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11. 发明申请

US20090269273A1 OXYGEN EXTRACTION APPARATUS AND PROCESS 有权
标题翻译：氧气提取装置和工艺
公开(公告)号：US20090269273A1
公开(公告)日：2009-10-29
申请号：US12256877
申请日：2008-10-23
申请人： Rodney L. Burton , Peter J. Schubert , Filip Rysanek , Paul Fenoglio , Mike Hutches
发明人： Rodney L. Burton , Peter J. Schubert , Filip Rysanek , Paul Fenoglio , Mike Hutches
IPC分类号： C01B13/16 , B01D3/40
CPC分类号： B01D53/002 , B01D2256/12 , C01B13/0248
摘要： A facility and process capable of extracting oxygen in extraterrestrial environments from materials available in extraterrestrial environments, for example, on planets, planetoids, etc. The facility extracts oxygen from a mineral-containing solid material and is configured to form a free-falling molten stream of the solid material, evaporate at least a portion of the molten stream and produce a vapor containing gaseous oxygen, create a supersonic stream of the vapor, condense constituents of the supersonic stream to form particulates within the supersonic stream, separate the gaseous oxygen from the particulates, and then collect the gaseous oxygen.
摘要翻译：能够从外星环境中可用的材料（例如行星，飞机等）中提取地球环境中的氧的设备和方法。该设施从含矿物的固体材料中提取氧气并且被配置成形成自由落下的熔融流蒸发至少一部分熔融流并产生含有气态氧气的蒸汽，产生蒸汽的超音速流，冷凝超声流的成分以在超音速流内形成颗粒，将气态氧从颗粒，然后收集气态氧气。

12. 发明授权

US5924278A Pulsed plasma thruster having an electrically insulating nozzle and utilizing propellant bars 失效
标题翻译：具有电绝缘喷嘴并利用推进剂棒的脉冲等离子体推进器
公开(公告)号：US5924278A
公开(公告)日：1999-07-20
申请号：US832293
申请日：1997-04-03
申请人： Rodney L. Burton , Susan G. Delmedico , Michael Wilson
发明人： Rodney L. Burton , Susan G. Delmedico , Michael Wilson
IPC分类号： F03H1/00
CPC分类号： F03H1/0087 , F03H1/0012
摘要： A thruster includes a body having a cavity with a discharge end, an apparatus for generating an electric arc having a current path through the cavity between first and second locations, and a non-gaseous, non-liquid propellant material (26) that forms an ionized gas as an incident of being heated. The propellant material (26) is heated by the electric arc to produce an ionized gas in the cavity. The cavity is configured to cause the ionized gas to be expelled from the cavity through the discharge end of the cavity in a flow path that is substantially parallel to the electric arc and current path within the cavity. A thruster includes a body having a cavity with a discharge end, a substantially non-ablating, electrically insulating nozzle (30) having an inlet disposed adjacent to the discharge end and an outlet, a first electrode (32) disposed within the cavity, a second electrode (34) disposed adjacent to the outlet of the nozzle, an electric power supply connected to the first and second electrodes to generate an electric arc having a current path therebetween, and a non-gaseous, non-liquid propellant material that forms an ionized gas as an incident of being heated. The propellant material is heated by the electric arc to produce an ionized gas in the cavity. A method of producing plasma to be used to propel a mass includes the steps of providing a cavity with a discharge end, providing a non-gaseous, non-liquid propellant material that forms an ionized gas as an incident of being heated, generating an electric arc having a current path through the cavity between first and second locations, heating the propellant material to produce an ionized gas in the cavity; and expelling the ionized gas from the cavity through the discharge end of the cavity in a flow path that is substantially parallel to the electric arc and current path within the cavity.
摘要翻译：推进器包括具有排放端的空腔的主体，用于产生具有通过第一和第二位置之间的空腔的电流路径的电弧的装置和形成非气态非液体推进剂材料（26）的装置电离气体作为被加热的事件。推进剂材料（26）被电弧加热以在空腔中产生电离气体。空腔构造成使得离子化气体通过空腔的排放端在与空腔内的电弧和电流路径基本平行的流动路径中从腔排出。推进器包括具有排放端的空腔的本体，具有邻近排放端设置的入口和出口的基本上非消融的电绝缘喷嘴（30），设置在空腔内的第一电极（32），与喷嘴的出口相邻设置的第二电极（34），连接到第一和第二电极以产生其间具有电流路径的电弧的电力供应源和形成非气体的非液体推进剂材料电离气体作为被加热的事件。推进剂材料被电弧加热，以在空腔中产生电离气体。一种生产用于推进物料的等离子体的方法包括以下步骤：提供具有放电端的空腔，提供形成电离气体的非气态非液体推进剂材料，作为加热入口，产生电电弧具有通过第一和第二位置之间的空腔的电流路径，加热推进剂材料以在空腔中产生电离气体; 并且通过基本上平行于空腔内的电弧和电流路径的流动路径将来自空腔的电离气体排出空腔的排放端。

13. 发明授权

US4715261A Cartridge containing plasma source for accelerating a projectile 失效
标题翻译：含有等离子体源的墨盒用于加速射弹
公开(公告)号：US4715261A
公开(公告)日：1987-12-29
申请号：US657888
申请日：1984-10-05
申请人： Yeshayahu S. A. Goldstein , Derek A. Tidman , Rodney L. Burton , Dennis W. Massey , Niels K. Winsor
发明人： Yeshayahu S. A. Goldstein , Derek A. Tidman , Rodney L. Burton , Dennis W. Massey , Niels K. Winsor
IPC分类号： F41B6/00 , F41F1/00
CPC分类号： F41B6/00
摘要： A projectile is accelerated through a gun barrel bore by a cartridge containing a high temperature, high pressure plasma jet source. The cartridge has a geometry enabling it to be loaded into a breech bore of the gun. The plasma jet is supplied to the rear of the projectile and is derived by a tube having an interior wall forming a capillary passage. A discharge voltage applied between spaced regions along the capillary passage ionizes a dielectric to form a plasma. First and second ends of the passage are respectively open and blocked to enable and prevent the flow of plasma through them. The blocked end closes the breech bore.
摘要翻译：射弹通过枪管加速，内置高温高压等离子体喷射源。墨盒具有几何形状，使其能够被装载到枪的后膛孔中。等离子体射流被提供到射弹的后部，并由具有形成毛细管通道的内壁的管导出。沿着毛细通道施加在间隔区域之间的放电电压使电介质离子化以形成等离子体。通道的第一和第二端分别是开放和封闭的，以使等离子体流过它们。封闭端封闭后膛孔。

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