发明名称 Jet nozzle for solid fuelled rocket has reinforcing fastened on inner contour of nozzle structure and consists of fiber material with fibers orientated in circumferential direction
摘要 The jet nozzle for a rocket with solid fuel has a reinforcing extending in the circumferential direction of the nozzle structure and provided with a heat insulation on the outer side of the nozzle structure. The reinforcing (7,8) is fastened on the inner contour of the nozzle structure (3) and consists of a fiber material with the fibers orientated in the circumferential direction. At least the converging section (5) of the nozzle structure is provided with the reinforcing.
申请公布号 DE10245741(A1) 申请公布日期 2004.04.22
申请号 DE20021045741 申请日期 2002.10.01
申请人 BAYERN-CHEMIE GESELLSCHAFT FUER FLUGCHEMISCHE ANTRIEBE MBH 发明人 DEMPFLE, BENEDIKT;BAUER, KARL;KREMER, FRANS
分类号 F02K9/34;F02K9/97;(IPC1-7):F02K9/34 主分类号 F02K9/34
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