发明名称 |
AIRLINER TIGHT FUSELAGE COMPARTMENT SKIN FROM POLYMER COMPOSITE AND METHOD OF ITS FABRICATION |
摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering. Proposed skin is composed of laminar skin with gauze of reinforcing ribs. Said gauze comprises helical ribs with lateral surfaces shaped to ordinary right helix with said ribs turned in compartment end area and changing into left helix and vice versa, as well as lengthwise ribs turned in U-like direction at compartment end areas. Said ribs are uniformly distributed over compartment surface and arranged in continuous layers. Said ribs consist of layer of unidirectional fiber strands from composite material bonded together by polymer binder. Outer laminar skin of polymer composite is laid over said gauze of reinforcing ribs.EFFECT: higher strength in skin end area, reduced weight of joint between skin and mating structures.11 cl, 17 dwg |
申请公布号 |
RU2475412(C1) |
申请公布日期 |
2013.02.20 |
申请号 |
RU20110136029 |
申请日期 |
2011.08.29 |
申请人 |
OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "NAUCHNO-INZHENERNAJA KOMPANIJA" (OOO "NIK") |
发明人 |
BILASH VITALIJ KONSTANTINOVICH;KORNEEV ALEKSANDR NIKOLAEVICH;PAVLOV VLADIMIR ALEKSANDROVICH;MALYSHEVSKIJ ALEKSANDR NIKOLAEVICH;KATUKOV VJACHESLAV VLADIMIROVICH |
分类号 |
B64C1/06;B32B1/08;B32B3/12 |
主分类号 |
B64C1/06 |
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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