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Transformation Induced Plasticity in a High Entropy Alloy, Reusing Powder in Laser Powder Bed Fusion of Inconel 718, and Geometric Factor in Fracture Toughness of Nano-Layered Composites.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Transformation Induced Plasticity in a High Entropy Alloy, Reusing Powder in Laser Powder Bed Fusion of Inconel 718, and Geometric Factor in Fracture Toughness of Nano-Layered Composites./
作者:	Bhowmik, Shubhrodev.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2021,
面頁冊數:	141 p.
附註:	Source: Masters Abstracts International, Volume: 83-04.
Contained By:	Masters Abstracts International83-04.
標題:	Materials science. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28715728
ISBN:	9798460435449

Transformation Induced Plasticity in a High Entropy Alloy, Reusing Powder in Laser Powder Bed Fusion of Inconel 718, and Geometric Factor in Fracture Toughness of Nano-Layered Composites.
Bhowmik, Shubhrodev.

Transformation Induced Plasticity in a High Entropy Alloy, Reusing Powder in Laser Powder Bed Fusion of Inconel 718, and Geometric Factor in Fracture Toughness of Nano-Layered Composites. - Ann Arbor : ProQuest Dissertations & Theses, 2021 - 141 p.

Source: Masters Abstracts International, Volume: 83-04.

Thesis (M.S.)--University of New Hampshire, 2021.

This item must not be sold to any third party vendors.

This research explores the effects of processing history and compressive strain on a microstructurally flexible high entropy alloy (HEA), Fe42Mn28Co10Cr15Si5 (in at%) - named DP-5Si-HEA. The material was characterized by electron backscatter diffraction (EBSD), scanning electron microscopy (SEM), and neutron diffraction. The as-rolled material had metastable gamma austenite (γ), stable sigma (σ), and stable epsilon martensite (ε) phases at room temperature. Friction stirrer processing (FSP) at different tool speeds changed the microstructure by decreasing the grain size and varying the phase fractions because of the low stacking fault energy of the chosen HEA. The HEA exhibited peak ultimate tensile strength of ~1850 MPa because of refined microstructure, transformation induced plasticity (TRIP) because of γ→ε phase transformation, and transformation-induced Hall-Petch-type barrier effect. Furthermore, an investigation on the effect of reusing powder on compressive, tensile, and creep properties of Inconel 718 (IN 718) fabricated by laser powder bed fusion (LPBF) was carried out. To achieve that, room, and high temperature (6000C, 6500C,7000C, 7500C) tensile tests, room temperature compression tests, and high temperature (5500C, 6500C, 7000C) tensile creep tests for samples prepared by both virgin as well as a reused powder in LPBF were performed. The study showed the reused powder had higher strength at room and high-temperature tensile tests except for 6500C. The virgin powder lasted longer at 550C and 650C creep tests, but the reused powder lasted longer at 700C. It was concluded in this study that the parts made by virgin powder samples should be used for temperatures at creep conditions until 650C for real-life applications. Moreover, finite element analyses were carried out on micro single edge notched bend (MSENB) specimens to obtain fracture toughness of Cu/TiN and Al/TiN nanocomposites within the realm of Linear Elastic Fracture Mechanics. The shape function or geometric factor was first calculated by considering the effects of the geometry, the cono-spherical indenter stress field, and the phase interface shielding/anti-shielding on the crack tip driving force. It was found that adding either Al or Cu nanolayers to TiN nanolayers did not weaken or significantly improve fracture toughness relative to the single TiN thin film. Based on the results, some recommendations were also made for future experiments.

ISBN: 9798460435449Subjects--Topical Terms:

543314
Materials science.
Subjects--Index Terms:

Plasticity

Transformation Induced Plasticity in a High Entropy Alloy, Reusing Powder in Laser Powder Bed Fusion of Inconel 718, and Geometric Factor in Fracture Toughness of Nano-Layered Composites.
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300 $a 141 p.
500 $a Source: Masters Abstracts International, Volume: 83-04.
500 $a Advisor: Knzevic, Marko.
502 $a Thesis (M.S.)--University of New Hampshire, 2021.
506 $a This item must not be sold to any third party vendors.
520 $a This research explores the effects of processing history and compressive strain on a microstructurally flexible high entropy alloy (HEA), Fe42Mn28Co10Cr15Si5 (in at%) - named DP-5Si-HEA. The material was characterized by electron backscatter diffraction (EBSD), scanning electron microscopy (SEM), and neutron diffraction. The as-rolled material had metastable gamma austenite (γ), stable sigma (σ), and stable epsilon martensite (ε) phases at room temperature. Friction stirrer processing (FSP) at different tool speeds changed the microstructure by decreasing the grain size and varying the phase fractions because of the low stacking fault energy of the chosen HEA. The HEA exhibited peak ultimate tensile strength of ~1850 MPa because of refined microstructure, transformation induced plasticity (TRIP) because of γ→ε phase transformation, and transformation-induced Hall-Petch-type barrier effect. Furthermore, an investigation on the effect of reusing powder on compressive, tensile, and creep properties of Inconel 718 (IN 718) fabricated by laser powder bed fusion (LPBF) was carried out. To achieve that, room, and high temperature (6000C, 6500C,7000C, 7500C) tensile tests, room temperature compression tests, and high temperature (5500C, 6500C, 7000C) tensile creep tests for samples prepared by both virgin as well as a reused powder in LPBF were performed. The study showed the reused powder had higher strength at room and high-temperature tensile tests except for 6500C. The virgin powder lasted longer at 550C and 650C creep tests, but the reused powder lasted longer at 700C. It was concluded in this study that the parts made by virgin powder samples should be used for temperatures at creep conditions until 650C for real-life applications. Moreover, finite element analyses were carried out on micro single edge notched bend (MSENB) specimens to obtain fracture toughness of Cu/TiN and Al/TiN nanocomposites within the realm of Linear Elastic Fracture Mechanics. The shape function or geometric factor was first calculated by considering the effects of the geometry, the cono-spherical indenter stress field, and the phase interface shielding/anti-shielding on the crack tip driving force. It was found that adding either Al or Cu nanolayers to TiN nanolayers did not weaken or significantly improve fracture toughness relative to the single TiN thin film. Based on the results, some recommendations were also made for future experiments.
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653 $a Plasticity
653 $a High entropy alloy
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653 $a Inconel 718
653 $a Geometric factor
653 $a Fracture toughness
653 $a Nano-layered composites
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