Abstract: This universal technology eternal zero carbon, thermal electric clean engines and gas turbines, with universal cryogenic eternal systems converting all gases in cryogenic working fluids, for solar/atmospheric and geo thermal energy eternal systems, is eliminating 100% all the fossil fuels from energy and universal mobility, variable power, with constant maximum compression pressure and constant maximum combustion pressure, resulting constant maximum efficiency in all the variable eternal power electric generation and universal mobility systems.

Abstract: Total Synergetic Integration of all eternal energy solar atmospheric, wind, geo thermal universal fuel capabilities with maximum absolute efficiency.

Abstract: The invention relates to the universal, and supreme cross hyperbaric, hybrid, direct transformation systems of any and all forms of thermal energies, directly in electric energy, based on the maximum absolute efficiency, of the thermodynamic, cross hyperbaric thermal electric engine, associated with all forms of operations and structures, including, general linear and rotary electric generators, integrating all the thermal energies, produced by the internal combustion engine, including the homogenous fuels combustion, activated by the super aero self-injection, and by the universal alternatively convertible engine in compressor, and expander, for braking energy hybrid recovery, including for total distributed energy production, by universal mobility systems.

Abstract: The invention is a universal aero, naval and space, one class integrated technology, originated from a common, fundamental unique basic absolute maximum efficiency technology, total endothermic, hyperbaric, adiabatic and stoichiometric maximum power capacity, with unlimited pressure ratio, which is the unification of the way to produce a top absolute efficiency by cryogenic electrification of all the transportation systems from ground to the entire universe.

Abstract: This invention relates to absolute universal engine for aviation, from ground to orbit and space, by total integration of all modes of operation, turbo fan subsonic, turbo jets supersonic, turbo air ram rockets, and turbo space rockets, <<<One Engine From Ground to Orbit>>>

Abstract: A system and method for orienting first and second reaction turbines relative to an axis of rotation responds to a fluid flow having a flow orientation axis. The fluid flow is received in a casement. The casement has first and second endplates situated parallel and spaced apart along the axis of rotation. A first half of the fluid flow drives the first reaction turbine to rotate with a first spin orientation in a plane perpendicular to the axis of rotation to produce a first torque about the axis of rotation. The second half of the fluid flow drives the second reaction turbine, offset from the casement plane relative to the first reaction turbine, with a second spin orientation opposite the first spin orientation to produce a second torque about the axis of rotation. The casement is oriented about the axis of rotation in response to the first and second torques.

Abstract: An apparatus for driving a turbine connected to a generator for generating power to supply to a grid the power derived from a rotating shaft includes a transmission for selectably driving either of a compressor or a direct current motor generator. The compressor compresses ambient air changing phase to liquid air. The direct current motor generator generates a current at a constant voltage for water electrolysis. A first bell containing a cathode collects elemental hydrogen; a second bell containing an anode collects elemental oxygen. The elemental hydrogen burns in the presence of the elemental oxygen to produce a highly energetic exhaust. A valve selectably admits either of the highly compressed air or the highly energetic exhaust into the turbine to drive the turbine thereby energizing the generator to supply the grid.