2019
DOI: 10.1016/j.apsusc.2019.04.070
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Bonding temperature effects on the wide gap transient liquid phase bonding of Inconel 718 using BNi-2 paste filler metal

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Cited by 20 publications
(2 citation statements)
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“…With the rapid development of current technology, the maintenance of turbine blades is becoming more and more rigorous [ 12 ]. As a result, relatively large cracks or worn areas (>1.5 mm) are discovered in aerospace components, where the narrow gap TLP bonding technique would be inadequate [ 13 ]. For wide-gap brazing, the selection and design of the filler metal composition is the key factor to improve the brazing performance [ 14 , 15 , 16 , 17 , 18 , 19 ].…”
Section: Introductionmentioning
confidence: 99%
“…With the rapid development of current technology, the maintenance of turbine blades is becoming more and more rigorous [ 12 ]. As a result, relatively large cracks or worn areas (>1.5 mm) are discovered in aerospace components, where the narrow gap TLP bonding technique would be inadequate [ 13 ]. For wide-gap brazing, the selection and design of the filler metal composition is the key factor to improve the brazing performance [ 14 , 15 , 16 , 17 , 18 , 19 ].…”
Section: Introductionmentioning
confidence: 99%
“…However, the inclusion of melting point depressants (MPDs), such as boron, silicon, and phosphorus, in the nickelbased filler alloy can lead to the formation of eutectic phases like borides, silicides, and phosphides during the cooling stage, adversely affecting the mechanical properties of brazed joints. [9][10][11][12][13] To address this issue, transient liquid phase (TLP) bonding, also known as diffusion brazing, emerges as an effective method. TLP bonding involves three distinct stages: base metal dissolution, isothermal solidification, and solid-state homogenization.…”
mentioning
confidence: 99%