Utilize este identificador para referenciar este registo: https://hdl.handle.net/1822/91953

TítuloMulti-material Inconel 718 – Aluminium parts targeting aerospace applications: A suitable combination of low-weight and thermal properties
Autor(es)Marques, A.
Guimaraes, B.
Bartolomeu, Flávio
Miranda, G.
Silva, Filipe Samuel
Carvalho, O.
Palavras-chaveInconel 718
Aluminium
Hot pressing
Laser surface texturing
Aerospace applications
Rockets Weight reduction
Thermal conductivity
Data2023
EditoraElsevier
RevistaOptics and Laser Technology
CitaçãoMarques, A., Guimarães, B., Bartolomeu, F., Miranda, G., Silva, F. S., & Carvalho, O. (2023, February). Multi-material Inconel 718 – Aluminium parts targeting aerospace applications: A suitable combination of low-weight and thermal properties. Optics & Laser Technology. Elsevier BV. http://doi.org/10.1016/j.optlastec.2022.108913
Resumo(s)In this study, the combination of Inconel 718 (IN718) alloy, widely used in aerospace applications, and a highly conductive low-density Aluminium (Al) was hypothesized to achieve a disruptive solution with improved thermal conductivity and significantly lower weight, key aspects of aerospace industry. A multi-material IN718 - Al solution was designed and later fabricated by combining laser surface texturing and hot-pressing techniques. The multi-material IN718 - Al specimens were produced without significant defects and exhibited a significantly lower density than the IN718 bulk (<13 %), contributing to a weight decrease which can be considered strongly beneficial for improving energy efficiency of aerospace components. The Vickers' microhardness measurements were coherent results with literature and the interface between the two dissimilar materials exhibited a good metallurgical bonding with no significant diffusion of elements. The thermal conductivity of the multi-material IN718 - Al solution was 1.87 times higher than that of IN718 bulk. Multi-material IN718 - Al specimens have shown a high potential to decrease weight and enhance the thermal efficiency of an aerospace component.
TipoArtigo
URIhttps://hdl.handle.net/1822/91953
DOI10.1016/j.optlastec.2022.108913
ISSN0030-3992
Versão da editorahttps://www.sciencedirect.com/science/article/pii/S0030399222010593
Arbitragem científicayes
AcessoAcesso restrito UMinho
Aparece nas coleções:CMEMS - Artigos em revistas internacionais/Papers in international journals

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