发明名称 TUBE HAVING A HYBRID-TYPE STRUCTURE, IN PARTICULAR FOR AN AIRCRAFT SEAT
摘要 The invention relates to a hybrid tube (22), in particular for an aircraft seat structure S, said structure comprising ribs (10) intended to receive the hybrid tube (22), said hybrid tube (22) including a monolithic carbon tube (24) and at least one sleeve (26) made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-moulding.
申请公布号 WO2016016538(A1) 申请公布日期 2016.02.04
申请号 WO2015FR51948 申请日期 2015.07.16
申请人 EPSILON COMPOSITE 发明人 PORTOLES, JOSÉ;NOGUES, DOMINIQUE;LANDAIS, MATTHIEU
分类号 B64D11/06 主分类号 B64D11/06
代理机构 代理人
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