发明名称 COMPONENTE DE AERONAVE CON PANELES RIGIDIZADOS CON LARGUERILLOS CON DOS TIPOS DE ENSANCHAMIENTOS LOCALES.
摘要 <p>Aircraft component which comprises at least one panel (11) of composite material, formed by a skin (13) and a plurality of stiffening stringers (15) which are configured with a core (17) and a base (19) of width (A), said stiffening stringers (15) comprising first local flarings (21) of their bases (19) intended to provide areas for joining with other parts located in flat zones of the skin (13) and second local flarings (23) of their bases (19) which are intended to provide areas for joining with other parts located in zones of the skin (13) which include change-in-thickness ramps (33), being configured in the form of two end sections (41, 45) located above flat zones of the skin (13) and a central section (43) located above one of said ramps (33) of the skin (13), one of said end sections (41, 45) acting as an area for joining with other parts.</p>
申请公布号 ES2393102(B1) 申请公布日期 2013.11.21
申请号 ES20100031012 申请日期 2010.06.30
申请人 AIRBUS OPERATIONS, S.L. 发明人 GRANADO MACARRILLA, JOSE ORENCIO;MARTINEZ VALDEGRAMA, VICENTE;LOZANO SEVILLA, ALBERTO
分类号 B64C3/18;B64C1/06 主分类号 B64C3/18
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