发明名称 |
COMPONENT FOR AN AIRPLANE STRUCTURE, METHOD FOR MANUFACTURING A COMPONENT FOR AN AIRPLANE STRUCTURE AND USE OF THE COMPONENT AS A CRACK ARRESTOR |
摘要 |
A component suitable as a crack arrestor or Doppler for an airplane structure comprises at least one first cover layer (3) forming a first skin surface (5) of the component (1), wherein the first cover layer (3) contains substantially aluminum or an aluminum alloy, and a base member (2) containing titanium or a titanium alloy. A first work piece made of titanium or a titanium alloy and a second work piece made of aluminum or an aluminum alloy are prepared for the manufacture of the component (1). The first work piece is connected to the second work piece through plating. |
申请公布号 |
WO2009138921(A1) |
申请公布日期 |
2009.11.19 |
申请号 |
WO2009IB51881 |
申请日期 |
2009.05.07 |
申请人 |
EADS DEUTSCHLAND GMBH;HECKENBERGER, ULRIKE;HOLZINGER, VITUS;VLCEK, JOHANNES |
发明人 |
HECKENBERGER, ULRIKE;HOLZINGER, VITUS;VLCEK, JOHANNES |
分类号 |
B32B15/00;B23K20/04;F28F21/00 |
主分类号 |
B32B15/00 |
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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