首页> 外国专利> Pulsed supersonic gas flow injector for use in study of thermonuclear fusion plasmas has first chamber with gas under pressure on either side of free piston

Pulsed supersonic gas flow injector for use in study of thermonuclear fusion plasmas has first chamber with gas under pressure on either side of free piston

机译:用于研究热核聚变等离子体的脉冲式超声波气体流动注射器,其第一个腔室的自由活塞两侧均带有压力气体

摘要

A pulsed supersonic gas flow injector has a first chamber (2) in which the gas to be injected is located under pressure on either side of a free piston (4). It has a propulsion unit (12) for the piston and a supersonic gas ejection tube (6) connected to the first chamber via an aperture (8) controlled by a valve (10) actuated by the free piston striking it. The propulsion unit is designed to create a difference in injected gas pressure on opposite sides of the piston, and has a second chamber (14) in which the injected gas is located under pressure on either side of a controlled piston (16).
机译:脉冲超音速气流喷射器具有第一腔室(2),要喷射的气体在压力作用下位于自由活塞(4)的任一侧。它具有用于活塞的推进单元(12)和通过孔(8)连接到第一腔室的超音速气体喷射管(6),该孔由阀(10)控制,该阀由自由活塞撞击而被致动。推进单元被设计成在活塞的相对侧上产生喷射气体压力的差异,并且具有第二腔室(14),在该腔室中,喷射气体在压力下位于受控活塞(16)的任一侧上。

著录项

  • 公开/公告号FR2850298A1

    专利类型

  • 公开/公告日2004-07-30

    原文格式PDF

  • 申请/专利权人 COMMISSARIAT A LENERGIE ATOMIQUE;

    申请/专利号FR20030000910

  • 发明设计人 MARTIN GILLES;

    申请日2003-01-28

  • 分类号B01J19/26;

  • 国家 FR

  • 入库时间 2022-08-21 22:39:14

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