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    • 2. 发明申请
    • Electron-Coupled Transformer
    • 电子耦合变压器
    • US20150255210A1
    • 2015-09-10
    • US14718334
    • 2015-05-21
    • Advanced Fusion Systems LLC
    • Curtis A. Birnbach
    • H01F38/00
    • H01F38/00G21B1/00G21B1/03G21B1/23G21D7/00H05G2/001Y02E30/14
    • An Electron-coupled transformer for generating a high voltage output pulse as an amplified version of an input pulse comprises a cylindrical triode electron tube with a central anode along main axis and a grid and cathode radially spaced from the anode. The anode has a first end connected to ground and a second end insulated with respect to said ground. The cathode and the grid form a traveling wave electron gun that produces a wave of ground potential in the Transverse Electric Mode, which causes electrons stored in the cathode-grid gap to be extracted from said gap. The extracted electrons form a radially symmetric collapsing traveling wave that sweeps as a wave along the anode at the speed of light, causing a voltage output pulse on the second end of the anode whose magnitude is an amplified version of an input pulse applied to the cathode.
    • 用于产生作为输入脉冲的放大版本的高电压输出脉冲的电子耦合变压器包括具有沿着主轴线的中心阳极和与阳极径向间隔开的栅极和阴极的圆柱形三极管电子管。 阳极具有连接到地的第一端和相对于所述接地绝缘的第二端。 阴极和栅格形成行横波电子枪,其在横向电模式中产生接地电位波,这导致存储在阴极栅格间隙中的电子从所述间隙中提取。 提取的电子形成径向对称的塌缩行波,其以光速沿着阳极扫过波,从而在阳极的第二端产生电压输出脉冲,其大小是施加到阴极的输入脉冲的放大形式 。
    • 3. 发明申请
    • APPARATUS AND PROCESS FOR PENETRATION OF THE COULOMB BARRIER
    • 装置框架的设备和方法
    • US20130287156A1
    • 2013-10-31
    • US13870239
    • 2013-04-25
    • Azaroghly YAZDANBOD
    • Azaroghly YAZDANBOD
    • G21B1/00
    • G21B1/00G21B3/006
    • A device and method for penetrating the Coulomb barrier is disclosed. An electrode is positioned within a hollow shell, the shell enclosing an inner space containing a fusion reactive fuel such as deuterium. The inner space with the fuel is coaxially centered about the electrode, and a confinement layer made of a high dielectric strength material is located at the outer edge of the inner space, on the inside surface of the spherical shell. A high voltage power source charges the electrode, which causes a tightly packed fusion fuel nucleus cloud such as a deuteron cloud to form on the inner face of the confinement layer, facilitating coulomb barrier penetration. Using the device of the invention, conditions can also be created which enable Coulomb barrier penetration by firing nuclei towards the cloud of nuclei by applying high voltage pulses to the electrode.
    • 公开了一种用于穿透库仑屏障的装置和方法。 电极位于中空壳体内,壳体包围含有诸如氘的融合反应性燃料的内部空间。 具有燃料的内部空间以电极为中心,并且由高介电强度材料制成的限制层位于球形外壳的内表面上的内部空间的外边缘。 高压电源为电极充电,这导致紧密封装的融合燃料核云如氘云在限制层的内表面上形成,有利于库仑势垒穿透。 使用本发明的装置,也可以产生条件,其通过向电极施加高电压脉冲使得核向核的核发射库仑屏障穿透。
    • 5. 发明申请
    • Aircraft also called a spacecraft, an aerospace craft, or a submersible craft
    • 飞机还称为航天器,航空航天工具或潜水艇
    • US20100243816A1
    • 2010-09-30
    • US12661559
    • 2010-03-19
    • Gary Richard Gochnour
    • Gary Richard Gochnour
    • B64G1/40
    • B64C39/001B64C29/0025B64D27/22B64G1/405B64G1/422G21B1/00H02K7/1823H05H1/54Y02E30/10
    • The invention relates to a plasma based aircraft maintained in a flight mode by rotating plasma vortices located above and beneath said aircraft. Said aircraft is comprised of chromium steel, or higher ferrochromium steel can be used. Said aircraft receives energy from aircraft produced plasma obtained from the atmosphere.Produced energy is stored within craft oscillatory circuit and plasma vortices. When energy from craft capacitance system is depleting, energy can be obtained from craft inductance system from craft magnetic field.Said craft is capable of space flight, use as a submersible craft, boring device, or lifting device. Particle propulsion in space will be accomplished utilizing metal ions stored within craft capacitor plates.Said craft is opaque to electromagnetic radiation, and also absorbs radiation directed at craft.Said craft is capable of verticle ascent, descent and landing, and is lenticular in shape.Said aircraft can operate within earth radiation belts safely.
    • 本发明涉及通过旋转位于所述飞机上方和下方的等离子体旋涡来维持飞行模式的基于等离子体的飞行器。 所述飞机由铬钢组成,也可使用较高的铬铁钢。 所述飞机从大气中获得的飞机产生的等离子体获得能量。 产生的能量存储在工艺振荡电路和等离子体旋涡中。 当工艺电容系统的能量耗尽时,能从工艺磁场的工艺电感系统获得能量。 所述工艺能够进行太空飞行,用作潜水艇,钻孔装置或起重装置。 使用存储在工艺电容器板内的金属离子将实现空间中的粒子推进。 所述工艺对电磁辐射是不透明的,并且还吸收指向工艺的辐射。 所述工艺能够垂直上升,下降和着陆,并且具有透镜形状。 所述飞机可以安全地操作地球辐射带。
    • 6. 发明申请
    • Controlled fusion in a field reversed configuration and direct energy conversion
    • 控制融合在一个领域反向配置和直接能量转换
    • US20100002823A1
    • 2010-01-07
    • US12380012
    • 2009-02-20
    • Hendrik J. MonkhorstNorman Rostoker
    • Hendrik J. MonkhorstNorman Rostoker
    • G21B1/05
    • H05H1/12G21B1/00G21B1/052G21B1/11G21D7/00H05H1/14Y02E30/122Y02E30/126
    • A system and apparatus for controlled fusion in a field reversed configuration (FRC) magnetic topology and conversion of fusion product energies directly to electric power. Preferably, plasma ions are magnetically confined in the FRC while plasma electrons are electrostatically confined in a deep energy well, created by tuning an externally applied magnetic field. In this configuration, ions and electrons may have adequate density and temperature so that upon collisions ions are fused together by the nuclear force, thus forming fusion products that emerge in the form of an annular beam. Energy is removed from the fusion product ions as they spiral past electrodes of an inverse cyclotron converter. Advantageously, the fusion fuel plasmas that can be used with the present confinement and energy conversion system include advanced (aneutronic) fuels.
    • 用于在场反向配置(FRC)磁拓扑中的受控融合并将融合产物能量直接转换为电力的系统和装置。 优选地,等离子体离子被磁力限制在FRC中,而等离子体电子通过调谐外部施加的磁场而被静电限制在深能量阱中。 在这种结构中,离子和电子可以具有足够的密度和温度,使得在碰撞时,离子通过核力熔合在一起,从而形成以环形束形式出现的熔融产物。 当它们旋转通过反向回旋加速器的电极时,能量从熔融产物离子中去除。 有利地,可以与本限制和能量转换系统一起使用的熔融燃料等离子体包括先进的(非经济的)燃料。
    • 7. 发明授权
    • Controlled fusion in a field reversed configuration and direct energy conversion
    • 控制融合在一个领域反向配置和直接能量转换
    • US07459654B2
    • 2008-12-02
    • US10979598
    • 2004-11-01
    • Hendrik J. MonkhorstNorman Rostoker
    • Hendrik J. MonkhorstNorman Rostoker
    • B23K9/00
    • H05H1/12G21B1/00G21B1/052G21B1/11G21D7/00H05H1/14Y02E30/122Y02E30/126
    • A system and apparatus for controlled fusion in a field reversed configuration (FRC) magnetic topology and conversion of fusion product energies directly to electric power. Preferably, plasma ions are magnetically confined in the FRC while plasma electrons are electrostatically confined in a deep energy well, created by tuning an externally applied magnetic field. In this configuration, ions and electrons may have adequate density and temperature so that upon collisions they are fused together by the nuclear force, thus forming fusion products that emerge in the form of an annular beam. Energy is removed from the fusion product ions as they spiral past electrodes of an inverse cyclotron converter. Advantageously, the fusion fuel plasmas that can be used with the present confinement and energy conversion system include advanced (aneutronic) fuels.
    • 用于在场反向配置(FRC)磁拓扑中的受控融合并将融合产物能量直接转换为电力的系统和装置。 优选地,等离子体离子被磁力限制在FRC中,而等离子体电子通过调谐外部施加的磁场而被静电限制在深能量阱中。 在这种结构中,离子和电子可以具有足够的密度和温度,使得在碰撞时它们被核力熔合在一起,从而形成以环形束形式出现的熔融产物。 当它们旋转通过反向回旋加速器的电极时,能量从熔融产物离子中去除。 有利地,可以与本限制和能量转换系统一起使用的熔融燃料等离子体包括先进的(非经济的)燃料。
    • 8. 发明授权
    • Controlled fusion in a field reversed configuration and direct energy conversion
    • 控制融合在一个领域反向配置和直接能量转换
    • US07232985B2
    • 2007-06-19
    • US11130856
    • 2005-05-16
    • Hendrik J. MonkhorstNorman Rostoker
    • Hendrik J. MonkhorstNorman Rostoker
    • H01J40/14
    • H05H1/12G21B1/00G21B1/052G21B1/11G21D7/00H05H1/14Y02E30/122Y02E30/126
    • A system and apparatus for controlled fusion in a field reversed configuration (FRC) magnetic topology and conversion of fusion product energies directly to electric power. Preferably, plasma ions are magnetically confined in the FRC while plasma electrons are electrostatically confined in a deep energy well, created by tuning an externally applied magnetic field. In this configuration, ions and electrons may have adequate density and temperature so that upon collisions they are fused together by the nuclear force, thus forming fusion products that emerge in the form of an annular beam. Energy is removed from the fusion product ions as they spiral past electrodes of an inverse cyclotron converter. Advantageously, the fusion fuel plasmas that can be used with the present confinement and energy conversion system include advanced (aneutronic) fuels.
    • 用于在场反向配置(FRC)磁拓扑中的受控融合并将融合产物能量直接转换为电力的系统和装置。 优选地,等离子体离子被磁力限制在FRC中,而等离子体电子通过调谐外部施加的磁场而被静电限制在深能量阱中。 在这种结构中,离子和电子可以具有足够的密度和温度,使得在碰撞时它们被核力熔合在一起,从而形成以环形束形式出现的熔融产物。 当它们旋转通过反向回旋加速器的电极时,能量从熔融产物离子中去除。 有利地,可以与本限制和能量转换系统一起使用的熔融燃料等离子体包括先进的(非经济的)燃料。
    • 9. 发明申请
    • Fusion energy system and plasma propulsion aircraft to produce electricity from a controlled nuclear fusion reaction
    • 融合能量系统和等离子体推进飞机从受控的核聚变反应产生电力
    • US20060102795A1
    • 2006-05-18
    • US11137643
    • 2005-05-25
    • Gary Gochnour
    • Gary Gochnour
    • B64G1/40
    • B64C39/001B64C29/0025B64D27/22B64G1/405B64G1/422G21B1/00H02K7/1823H05H1/54Y02E30/10
    • The invention relates to plasma based aircraft maintained in a flight-mode by an uplifting Larmor gyro orbiting particle field, and an extensive capacitor system. Said aircraft is comprised of chromium steel, or higher ferrochromium steel can also be used. Said aircraft system can operate utilizing only energy required to initiate operation of said craft. The energy to start said craft is from energy stored within said capacitor system, and said energy also obtained from the operating environment. Said craft, is immediately capable of space flight, use as a submersible craft, or use as an energy source in an artificial environment. Said craft is opaque, invisible within the visible spectrum, invisible to electromagnetic radiation, and absorbs radiation it produces. Said aircraft is capable of soundless flight. Said aircraft is capable of verticle ascent, descent and landing. Said aircraft can operate within earth radiation belts. Said aircraft is capable of speeds in excess of the fastest aerodynamic aircraft, said aircraft navigates within a particle field at a faster rate than conventional aerodyamic aircraft within the atmosphere. Said aircraft, with two larger, faster aircraft, comprised of magnesium aluminum material, can attain ignition of a formed fusion spherical plasma on roof of said ferromagnetic, smaller craft, utilizing the fuels boron B-11 isotope and regular hydrogen with no radiation, cooling needed.
    • 本发明涉及通过提升Larmor陀螺运动轨道粒子场维持在飞行模式中的基于等离子体的飞行器以及广泛的电容器系统。 所述飞机由铬钢组成,也可使用较高的铬铁。 所述飞行器系统可以仅利用所需的能量来启动所述飞行器的操作。 启动所述工艺的能量来自存储在所述电容器系统内的能量,并且所述能量也从操作环境获得。 所述工艺,立即能够进行太空飞行,用作潜水艇,或在人造环境中用作能源。 所述工艺是不透明的,在可见光谱内不可见,电磁辐射不可见,并吸收其产生的辐射。 所说的飞机能够无声飞行。 所述飞机能够上升,下降和降落。 所述飞机可以在地球辐射带内操作。 所述飞机能够超过最快的空气动力飞机的速度,所述飞机在颗粒场内以比大气中的常规空气动力飞机更快的速度航行。 所述飞机具有两个更大,更快的飞机,包括镁铝材料,可以利用所述铁磁体,较小的工艺的屋顶上的形成的熔化球形等离子体点燃,利用燃料硼B-11同位素和常规氢气,无辐射,冷却 需要的