发明名称 Tube support for e.g. aircraft, has support portion supporting tube, where support is folded around axis parallel to rectilinear direction to form non coplanar flaps, where flaps are integrated to fixation portion at folding edge of sheet
摘要 <p>The support (21) has a support portion (23) supporting a tube, where the support is formed from a sheet extending between two portions along a rectilinear direction (24). The support is folded around an axis (25) parallel to the direction so as to form two non coplanar flaps (25a, 25b), where the flaps are integrated to a fixation portion (22) at a folding edge of the sheet. The portion (22) has two tabs, where each flap is integrated to the tab at the edge. The flaps form a V sectional spanwise beam (P25) integrated to the portion (22) that fixes a casing to a clamping plate (5).</p>
申请公布号 FR2914275(A1) 申请公布日期 2008.10.03
申请号 FR20070002231 申请日期 2007.03.27
申请人 SNECMA SOCIETE ANONYME 发明人 CASTEL ANDRE;PHAM LUCIEN PAUL;STEPHAN MARC
分类号 B64D33/00;F02C7/00 主分类号 B64D33/00
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