发明名称 Fusion energy system and plasma propulsion aircraft to produce electricity from a controlled nuclear fusion reaction
摘要 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.
申请公布号 US2006102795(A1) 申请公布日期 2006.05.18
申请号 US20050137643 申请日期 2005.05.25
申请人 发明人 GOCHNOUR GARY R.
分类号 B64G1/40 主分类号 B64G1/40
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