发明名称 |
JOINED COMPOSITE STRUCTURE WITH GRADED COEFFICIENT OF THERMAL EXPANSION FOR EXTREME ENVIRONMENT APPLICATION |
摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide an integrated structure of members having coefficient of thermal expansion (CTE) different from one another. <P>SOLUTION: The integrated composite structure having a gradient coefficient of thermal expansion (CTE) is formed by selecting a plurality of layers made of materials having gradient CTEs and by employing a joining method such as welding, brazing or solid-state bonding. After that, the integrated composite billet or near net shape is processed so as to produce a first surface for mounting a first structural member having a first CTE and to produce a second surface for mounting a second structural member having a second CTE. <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
申请公布号 |
JP2010006054(A) |
申请公布日期 |
2010.01.14 |
申请号 |
JP20090105216 |
申请日期 |
2009.04.23 |
申请人 |
BOEING CO:THE |
发明人 |
YOUSEFIANI ALI;COMFORT JOHN M;VOLLMER JOHN G;HAND MICHAEL L |
分类号 |
B32B7/02;B23K1/19;B23K20/12;B23K33/00;B23K103/18;F16B11/00 |
主分类号 |
B32B7/02 |
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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