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公开(公告)号：US20130047578A1
公开(公告)日：2013-02-28
申请号：US13223041
申请日：2011-08-31
CPC分类号： B64G1/402 , B64G1/404 , F02K9/72 , F02K9/94 , F03H1/00 , F03H1/0006 , F03H1/0012 , F03H1/0043 , F03H1/005 , F03H1/0062 , F03H1/0068 , F03H1/0075
摘要： A spacecraft propulsion system has at least one chemical thruster, at least one electric thruster, a propellant supply arrangement that stores a propellant and a propellant conditioning arrangement configured to convert propellant into chemical species in a thermodynamic phase that can be readily ionized. The propellant is commonly supplied from the propellant storage device to each of the chemical thruster and the electric thruster. The chemical thruster has a gas generator and a high thrust accelerator; the electric thruster has a plasma generator and a high specific impulse accelerator. The propellant supply arrangement is configured to control flow of the propellant from the propellant supply arrangement to the gas generator and the propellant conditioning arrangement, and a first flow path connects propellant supply arrangement with the gas generator, and a second flow path connects propellant supply arrangement with the plasma generator.
摘要翻译： 航天器推进系统具有至少一个化学推进器，至少一个电推进器，推进剂供应装置，其存储推进剂和推进剂调节装置，所述推进剂调节装置构造成将推进剂转化为能容易地电离的热力学相中的化学物质。 推进剂通常从推进剂储存装置提供给每个化学推进器和电推进器。 化学推进器具有气体发生器和高推力加速器; 电推进器具有等离子体发生器和高比冲速加速器。 推进剂供应装置被配置为控制推进剂从推进剂供应装置到气体发生器和推进剂调节装置的流动，并且第一流动路径将推进剂供应装置与气体发生器连接，第二流动路径连接推进剂供应装置 与等离子发生器。
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公开(公告)号：US20120167548A1
公开(公告)日：2012-07-05
申请号：US13203774
申请日：2011-05-27
申请人： Aaron Kombai Knoll
发明人： Aaron Kombai Knoll
IPC分类号： F03H1/00
CPC分类号： F03H1/0056 , F03H1/00 , F03H1/0037 , F03H1/0062 , F03H1/0068 , F03H1/0075
摘要： A plasma thruster includes a plasma chamber having first and second axial ends, the first of which is open, an anode located at the second axial end, and a cathode. The cathode and anode are arranged to produce an electric field having at least a component in the axial direction of the thruster. A magnet system including a plurality of magnets is spaced around the thruster axis, each magnet having its north and south poles spaced around the axis.
摘要翻译： 等离子体推进器包括等离子体室，其具有第一和第二轴向端部，第一和第二轴向端部，第一轴向端部是敞开的，位于第二轴向端部的阳极和阴极。 阴极和阳极被布置成产生至少在推进器的轴向方向上的分量的电场。 包括多个磁体的磁体系统围绕推进器轴线间隔开，每个磁体的北极和南极围绕轴线间隔开。
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公开(公告)号：US20100107596A1
公开(公告)日：2010-05-06
申请号：US12513916
申请日：2007-11-11
IPC分类号： F03H1/00
CPC分类号： F03H1/0075
摘要： A low power hall thruster is provided that is effective for micro-spacecrafts and nano-spacecrafts as well as mini-spacecrafts. The hall thruster comprises a co-axial acceleration channel capable of being applied with predominantly-radial magnetic field and a co-axial anode within a cavity capable of being applied with substantially longitudinal magnetic field. A cathode-compensator is placed beyond the acceleration channel and magnetic system is provided capable of generating the radial magnetic field within the co-axial acceleration channel and the longitudinal magnetic field within the co-axial anode. An electrically isolated gas distributor is also provided.
摘要翻译： 提供了一种低功率霍尔推进器，对微型航天器和纳米航天器以及微型航天器有效。 霍尔推进器包括能够施加主要径向磁场的同轴加速通道和能够施加基本上纵向磁场的空腔内的同轴阳极。 阴极补偿器放置在加速通道之外，并且提供磁系统，其能够在同轴加速通道内和同轴阳极内的纵向磁场产生径向磁场。 还提供了电气隔离的气体分配器。
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公开(公告)号：US07579780B2
公开(公告)日：2009-08-25
申请号：US11866062
申请日：2007-10-02
IPC分类号： H05B31/26
CPC分类号： H05H1/54 , F03H1/0018 , F03H1/0075 , H05H7/00
摘要： A power supply apparatus for controlling an ion accelerator includes a controller configured to adjust magnitude of ion acceleration in the ion accelerator. The controller controls an anode voltage applied to an anode electrode of the ion accelerator, a gas flow rate of gas flowing through a gas flow rate regulator of the ion accelerator, and magnetic flux density at an ion exit of the ion accelerator to satisfy a formula given as follows: 500 × 10 9
摘要翻译： 用于控制离子加速器的电源装置包括控制器，其被配置为调节离子加速器中的离子加速度的大小。 控制器控制施加到离子加速器的阳极的阳极电压，流过离子加速器的气体流量调节器的气体的气体流量和离子加速器的离子出口处的磁通密度，以满足公式 给出如下：
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公开(公告)号：US07560870B2
公开(公告)日：2009-07-14
申请号：US11613479
申请日：2006-12-20
IPC分类号： H01J27/02
CPC分类号： H05H1/54 , F03H1/0018 , F03H1/0075
摘要： A power supply apparatus for controlling a Hall thruster which is an ion accelerator includes an anode power supply for applying anode voltage Va to an anode of the Hall thruster, inner and outer coil power supplies for supplying coil current Ic to each of inner and outer magnetic field generating coils of the Hall thruster, a gas flow rate controller for regulating gas flow rate Q via a gas flow rate regulator, and a control unit. The control unit adjusts the magnitude of ion acceleration by the Hall thruster by controlling the anode voltage Va, the gas flow rate Q and the coil current Ic according to a quantity expressed by a function related to the anode voltage Va and the coil current Ic.
摘要翻译： 用于控制作为离子加速器的霍尔推进器的电源装置包括用于将阳极电压Va施加到霍尔推进器的阳极的阳极电源，用于将线圈电流Ic提供给内部和外部磁体的内部和外部线圈电源 霍尔推进器的场产生线圈，用于通过气体流量调节器调节气体流量Q的气体流量控制器和控制单元。 控制单元通过根据与阳极电压Va和线圈电流Ic相关的函数表示的量来控制阳极电压Va，气体流量Q和线圈电流Ic来调节霍尔推进器的离子加速度的大小。
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公开(公告)号：US20090134804A1
公开(公告)日：2009-05-28
申请号：US11998083
申请日：2007-11-28
CPC分类号： H05H1/54 , F03H1/0075
摘要： The present patent letters discloses a Hall Current accelerator with a solenoid Hall field, a collimated gas source, an anode, intermediate Hall effect ionization magnetic field structures and intermediate acceleration electrodes. The Hall field in this case is the end cusp field(s) of a common solenoid magnetic field.
摘要翻译： 本专利文献公开了具有螺线管霍尔场，准直气源，阳极，中间霍尔效应电离磁场结构和中间加速电极的霍尔电流加速器。 在这种情况下，霍尔场是公共电磁铁磁场的末端尖点场。
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公开(公告)号：US07500350B1
公开(公告)日：2009-03-10
申请号：US11044471
申请日：2005-01-28
CPC分类号： H05H1/54 , F03H1/0075
摘要： A Hall thruster includes inner and outer electromagnets, with the outer electromagnet circumferentially surrounding the inner electromagnet along a centerline axis and separated therefrom, inner and outer poles, in physical connection with their respective inner and outer electromagnets, with the inner pole having a mostly circular shape and the outer pole having a mostly annular shape, a discharge chamber separating the inner and outer poles, a combined anode electrode/gaseous propellant distributor, located at an upstream portion of the discharge chamber and supplying propellant gas and an actuator, in contact with a sleeve portion of the discharge chamber. The actuator is configured to extend the sleeve portion or portions of the discharge chamber along the centerline axis with respect to the inner and outer poles.
摘要翻译： 霍尔推进器包括内部和外部电磁体，其中外部电磁体沿着中心线轴向周向地包围内部电磁体并与其分离，内部和外部磁极与它们各自的内部和外部电磁体物理连接，内部极大部分为圆形 形状，外极具有大致环形形状，分隔内极和外极的放电室，组合的阳极电极/气体推进剂分配器，其位于排放室的上游部分并且供应推进剂气体和致动器，其与 排出室的套筒部分。 致动器构造成使排出室的套筒部分或部分沿着相对于内极和外极的中心线轴线延伸。
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公开(公告)号：US07459858B2
公开(公告)日：2008-12-02
申请号：US11301857
申请日：2005-12-13
申请人： Vladimir J. Hruby , Bruce Pote , Rachel A. Tedrake , Lawrence T. Byrne , James J. Szabo, Jr. , Juraj Kolencik
发明人： Vladimir J. Hruby , Bruce Pote , Rachel A. Tedrake , Lawrence T. Byrne , James J. Szabo, Jr. , Juraj Kolencik
CPC分类号： F03H1/0075 , H05H1/54
摘要： A Hall thruster with a shared magnetic structure including a plurality of plasma accelerators each including an anode and a discharge zone for providing plasma discharge. An electrical circuit having one or more cathodes connected to the plurality of plasma accelerators emits electrons that are attracted to the anode in each of the plasma accelerators. A shared magnetic circuit structure establishes a transverse magnetic field in each of the plurality of plasma accelerators that creates an impedance to the flow of electrons toward the anode in each of the plurality of plasma accelerators and enables ionization of a gas moving through one or more of the plurality of plasma accelerators. The impedance localizes an axial electric field in the plurality of plasma accelerators for accelerating ionized gas through the one or more of the plurality of plasma accelerators to create thrust.
摘要翻译： 具有共享磁性结构的霍尔推进器，其包括多个等离子体加速器，每个等离子体加速器包括用于提供等离子体放电的阳极和放电区域。 具有连接到多个等离子体加速器的一个或多个阴极的电路发射在每个等离子体加速器中被吸引到阳极的电子。 共享磁路结构在多个等离子体加速器中的每一个中建立横向磁场，该多个等离子体加速器在多个等离子体加速器中的每个等离子体加速器中产生电流朝向阳极的阻抗，并且能够电离通过一个或多个 多个等离子体加速器。 所述阻抗使多个等离子体加速器中的轴向电场定位，用于加速通过所述多个等离子体加速器中的一个或多个的离子化气体以产生推力。
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89.发明授权Combined radio frequency and hall effect ion source and plasma accelerator system 有权组合射频和霍尔效应离子源和等离子加速器系统公开(公告)号：US07420182B2
公开(公告)日：2008-09-02
申请号：US11412619
申请日：2006-04-27
申请人： Vladimir Hruby , Kurt Hohman , Thomas Brogan
发明人： Vladimir Hruby , Kurt Hohman , Thomas Brogan
IPC分类号： H01J27/00
CPC分类号： H01J27/143 , F03H1/0075 , H01J27/16 , H05H1/54
摘要： This invention features a combined radio frequency (RF) and Hall Effect ion source and plasma accelerator system including a plasma accelerator having an anode and a discharge zone, the plasma accelerator for providing plasma discharge. A gas distributor introduces a gas into the plasma accelerator. A cathode emits electrons attracted to the anode for ionizing the gas and neutralizing ion flux emitted from the plasma accelerator. An electrical circuit coupled between the anode and the cathode having a DC power source provides DC voltage. A magnetic circuit structure including a magnetic field source establishes a transverse magnetic field in the plasma accelerator that creates an impedance to the flow of the electrons toward the anode to enhance ionization of the gas to create plasma and which in combination with the electric circuit establishes an axial electric field in the plasma accelerator. An RF power source provides RF power to at least one electrode disposed about and/or inside the plasma accelerator that induces current for ionizing the gas to create the plasma such that the axial electric field accelerates ions through the plasma accelerator to provide ion flux.
摘要翻译： 本发明的特征在于组合射频（RF）和霍尔效应离子源和等离子体加速器系统，其包括具有阳极和放电区域的等离子体加速器，用于提供等离子体放电的等离子体加速器。 气体分配器将气体引入等离子体加速器。 阴极发射吸附到阳极的电子，用于电离气体并中和从等离子体加速器发射的离子通量。 耦合在具有DC电源的阳极和阴极之间的电路提供DC电压。 包括磁场源的磁路结构在等离子体加速器中形成横向磁场，该横向磁场对电子向阳极的流动产生阻抗，以增强气体的电离以产生等离子体，并且与电路组合形成等离子体 等离子体加速器中的轴向电场。 射频功率源向等离子体加速器周围和/或内部设置的至少一个电极提供RF功率，该电极引起用于电离气体的电流以产生等离子体，使得轴向电场通过等离子体加速器加速离子以提供离子通量。
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公开(公告)号：US20070145901A1
公开(公告)日：2007-06-28
申请号：US11613479
申请日：2006-12-20
IPC分类号： H01J7/24
CPC分类号： H05H1/54 , F03H1/0018 , F03H1/0075
摘要： A power supply apparatus for controlling a Hall thruster which is an ion accelerator includes an anode power supply for applying anode voltage Va to an anode of the Hall thruster, inner and outer coil power supplies for supplying coil current Ic to each of inner and outer magnetic field generating coils of the Hall thruster, a gas flow rate controller for regulating gas flow rate Q via a gas flow rate regulator, and a control unit. The control unit adjusts the magnitude of ion acceleration by the Hall thruster by controlling the anode voltage Va, the gas flow rate Q and the coil current Ic according to a quantity expressed by a function related to the anode voltage Va and the coil current Ic.
摘要翻译： 用于控制作为离子加速器的霍尔推进器的电源装置包括用于将阳极电压Va施加到霍尔推进器的阳极的阳极电源，用于将线圈电流Ic提供给内部和外部磁体的内部和外部线圈电源 霍尔推进器的场产生线圈，用于经由气体流量调节器调节气体流量Q的气体流量控制器和控制单元。 控制单元通过根据与阳极电压Va和线圈电流Ic相关的函数表示的量来控制阳极电压Va，气体流量Q和线圈电流Ic来调节霍尔推进器的离子加速度的大小。
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