(19) United States US 20080061 191A1 (12) Patent Application Publication (10) Pub. No.: US 2008/0061191 A1 G0chnour (43) Pub. Date: Mar. 13, 2008 (54) MULTI-FUNCTIONAL HIGH ENERGY PLASMA AIRCRAFT AND NUCLEAR FUSON SYSTEM TO PRODUCE ENERGY FROM A CONTROLLED NUCLEAR FUSION REACTION (76) Inventor: Gary Richard Gochnour, Seattle, WA (US) Correspondence Address: Gary Richard Gochnour Apt Nr. 426 747 N. 135th Street Seattle, WA 98.133 (US) (21) Appl. No.: 11/728,080 (22) Filed: Mar. 23, 2007 Related U.S. Application Data (63) Continuation-in-part of application No. 11/137,643, filed on May 25, 2005, now abandoned, which is a continuation-in-part of application No. 10/841,702, filed on May 6, 2004, now abandoned. (60) Provisional application No. 60/468.598, filed on May 6, 2003. Publication Classification (51) Int. Cl. B64G L/40 (2006.01) (52) U.S. Cl. .......................................................... 244/171.5 (57) ABSTRACT The invention relates to a plasma based aircraft maintained in a flight mode by either post nuclear fusion reaction plasma contained rotating vortices above and beneath said aircraft, or a pre-nuclear fusion reaction aircraft flight mode com prising use of said rotating Vortices and a plasma gun when needed. Said aircraft is comprised of chromium steel, or higher ferrochromium steel can be used. Said aircraft requires no external fuel Source, said aircraft receives energy from aircraft produced plasma and electric energy. Starting energy is stored in aircraft capacitance system. Said craft is capable of space flight, use as a Submersible craft, boring device, or lifting device. Said aircraft can also be utilized in an artificial domed environment to produce heat, light, a light mist, energy, and can regenerate an atmosphere, and produce an atmosphere, and other uses. Said craft does not require an external source of fuel for space flight or for submersible use. Particle propulsion in space will be used utilizing metal ions stored in said craft capacitor plates. Said craft is opaque, invisible within the visible spectrum, and invisible to electromagnetic radiation, and absorbs radiation it produces. Said aircraft is capable of verticle ascent, descent and landing. Said aircraft can operate within earth radiation belts safely, and for extended periods of time. Said aircraft with two larger aircraft comprised of magnesium aluminum material, can achieve ignition of a B-11 fusion spherical plasma, formed by Smaller craft electrolysis sys tem, with no radiation or cooling required and store pro duced energy in craft plasma Vortices. - - -55 Patent Application Publication Mar. 13, 2008 Sheet 1 of 24 US 2008/0061191 A1 - - -55 Patent Application Publication Mar. 13, 2008 Sheet 2 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 3 of 24 US 2008/0061191 A1 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 5 of 24 Patent Application Publication Mar. 13, 2008 Sheet 6 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 7 of 24 US 2008/0061191 A1 408 - C Patent Application Publication Mar. 13, 2008 Sheet 8 of 24 US 2008/0061191 A1 -ce Patent Application Publication Mar. 13, 2008 Sheet 9 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 10 of 24 US 2008/0061191 A1 70 fad Patent Application Publication Mar. 13, 2008 Sheet 11 of 24 US 2008/0061191 A1 Fig. 9A Patent Application Publication Mar. 13, 2008 Sheet 12 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 13 of 24 US 2008/0061191 A1 s Patent Application Publication Mar. 13, 2008 Sheet 14 of 24 US 2008/0061191 A1 | | 70 f(b 701b." 701, 70 a 413e 70fc. 703d 703c City 703d 702d 4fn 703c / 4.13m 703b 4,3 703d' 703b' O O Fig. 9D Patent Application Publication Mar. 13, 2008 Sheet 15 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 16 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 17 of 24 US 2008/0061191 A1 Fig. 9G Patent Application Publication Mar. 13, 2008 Sheet 18 of 24 US 2008/0061191 A1 Patent Application Publication Mar. 13, 2008 Sheet 19 of 24 US 2008/0061191 A1