Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal

Inconel 718 is a common material used in the aircraft industry such as in the turbine blades of an aircraft engine. They are subjected to extreme stresses constantly and therefore require regular maintenance for the engine to remain operational. Brazing is a repair process that fuses two metals by h...

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Main Author: Chan, Chee Choong
Other Authors: Tan Ming Jen
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/75727
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-757272023-03-04T19:28:48Z Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal Chan, Chee Choong Tan Ming Jen School of Mechanical and Aerospace Engineering DRNTU::Engineering::Materials::Testing of materials Inconel 718 is a common material used in the aircraft industry such as in the turbine blades of an aircraft engine. They are subjected to extreme stresses constantly and therefore require regular maintenance for the engine to remain operational. Brazing is a repair process that fuses two metals by heating and melting a brazing alloy that bonds to the two pieces of parent meterial and joins them. However, brazing also induces undesirable mechanical properties on the brazed joints due to the high temperature of the brazing process. Thus, post weld heat treatment (PWHT) is used to recover and sometimes improve its mechanical properties. The aim of the project is to determine the most effective PWHT by analysing the microstructure, hardness, tensile properties and fractography of the Inconel 718 brazed joints using the BNi-2 filler metal. Scanning electron microscope (SEM) and electron backscatter diffraction (EBSD) system were used to study the fracture surfaces and phase composition respectively. Specimens underwent a combination of solution heat treatment at 980°C for 1 hour as well as aging at 760°C for 4 hours followed by 660°C for 4 hours. The purpose of aging is to precipitate strengthening γ´ and γ´´ phases, while solution heat treatment dissolves detrimental δ phase. Joints that were brazed had a brazing gap above the maximum brazing clearance (MBC) and so they fail at the joint centreline due to the formation of brittle eutectic phases. Hardness generally increased from the base metal to the filler metal. The hardest and strongest brazed joint was the specimen which underwent the solution strengthening and aging process. Future research can include the analysis of more mechanical properties in the selection of the most effective PWHT. Bachelor of Engineering (Aerospace Engineering) 2018-06-11T08:43:12Z 2018-06-11T08:43:12Z 2018 Final Year Project (FYP) http://hdl.handle.net/10356/75727 en Nanyang Technological University 81 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Materials::Testing of materials
spellingShingle DRNTU::Engineering::Materials::Testing of materials
Chan, Chee Choong
Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
description Inconel 718 is a common material used in the aircraft industry such as in the turbine blades of an aircraft engine. They are subjected to extreme stresses constantly and therefore require regular maintenance for the engine to remain operational. Brazing is a repair process that fuses two metals by heating and melting a brazing alloy that bonds to the two pieces of parent meterial and joins them. However, brazing also induces undesirable mechanical properties on the brazed joints due to the high temperature of the brazing process. Thus, post weld heat treatment (PWHT) is used to recover and sometimes improve its mechanical properties. The aim of the project is to determine the most effective PWHT by analysing the microstructure, hardness, tensile properties and fractography of the Inconel 718 brazed joints using the BNi-2 filler metal. Scanning electron microscope (SEM) and electron backscatter diffraction (EBSD) system were used to study the fracture surfaces and phase composition respectively. Specimens underwent a combination of solution heat treatment at 980°C for 1 hour as well as aging at 760°C for 4 hours followed by 660°C for 4 hours. The purpose of aging is to precipitate strengthening γ´ and γ´´ phases, while solution heat treatment dissolves detrimental δ phase. Joints that were brazed had a brazing gap above the maximum brazing clearance (MBC) and so they fail at the joint centreline due to the formation of brittle eutectic phases. Hardness generally increased from the base metal to the filler metal. The hardest and strongest brazed joint was the specimen which underwent the solution strengthening and aging process. Future research can include the analysis of more mechanical properties in the selection of the most effective PWHT.
author2 Tan Ming Jen
author_facet Tan Ming Jen
Chan, Chee Choong
format Final Year Project
author Chan, Chee Choong
author_sort Chan, Chee Choong
title Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
title_short Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
title_full Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
title_fullStr Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
title_full_unstemmed Post-braze heat treatment of Inconel 718 alloy with BNi-2 filler metal
title_sort post-braze heat treatment of inconel 718 alloy with bni-2 filler metal
publishDate 2018
url http://hdl.handle.net/10356/75727
_version_ 1759855095357374464