optimal machining parameters were obtained using the Taguchi method. The optimal surface roughness value acquired using the L9 orthogonal array is fairly similar to the value obtained using the full factorial technique, according to a comparison of the results. Additionally, a mathematical tool called ANFIS was used to simulate the optimization process and anticipate the surface roughness values.

show abstract

Section: Introductionmentioning

confidence: 52%

Optimization of Surface Roughness: Effect of Machining Parameters on EN23

Barnwal¹,

Mishra

Prasad

2022

Advances in Transdisciplinary Engineering

View full text Add to dashboard Cite

show abstract

“…Triplane (Three wings) Some of the advanced materials used in aircraft wing construction is advanced lightweight aluminum alloys and composite materials. 50 Depending upon the vertical location and wing position to the fuselage centreline, it is of four types namely, parasol wing, mid-wing, high wing, and low wing. The wing location plays a major role in aircraft design including tail design, the center of gravity, and landing gear design.…”

Section: High and Low Wingsmentioning

confidence: 99%

“… Monoplane (One wing) Biplane (Two wings) Triplane (Three wings) Some of the advanced materials used in aircraft wing construction is advanced lightweight aluminum alloys and composite materials. 50…”

Section: Aluminium Alloys In Aerospace Applicationsmentioning

confidence: 99%

Metal additive manufacturing of commercial aerospace components – A comprehensive review

Rajyalakshmi

Munusamy

Vignesh

et al. 2022

Proceedings of the Institution of Mechanical Engineers, Part E:

View full text Add to dashboard Cite

Metal additive manufacturing (AM) has matured and grown from its infancy in the research stage to the fabrication of new and advanced components for its supreme applications. AM is a lead for the advanced manufacturing processes with an increased and advanced potential to revolutionize the manufacturing domain. It could exhibit a progressive change in the project and design paradigms. In the past decade, the use of metal AM process in the aerospace industry to build, repair various components for military applications and several outer space vehicle fabrications have occupied higher potential among various other manufacturing industries. In addition to it, many studies have made it a more versatile, common, and safer technology for the design and fabrication of components with the introduction of novel processes, materials, technologies, cost efficiency, and process design. In the present review article, the use of advanced aluminum alloys in the AM of fuselage, horizontal stabilizer, and high and low wings has gained increased advantages in the aerospace industry. Various components of wings and fuselage with its merits and demerits in AM processing are discussed. The outstanding issues in AM process and steps to overcome with post-processing techniques are elaborated. Finally, the future scope and research directions of the AM process involved in the fabrication of selected components are discussed.

show abstract

“…MMCs with various matrix metals, such as copper, aluminum, nickel, and iron, are reinforced with various ceramics particles, such as MgO, TiC, Al 2 O 3, and SiC, to increase strength through multiple strengthening mechanisms at room temperature. These include the fabrication of thermal dislocations due to a mismatch in the composite thermal expansion coefficients and the addition of refinement crystallite to the matrix microstructure [1][2][3].…”

Section: Introductionmentioning

confidence: 99%

Effects of Mg and MgO Nanoparticles on Microstructural and Mechanical Properties of Aluminum Matrix Composite Prepared via Mechanical Alloying

Abuchenari

Khozani

2021

jcc

View full text Add to dashboard Cite

Aluminum-based composites reinforced with ceramic particles have been used for many applications because of their high hardness, good wear resistance, low weight, and low thermal expansion coefficient. The Al-MgO/Mg composite was prepared in the present study. The effects of milling time and amounts of initial Mg and MgO were studied on the properties of the composite. The milled powder mixtures were subsequently analyzed by the XRD and SEM tests. Crystal sizes and internal strains were calculated using XRD data and the Williamson-Hall equation. The hardness of samples was measured by the Vickers method. The results showed that the lattice parameter significantly increased by increasing the amount of Mg. During the milling, the crystallite size, and simultaneously internal strain and hardness increased by increasing amounts of Mg and MgO. The results also showed that the effects of Mg on the composite properties were higher than MgO particles.

show abstract

Machinability Analysis and ANFIS modelling on Advanced Machining of Hybrid Metal Matrix Composites for Aerospace Applications

Cited by 54 publications

References 25 publications

Optimization of Surface Roughness: Effect of Machining Parameters on EN23

Optimization of Surface Roughness: Effect of Machining Parameters on EN23

Metal additive manufacturing of commercial aerospace components – A comprehensive review

Effects of Mg and MgO Nanoparticles on Microstructural and Mechanical Properties of Aluminum Matrix Composite Prepared via Mechanical Alloying

Contact Info

Product

Resources

About