Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/3787
Full metadata record
DC FieldValueLanguage
dc.contributor.authorBehera, Ajit-
dc.contributor.authorMallick, Priyabrata-
dc.date.accessioned2022-12-08T05:38:53Z-
dc.date.available2022-12-08T05:38:53Z-
dc.date.issued2022-11-
dc.identifier.citation76th Annual Technical Meeting of the Indian Institute of Metals, Hyderabad,13-16 November 2022en_US
dc.identifier.urihttp://hdl.handle.net/2080/3787-
dc.descriptionCopyright belongs to proceeding publisheren_US
dc.description.abstractAdditive Manufacturing has proven to be a demanding technique in a wide range for the aero-vehicle industries. This investigation focused on the evolution of aero-turbine blades from conventional manufacturing technique to the additive manufacturing technique. Additive Manufacturing is known as rapid prototyping or 3-D printing technique involving layer-by-layer construction process that can develop a turbine blade with a wide range of parameters to design the turbine blade and reduce cost and weight compared to the conventional production processes. This presentation discusses various additive manufacturing techniques suitable for manufacturing high-temperature turbine blades, such as selective laser melting, selective laser sintering, electron beam melting, laser engineering network form, and electron beam fabrication free form. The associated parameter of AM such as particle size and shape, powder bed density, residual stresses, porosity, and roughness are discussed here.en_US
dc.subjectAdditive Manufacturingen_US
dc.subjectTurbine bladeen_US
dc.subjectDesigningen_US
dc.subjectPorosityen_US
dc.subjectDensityen_US
dc.titleAdditive Manufactured Aero-turbine Bladeen_US
dc.typePresentationen_US
Appears in Collections:Conference Papers

Files in This Item:
File Description SizeFormat 
2022_NMD-ATM_ABehera_Additive.pdf1.29 MBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.