公开(公告)号：US20170025935A1

公开(公告)日：2017-01-26

申请号：US14807943

申请日：2015-07-24

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: H02K33/00 ,  H02K41/02

CPC classification number: H02N11/002 ,  B64G1/52 ,  B64G1/66 ,  B64G9/00 ,  H02N99/00

Abstract: The electromagnetic field generator includes a shell, an electrostatic generator, a power plant, a thermoelectric generator, and an electric motor. The shell has embedded polycrystalline ferroelectric ceramic material which is polarized such that the ceramic material exhibits strong Piezoelectric Effect properties thus inducing high frequency vibrations. The shell may be further doped with radioactive elements which under high frequency vibrations induce gamma ray emission. The electrostatic generator is for charging up the shell and is disposed within the shell. The power plant is to generate thermal power, and is disposed within the sphere. The thermoelectric generator is to convert the thermal power generated by the power plant to electrical energy. The electric motor powered by the electrical energy generated by the thermoelectric generator, and supplies input voltage such that the shell spins at high angular speeds, vibrates at high frequencies, and generates an electromagnetic field.

Abstract translation: 电磁场发生器包括外壳，静电发生器，发电厂，热电发电机和电动马达。 壳体具有嵌入的多晶铁电陶瓷材料，其极化，使得陶瓷材料表现出强的压电效应，从而引起高频振动。 壳可以进一步掺杂放射性元素，其在高频振动下引起γ射线发射。 静电发生器用于对壳体充电并且设置在壳体内。 发电厂将产生火力，并设置在球体内。 热电发电机将发电厂产生的火电转换为电能。 电动马达由热电发电机产生的电能供电，并提供输入电压使壳体以高角速度旋转，并以高频率振动，产生电磁场。

公开(公告)号：US20190295733A1

公开(公告)日：2019-09-26

申请号：US15928703

申请日：2018-03-22

Applicant: SALVATORE PAIS

Inventor： SALVATORE PAIS

IPC: G21B1/05 ,  G21B1/17 ,  G21B1/21

Abstract: A plasma compression fusion device which includes a hollow duct and at least one pair of opposing counter-spinning dynamic fusors. The hollow duct includes a vacuum chamber disposed within the hollow duct. Each dynamic fusor has a plurality of orifices and an outer surface which is electrically charged. In combination, the pair(s) of dynamic fusors create a concentrated magnetic energy flux and electromagnetic radiation within the vacuum chamber, whereby the concentrated magnetic energy flux compresses a mixture of gases that are injected through the orifices to the vacuum chamber such that a plasma core is created, and the to electromagnetic radiation heats the plasma core, while produced magnetic fields confine the plasma core between the dynamic fusors, such that when an additional mixture of gases is introduced into the plasma core through the orifices, an energy gain is created.

公开(公告)号：US10135366B2

公开(公告)日：2018-11-20

申请号：US14807943

申请日：2015-07-24

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: H01L41/113 ,  H02N11/00 ,  B64G1/52 ,  B64G1/66 ,  B64G99/00 ,  H02N99/00

Abstract: The electromagnetic field generator includes a shell, an electrostatic generator, a power plant, a thermoelectric generator, and an electric motor. The shell has embedded polycrystalline ferroelectric ceramic material which is polarized such that the ceramic material exhibits strong Piezoelectric Effect properties thus inducing high frequency vibrations. The shell may be further doped with radioactive elements which under high frequency vibrations induce gamma ray emission. The electrostatic generator is for charging up the shell and is disposed within the shell. The power plant is to generate thermal power, and is disposed within the sphere. The thermoelectric generator is to convert the thermal power generated by the power plant to electrical energy. The electric motor powered by the electrical energy generated by the thermoelectric generator, and supplies input voltage such that the shell spins at high angular speeds, vibrates at high frequencies, and generates an electromagnetic field.

公开(公告)号：US20170313446A1

公开(公告)日：2017-11-02

申请号：US15141270

申请日：2016-04-28

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: B64G1/40

CPC classification number: B64G1/409

Abstract: A craft using an inertial mass reduction device comprises of an inner resonant cavity wall, an outer resonant cavity, and microwave emitters. The electrically charged outer resonant cavity wall and the electrically insulated inner resonant cavity wall form a resonant cavity. The microwave emitters create high frequency electromagnetic waves throughout the resonant cavity causing the resonant cavity to vibrate in an accelerated mode and create a local polarized vacuum outside the outer resonant cavity all.

公开(公告)号：US07080504B2

公开(公告)日：2006-07-25

申请号：US10897699

申请日：2004-07-23

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: F03H1/00 ,  G21D1/00 ,  H05B1/00

CPC classification number: F23C99/001 ,  F02C7/264 ,  F23C2900/99003 ,  F23R3/00 ,  F23R2900/00006 ,  Y02T50/671

Abstract: The invention is a turbojet propulsion system which includes a compressor section, a turbine section coupled by a shaft to the compressor section, a combustion section mounted between the compressor section and the turbine section, and an exhaust duct coupled to the aft end of said turbine section. A fuel delivery system is incorporated for supplying fuel to the combustion section. A laser assembly provides electromagnetic radiation to the combustion section. An electrical generator coupled to the turbine driven shaft powers the laser assembly.

Abstract translation: 本发明是涡轮喷气推进系统，其包括压缩机部分，通过轴连接到压缩机部分的涡轮部分，安装在压缩机部分和涡轮部分之间的燃烧部分，以及联接到所述涡轮机的后端的排气管道 部分。 燃料输送系统被结合用于向燃烧部分供应燃料。 激光组件向燃烧部分提供电磁辐射。 联接到涡轮驱动轴的发电机为激光组件供电。

公开(公告)号：US20060016169A1

公开(公告)日：2006-01-26

申请号：US10897699

申请日：2004-07-23

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: F03H1/00 ,  F02C7/264

CPC classification number: F23C99/001 ,  F02C7/264 ,  F23C2900/99003 ,  F23R3/00 ,  F23R2900/00006 ,  Y02T50/671

Abstract: The invention is a turbojet propulsion system which includes a compressor section, a turbine section coupled by a shaft to the compressor section, a combustion section mounted between the compressor section and the turbine section, and an exhaust duct coupled to the aft end of said turbine section. A fuel delivery system is incorporated for supplying fuel to the combustion section. A laser assembly provides electromagnetic radiation to the combustion section. An electrical generator coupled to the turbine driven shaft powers the laser assembly.