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device for the separation of pipelines of hydraulic systems of spacecraft in weightless environment

机译:失重环境下航天器液压系统管道分离装置

摘要

1.the device u0434u043bu00a0 u0440u0430u0437u044au0435u0434u0438u043du0435u043du0438u00a0 pipelines of hydraulic systems of spacecraft in u0443u0441u043bu043eu0432u0438u00a0u0445 weightlessness, containing the terminal node with parallel u0442u00a0u0433u0430u043cu0438, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 so that, with a view to u0438u0441u043au043bu044eu0447u0435u043du0438u00a0 u0432u044bu043fu043bu0435u0441u043au0438u0432u0430u043du0438u00a0 working fluid of hydraulic system pipes u0440u0430u0437u044au0435u0434u0438u043du00a0u0435u043cu044bu0445 spacecraft by u043eu0431u0435u0441u043f u0435u0447u0435u043du0438u00a0 glide and u0441u043du0438u0436u0435u043du0438u00a0 efforts we undock,it is the terminal node in the form of detachable clips installed at the ends of the pipeline and interconnected by parallel u0442u00a0u0433u0430u043cu0438, one of the u0436u0438u043cu043eu0432 is still installed in this u0446u0435u043du0442u0440u0438u0440u0443u044eu0449u0435u0439 bung with a spherical surface, and the conical surface of the u043au043eu043du0442u0430u043au0442u0438u0440u0443u044eu0449u0438u043c her clarification u0435u043cu043du044bu043c emphasis with rough set on its internal surface u0443u043fu043bu043eu0442u043du0438u0442u0435u043bu0435u043c,covering the surface of the pipeline, and the other clamp is equipped with a fixing u0431u0443u0440u0442u043eu043c, u043eu043fu0438u0440u0430u044eu0449u0438u043cu0441u00a0 on the stationary flange made on the pipeline.;2. device for u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 1, so that the parallel u0442u00a0u0433u0438 implemented in the form of u0442u0430u043du0434u0435u0440u043eu0432.
机译:1. u0443 u0441 u043b u043e 中的航天器液压系统管道设备 u0434 u043b u00a0 u0440 u0430 u0437 u044a u0435 u0434 u0438 u043d u0435 u043d u043d u0438 u00a0 u0432 u0438 u00a0 u0445失重,包含具有并行 u0442 u00a0 u0433 u0430 u043c u0438, u043e u0442 u043b u0438 u0447 u0430uu u00a0,以便查看 u0438 u0441 u043a u043b u044e u0447 u0435 u043d u0438 u00a0 u0432 u044b u043f u043b u0435 u0435 u0441 u043a u0438 u0432 u0430 u04e u043d u0438 u00a0液压系统管道的工作流体 u0440 u0430 u0437 u044a u0435 u0435 u0434 u0438 u043d u00d0 u0435 u0435 u043c u044b u0445航天器由 u043e u0431 u0435 u0435 u0447 u0435 u043d u0438 u00a0滑行和 u0441 u043d u0438 u0436 u0435 u043d u0438 u00a0我们努力取消停靠,它是以可分离夹的形式安装在终端的末端管道并通过并行 u0442 u00a0 u0433 u0430 u043c u0438(其中一个 u0436 u0438)互连 u043c u043e u0432仍安装在此 u0446 u0435 u043d u0442 u0440 u0438 u0440 u0443 u044e u0449 u0435 u0439带有球形表面和圆锥形表面的 u043a u043e u043d u0442 u0430 u043a u0442 u0438 u0440 u0443 u044e u0449 u0438 u043c她的说明 u0435 u043c u043d u044b u043c内表面粗糙设置 u0443 u043f u043b u043e u0442 u043d u0438 u0442 u0435 u043b u0435 u043c,覆盖管道的表面,另一个夹具配有固定件 u0431 u0443 u0440 u0442 u043e u043c,管道上的固定法兰上的u043e u043f u0438 u0440 u0430 u044e u0449 u0438 u043c u0441 u00a0; 2。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0435 u0435 u0441 u00a0 1的设备,因此并行的 u0442 u00a0 u0433 u0438以 u0442 u0430 的形式实现u043d u0434 u0435 u0440 u043e u0432。

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