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1. 发明申请

US20100243816A1 Aircraft also called a spacecraft, an aerospace craft, or a submersible craft 审中-公开
标题翻译：飞机还称为航天器，航空航天工具或潜水艇
公开(公告)号：US20100243816A1
公开(公告)日：2010-09-30
申请号：US12661559
申请日：2010-03-19
申请人： Gary Richard Gochnour
发明人： Gary Richard Gochnour
IPC分类号： B64G1/40
CPC分类号： B64C39/001 , B64C29/0025 , B64D27/22 , B64G1/405 , B64G1/422 , G21B1/00 , H02K7/1823 , H05H1/54 , Y02E30/10
摘要： 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.
摘要翻译：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。

2. 发明申请

US20100294881A1 Electrolysis system 审中-公开
标题翻译：电解系统
公开(公告)号：US20100294881A1
公开(公告)日：2010-11-25
申请号：US12661574
申请日：2010-03-19
申请人： Gary Richard Gochnour
发明人： Gary Richard Gochnour
IPC分类号： B64C39/00
CPC分类号： B64C39/001 , B64C29/0025 , B64D27/22 , B64G1/405 , B64G1/422 , G21B1/00 , H02K7/1823 , H05H1/54 , Y02E30/10
摘要： The invention relates to an electrolysis system. Said system can be utilized in a nuclear fusion process, on roof of a ferromagnetic aircraft in preferred embodiment.Said electrolysis system will utilize electric energy produced by said aircraft at no cost. Said energy will be provided to an array of electrodes to electrolyze water or seawater to produce protons and electrons, and with B-11 isotope ions, vaporized out of source on board craft, a fusion spherical plasma can be produced on roof of said aircraft, for a nuclear fusion reaction. Stored energy produced by electrolysis system, can also be used for other purposes.Said fusion spherical plasma is produced at essentially no cost, other than cost of electrolysis system and aircraft.Three aircraft will be utilized in preferred embodiment, all three craft utilizing an electrolysis system, though only one craft, the ferromagnetic craft alone, producing the B-11 isotope ion.
摘要翻译：本发明涉及一种电解系统。所述系统可以在优选实施例中在铁磁飞机的屋顶上的核聚变过程中使用。所述电解系统将以免费的方式利用所述飞机产生的电能。所述能量将被提供给电极阵列以电解水或海水以产生质子和电子，并且与B-11同位素离子从船上的源头蒸发出来，可以在所述飞行器的屋顶上产生融合的球形等离子体，用于核聚变反应。由电解系统产生的储能也可用于其他用途。除了电解系统和飞机的成本之外，所述熔融球形等离子体基本上没有成本地生产。在优选实施例中将使用三架飞机，所有这三种技术利用电解系统，尽管只有一种工艺，单独的铁磁工艺，产生B-11同位素。

3. 发明申请

US20110000185A1 Fusion energy process 审中-公开
标题翻译：融合能量过程
公开(公告)号：US20110000185A1
公开(公告)日：2011-01-06
申请号：US12661556
申请日：2010-03-19
申请人： Gary Richard Gochnour
发明人： Gary Richard Gochnour
IPC分类号： F03H99/00 , F03H1/00
CPC分类号： B64C39/001 , B64C29/0025 , B64D27/22 , B64G1/405 , B64G1/422 , G21B1/00 , H02K7/1823 , H05H1/54 , Y02E30/10
摘要： This invention relates to a nuclear fusion reaction process utilizing a B-11 isotope ion spherical plasma. Said spherical plasma will be formed on roof of a ferromagnetic chromium steel hulled aircraft, utilizing two larger magnesium based aircraft.Said spherical plasma is formed by raising a pyramid shaped device with a slotted glass ball electrode on top, on roofs of said air-craft. Only the smaller craft will utilize the fusion fuels, B-11 isotope ion and H-1 atom, in forming said spherical plasmas.The two larger craft will apply pressure toward smaller craft, and coalesce their plasmas into the smaller plasma.By forming this induced magnetic field, an electron current existing in larger applied magnetic field, is raised to middle of smaller aircraft spherical plasma.Ignition can be accomplished with land based neutral beam, FIG. 15. Produced energetic charged particles, electric energy, can be stored within craft plasma vortices and beamed to power stations.
摘要翻译：本发明涉及利用B-11同位素离子球形等离子体的核聚变反应方法。所述球形等离子体将在铁磁铬钢船体的屋顶上形成，使用两台较大的镁基飞机。所述球形等离子体是通过在顶部具有开槽玻璃球电极的顶角上升高金字塔形的装置而形成的。只有较小的工艺才能使用聚合燃料B-11同位素和H-1原子来形成所述球形等离子体。两个较大的工艺将对较小的工艺施加压力，并将其等离子体聚结成更小的等离子体。通过形成这种感应磁场，存在于较大施加磁场中的电子电流升高到较小的飞机球形等离子体的中间。点火可以用陆基中性束实现， 15.产生能量的带电粒子，电能可以存储在工艺等离子体旋涡中并且被发射到发电站。

4. 发明申请

US20100243796A1 Plasma gun system utilizing an aerospace craft 审中-公开
标题翻译：等离子枪系统利用航空航天工艺
公开(公告)号：US20100243796A1
公开(公告)日：2010-09-30
申请号：US12661572
申请日：2010-03-19
申请人： Gary Richard Gochnour
发明人： Gary Richard Gochnour
IPC分类号： B64C39/00
CPC分类号： B64C39/001 , B64C29/0025 , B64D27/22 , B64G1/405 , B64G1/422 , G21B1/00 , H02K7/1823 , H05H1/54 , Y02E30/10
摘要： This invention relates to a plasma gun utilized in a plasma based aircraft maintained in a flight mode by rotating plasma vortices located above and beneath said aircraft. Plasma produced by aircraft is utilized by said plasma gun to facilitate initial take off of craft, and also to accelerate aircraft speed, or, within an emergency, as needed.Said aircraft can also eject plasma through aircraft central shaft or within any direction from sides of said craft, for escape, evasion or normal accelerated flight.Preferred embodiment for said plasma gun, is a coaxial plasma gun, utilizing the large capacitance potential of aircraft, the large supply of aircraft produced plasma off said capacitors, or from uninsulated conducting wires, and also utilizing the strong Lorentz force existing within craft.The plasma produced by ionization within craft strong magnetic field, will enable this craft to rapidly avoid impediments to flight, or oncoming dangers.
摘要翻译：本发明涉及一种等离子体枪，其用于通过旋转位于所述飞行器上方和下方的等离子体涡旋而保持在飞行模式中的等离子体飞行器。所述等离子体枪利用飞行器产生的等离子体，以便于初始起飞，并根据需要在紧急情况下加速飞行器速度。所述飞机还可以通过飞行器中心轴或从所述飞行器的侧面的任何方向喷射等离子体，以用于逃逸，逃避或正常的加速飞行。用于所述等离子体枪的优选实施例是同轴等离子体枪，利用飞机的大电容势，大量供应的飞机从所述电容器产生等离子体，或者从非绝缘导线产生等离子体，还利用存在于工艺中的强洛伦兹力。在工艺强磁场内通过电离产生的等离子体将使该工艺能够快速避免飞行障碍或迎接危险。

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