发明名称 AN AIRCRAFT STRUCTURE WITH STRUCTURAL NON-FIBER REINFORCING BONDING RESIN LAYER
摘要 <p>The present invention regards an aircraft structure comprising an aerodynamic composite shell (7), the interior face (9) of which in whole or in part is bonded with at least one two- or three-dimensional structural composite part (11) by means of a bonding material (15). It also regards a method of manufacture of the aircraft structure. The bonding material (15) comprises a non-structural fiber reinforced resin system, wherein at least one portion of the bonding material, which portion spatially corresponds with an interior face filling volume (21), is thicker than other portions of the bonding material (15), due to settlement of resin of the non-structural fiber reinforced resin system in said interior face filling volume (21) during the viscous phase of the curing of the non-structural fiber reinforced resin system.</p>
申请公布号 WO2013089598(A1) 申请公布日期 2013.06.20
申请号 WO2011SE51501 申请日期 2011.12.12
申请人 SAAB AB;GRANKAELL, TOMMY;HALLANDER, PER;PETERSSON, MIKAEL;WEIDMANN, BJOERN 发明人 GRANKAELL, TOMMY;HALLANDER, PER;PETERSSON, MIKAEL;WEIDMANN, BJOERN
分类号 B64C3/20;B29C65/02;B29C65/48;B29C70/54;B29L31/30;B64C1/12;B64C3/24 主分类号 B64C3/20
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