首页> 外国专利> METHOD FOR CLEANING OF ROCKET SEPARATING PART FROM LIQUID TOXIC REMAINS OF ROCKET FUEL COMPONENTS AND DEVICE FOR ITS REALISATION

METHOD FOR CLEANING OF ROCKET SEPARATING PART FROM LIQUID TOXIC REMAINS OF ROCKET FUEL COMPONENTS AND DEVICE FOR ITS REALISATION

机译:火箭燃料成分的液体毒瘾中分离火箭的方法及其实现的装置

摘要

FIELD: aviation.;SUBSTANCE: invention is related to rocket space engineering, namely to carrier rockets with liquid rocket propellant engines. Method for cleaning of rocket separating part from liquid toxic remains of rocket fuel components on passive area of flight is based on gasification of fuel remains in fuel tank and their supply through manifolds by means of connection pipelines into oxidant tank and then to surrounding space. Device comprises displacement reservoir with filling-drain valve, ball-balloon, pyrovalves, pyromembrane, powder rocket engines for untwisting of rocket separating part body, control unit. Device additionally comprises connection pipelines with pyromembranes, flow pipeline of oxidant upstream main oxidant valve, drain valve, which is installed on upper bottom of oxidant reservoir, reduction gear connected to electric pneumatic valve and displacement reservoir.;EFFECT: possibility is achieved to preserve specified coordinates of fall regions and to reduce ecological effect of separating parts, which use toxic components of rocket fuel.;3 cl, 1 dwg
机译:技术领域本发明涉及火箭太空工程,即涉及带有液体火箭推进剂发动机的运载火箭。在被动飞行区域中从火箭燃料成分的液体有毒残留物中清除火箭分离部件的方法是基于燃料罐中的残留燃料的气化,并通过连接管道将其通过歧管供应到氧化剂罐,然后再输送到周围空间。该装置包括带有排水阀的排量储存器,球形气球,热管,热膜,用于解开火箭分离部件本体的粉末火箭发动机,控制单元。该装置还包括:带有吡咯烷膜的连接管道,氧化剂上游主氧化剂阀的流路,安装在氧化剂容器上部底部的排放阀,与电动气动阀和排量容器连接的减速器。下降区域的坐标并减少使用火箭燃料的有毒成分的分离部分的生态影响。; 3 cl,1 dwg

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号