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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|