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    • 5. 发明授权
    • Process for the production of electric energy for spacecraft utilizing the collection of charged particles in space
    • US09302792B1
    • 2016-04-05
    • US13999916
    • 2014-03-31
    • Eugene B. Pamfiloff
    • Eugene B. Pamfiloff
    • B64G1/42G21H1/02
    • B64G1/421G21H1/02G21H7/00
    • The process of the present application facilitates the production of electric energy for spacecraft by the seizure of beta-minus particles and electrons present in the medium of space above and beyond the planet's atmosphere. The features of the subject process make each spacecraft independent from domestic energy sources as are typically required by other electrical systems. In terms of energy production, the subject process will outperform all of the traditional systems applied to spacecraft including photovoltaic setups, fuel cells, batteries and nuclear systems. Photovoltaic panels situated in space are quickly degraded by bombarding cosmic ray particles and solar wind emissions. Since fuel cells require very high operating temperatures, it exposes the craft, its instrumentation and occupants to constant danger. By utilizing the process of the present application, it is no longer necessary for spacecraft to carry large quantities of chemicals for batteries, fuels and oxidizers for fuel cell generators, hazardous nuclear generators or large bulky photovoltaic panels subject to frequent malfunction. It is an innovative process for the production of electric energy by the attraction and seizure of beta-minus particles and electrons emitted from the Sun's corona as part of the solar wind that permeates the heliosphere. Because it captures free electrons directly, it does not consume power to convert one form of energy into another. It functions continuously throughout and beyond the heliosphere. It can be scaled to accommodate the electric power requirements of all spacecraft, including satellites and space stations. The process will accommodate the electric needs of base stations and surface vehicles situated on various moons and asteroids throughout the solar system including the planets Mercury and Mars. Some of the terms that describe the advantages of the process of the present application are simplicity, efficiency, adaptability, versatility, low energy consumption, and high productivity. Consequently, a reliable, enduring and safe electric power source for space craft has not been available until the development of the process of the present application.
    • 7. 发明授权
    • Electrostatic process to shield spacecraft and occupants from solar wind and cosmic radiation
    • 屏蔽航天器和乘客免受太阳风和宇宙辐射的静电过程
    • US09469421B1
    • 2016-10-18
    • US15090203
    • 2016-04-04
    • Eugene B. Pamfiloff
    • Eugene B. Pamfiloff
    • B64G1/42G21H1/02G21H7/00B64G1/54B64G1/44
    • B64G1/54B64G1/421B64G1/44G21F3/00G21H1/02G21H7/00
    • The present application is the first pragmatic process capable of shielding spacecraft and occupants from destructive impact and penetration of the crafts' exterior walls by positively charged particles of cosmic rays and solar wind. The technology also protects the craft from internal cascading secondary radiation caused by energetic particles that strike the surface and those that penetrate to the interior. Particles posing the highest level of danger to spacecraft are low and high energy protons, positive ions and few-particle nuclei. Accordingly, a reliable, enduring and safe shielding mechanism for spacecraft has not been available until the development of the present application. The shielding is accomplished by conveying a positive electric charge to the atoms and molecules of the exterior surface. Incoming particles are diverted and deflected from the surface by an established electric field derived through an advanced electric system that utilizes electrons emitted by solar wind as electric energy.
    • 本应用是第一个实用的过程,能够屏蔽航天器和乘员免受宇宙射线和太阳风的带正电颗粒的工艺外墙的破坏性冲击和穿透。 该技术还可以保护工艺免受内部级联二次辐射,这些二次辐射是由能量粒子撞击到表面和穿透到内部的能量颗粒引起的。 对航天器造成最高危险的粒子是低能量质子,高能量质子,正离子和几粒子核。 因此,在本申请的开发之前,对于航天器的可靠,持久和安全的屏蔽机制尚不可用。 通过将正电荷传送到外表面的原子和分子来实现屏蔽。 通过利用由太阳风发射的电子作为电能的先进电气系统导出的已建立的电场,将进入的颗粒从表面转向并偏转。
    • 8. 发明申请
    • DEVICE AND PROCESS FOR THE GENERATION OF ELECTRICAL ENERGY
    • 电能产生装置及工艺
    • US20160049839A1
    • 2016-02-18
    • US14781678
    • 2014-04-07
    • ARION TECNOLOGIA BRASIL-GESTÃO DE ATIVOS S/A
    • Gerson SILVA PAIVASebastião FLORENTINO DA SILVA
    • H02K3/28G21H7/00H02K11/00
    • H02K3/28G21H7/00H02K11/0094H02N11/008
    • A muonic electromagnetic generator for generating electrical energy is provided and includes a generator that is connectable to at least one source of electric energy with a lower power than the power generated by the generator. The generator includes at least one outer electric coil, at least one inner electric coil, situated substantially inside the outer electric coil, and an oscillator. The oscillator is connected between the source of electrical energy and the outer electric coil. When the outer electric coil is connected to a source of electric energy via an oscillator that was previously tuned to emit a frequency corresponding to a certain fraction specific to the Compton frequency of a muon, the muonic energy is absorbed by an inner electric coil, and this energy can be used to feed any external load. This muonic energy can be significantly greater than the power of the source of energy
    • 提供了用于产生电能的muonic电磁发生器,并且包括能够以比由发电机产生的功率更低的功率连接到至少一个电能源的发电机。 发电机包括至少一个外部电线圈,至少一个内部电线圈,其基本上位于外部电线圈内部,以及振荡器。 振荡器连接在电能源和外部电线圈之间。 当外部电气线圈经由振荡器连接到电源时,该振荡器先前被调谐以发射对应于与μon的康普顿频率相关的特定分数的频率,该能量被内部电线圈吸收,并且 这种能量可用于馈送任何外部负载。 这个能量能量明显大于能源的能量