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Ceramic-carbon jet nozzle exhaust pipe for a rocket engine has flange for fixing the exhaust pipe to the end of the combustion chamber nozzle

机译:火箭发动机的陶瓷碳喷嘴喷嘴排气管具有法兰,用于将排气管固定到燃烧室喷嘴的端部

摘要

A carbon framework structure for the jet nozzle exhaust pipe (1) for a rocket engine is obtained by coiling, and a flange for fixing the exhaust pipe (1) to the end of the nozzle (2) from the combustion chamber is integrated with a continuous line of fibers of the framework of carbon fibers coiled up in the exhaust pipe (1) . Preferred Features: The flange can be in the form of a conical expansion of the exhaust pipe (1), or can be in the form of a conical extension of the exhaust pipe (1) which comprises an additional folded section for axially receiving screws that fix the flange to the combustion chamber. The jet nozzle exhaust pipe (1) comprises a fixed section and a deployable section (4). An interface connection is located between the sections of the exhaust pipe on a flange at the inlet of the deployable section (4) of the exhaust pipe (1), the flange being integrated with a continuous line of fibers of the framework of carbon fibers coiled up in the deployable section (4) of the jet nozzle. The interface connection comprises an interface ring made of carbon/silicon carbide (C/SiC) on the fixed section (3) of the exhaust pipe (1). Locking tabs distributed at the periphery of the interface connection, and made of C/SiC, are integrated by a machining cutting operation performed on the interface ring once it has hardened. The deployable section (4) of the exhaust pipe (1) comprises an upper segment (5) and a lower segment (6). An interface connection (9) is located between the segments of the jet nozzle at the inlet of the lower section of the jet nozzle having a flange, integrated with a continuous line of fibers in the framework of carbon fibers coiled up in the lower segment (6) of the jet nozzle. One or more of the coiled-up flanges are reinforced by a prefabricated carbon fiber lap.
机译:通过盘绕获得用于火箭发动机的喷嘴排气管(1)的碳骨架结构,并且用于将排气管(1)从燃烧室固定到喷嘴(2)的端部的凸缘与玻璃制成一体。碳纤维骨架的连续纤维盘绕在排气管(1)中。优选特征:凸缘可以呈排气管(1)的锥形膨胀的形式,或者可以呈排气管(1)的锥形延伸的形式,其包括用于轴向容纳螺钉的附加折叠部分。将法兰固定到燃烧室。喷嘴排气管(1)包括固定部分和可展开部分(4)。接口连接位于排气管(1)的可展开部分(4)入口处的法兰上的排气管各部分之间,该法兰与盘绕的碳纤维框架的连续纤维线集成在一起向上位于喷嘴的可展开部分(4)中。所述接口连接件包括在排气管(1)的固定部分(3)上的由碳/碳化硅(C / SiC)制成的接口环。一旦接口环变硬,分布在接口连接外围的锁舌由C / SiC制成,通过对接口环进行机加工切割而集成在一起。排气管(1)的可展开部分(4)包括上段(5)和下段(6)。接口连接(9)位于喷嘴下部的入口处,喷嘴的各个部分之间具有法兰,该凸缘与在下部部分中盘绕的碳纤维框架中的纤维连续线集成在一起( 6)的喷嘴。一个或多个盘绕的法兰由预制碳纤维搭接片加固。

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