WO2013137858A2

WO2013137858A2 - Universal thermal electric energy and mobility systems

Info

Publication number: WO2013137858A2
Application number: PCT/US2012/028837
Authority: WO
Inventors: Marius Angelo Paul
Original assignee: General Energy And Universal Mobility Systems Llc
Priority date: 2012-03-12
Filing date: 2012-03-12
Publication date: 2013-09-19

Description

UNIVERSAL THERMAL ELECTRIC ENERGY AND MOBILITY SYSTEMS

DEFINITION OF THE INVENTION THE INVENTION IS THE FUNDAMENTAL UNIVERSAL THERMAL ELECTRIC

DIRECT THERMAL ENERGY CONVERSION IN ELECTRIC ENERGY, AND MOBILITY SYSTEM, INTEGRATED AND USING ALL THE FORMES OF AVAILABLE ENERGY SOURCES, FOR UNIVERSAL COMBINED

APPLICATIONS.

ENERGY POWER PLANTS, STATIONARY AND/OR MOBILE, AND ALL FORMES OF

TRANSPORTATION SYSTEMS, ON LAND, ALL NAVAL ON SURFACE AND SUBMARINES AND AIR, ARE THE UNIVERSAL APLICABILITY OF THIS INVENTION.

ANY FUELS, FROM ANY SOURCES, LIQUIDS, GASES, GEO THERMAL,

WIND, SOLAR, AND NUCLEAR, ARE THE UNLIMITED CAPACITY TO PRODUCE ELECTRIC ENERGY AND TRANSPORTATION, WITH UNLIMITED RANGE AND UNLIMITED TIME OF OPERATION.

THE UNIVERSAL ENGINE SYSTEM, IS USING INTERNAL COMBUSTION SYSTEMS, EXTERNAL

COMBUSTION, OPEN THERMAL CYCLES, CLOSED CYCLES, AEROBIC AND ANAEROBIC.

THE SPECIAL NAVAL SUBMARIN APPLICATION, FOR USING THE ELECTRIC POWER TO

ELECTROLISE THE SEA WATER, FOR PRODUCTION OF HYDROGEN AND OXYGEN,

LIQUEFIED AND STORED WILL BE USED ON SUBMARINE ANAEROBIC LONG DRIVE OPERATION.

THE THERMAL EFFICIENCY CAN REACH MAXIMUM ABSOLUTE LEVEL OF CARNOT- PAUL CYCLES.

THE FUNDAMENTAL CAPACITY TO CREATE AND USE UNIQUE HOMOGENOUSE CONTROLLED COMBUSTION OF ANY FUELS, IS THE BASE FOR UNIVERSAL FUEL CAPABILITY.

THE BASIC MECHANICAL SYSTEM OF OPERATION IS THE UNIVERSAL CROSS HYPERBARIC, AND HYBRID SYSTEM, OF THERMAL AND DIRECT LINEAR ELECTRIC GENERATORS INTEGRATED POWER SYSTEM.

THE UNIQUE REVOLUTIONARY THERMAL CYCLE, USING ALL THE ENGINE STROKES FOR POWER, AND ELIMINATION OF NONE- POWER STROKES, INTAKE, EXHAUST AND COMPRESSION IS PRODUCING THE MAXIMUM ABSOLUTE POWER DENSITY, AND MAXIMUM ABSOLUTE EFFICIENCY.

BRIEF DESCRIPTION OF THE INVENTION.

THE FIRST FUNDAMENTAL BASE OF ENTIRE INVENTION, IS THE UNIVERSAL CROSS HYPERBARIC ENGINE, WHICH IS THE SYSTEM INTEGRATOR OF ALL THE SYSTEMS OF OPERATION, INDICATED IN THE

DEFINITION OF THE INVENTION, OF THERMAL AND ELECTRIC COMBINED POWER, PRODUCED BY A LINEAR ELECTROMAGNETIC SYNCRON GENERATOR, INTEGRATED IN THE LINEAR MOVING CROSS HYPRBARIC MECHANISM, CONNECTING THE TWO OPPOSED PISTONS.

THE SECOND FUNDAMENTAL FEATURE OF THE INVENTION, IS THE TURBO COMPOUND ENGINE SYSTEM WITH EXTERNAL HOMOGENOUSE CONTROLLED UNIVERSAL COMBUSTION, AND WITH

TWO STROKE OPERATION, CONTROLLED BY INTAKE AND EXHAUST PORTS.

THE THIRD FUNDAMENTAL FEATURE OF THE INVENTION, IS THE TURBO COMPOUND ENGINE SYSTEM, WITH EXTERNAL HOMOGENOUSE CONTROLLED UNIVERSAL COMBUSTION, CAPABLE TO OPERATE IN TWO OR FOUR STROKE CONTROLLED BY CONVENTIONAL OR ELECTRO HYDRAULIC VALVES FOR INTAKE AND EXHAUST VALVES. THE FOURTH FUNDAMENTAL FEATURE OF THE INVENTION, IS THE ASSOCIATION AND COMBINED OPERATION WITH ANY EXTERNAL SOURCE OF ENERGY, CAPABLE TO PRODUCE HIGH PRESSURE, AND HIGH TEMPERATURE CONTINUOUS WORKING FLUIDS, OF GASES,OR STEAM, FROM ANY SOURCES OF THERMAL ENERGY, NATURAL, ETERNAL, INCLUDING NUCLEAR, WITH CLOSED CYCLE OPERATION.

THE FIFTH FUNDAMENTAL OPERATIONAL STRUCTURE OF THE INVENTION, IS THE CROSS HYPERBARIC HYBRID WORKING ENG INE IN CLOSED OR OPEN ENERGY CYCLE IN ASSOCIATION

WITH ANY AND ALL SOURCES OF ENERGY, NATURAL, ETERNAL, INCLUDING NUCLEAR.

THE SIXTH FUNDAMENTAL OPERATION OF HOMOGENOUS UNIVERSAL FUEL CAPABILITY, OF ANY LIQUID OR GASEOUS FUELS, INDIVIDUALY OR SELECTIC AND OR COMBINED IN ANY PROPORTIONS, INCLUDING EXTERNAL SOURCES OF ANY FORM OF ENERGY, INCLUDING NUCLEAR.

BRIEF DESCRIPTION OF THE DESIGNS, REPRESENTED THE SPIRIT OF THE INVENTION.

FIG. 1 IS THE UNIVERSAL CROSS HYPERBARIC THERMAL LINIAR ELECTROMAGNETIC HYBRID ENGINE.

FIG. 2 IS THE EXTERNAL HOMOGENOUSE COMBUSTION, TURBO COMPOUND ENGINE

TWO CYCLE ENGINE.

FIG. 3 IS THE EXTERNAL HOMOGENOUSE COMBUSTION, TURBO COMPOUND ENGINE

WORKING IN TWO OR FOUR CYCLE ENGINE.

FIG. 4 IS THE EXTERNAL CLOSED CYCLE UNIVERSAL ENGINE WORKING IN ASSOCIATION

UNIVERSAL EXTERNAL SOURCE OF ENERGY PRODUCING WORKING, HIGH ENERGY FLUIDS.

FIG. 5 IS THE UNIVERSAL-TOTAL MAXIMUM ABSOLUT CROSS HYPERBARIC HYBRID ENGINE WORKING WHICH IS THE SUPREME CONVERSION OT YOTAL THRMAL ENERGY DIRECT IN ELECTRIC ENERGY WITHOUT ANY MECHANICAL POWER PRODUCTION, USING ALL FORMS OF ENERGY AVAILABLE INCLUDING ALL EXTERNAL SOURCE OF ENERGY.

IN THE FIG.l, IS DEPICTED THE UNIVERSAL CROSS HYPERBARIC HYBRID THERMAL ELECTRIC ENGINE SYSTEMS, COMPOSED FROM GENERIC NUMBER (10), THE CENTRAL BODY 1, THE TWO CILINDERS 2, AND 3, PROVIDED WITH PISTONS 4, AND 5, COVERED BY TOP HEADS 6, AND 7, PROVIDED WITH INTAKE PO RTS 8, AND 9, EXHAUST PORTS 11, AND 12, EACH CYLINDER, IS PROVIDED WITH COMBUSTION

CHAMBER 13, AND 14.

BOTH PISTONS ARE CONNECTED WITH THE CENTRAL BAR 15, AND THE CROSS BAR 16, ARTICULATED WITH CONNECTING ROADS 17,AND 18, DRIVING THE MONO CRANKSHAFT 19,AND 20. GEARED IN ONE/ONE BY THE GEARS 21, AND 22 . ON THE SAME CENTRAL BAR 15, IS INCLUDED THE MOBIL LINEAR ELECTROMAGNETIC INDUCER 16, MOVING ALTERNATIVELY IN THE LINEAR ELECTRO BOBINE, POWER GENERATOR. THE ALTERNATIVE LINEAR ELECTRIC GENERATOR 23 IS PODUCING AN IDEAL SYNCRO SYNUSODAL AC ENERGY PRODUCTION 24.

EACH STROKES IS PRODUCING A COMPLETE POWER ROTATION, WITH OUT ANY

NONE POWER MOVEMENT.

THE COUNTER SYMETRIC ROTATION OF THE CRANK SHAFTS 18, AND 19, IS ARTICULATING THE

CONNECTING ROADS 17, AND 18, IN SYMETRIC EQUAL AND OPOSITION OPERATION, ELIMINATING THE SIDE FORCES. ALL THE CROSS BAR MECHANISM AND THE PISTIONS, ARE IN PERMANENT EQUILIBRIUM BALANCE, WITH ZERO INERTIA FORCES, ZERO VIBRATION AND ZERO FRICTION SIDE FORCES, BETWEEN PISTONS AND CYLINDER LINERS. «<REAL FLYING PISTONS»>.

IN THE FIG.2 (A)IS DEPICTED GENERICALLY BY THE NUMBER (20.1) THE TURBO COMPOUND HYPERBARIC ENGINE WITH EXTERNAL HOMOGENOUS CONTROLLED COMBUSTION CHAMBER

32, AND CYLINDER 33, PROVIDED WITH THE PISTON 34, INDICATED ON THE BOTTOM POSITION CENTER, UN COVERING THE INTAKE PORTS 35, AND THE EXHAUST PORTS 36.

THE PISTON IS PROVIDED WITH THE PISTONS RINGS 37, 38, AND 39, AND A CROSS COMMUNICATION CHANELL 40 WITH A TOP COMBUSTION OPENING 41, AND A BOTTOM OPENING 42.

IN THIS POSITION THE PISTON 34 AT BOTTOM DEAD CENTER, THE INTAKE FRESH 44 AIR/ OXIGEN IS PRODUCING THE SCAVENGING OF THE EXHAUST GASES 45,

REPLANISHING THE NEW FRESH CHARGE OF AIR/OXYGEN, FOR THE NEXT WORKING STROKE OF COMPRESSING AND COMBUSTION.

IN THE FIG.2 (B), IS DEPICTED THE PISTON 34, IN THE TOP DEAD CENTER, AT THE END OF COMPRESSION, AND START OF COMBUSTION, BY THE INJECTION OF THE COMPRESSED AIR/OXYGEN, IN THE

HOMOGENOUSE COMBUSTION CHAMBER 32 , PROVIDED BY FUELS MIXED WITH RESIDUAL HOT GASES, FROM THE PREVIOUSE COMBUSTION HOMOGENOUSE CYCLE TIME.

THE PRESENCE OF HOT RESIDUAL GASES AND FUEL MIXTURE, VAPORIZED, HEATED WITHOUT

AIR/OXYGEN ALONG 360 DEG., TIME IS CREATING A PLASMA GAS FUEL, OF EXTRAORDINARY PRE LIMINARY HOMOGENOUS CONDITIONS, FOR THE MOMENT OF AIR/ OXYGEN INJECTION AND FINAL COMBUSTION.

THE SEPARATION OF THE FUEL HOMOGENOUSE MIXTURE, FROM THE AIR/OXYGEN, ALONG ALLTHE COMPRESSION OF THE AIR/OXYGEN, IS SOLVING NATURALLY THE TYPICAL UNCONTROLLED

COMBUSTION OF ALL ACTUAL UN SUCCESSFUL DEVELOPMENT FOR CONTROLLING THE HOMOGENOUSE COMBUSTION.

BY DEFINITION, OUR INVENTION, IS ABLE TO RAISE THE COMPRESSION PRESSURE AND SUPER

CHARGING TO UNLIMITED LEVEL, WITH COMPLETE CONTROL OF THE HOMOGENOUSE COMBUSTION PROCESS.

OUR INVENTION IS ELIMINATING ALLTHE FUEL CHARACTERISTICS OF OCTANE, AND CETANE NUMBER MAKING THE ENGINE UNIVERSAL FUEL CAPABILITY.

THE TURBO COMPOUND SYSTEM OF OPERATION IS PRODUCED BY THE ELECTRIC DRIVEN COMPRESSOR

46, 48, SUPLYING AI/OXYGEN FROM THE SEPARATOR DEVICE 47, AND INJECTING THE COMPRESSED AIR/ OXYGEN IN THE INTAKE PORTS 35.

THE EXHAUST GASES 45 ARE CONDUCTED IN THE GAS TURBINE 49, DRIVING THE ELECTRIC GENERATOR 50

THE MAIN CHARACTERISTIC OF THE TURBO COMPOUND SUPERCHARGING IS THE CONSTANT PRESSURE OF COMPRESSED AIR/OXYGEN INDEPENDENT FROM LEVEL OF LOAD FROM FULL POWER TO MINIMUM LOADS, CREATING A CONSTANT MAXIMUM EFFICIENCY IN ALL THE OPERATION TIME.

IN THE FIG. 3, (37 A) IS DEPICTED THE UNIVERSAL TURBO COMPOUND TWO-FOUR CiCLE, FOR

HOMOGENOUS CONTROLLED COMBUSTION ENGINE SYSTEM, INDICATED THE CYLINDER 38 PROVIDED WITH THE PISTON 39 IN THE BOTTOM DEAD CENTER.

THE CYLINDER IS PROVIDED, WITH TOP ELECTRO HYDRAULIC VALVES 40 AND 41, CAPABLE TO

PROGRAMBALE OPERATING VALVES ON TWO OR FOUR CYCLE.

THE CYLINDER IS PROVIDED WITH THE EXTERNAL HOMOGENOUSE COMBUSTION CHAMBER 42.

IN THE FIG.37A, POSITION PISTON IS AT THE BOTTOM DEAD CENTER, CAPABLE TO OPERATE

ALTERNATIVELY ON TWO OR FOUR CYCLE MODE. IN THE FIG. 37 B, THE PISTON 39, IS ON THE TOP DEAD CENTER, AT THE END OF COMPRESSION OF THE AIR/OXIGEN IN THE HOMOGENOUSE COMBUSTION CHAMBER 42, PROVIDED WITH PRE UMINARY FUEL HOT GAS PLASMA MIXTURE, FOR PERFECT CONTROLLED HOMOGENOUSE COMBUSTION, DESCRIBED IN THE FIG.2.

THE TURBO COMPOUND SUPERCHARGING SYSTEM, OF CONSTANT PRESSURE, IS ACHIEVED BY THE ELECTRIC DRIVEN AIR/OXYGEN COMPRESSOR 43, 44, SUPPLYIED FROM AIR/OXYGEN SEPARATOR FROM NYTROGEN, INJECTING FRESH CHARGE 45, IN THE ENGINE CYLINDER 38.

THE EXHAUST GASES 46 ARE CONDUCTED IN THE GAS TURBINE 47 , DRIVING THE ELECTRIC GENERATOR 48.

THE CROSS CHANELL 30, 31, 32, IS THE CHANELL OF COMMUNICATION BETWEEN THE TOP OF THE PISTON AT THE TOP DEAD CENTER INJECTING THE FRESH AIR/OXYGEN IN THE HOMOGENOUSE

COMBUSTION CHAMBER 42.

IN THE FIG.4, ARE INDICATED THE SAME, TURBO COMPOUND UNIVERSAL CONTROLLED HOMOGENOUSE COMBUSTION TECHNOLOGY INDICATED IN THE FIG. 3, ASSOCIATED WITH THE UNIVERSAL SOURCE OF HEAT, AND SUPPLIER FOR HOT HIGH PRESSURE WORKING FLUIDS 50C ( 49C), IN THE PERMANENT COMMUNICATION EXTERNAL PORT 51, IN ALTERNATIVE CONNECTION WITH THE PORT 32, OF THE CROSS CHANELL 30, COMMUNICATING TO THE TOP PISTON OPENING 31, CONDUCTING THE WORKING FLUID FOR POWER STROKE.

THE ASSOCIATED UNIVERSAL HEAT AND PRESSURE SOURCE WORKING UNIT 49C, IS GENERICALLY ANY HEAT DEVICE ENERGY UNIT, OF ANY KIND, BASED ON ANY FORMES OF POWER GENERATION, WITH CONTINUSE EXTERNAL COMBUSTION, WIND, SOLAR, ETERNAL ENERGY, UNIVERSAL EXTERNAL

COMBUSTION, INCLUDING NUCLEAR REACTOR, COOLED BY ANY PROPER FLUID TRANSFORMED IN STEAM OF HIGH PRESSURE AND HOT TEMPERATURE 50C.

THE EXPANDED WORKING FLUID IS EXHAUSTED THROUGH CHANELL 51A, AND 52A, IN THE CONDENSOR

53, AND THE LIQUID CONDENSED FLUID IS CONDUCTED AND PRESSURIZED BY THE HYDRAULIC PUMP

55, BACK IN THE HEAT GENERATOR 49C, OPERATING IN A CLOSED THERMAL CYCLE.

THE COOLING FLUID FOR COOLING THE CONDENSOR 57,59, IS FINISHING THE CLOSED CYCLE

OPERATION.

THE NUCLEAR OPERATION IS PRODUCING UNLIMITED OPERATION MODE, FOR UNLIMITED RANGE AN UNLIMITED TIME, FOR ANY VEHICLES, OF ANY KIND, OR FOR ENDLESS POWER GENERATION.

IN THE FIG.5, IS INDICATED THE UNIVERSAL CROSS HYPERBARIC HYBRID ENGINE DESCRIBED IN THE FIG.l, ASSOCIATED IN A SYMETRIC TOTAL ABSOLUTE ENERGY PROVIDED WITH ALL THE PREVIOUSE DESCRIBED CAPABILITIES, AND THE PERMANENT CONNECTION, BY THE CENTRAL UNITED, CENTRAL COMMON CYLINDER 60 WITH DOUBLE OPPOSED INTAKE PISTONS 62, AND EXHAUST PISTONS 63, WITH TOTAL CONVERSION OF TEHERMAL ENERGY BY BOTH LINEAR ELECTRIC SYNUSOIDAL GENERATORS 64, AND 65.

THE UNITED ENERGETIC DOUBLE CROSS HYPERBARIC ENGINES OF FIG.l IS IN CONNECTION WITH ALL THE SOURCES OF INTERNAL AND EXTERNAL HEAT, WORKING HIGH PRESSURE, HIGH TEMPERATURE, DESCRIBED IN THE PREVIOUSE FIGURES.

THIS UNIVERSAL CROSS HIPERBARIC, HYBRID ENGINE, IS THE ABSOLUTE UNIVERSAL POWER TOP MAXIMUM EFFICIENT THERMAL TOTAL ELECTRIC SYSTEM IN THE WORLD. U NIVERSAL ENERGY AND MOBILITY SYSTEMS.

DEFINITION OF THE INVENTION THE INVENTION IS THE FUNDAMENTAL GENERAL AND UNIVERSAL ENERGY AND MOBILITY SYSTEM, INTEGRATED AND USING ALL THE FORMES OF

AVAILABLE ENERGY SOURCES, FOR UNIVERSAL COMBINED APPLICATIONS.

ENERGY POWER PLANTS, STATIONARY AND/OR MOBILE, AND ALL FORMES OF

TRANSPORTATION SYSTEMS, ON LAND, NAVAL AND AIR, ARE THE UNIVERSAL

APLICABILITY OF THIS INVENTION.

ANY FUELS, FROM ANY SOURCES, LIQUIDS, GASES, GEO THERMAL,

WIND, SOLAR, AND NUCLEAR, ARE THE UNLIMITED CAPACITY TO PRODUCE ENERGY AND

TRANSPORTATION, WITH UNLIMITED RANGE AND UNLIMITED TIME OF OPERATION.

THE UNIVERSAL ENGINE SYSTEM, IS USING INTERNAL COMBUSTION SYSTEMS, EXTERNAL

COMBUSTION, OPEN THERMAL CYCLES, CLOSED CYCLES, AEROBIC AND ANAEROBIC.

THE THERMAL EFFICIENCY CAN REACH MAXIMUM ABSOLUTE LEVEL OF CARNOT- PAUL CYCLES.

THE BASIC MECHANICAL SYSTEM OF OPERATION IS THE UNIVERSAL CROSS HYPERBARIC, AND HYBRID SYSTEM, OF THERMAL AND ELECTRIC INTEGRATED POWER SYSTEM.

THE UNIQUE REVOLUTIONARY THERMAL CYCLE, USING ALL THE ENGINE STROKES FOR POWER, AND ELIMINATION OF NONE- POWER STROKES, INTAKE EXHAUST AND COMPRESSION IS PRODUCING THE MAXIMUM ABSOLUTE POWER DENSITY, AND MAXIMUM ABSOLUTE EFFICIENCY.

BRIEF DESCRIPTION OF THE INVENTION.

DEFINITION OF THE INVENTION, OF THERMAL AND ELECTRIC POWER.

TWO STROKE OPERATION, CONTROLLED BY INTAKE AN EXHAUST PORTS.

THE THIRD FUNDAMENTAL FEATURE OF THE INVENTION, IS THE TURBO COMPOUND ENGINE SYSTEM, WITH EXTERNAL HOMOGENOUSE CONTROLLED UNIVERSALCOMBUSTION, CAPABLE TO OPERATE IN TWO OR FOUR STROKE CONTROLLED BY CONVENTIONAL OR ELECTRO HYDRAULIC VALVES FOR INTAKE AND EXHAUST VALVES.

THE FOURTH FUNDAMENTAL FEATURE OF THE INVENTION, IS THE ASSOCIATION AND COMBINED OPERATION WITH ANY EXTERNAL SOURCE OF ENERGY, CAPABLE TO PRODUCE HIGH PRESSURE, AND HIGH TEMPERATURE CONTINUOUS WORKING FLUIDS, OF GASES,OR STEAM, FROM ANY SOURCES OF THERMAL ENERGY, NATURAL, ETERNAL, INCLUDING NUCLEAR, WITH CLOSED CYCLE OPERATION. THE FIFTH FUNDAMENTAL OPERATIONAL STRUCTUREW OF THE INVENTION, IS THE CROSS HYPERBARIC HYBRID WORKING ENGINE IN CLOSED OR OPEN ENERGY CYCLE IN ASSOCIATION WITH ANY AND ALL SOURCES OF ENERGY, NATURAL, ETERNAL, INCLUDING NUCLEAR.

BRIEF DESCRIPTION OF THE DESIGNS, REPRESENTED THE SPIRIT OF THE INVENTION. FIG.I1 IS THE UNIVERSAL CROSS HYPERBARIC HYBRID ENGINE

FIG.I2 IS THE EXTERNAL HOMOGENOUSE COMBUSTION, TURBO COMPOUND ENGINE

TWO CYCLE ENGINE.

FIG.I3 IS THE EXTERNAL HOMOGENOUSE COMBUSTION, TURBO COMPOUND ENGINE

WORKING IN TWO OR FOUR CYCLE ENGINE.

FIG.I4 IS THE EXTERNAL CLOSED CYCLE UNIVERSAL ENGINE WORKING IN ASSOCIATION

UNIVERSAL EXTERNAL SOURCE OF ENERGY PRODUCING WORKING, HIGH ENERGY FLUIDS.

FIG.I5 IS THE UNIVERSAL CROSS HYPERBARIC HYBRID ENGINE WORKING WITH EXTERNAL COMBUSTION OR EXTERNAL SOURCE OF ENERGY.

IN THE FIGI1, IS DEPICTED THE UNIVERSAL CROSS HYPERBARIC HYBRID THERMAL ELECTRIC ENGINE SYSTEMS, COMPOSED FROM GENERIC NUMBER (10), AND (10.1 INCLUDING THE CENTRAL BODY 1, THE TWO CILINDERS 2, AND 3, PROVIDED WITH PISTONS 4, AND 5, COVERED BY TOP HEADS 6, AND 7, PROVIDED WITH INTAKE PORTS 8, AND 9, EXHAUST PORTS 11, AND 12, EACH CYLINDER, IS PROVIDED WITH COMBUSTION CHAMBER 13, AND 14.

BOTH PISTONS ARE CONNECTED WITH THE CENTRAL BAR 15, AND THE CROSS BAR 16, ARTICULATED WITH CONNECTING ROADS 17,AND 18, DRIVING THE MONO CRANKSHAFTS 18a, AND 19a, GEARED IN ONE/ONE BY THE GEARS 20, AND 21.

EACH STROKES IS PRODUCING A COMPLETE POWER ROTATION, WITH OUT ANY

NONE POWER MOVEMENT.

THE COUNTER SYMETRIC ROTATION OF THE CRANK SHAFTS 18a, AND 19a, IS ARTICULATING THE CONNECTING ROADS 17, AND 18, IN SYMETRIC EQUAL AND OPOSITION OPERATION, ELIMINATING THE SIDE FORCES.

ALL THE CROSS BAR MECHANISM AND THE PISTIONS, ARE IN PERMANENT EQUILIBRIUM BALANCE, WITH ZERO INERTIA FORCES, ZERO VIBRATION AND ZERO FRICTION SIDE FORCES, BETWEEN PISTONS AND CYLINDER LINERS. «<REAL FLYING PISTONS»>.

Ii.t-

IN THE FIG.(i©i2), IS INDICATED THE CROSS SECTION SHAPE OF THE ENGINE, PROVIDED WITH TWO ELECTRIC ROTARY ELECTRIC GENERATORS 20a,AND 21a, DRIVEN BY THE RESPECTIVE CRANKSHAFTS 18a, AND 19a. IN DRIVING OPPOSITION BY THE 1/1 RATIO, ALL THE POWER ROTATION.

IN THE FIGJ2 (A)IS DEPICTED GENERICALLY BY THE NUMBER (20.1) THE TURBO COMPOUND HYPERBARIC ENGINE WITH EXTERNAL HOMOGENOUS CONTROLLED COMBUSTION CHAMBER

22,AND CYLINDER 23, PROVIDED WITH THE PISTON 24, INDICATED ON THE BOTTOM POSITION CENTER, UN COVERING THE INTAKE PORTS 25 AND THE EXHAUST PORTS 26. THE PISTON IS PROVIDED WITH THE PISTONS RINGS 27, 28, AND 29, AND A CROSS COMMUNICATION CHANELL 30 WITH A TOP

COMBUSTION OPENING 31, AND A BOTTOM OPENING 32. IN THIS POSITION THE PISTON 24 AT BOTTOM DEAD CENTER, THE INTAKE FRESH 33 AIR/ OXIGEN IS PRODUCING THE SCAVENGING OF THE EXHAUST GASES 34, REPLANISHING THE NEW FRESH CHARGE OF AIR/OXYGEN, FOR THE NEXT WORKING STROKE OF COMPRESSING AND COMBUSTION.

IN THE FIGI2 (B), IS DEPICTED THE PISTON 24, IN THE TOP DEAD CENTER, AT THE END OF COMPRESSION, AND START OF COMBUSTION, BY THE INJECTION OF THE COMPRESSED AIR/OXYGEN, IN THE

HOMOGENOUSE COMBUSTION CHAMBER 22 , PROVIDED BY FUELS MIXED WITH RESIDUAL HOT GASES, FROM THE PREVIOUSE COMBUSTION HOMOGENOUSE TIME.

THE PRESENCE OF HOT RESIDUAL GASES AND FUEL MIXTURE, VAPORIZED, HEATED WITHOUT

CHARGING TO UNLIMITED LEVEL, WITH COMPLETE CONTROL OF THE HOMOGENOUSE

COMBUSTIONPROCESS.

OUR INVENTION IS ELIMINATING ALL THE FUEL CHARACTERISTICS OF OCTANE, AND CETANE NUMBER MAKING THE ENGINE UNIVERSAL FUEL CAPABILITY.

35, 36, SUPLYING AI/OXYGEN FROM THE SEPARATOR DEVICE 37, AND INJECTING THE COMPRESSED AIR/ OXYGEN IN THE INTAKE PORTS 33.

THE EXHAUST GASES 34 ARE CONDUCTED IN THE GAS TURBINE 37, DRIVING THE ELECTRIC GENERATOR 36A.

THE MAIN CHARACTERISTIC OF THE TURBO COMPOUND SUPERCHARGING IS THE CONSTANT PRESSURE OF COMPRESSED AIR/OXYGEN INDEPENDENT FROM LEVEL OF LOAD FROM FULL POER TO MINIMUM LOADS, CREATING A CONSTANT MAXIMUM EFFICIENCY IN ALL THE OPERATION TIME.

IN THE FIGJ3, (37 A) IS DEPICTED THE UNIVERSAL TURBO COMPOUND TWO-FOUR CICLE, FOR

PROGRAMBALE OPERATING VALVES ON TWO OR FOUR CYCLE.

THE CYLINDER IS PROVIDED WITH THE EXTERNAL HOMOGENOUSE COMBUSTION CHAMBER 42.

ALTERNATIVELY ON TWO OR FOUR CYCLE MODE.

IN THE FIG. 37 B, THE PISTON 39, IS ON THE TOP DEAD CENTER, AT THE END OF COMPRESSION OF THE AIR/OXIGEN IN THE HOMOGENOUSE COMBUSTION CHAMBER 42, PROVIDED WITH PRE LIMINARY FUEL HOT GAS PLASMA MIXTURE, FOR PERFECT CONTROLLED HOMOGENOUSE COMBUSTION, DESCRIBED IN THE FIGI2.

THE TURBO COMPOUND SUPERCHARGING SYSTEM, OF CONSTANT PRESSURE, IS ACHIEVED BY THE ELECTRIC DRIVEN AIR/OXYGEN COMPRESSOR 43, 44, SUPPLYIED FROM AIR/OXYGEN SEPARATOR FOR NYTROGEN, INJECTING FRESH CHARGE 45, IN THE ENGINE CYLINDER 38.

THE EXHAUST GASES 46 ARE CONDUCTED IN THE GAS TURBINE 47 , DRIVING THE ELECTRIC GENERATOR 48. THE CROSS CHANELL 30, 31, 32, IS THE CHANELL OF COMMUNICATION BETWEEN THE TOP OF THE PISTON AT THE TOP DEAD CENTER INJECTING THE FRESH AIR/OXYGEN IN THE HOMOGENOUSE COMBUSTION CHAMBER 42.

IN THE FIGI4, ARE INDICATED THE SAME, TURBO COMPOUND UNIVERSAL CONTROLLED HOMOGENOUSE COMBUSTION TECHNOLOGY INDICATED IN THE FIG J 3, ASSOCIATED WITH THE UNIVERSAL SOURCE OF HEAT, AND SUPPLIER FOR HOT HIGH PRESSURE WORKING FLUIDS 50 ( 49C), IN THE PERMANENT COMMUNICATION EXTERNAL PORT 51, IN ALTERNATIVE CONNECTION WITH THE PORT 32, OF THE CROSS CHANELL 30, COMMUNICATING TO THE TOP PISTON OPENING 31, CONDUCTING THE WORKING FLUID FOR POWER STROKE.

COMBUSTION, INCLUDING NUCLEAR REACTOR, COOLED BY ANY PROPER FLUID TRANSFORMED IN STEAM OF HIGH PRESSURE AND HOT TEMPERATURE 50.

55, BACK IN THE HEAT GENERATOR 49C, OPERATING IN A CLOSED THERMAL CYCLE.

OPERATION.

IN THE FIGJ5, IS INDICATED THE UNIVERSAL CROSS HYPERBARIC HYBRID ENGINE DESCRIBED IN THE FIGJ1, PROVIDED WITH ALL THE PREVIOSE DESCRIBED CAPABILITIES, AND THE EXTERNAL PERMANENT CONNECTION PORT 60, AND EXHAUST ELECTRO HYDRAULIC MONO OR MULTIPLE VALVES 61, IN CONNECTION WITH ALL THE SOURCES OF EXTERNAL HEAT, WORKING HIGH PRESSURE, HIGH

TEMPERATURE, DESCRIBED IN THE PREVIOUSE FIGURES.

THIS UNIVERSAL CROSS HIPERBARIC, HYBRID ENGINE, IS THE ABSOLUTE UNIVERSAL POWER TOP MAXIMUM EFFICIENT THERMAL SYSTEM IN THE WORLD.

Claims

WHAT IS CLAIMED,

1. A FUNDAMENTAL, GENERAL AND UNIVERSAL INTEGRATED ENERGY AND MOBILITY SYSTEM, CAPABLE TO USE ALL THE FORMES OF AVAILABLE ENERGY SOURCES, THERMAL, ETERNAL NATURAL, WIND, SOLAR,GEO THERMAL, FROM ANY AND ALL GENERAL FUELS, INCLUDING NUCLEAR, BY INTERNAL AND EXTERNAL COMBUSTION, SPARK AND/OR COMPRESSION

IGNITION, OF AIR/ OXYGEN FUEL MIXTURES, AND OR BY ANY POWER ACTING EXTERNAL FLUIDS, PRODUCED BY EXTERNAL THERMAL POWER GENERATORS, INCLUDING HOMOGENOUSE FUEL MIXTURE, OF ANY FUELS INDIVIDUALLY OR MIXED IN ANY PROPORTIONS, FORMING A THERMAL ENERGY PLASMA COMBINED WITH RECIRCULATED EXPANDED CAPTURED PORTIONS OF RESIDUAL COMBUSTION GASES, AND FUELS, IN A TOTAL CONTINUOUS RESIDENT TIMES OF 360 DEGREE TOTAL CONTINUOUS THERMAL CYCLE, PRODUCING EFECTIVE CONTINUOUSE POWER GENERATION, WITHOUT DISCONTINUAL UNPRODUCTIVE POWER GENERATION PHASES, FINALLY THE ENTIRE ENGINE SYSTEM IS REDUCED AT TWO CYLINDERS, AND NO MORE MULTI CYLINDERS ENGINE OF ANY SIZE FROM SMALLEST TO UNLIMITED MAXIMUM POWER.

2. A FUNDAMENTAL, GENERAL AND UNIVERSAL INTEGRATED ENERGY AND MOBILITY SYSTEM, OF CLAIM ONE, IS BASED ON A TWO CYLINDERS HYPERBARIC UNIVERSAL POWERR SYSTEMS TRANSFORMING ALL THE POWER PRODUCED BY ALL SOUCES OF AVAILABLE THERMAL ENERGIES, IN EFFECTIVE MECHANICAL POWER, BY A COMBINED MECHANICAL SYSTEM, COMPOSED BY A TWO OPOSED CYLINDERS, HAVING TWO OPPOSED PISTONS, CONNECTD IN TANDEM ALTERNATIVE SUCCESSIVE POWER STROKES, AND CONTINUOUS OPPOSED

OPERATION AND ACTIONS, BY A CENTRAL COMMON BAR, AN ARTICULATED CROSS BAR, ACTING SYMETRIC TWO CONNECTING RODS, DRIVING IN COUNTER SYMETRIC ROTATION, TWO MONO CRANCKS SHAFTS, PROVIDED WITH COUNTER BALANCING WEIGHTS, AGREGATED IN A SYMETRIC ONE TO ONE, SYMETRIC COUNTER ROTATION, BY COUNTER ROTATING GEARS, FORMING A PERMANENT DYNAMICALLY MECHANISM IN PERMANENT DYNAMIC ECHILIBRIUM, ELIMINATING ALL THE INERTIAL LINIAR AND ROTATING CENTRIFUGAL FORCES, AND

ELIMINATING ALL THE SIDE FORCES BETWEEN THE PISTONS AND CYLINDER LINERS BY THE OPPOSED SYMETRICAL ARANGED CONNECTING RODS, AND COUNTER ROTATING SYMETRIC CRANKSHAFTS.

3. THE CYLINDERS, OF CLAIM ONE AND TWO, CAN FUCTIONAL OPERATED, IN TWO CYCLE, OR FOUR CYCLE, OF INTERNAL AND EXTERNAL COMBUSTION ENGINES, OPEN CYCLE AND CLOSED UNAEROBIC CYCLES, FOR SUBMARINES, AND SPACE VEHICLES; CAN BE SELECTIVE OPERATING LIKE COMPRESSORS, OR EXPANDERS OF ANY ENERGETIC FLUIDS, STEAM, HIGH PRESSURES AIR, OR SOURCES OF NATURAL GASES, AND PETROLEUM GASES, GEO THERMAL ENERGY, WIND, SOLAR HEAT EXCHANGER , AND BY NUCLEAR ENERGY WORKING HIGH PRESSURE AND THERMAL FLUIDS.

4. THE PRODUCED POWER, FROM CLAIMS ONE, TWO AND THREE, CAN BE TRANSFORMED IN ALL FORMES OF MECHANICALLY AND/OR HYDRAULICALLY POWER, OR DIRECT ELECTRIC ENERGY, BY ELECTRIC ROTARY POWER GENERATORS DRIVEN BY THE COUNTER ROTATING

CRANKSHAFTS, IN A SYNCRON OR ASYNCRON DIRECT CURENT OR ALTERNATIVE CURENT ELECTRIC OUTPOUT SUPPLY, TO GENERAL AND UNIVERSAL PROPULSION SYSTEMS, FOR ANY AND ALL UNIVERSAL MOBILITY VEHICLES, OF LAND, NAVAL SURFACE, OR SUBMARINES, AIR AND SPACE VEHICLES.

ALL THE POWER GENERATING SYSTEMS, OF CLAIMS ONE AND TWO, CAN FORME DISTRIBUTED POWER SYSTEMS, OF ANY SIZE, AND ANY POWER, FOR ANY AND ALL GENERAL UNIVERSAL APPLICATIONS, OF STATIONARY POWERR PLANTS, OR AND GENERAL UNIVERSAL MOBILITY POWER SYSTEMS, HYBRID PLUG IN AND/OR PLUG OUT GENERAL OPERATIONS.

THE UNIVERSAL ENERGY AND MOBILITY SYSTEMS, OF CLAIM ONE , CAN BE A GENERAL , UNIVERSAL HOMOGENOUSE ENGINE OPERATING SYSTEMS, BASED AND COMPOSED FROM ONLY TWO ENGINE CYLINDERS, OF TWO OR FOUR CYCLES OPERATING SYSTEMS, PROVIDED WITH SPECIAL WORKING AND CYCLE CONTROL PISTONS, PROVIDED WITH SPECIFIC OPERATING FUNCTIONS, AND SEALED BY SPECIFIC PISTON RINGS, HAVING TOP COMBUSTION CHAMBER, CONNECTED BY THERMAL INSULATED INTERNAL CHANELLS, WITH BOTTOM CONNECTION OPENINGS, FOR CONNECTING EXTERNAL HOMOGENOUSE COMBUSTION CHAMBERS,IN WHICH THE PISTONS ARE CONTROLLING THE INTAKE OF AIR OR OXYGEN AND EXHAUST GASES SYSTEMS, CONTROLLING THE COMPRESSION, AND STARTING THE COMBUSTION OF

HOMOGENOUSE PLASMA FUEL SYSTEMS, AND THE RETAINER OF PORTIONS OF PARTIAL EXPANDED COMBUSTION GASES, IN THE ASSOCIATED HOMOGENOUSE COMBUSTION

CHAMBER,IN WHICH WIL BE INJECTED ANY AND ALL FUELS, LIQUID, OR GAS, INDIVIDUALL OR COMBINED IN ANY PROPORTIONS TO FORM WITH THE RETANED PARTIALLY EXPANDED COMBUSTION GASES, A HOMOGENOUSE PLASMA FUELS, AND RETAINED PARTIALLY EXPANDED COMBUSTED GASES, FORMING A PLASMA CAPTURED IN A SPECIFIC MOMENT. FROM THE COMPRESSION AND EXPANSION STROKE.

THE ENTIRE HOMOGENOUSE CONTROLLED COMBUSTION SYSTEM , FROM CLAIME ONE, AND TWO, HAVE THE FUNDAMENTAL CHARACTERISTIC OF INDEPENDENTLY CONTROLLED

COMPRESSING OF THE AIR OR OXYGEN AT ANY AND MAXIMUM PRESSURE RATIOS, AND TOTALLY SEPARATED FUEL HOMOGENOUSE MIXTURE, RESIDENT IN THE ASSOCIATED

COMBUSTION CHAMBER, UNTIL THE MOMENT OF INJECTING THE AIR/OXIGEN IN THE

HOMOGENOUS PLASMA SEPARATED FUEL MIXTURE PRODUCING A CONTROLLED PERFECT COMBUSTION.

THE COMPLETE OPERATION ENGINE SYSTEMS OF CLAIME ONE AND TWO, IS ASSOCIATED WITH AN ELECTRIC TURBO COMPOUND SYSTEMS, COMPOSED FROM AN ELECTRIC DRIVEN ROTARY COMPRESSOR, FOR AIR OR OXYGEN SEPARATED AND ELIMINATING THE NITROGEN, SUPPLYING CONSTANT PRESSURE HUMID AIR OR OXYGEN, IN THE INTAKE PORTS OF THE ENGINE CYLINDERS, AND AN EXHAUST GASES TURBINE, DRIVING ELECTRIC POWER GENERATORS, WITHOUT WAIST GASES, THE COMBINED ENGINE POWER GENERATION, AND THE ASSOCIATED ELECTRIC TURBO COMPOUNDING SYSTEM,IS PRODUCING A COMBINED ENERGY SYSTEM, WHICH IS OPERATING AT CONSTANT PRESSURE, PRODUCING CONSTANT MAXIMUM

EFFICIENCY IN ALL THE SPECTRUM OF OPERATION FROM FULL TO PART LOADS.

9. THE COMPLETE AND UNIVERSAL ENERGY AND ENGINE SYSTEM CAN OPERATE AT UNIQUE HIGH PRESSURE FOR SUPER CHARGING, OF 10/1, AIR OR OXIGEN WITHOUT NYTROGEN,

COMPRESSION AND COMBUSTION AT MORE THAN 300 BAR, AND TOTAL COMBINED

EXPANSION RATIO OF/ OR MORE THAN 300/1 PRESSURE RATIO , RESULTING MORE THAN 80% CONSTANT THERMAL EFICIENCY, AND MINIMUM EXHAUST TEMPERATURE, CLOSED TO CONDENSING THE PURE WATER, RESULT OF HYDROGEN COMBUSTION, AND TOTAL

ELIMINATION OF NOX POLLUTION, AND MINIMUM C02 PRODUCTION RESULT OF MAXIMUM ABSOLUTE EFFICIENCY

10. THE ENTIRE UNIVERSAL ENGINE HYPERBARIC SYSTEM OF CLAIME ONE, AND TWO, CAN BE OPERATED ON EXTERNAL CLOSED CYCLE, UNAEROBIC NUCLEAR SYSTEM, FOR SUBMARINES AND SPACE VEHICLES, BY PRODUCING HIGH PRESSURE WORKING FLUIDS, CONNECTING PERMANENTELY, THE NUCLEAR REACTOR, WITH THE ASSOCIATED EXTERNAL CHAMBER,AND THE CONTROLLING WORKING OPPOSED CYLINDERS AND PISTONS, BY THE EXHAUST ELECTRIC OPERATING VALVE SYSTEM, CONTROLLING THE EXPANSION CYCLE AND THE RECIRCULATED WORKING FLUID, TO A CONDENSING UNIT AND THE WORKING LIQUID FLUID TO BE HIGH PRESSURE REINJECTED IN THE NUCLEAR REACTOR FOR COOLING AND GENERATING CONTINUOUSE HIGH PRESSURE ENERGETING WORKING FLUID, EXPANDED IN THE HYPERBARIC ENGINE GENERATING DIRECT ELECTRIC ENERGY.