Descripción
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In the study we choose a horizontal tale rib of an A320 aircraft, that is developing a new version, Neo, to reduce operating costs. We choose 12th rib, penult rib near tip stabilizer, a surface with high crash risk. We are trying to achieve equivalent configuration of layers, using substitute materials with thermoplastic matrix, it?s high fracture resistance, instead of used material, with a epoxi polimeric thermostable matrix reinforced with carbon fibres. Nature of thermoplastic resin awards high density, that it becomes in increase rib weight. However, if we consider the joint elements of horizontal stabilizer (ribs, keel beam, spars, stringers, skin panels), and these can be join with welding. Total weight of whole will cause lightening because of removal bolts, rivets and fittings. Added thermoplastic compounds result in save maintenance and recycled tasks. We prove technical and economic feasibility to replace thermostable matrix with thermoplastic matrix. | |
Internacional
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No |
Nombre congreso
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6th International Conference on Industrial Engineering and Industrial Management XVI Congreso de Ingeniería de Organización |
Tipo de participación
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960 |
Lugar del congreso
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VIGO |
Revisores
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Si |
ISBN o ISSN
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978-84-938642-5-5 |
DOI
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Fecha inicio congreso
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18/07/2012 |
Fecha fin congreso
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20/07/2012 |
Desde la página
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840 |
Hasta la página
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846 |
Título de las actas
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Industrial Engineering: Overcoming the Crisis |