发明名称 |
Carrier structure for turbo-propeller, has lower part that is fixed in dismountable way on upper part by pin, cavity, and bore, where lower part has girders extending in longitudinal direction and connecting lower arches |
摘要 |
<p>The structure has an upper part (20) mounted integrally with an armature (110) of a wing and comprising a longitudinal beam (26) arranged between a front arch (22) and a rear arch (24). A lower part (30) has lower arches and girders that extend in longitudinal direction and connect the lower arches. The lower part is fixed in a dismountable way on the upper part by a pin, cavity (52), and bore (54). An independent claim is also included for an assembly comprising a carrier structure.</p> |
申请公布号 |
FR2851226(A1) |
申请公布日期 |
2004.08.20 |
申请号 |
FR20030002000 |
申请日期 |
2003.02.19 |
申请人 |
SNECMA MOTEURS |
发明人 |
PICARD JEAN LOUIS;MAZEAUD GEORGES |
分类号 |
B64D27/26;B64D27/12;B64D27/16;B64D29/02;B64D29/06;B64D29/08;(IPC1-7):B64D27/26 |
主分类号 |
B64D27/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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