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
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