首页> 外国专利> METHOD FOR FILLING HELIUM The cylinders of launch vehicles and spacecraft and filling system HELIUM The cylinders of carrier rockets and spacecraft

METHOD FOR FILLING HELIUM The cylinders of launch vehicles and spacecraft and filling system HELIUM The cylinders of carrier rockets and spacecraft

机译:填充氦气的方法运载火箭和航天器的气瓶以及填充系统氦气运载火箭和航天器的气瓶

摘要

1.a helium gas vehicle cylinders launch vehicles and spacecraft, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 in heating and filling the obtained helium side cylinders, exce u0447u0430u044eu0449u0438u0439u0441u00a0, u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 cooling gaseous u0433u0435u043bu0438u00a0 asleep until the temperature u0432u044bu043cu043eu0440u0430u0436u0438u0432u0430u043du0438u00a0 harmful impuritiesfiltration and subsequent heating to the permissible temperature of sealing elements u0434u043bu00a0 on-board systems to control the pressure at the entrance and exit of u043au0440u0438u043eu0441u0442u0430u0442u0430, further u0437u0430u043fu043eu043bu043du00a0u044eu0442 threefold obtained helium side cylinders, u0434u0440u0435u043du0438u0440u0443u044eu0442 him, and then u0437u0430u043fu043eu043bu043du00a0u044eu0442 side cylinders to work u0434u0430u0432u043bu0435u043du0438 u00a0,in the case of the change u0434u0430u0432u043bu0435u043du0438u00a0 at the entrance and exit of u043au0440u0438u043eu0441u0442u0430u0442u0430 over 1 mpa put the second cryostat.;2.helium cylinder filling system in launch vehicles and spacecraft, u0441u043eu0441u0442u043eu00a0u0449u0430u00a0 of helium through the line to the electronic receiver, uk u0440u043eu043du0430u0433u0440u0435u0432u0430u0442u0435u043bu0435u043c, u0441u0432u00a0u0437u0430u043du043du044bu043c through reservoir installed to seal u0440u0435u0433u0443u043bu0438u0440u043eu0432u043eu0447u043du043eu0439 fittings with on-board cylinders, pipeline with the it stop fittings and a reservoir u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 orderit is fitted with the nitrogen and the additional u0433u0435u043bu0438u0435u0432u044bu043c receivers, not less than u0434u0432u0443u043cu00a0 u043au0440u0438u043eu0441u0442u0430u0442u0430u043cu0438, united with the u044du043bu0435u043au0442u0440u043eu043du0430u0433u0440u0435u0432u0430u0442u0435u043bu0435u043c performed no less than to tre u043cu00a0 u0437u043cu0435u0435u0432u0438u043au0430u043cu0438 and through pipelines installed on same fittings - the tank, each of u0433u0435u043bu0438u0435u0432u044bu0445 receivers is connected with one of the cri spending the rest.one coil u044du043bu0435u043au0442u0440u043eu043du0430u0433u0440u0435u0432u0430u0442u0435u043bu00a0 informs the nitrogen receiver with each of the u043au0440u0438u043eu0441u0442u0430u0442u043eu0432 and each of the u043eu0441u0442u0430u0432u0448u0438u0445u0441u00a0 coils located between the u043au0440u0438u043eu0441u0442u0430u0442u043eu043c and the collector, with a valve and manifold combined into a common collector of the established it stop fittings and seal u0440u0435u0433u0443u043bu0438u0440u043eu0432 the reservoir u043eu0447u043du0430u00a0 printing is done in a u044du043bu0435u043au0442u0440u043eu043fu043du0435u0432u043cu043eu043au043bu0430u043fu0430u043du043eu0432,one of which normally is open and the other normally - closed and between them and the common collector of the installed non-return valves.
机译:1.a氦气气瓶运载火箭和航天器 u0437 u0430 u043a u043b u044e u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0加热并填充获得的氦气侧气瓶, u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0, u043e u0441 u0443 u0449 u0435 u0441 u0442 u0432 u043b u00a0 u044e u0442冷却气态 u0433 u0435 u043 u00a0睡着直到温度 u0432 u044b u043c u043e u0440 u0430 u0436 u0438 u0432 u0430 u043d u0438 u00a0有害杂质过滤并随后加热到密封元件的允许温度 u0434 u043b u00a0车载系统来控制 u043a u0440 u0438 u043e u0441 u0442 u0430 u0442 u0430 u0430 u0442 u0430 u04e u0430 u04e u04e u04e u043b u0430 u043f u0442获得三倍的氦气侧气瓶, u0434 u0440 u0435 u043d u0438 u0440 u0443 u044e u0442他,然后是 u0437 u0430 u043f u043e u043b u043d u043d u00a0 u044e u0442气瓶工作 u0434 u0430 u0 432 u043b u0435 u043d u0438 u00a0,在 u043a u0440 u0438 u043e u0441的入口和出口处更改为 u0434 u0430 u0432 u043b u0435 u043d u043d u0438 u00a0 u0442 u0430 u0442 u0430超过1 mpa放置了第二个低温恒温器; 2.运载火箭和航天器中的氦气钢瓶填充系统, u0441 u043e u0441 u0442 u043e u00a0 u0449 u0430 u00a0穿过氦气到电子接收器的线路,英国 u0440 u043e u043d u0430 u0433 u0440 u0435 u0432 u0430 u0442 u0435 u043b u0435 u0435 u043c, u0441 u0432 u0432 u00a0 u0437 u0430 u043d u043d u044b u043c通过安装的油箱来密封 u0440 u0435 u0433 u0443 u043b u0438 u0440 u043e u0432 u043e u0447 u043d u043e u0439带有车载气缸的配件,带有止动装置的管道配件和储罐 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0订单中装有氮气,另外的 u0433 u0435 u0435 u043b u0438 u0435 u0432 u044b u043c接收者,不少于 u0434 u0432 u0443 u043c u00a0 u043a u04 40 u0438 u043e u0441 u0442 u0430 u0442 u0430 u043c u0438,与 u044d u043b u0435 u043a u0442 u0440 u043e u043d u0430 u0433 u0440 u0435 u0432 u0430 u0442 u0435 u043b u0435 u043c的执行效果至少要达到 u043c u00a0 u0437 u043c u0435 u0435 u0432 u0438 u043a u0430 u043c u043c u0438并通过安装在同一配件上的管道-储罐,每个 u0433 u0435 u043b u0438 u0435 u0432 u044b u0445接收器均与其余一个cri连接。一个线圈 u044d u043b u0435 u043a u0442 u0440 u043e u043d u0430 u0433 u0440 u0435 u0432 u0430 u0442 u0435 u043b u00a0将每个 u043a u0440 u0438 u043e u0441 u0442 u0430 u04430 u0442 u043e u0432以及每个 u043e u0441 u0442 u0430 u0432 u0448 u0438 u0445 u0441 u00a0线圈之间的 u043a u0440 u0438 u043e u0441 u0442 u0430 u0430 u0442 u043e u043c和收集器之间将阀和歧管组合成已建立的公用收集器,然后将其停止并密封 u0440 u0435 u0 433 u0443 u043b u0438 u0440 u043e u0432 u043e u0447 u043d u043d u0430 u00a0的打印是在 u044d u043b u0435 u043a u0442 u0440 u0440 u043e u043f u043d u0435中完成的 u0432 u043c u043e u043a u043b u0430 u043f u0430 u043d u043e u0432,其中一个常开,另一个常闭-在它们与已安装的止回阀的公共收集器之间。

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