发明名称 Rotor inductance propulsion system
摘要 The invention is a spacecraft having a circular, domed hull around which dual electrically-charged rotors one above the other are counter-rotating on the edge of the hull. Embedded in the hull are three solenoids which create a positive vector potential at the rotors. The surface charge density times the radius times the vector potential times the area of the rotors creates an angular momentum in the vertical direction. This angular momentum produces a positive spacetime curvature over the dome of the hull and a negative spiking spacetime compression over the rotors. By machining circumferential grooves of decreasing height along the radius of the rotor, a negative surface inductance is generated. This negative inductance gradient times the negative spacetime compression time the rotor current density squared times the rotor area squared is a positive lift force on the spacecraft.
申请公布号 US2003230675(A1) 申请公布日期 2003.12.18
申请号 US20020170847 申请日期 2002.06.12
申请人 ST. CLAIR JOHN QUINCY 发明人 ST. CLAIR JOHN QUINCY
分类号 B64C39/00;B64G1/40;F03H99/00;G21K1/00;(IPC1-7):B64G1/40;B64G1/42 主分类号 B64C39/00
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