发明名称 Cooled structure production method - forms tube wall of small pipes with covering layer thicker at mounting flange and spark-erodes openings in pipes for coolant at flange seat
摘要 A wall (2) is produced to more than the desired length, the layer (4) being thicker at the flange than elsewhere. It is then machined to length, and a seat (5) for the flange (9) is machined in it. At the seat, holes (6) for the coolant are formed through the layer and the outside walls of the pipes (3) by spark-erosion or mechanically. The flange is then fitted onto the seat and welded to the layer, and the pipe ends are sealed off individually by welding filler-pieces (7) into them. USE/ADVANTAGE - For a back-pressure combustion chamber for hypersonic propulsion. It is simple, strong, and gives good sealing and flow characteristics, and easy inspection and repair of all joints.
申请公布号 DE4304559(C1) 申请公布日期 1994.03.24
申请号 DE19934304559 申请日期 1993.02.16
申请人 DEUTSCHE AEROSPACE AG, 80804 MUENCHEN, DE 发明人 SCHENKEL, TILMAN, DIPL.-ING., 8098 PFAFFING, DE;BREY, KARL, DIPL.-ING., 8000 MUENCHEN, DE
分类号 B23P15/00;F02K9/64;(IPC1-7):B23P15/26 主分类号 B23P15/00
代理机构 代理人
主权项
地址