发明名称 Method of forming a rocket thrust chamber
摘要 Molten metal is sprayed onto the outer shell 32 of a cooling tube bundle 10, and the ends of tubes 18, 20 are covered with predetermined thicknesses of the metal 52, 54. Circumferentially extending manifold channels 60, 64 that intersect each of the tube ends 18, 20 are then machined into the predetermined thicknesses of metal, and mating assemblies 74, 76 are attached to enclose the manifold channels 60, 64. <IMAGE>
申请公布号 EP1005949(B1) 申请公布日期 2003.06.11
申请号 EP19990309528 申请日期 1999.11.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WRIGHT, ROBERT J.
分类号 B23P15/00;B64G1/00;F02K9/64;F02K9/97 主分类号 B23P15/00
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