发明名称 Method for manufacturing components for rocket construction
摘要 <p>The nickel is deposited on a base material, to form nickel coated base material by nickel vapor deposition method. The nickel coated base material is processed, to form component. The base material is composed of ceramic fiber composite structure, milled metallic base structure and individual tubular element. The base material has open cooling channels (25) and closed cooling channels.</p>
申请公布号 EP1854905(A1) 申请公布日期 2007.11.14
申请号 EP20070008991 申请日期 2007.05.04
申请人 ASTRIUM GMBH 发明人 GROEBER, JOSEF;TAUBENBERGER, GERHARD;STAHN, BERNHARD
分类号 C23C16/16;C23C16/02;C23C16/04;C23C16/56 主分类号 C23C16/16
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