发明名称 Faserverstärktes thermoplastisches Blatt, insbesondere eines eingelassenen Heckrotors und sein Herstellungsverfahren
摘要 The blade has its lower (overpressure) face covering (6a) and top (suction) face covering (6b) of its shell, its front filling body (9) and its rear filling body (10) and its spar (7) all made of a composite material having the same thermoplastic matrix, preferably made of PEEK, preferably reinforced with carbon fibres. The spar (7) is extended outside the shell by an integrated root part having a connection attachment, in the form of a loop or laminated, in the same thermoplastic composite. The process consists in assembling, by melting under pressure, all the blade components made of thermoplastic composite, in a single operation, after manufacture of these components in the form of prefabricated elementary components. <IMAGE>
申请公布号 DE69307855(D1) 申请公布日期 1997.03.13
申请号 DE1993607855 申请日期 1993.12.20
申请人 EUROCOPTER FRANCE, MARIGNANE, FR 发明人 COFFY, RENE LOUIS, F-13960 SAUSSET LES PINS, FR
分类号 B64C11/20;B29B15/08;B29C70/08;B29C70/34;B29D99/00;B64C11/06;B64C11/26;B64C27/46;B64C27/473;B64C27/82;(IPC1-7):B64C27/46;B29D31/00;B64C27/45 主分类号 B64C11/20
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