发明名称 Metallmatrixverbundkörper mit hoher Steifigkeit und hoher Stabilität in Längsrichtung
摘要 <p>A long metal matrix composite material part comprises 35-45 vol.% aluminum alloy matrix and 65-55 vol.% continuous carbon fibers arranged in successive layers parallel to the length direction.≥90% of the fibers are ultra-high modulus fibers which are oriented, to the length direction, at 0 to plus or minus 5 degrees in 25-60% of the layers and at plus or minus 20 to plus or minus 40 degrees in the other layers. An Independent claim is also included for a similar long metal matrix composite material part in which the matrix comprises a magnesium alloy and the ultra-high modulus carbon fibers are oriented at 0 to plus or minus 5 degrees to the length direction in≥90% of the layers.</p>
申请公布号 DE69807306(T2) 申请公布日期 2003.04.17
申请号 DE1998607306T 申请日期 1998.12.01
申请人 EUROPEAN AERONAUTIC DEFENCE AND SPACE CO. - EADS FRANCE, PARIS 发明人 BILLAUD, LAETITIA;GAUDIN, JOCELYN;NIVET LUTZ, MARTINE;PONCY, JOEL
分类号 B22D19/14;B32B15/14;C22C47/00;C22C47/08;C22C49/06;C22C49/14;C22C101/10;D01F9/12;(IPC1-7):C22C49/14 主分类号 B22D19/14
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