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Journal ArticleDOI

Effect of Bonding Time on Dissimilar Transient Liquid Phase (TLP) Bonding of IN939 to IN625 Superalloys: Microstructural Characterization and Mechanical Properties

TLDR
In this article, the microstructure and mechanical properties of transient liquid phase (TLP) bonded joints between dissimilar precipitation hardened IN939 and solid solution hardened IN625 with a Ni-Cr-Si-Fe-B filler alloy were studied.
Abstract
The microstructure and mechanical properties of transient liquid phase (TLP) bonded joints between dissimilar precipitation hardened IN939 and solid solution hardened IN625 with a Ni-Cr-Si-Fe-B filler alloy were studied. The TLP bonding was conducted in different bonding times (i.e., 15, 25, 35, 45, 60, and 90 minutes). Different phases, formed in the isothermally solidified zone (ISZ), on-cooling solidified zone, and diffusion affected zone (DAZ), were characterized using EDS, XRD, and EPMA analyses. A Ni-rich γ solid solution, CrB, and Ni3B were detected in the centerline of samples with incomplete isothermal solidification (i.e., 15 and 25 minutes), formed by binary and ternary eutectic reactions. Raising the time of bonding boosted isothermal solidification, resulting in a joint without deleterious eutectic microconstituents in bonding times of 35 minutes and higher. Chromium-rich borides were discovered in the DAZ of IN939, while the IN625-DAZ side was composed of chromium-molybdenum-rich borides. The concentration of alloying elements in the ISZ experienced an increment by further raising the bonding time to 90 minutes, creating a more homogenous bond with increased ISZ microhardness and mechanical properties. The highest shear strength (~ 92 and ~ 77 Pct that of the IN939 and IN625, respectively) and failure energy were attained for the 90-minutes sample. The fracture mechanism was also switched from a brittle semi-cleave morphology to a more ductile dimple-like morphology by increasing the bonding time from 15- to 90-minutes.

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Citations
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Journal ArticleDOI

Induction Brazing for Rapid Localized Repair of Inconel 718

TL;DR: In this article, a rapid brazing technique using induction coil was studied to evaluate its suitability for localized repair of Inconel 718, which was carried out using AMS 4777 Brazing paste at different temperatures (950 °C, 1050 °C and 1150 °C ) for various durations.
Journal ArticleDOI

Effect of diffusion brazing time on microstructure, isothermal solidification completion and microhardness distribution during joining of Nicrofer 5520 superalloy using a liquated Ni-Cr-B interlayer

TL;DR: In this paper , the effect of time on the microstructural evolution, distribution of elements, type of precipitated phases, and microhardness of diffusion brazed Nicrofer 5520 superalloy using a BNi-9 (Ni-15%Cr-3.7%B) interlayer was investigated.
Journal ArticleDOI

Effect of temperature on tensile behavior, fracture morphology, and deformation mechanisms of Nickel-based additive manufacturing 939 superalloy

TL;DR: In this paper , the deformation mechanism at room temperature is mainly controlled by a single slip system and as temperature rises to the intermediate temperature region, more slip systems are activated by thermal energy, which promotes the movement of dislocations.
Journal ArticleDOI

High temperature shear and thermal aging behavior of dissimilar transient liquid phase bonded Hastelloy X to Ni3Al intermetallic compound

TL;DR: In this paper , the authors investigated the thermal aging behavior of the transient liquid phase (TLP) bonds between Hastelloy X to Ni3Al IMC at temperature range of 800-900 °C.
Journal ArticleDOI

Diffusion brazing of GH536 polycrystalline superalloy with IC10 single crystal superalloy using BNi-2 interlayer

TL;DR: In this article , the effects of bonding temperature and time on the microstructure evolution and mechanical properties of the GH536/IC10 joints were investigated in detail, where the IC10 single crystal superalloy to GH536 polycrystalline super alloy was diffusion brazed using a BNi-2 filler alloy.
References
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Journal ArticleDOI

Microstructure and mechanical properties of Inconel 625 superalloy

TL;DR: In this article, the service-exposed Alloy 625 ammonia cracker tubes showed higher strength and lower ductility compared to the virgin material in the solution annealed state, and the dissolution of the Ni2(Cr,Mo)-phase exhibited significant influence upon yield strength (YS) but negligible effect on ductility.
Book

Introduction to Aerospace Materials

TL;DR: In this article, the main structural and engine materials used in aircraft, helicopters, and spacecraft in terms of their production, properties, performance, and applications are reviewed, focusing on recent developments and requirements.
Journal ArticleDOI

Inconel 625 lattice structures manufactured by selective laser melting (SLM): Mechanical properties, deformation and failure modes

TL;DR: In this article, the mechanical response of Inconel 625 lattice structures fabricated by Selective Laser Melting (SLM) has been investigated and the high ductility of the lattice enables novel insight into the structural mechanics of AM lattice and the associated deformation photography provides a reference for the validation and verification of numerical models of lattice behaviour.
Journal ArticleDOI

Effect of bonding temperature on microstructure development during TLP bonding of a nickel base superalloy

TL;DR: In this paper, the effect of bonding temperature on microstructure of a transient liquid phase (TLP)-bonded GTD-111 nickel base superalloy, using a Ni-Si-B interlayer, was investigated.
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