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<metadata xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/"><dc:title>Incremental sheet forming of metal-based composites used in aviation and automotive applications</dc:title><dc:creator>Trzepieciński,	Tomasz	(Avtor)
	</dc:creator><dc:creator>Najm,	Sherwan Mohammed	(Avtor)
	</dc:creator><dc:creator>Pepelnjak,	Tomaž	(Avtor)
	</dc:creator><dc:creator>Bensaid,	Kamel	(Avtor)
	</dc:creator><dc:creator>Szpunar,	Marcin	(Avtor)
	</dc:creator><dc:subject>aluminium alloys</dc:subject><dc:subject>bimetallic sheets</dc:subject><dc:subject>CARALL</dc:subject><dc:subject>composite sheets</dc:subject><dc:subject>GLARE</dc:subject><dc:subject>metal-based composites</dc:subject><dc:subject>sheet forming</dc:subject><dc:description>For several years, the aviation industry has seen dynamic growth in the use of composite materials due to their low weight and high stiffness. Composites are being considered as a means of building lighter, safer, and more fuel-efficient automobiles. Composite materials are the building material of a relatively new kind of unmanned aerial vehicle, commonly known as a drone. Incremental forming methods allow materials to be quickly formed without the need to manufacture conventional metal dies. Their advantage is the high profitability during the production of prototypes and a small series of products when compared with the conventional methods of plastic forming. This article provides an overview of the incremental forming capabilities of the more commonly produced aluminium- and titanium-based laminates, which are widely used in the aircraft industry. In addition, for composites that are not currently incrementally formed, i.e., aramid-reinforced aluminium laminates, the advantages and potential for incremental forming are presented.</dc:description><dc:date>2022</dc:date><dc:date>2022-10-12 09:46:36</dc:date><dc:type>Članek v reviji</dc:type><dc:identifier>141945</dc:identifier><dc:identifier>UDK: 621.7</dc:identifier><dc:identifier>ISSN pri članku: 2504-477X</dc:identifier><dc:identifier>DOI: 10.3390/jcs6100295</dc:identifier><dc:identifier>COBISS_ID: 125236995</dc:identifier><dc:language>sl</dc:language></metadata>
