发明名称 ROCKET ENGINE MEMBER AND A METHOD FOR MANUFACTURING A ROCKET ENGINE MEMBER
摘要 The invention relates to a liquid fuel rocket engine member (10). The member forms a body of revolution having an axis of revolution having an axis of revolution and a cross section that varies in diameter along said axis. The wall structure comprises a plurality of cooling channels (11). The outside of the wall structure includes a continuous sheet metal wall (14). The cooling channels (11) are longitudinally attached to the inside of the sheet metal wall. A method for manufacturing the rocket engine member (10) includes the steps of forming a sheet metal wall (14) having a wall section corresponding to the desired nozzle section, providing a plurality of channel members (15), and attaching the channel members (15) to the inside of the sheet metal wall (14).
申请公布号 WO02055863(A1) 申请公布日期 2002.07.18
申请号 WO2002SE00026 申请日期 2002.01.09
申请人 VOLVO AERO CORPORATION;HAEGGANDER, JAN;LUNDGREN, JAN;HALLQVIST, MATS 发明人 HAEGGANDER, JAN;LUNDGREN, JAN;HALLQVIST, MATS
分类号 F02K1/00;F02K9/48;F02K9/64;F02K9/97;(IPC1-7):F02K9/64 主分类号 F02K1/00
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