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RELATING MICROSTRUCTURE TO PROCESS VARIABLES IN BEAM-BASED ADDITIVE MANUFACTURING OF INCONEL 718Thompson, John Ryan 04 June 2014 (has links)
No description available.
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Heat Affected Zone Cracking of Allvac 718Plus Superalloy during High Power Beam Welding and Post-weld Heat TreatmentIdowu, Oluwaseun Ayodeji 08 April 2010 (has links)
The present dissertation reports the findings of a study of cracking behavior of a newly developed superalloy, Allvac 718Plus during high power beam welding and post-weld heat treatment. Microstructures of the base alloy, heat affected zone (HAZ) and fusion zone (FZ) of welded and post-weld heat treated (PWHT) coupons were examined by the use of standard metallographic techniques involving optical microscopy, analytical scanning electron microscopy (SEM) and analytical transmission electron microscopy. Moreover, grain boundary segregation behavior of boron atoms during pre-weld heat treatments was evaluated using secondary ion mass spectroscopic system.
In the first phase of the research, 718Plus was welded using a low and high heat input CO2 laser to assess its weld cracking response. Detailed examination of the welds by analytical electron microscopic technique revealed the occurrence of cracking in the HAZ of low heat input welds, while their FZ was crack free. However, both the FZ and HAZ of high heat input welds were crack-free. Resolidified constituents were observed along the cracked grain boundaries of the lower heat input welds, which indicated that HAZ cracking in this newly developed superalloy was associated with grain boundary liquation. However, despite a more extensive liquation of grain boundaries and grain interior in the HAZ of high heat input welds, no cracking occurred. This was attributed to the combination of lower welding stresses generated during cooling, and relaxation of these stresses by thick intergranular liquid.
Although HAZ cracking was prevented by welding with a high heat input laser, it resulted in a significant damage to the parent microstructure through its extensive liquation. Thus, the use of low heat input welding is desirable. However, this resulted in HAZ cracking which needs to be minimized or eliminated. Therefore, during the second phase of this research, the effects of pre-weld thermal processing on the cracking response of 718Plus were investigated. Results from the quantification of the cracking of the alloy showed that HAZ cracking may be significantly reduced or eliminated through an adequate selection of pre-weld thermal cycle.
In the third stage of this research, crack-free welds of 718Plus were post-weld heat treated using standard thermal schedules. A significant solid state cracking of the alloy occurred during the PWHT. The cracking was attributed to the presence of embrittling phases on HAZ grain boundaries, coupled with aging contraction stresses that are generated by a considerable precipitation of gamma prime phase during aging.
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Heat Affected Zone Cracking of Allvac 718Plus Superalloy during High Power Beam Welding and Post-weld Heat TreatmentIdowu, Oluwaseun Ayodeji 08 April 2010 (has links)
The present dissertation reports the findings of a study of cracking behavior of a newly developed superalloy, Allvac 718Plus during high power beam welding and post-weld heat treatment. Microstructures of the base alloy, heat affected zone (HAZ) and fusion zone (FZ) of welded and post-weld heat treated (PWHT) coupons were examined by the use of standard metallographic techniques involving optical microscopy, analytical scanning electron microscopy (SEM) and analytical transmission electron microscopy. Moreover, grain boundary segregation behavior of boron atoms during pre-weld heat treatments was evaluated using secondary ion mass spectroscopic system.
In the first phase of the research, 718Plus was welded using a low and high heat input CO2 laser to assess its weld cracking response. Detailed examination of the welds by analytical electron microscopic technique revealed the occurrence of cracking in the HAZ of low heat input welds, while their FZ was crack free. However, both the FZ and HAZ of high heat input welds were crack-free. Resolidified constituents were observed along the cracked grain boundaries of the lower heat input welds, which indicated that HAZ cracking in this newly developed superalloy was associated with grain boundary liquation. However, despite a more extensive liquation of grain boundaries and grain interior in the HAZ of high heat input welds, no cracking occurred. This was attributed to the combination of lower welding stresses generated during cooling, and relaxation of these stresses by thick intergranular liquid.
Although HAZ cracking was prevented by welding with a high heat input laser, it resulted in a significant damage to the parent microstructure through its extensive liquation. Thus, the use of low heat input welding is desirable. However, this resulted in HAZ cracking which needs to be minimized or eliminated. Therefore, during the second phase of this research, the effects of pre-weld thermal processing on the cracking response of 718Plus were investigated. Results from the quantification of the cracking of the alloy showed that HAZ cracking may be significantly reduced or eliminated through an adequate selection of pre-weld thermal cycle.
In the third stage of this research, crack-free welds of 718Plus were post-weld heat treated using standard thermal schedules. A significant solid state cracking of the alloy occurred during the PWHT. The cracking was attributed to the presence of embrittling phases on HAZ grain boundaries, coupled with aging contraction stresses that are generated by a considerable precipitation of gamma prime phase during aging.
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Design of cemented carbide with Ni-based superalloy binder strengthened with y’-Ni3Al precipitatesEdholm, Oscar January 2018 (has links)
Replacement of cobalt in cemented carbides has gained in attention recently because threats of regulations due to health issues (cancerogenic effect), increased demand from the electric vehicle industry and the questionable extraction from countries like Democratic Republic of Congo. In this report the use of Ni-based binder as an alternative binder for cemented carbides has been explored. The design is based on producing a Ni-based superalloy binder which contains dispersed Ni3Al Gamma Prime (γ’) -phase precipitates in the binder matrix. The investigation focuses on the design of cemented carbide compositions and processes that ensures the formation of γ’- precipitates, the control of their morphology and distribution as well as the effect of heat treatment. To do this a Ni-Al master alloy has been designed that enables the formation of γ’-precipitates in WC-Ni-Al-X systems, produced by conventional powder metallurgy process including standard free sintering. Furthermore, the addition of usual elements in the cemented carbide industry (such as Ti, Cr, Ta, Nb) and their effect on the stability of γ’-precipitates has been investigated. A method to reveal the precipitates including ion-polishing and electro-etching has been developed. Basic mechanical properties such as hardness and toughness have been investigated, revealing particular crack propagation in Ni-based binder reinforced with γ’-precipitates. It was found that the common variables in cemented carbide manufacturing influence all aspects regarding the stability of γ’-phase. By varying the powder type, binder composition and content, the carbon balance, the WC grain size and the heating/cooling steps; the formation of γ’-precipitates (size, morphology, distribution, etc.) can be controlled to tailor the properties of the cemented carbide. / Att hitta en ersättning av kobolt i hårdmetall har nyligen uppmärksammats bl.a. eftersom regleringar hotar användning av ämnet pga. dess cancerogenitet, en ökande efterfrågan från elfordonsindustrin samt den moraliskt tvivelaktiga utvinningen som sker i länder som Demokratiska Republiken Kongo. I denna rapport har användningen av ett nickel-baserat bindemedel som ett alternativt bindemedel för hårdmetaller undersökts. Designen är baserad på att producera en nickel-baserad superlegering som bindemedel som innehåller dispergerad Ni3Al Gamma Prim (γ’) – fas utfälld i bindemedlet. Utredningen fokuserar på designen av hårdmetallskompositioner och processer som försäkrar formationen av γ’-utfällningar, kontroller av dess morfologi, distributionen samt hur värmebehandlingar påverkar. För att kunna göra detta har en Ni-Al masterlegering skapats som möjliggör γ’-utfällningar i ett WC-Ni-Al-X system, producerat med konventionell pulvermetallurgiprocess inkluderat standard fri sintring. Dessutom har tillsatsen av vanliga ämnen i hårdmetallindustrin (such as TI, Cr, Ta, Nb) samt deras effekt på stabiliteten hos γ’-utfällningarna undersökts. En metod för att upptäcka utfällningarna, som inkluderar jonpolering och elektroetsning har utvecklats. Grundläggande mekaniska egenskaper som hårdhet och seghet har undersökts, vilket har avslöjat en speciell sprickutbredning i den nickelbaserade bindaren förstärkt med γ’-utfällningar. Det visade sig att de vanliga variablerna förenade med tillverkning av hårdmetall påverkar samtliga aspekter gällande stabiliteten hos γ’-utfällningar. Genom att variera pulvertyp, bindemedelkomposition och innehåll, kolbalansen, WC-kornstorlek och uppvärmning samt kylningssteg så påverkas bildningen av γ’-utfällningar (storlek, morfologi, distribution, etc..) som kan kontrolleras för att skräddarsy egenskaperna för hårdmetallen.
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