首页> 外国专利> 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

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

机译:用于固体燃料火箭的喷射喷嘴具有固定在喷嘴结构内轮廓上的加强件,并且由纤维材料制成,该纤维材料具有沿圆周方向定向的纤维

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.
机译:用于带有固体燃料的火箭的喷嘴具有在喷嘴结构的圆周方向上延伸的加强件,并且在喷嘴结构的外侧上具有绝热材料。加强件(7,8)固定在喷嘴结构(3)的内部轮廓上,并且由纤维材料构成,其中纤维在圆周方向上定向。至少喷嘴结构的会聚部分(5)设有加强件。

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