WO2015075742A2

WO2015075742A2 - Uses of exhaust gases of jet engine

Info

Publication number: WO2015075742A2
Application number: PCT/IN2014/000690
Authority: WO
Inventors: Prashant Ramchandra PAWAR
Original assignee: Pawar Prashant Ramchandra
Priority date: 2013-11-06
Filing date: 2014-10-31
Publication date: 2015-05-28
Also published as: WO2015075742A3; IN2013MU01624A

Abstract

This "Uses of exhaust gases of jet engine" invention related with automobile engineering, mechanical engineering, power engineering electrical engineering, hybrid engineering; and electrolysis process and environment safety and global warming too, then main technical problem of conventional internal combustion engine is that they are less fuel efficient and engine power get consume because of in case alternator 6 or alternator 55 or dynamo 72 driven by any type of IC engine, produce toxic exhaust gases too. To overcome from these above mentioned problem of any type of IC engine I invented the concept of the "turbo electricity and turbo electrolysis". By using my invention any type of IC engine get best mileage and any type of IC engine make eco friendly.

Description

Title of invention:

"USES OF EXHAUST GASES OF JET ENGINE".

DESCRIPTION OF MY INVENTION IS AS FOLLOW .THE FOLLOWING SPECIFICATION DESCRIBE THE INVENTION. THIS INVENTION RELATED WITH FIELD OF MECHANICAL ENGINEERING, AUTOMOBILE ENGINEERING, AERONAUTICAL ENGINEERING, AEROSPACE ENGINEERING, DEFENCE SYSTEM OF DIFFERENT COUNTRIES,AND POWER ENGINEERING, ELECTRICAL ENGINEERING, HYBRID ENGINEERING OR HYBRID TECHNOLOGY. THE MAIN FEATURE OF THIS INVENTION IS THAT IN THIS INVENTION I EXPLAIN DIFFERENT HYBRID FUEL OPTION USE IN IC ENGINE WITH CONVENTIONAL PETROLIUM FUEL OR WITHOUT CONVENTIONAL FUEL .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE IN THE CONSTRUCTION OF

TURBOFAN ENGINE 113.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE IN THE TURBOFAN ENGINE 113 THE LOW PRESSURE COMPRESSOR 125 AND LOW PRESSURE TURBINE 127 INSTALLED ON LOW PRESSURE SHAFT 129 AND HIGH PRESSURE COMPRESSOR 126 AND HIGH PRESSURE TURBINE 128 INSTALLED ON HIGH

PRESSURE SHAFT 130.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE IN THE TURBOFAN ENGINE 113 THE FUEL INJECTOR 131 AND SPARK PLUG 132 FITTED IN

COMBUSTION CHAMBER 135.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE WORKING OF TURBOFAN JET ENGINE 113 ON PRINCIPLE OF NEWTON'S THIRD LAW OF MOTION ; THIS LAW STATE THAT EVERY ACTION IN NATURE THERE IS AN EQUAL AND OPPOSITE REACTION.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE WHEN TURBOFAN ENGINE 113 GET START LOW PRESSURE COMPRESSOR 125 START ROTATING SO RESULT IN LOW PRESSURE COMPRESSOR 125 SUCK THE FRESH AIR 22 FROM ATMOSPHERE AND LOW PRESSURE COMPRESSOR 125 BLADE COMPRESS THIS FROM ATMOSPHERIC PRESSURE LEVEL TO HIGH PRESSURE LEVEL THAN ATMOSPHERIC PRESSURE LEVEL SO TEMPERATURE OF AIR 22 GET I CREASE. REFERRING TO FIGURE 1 CAN BE SEEN THAT THE HIGH PRESSURE COMPRESSOR 126 SUCK THIS COMPRESSED AIR WHICH IS ALREADY COMPRESSED BY LOW PRESSURE COMPRESSOE 125 AND HIGH PRESSURE COMPRESSOR 126 AGAIN COMPRESS THIS COMPRESSED AIR 22 FORM HIGH PRESSURE LEVEL TO VERY HIGHER PRESSURE LEVEL THAN ATMOSPHERIC PRESSURE LEVEL .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE IN SHORT IN WORKING COMBINATION OF HIGH PRESSURE COMPRESSOR 126 AND LOW PRESSURE COMPRESSOR 125 COMPRESS THE AIR 22 FROM ATMOSPHERIC PRESSURE LEVEL TO HIGH PRESSURE LEVEL .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE HIGH PRESSURE COMPRESSOR 126 SENT THIS COMRESSED AIR IN COMBUSTION CHAMBER 135 WHERE HIGH FLAMABLE FUEL INJETCED BY INJECTOR 131 AND SPARK PRODUCE BY SPARK PLUG 132 INTO COMPRESSED AIR ; SO RESULT IN FUEL 136 BURN WITH OXYGEN PRESENT IN THIS COMPRESSED AIR , HENCE TEMPERATURE AND PRESSURE OF COMRESSED AIR INCREASE AT VERY HIGH LEVEL IN COMBUSTION CHAMBER 135 AND AIR 22 AND FUEL 136 MIXURE CONVERT INTO HOT EXHAUST GASES 20.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE THIS HOT EXHAUST GASES 20 FIRST STRIKE ON HIGH PRESSURE TURBINE 128 WITH BIGEER PRESSURE AND KINETIC ENERGY SO RESULT IN HIGH PRESSURE TURBINE 128 START ROTATING AND PRESSURE AND TEMPRETURE OF HOT EXHAUST GASES 20 GET REDUCE AND THEN AGAIN THIS HOT EXHAUST GASES 20 STRIKE ON LOW PPRESSURE TURBINE 127 WITH PRESSURE AND KINETIC ENERGY ; SO RESULT IN PRESSURE AND TEMPRETURE OF HOT EXHAUST GASES 20 GET REDUCE AGAIN AND LOW PRESSURE TURBINE 127 START ROTATE AND HOT EXHAUST GASES 20 TRAVEL IN EXHAUST PIPE 5 AND MIX THROUGH ATMOSPHERE AND BIG THRUST . REFERRING TO FIGURE 1 CAN BE SEEN THAT THE WHEN HIGH PRESSURE TURBINE 128 AND LOW PRESSURE TURBINE 127 ROTATE DUE: TO STRIKE OF HOT EXHAUST GASES 20 THEN HIGH PRESSURE COMPRESSO 126 AND LOW PRESSURE COMPRESSOR 125 ALSO ROTATE BECAUSE HIGH PRESSURE COMPRESSOR 126 AND HIGH PRESSURE TURBINE 128 INSTALLED OR MOUNTED ON SHAFT 130 AND LOW! PRESSURE TURBINE 127 AND LOW PRESSURE COMPRESSOR 125 INSTALLED ON SHAFT 129 .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE SO RESULT IN AGAIN LOW PRESSURE COMPRESSOR 125 START ROTATING SO AGAIN RESULT IN LOW PRESSURE COMPRESSOR 125 SUCK TH E FRESH AIR 22 FROM ATMOSPHERE AND LOW PRESSURE COMPRESSOR 125 BLADE COMPRESS THIS FROM ATMOSPH ERIC PRESSU RE LEVEL TO HIGH PRESSURE LEVEL THAN ATMOSPHERIC PRESSURE LEVEL SO TEMPERATURE OF AIR 22 GET INCREASE.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE HIGH PRESSURE COMPRESSOR 126 SUCK THIS COMPRESSED AIR WHICH IS ALREADY COMPRESSED BY LOW PRESSU RE COMPRESSOE 125 AND HIGH. , PRESSURE COMPRESSOR 126 AGAIN COMPRESS THIS COMPRESSED AIR 22 FORM HIGH PRESSURE LEVEL TO VERY HIGHER PRESSURE LEVEL THAN ATMOSPHERIC PRESSURE LEVEL .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE IN SHORT IN WORKING COMBINATION OF HIGH PRESSURE COMPRESSOR 126 AND LOW PRESSURE COMPRESSOR 125 COMPRESS TH E AIR 22 FROM ATMOSPHERIC PRESSURE LEVEL TO HIGH PRESSURE LEVEL .

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE HIGH PRESSURE COMPRESSOR 126 SENT THIS COMRESSED AI R IN COMBUSTION CHAMBER 135 WHERE HIGH FLAMABLE FUEL INJETCED BY INJEcjrOR 131 AND SPARK PRODUCE BY SPARK PLUG 132 INTO COMPRESSED AIR ; SO RESULT IN FUEL 136 BURN WITH OXYGEN PRESENT IN THIS COMPRESSED AIR , HENCE TEMPERATURE AND

PRESf; IRE OF COMRESSED AIR INCREASE AT VERY HIGH LEVEL IN COMBUSTION CHAMBER 135 AND AIR 22 AND FUEL 136 MIXURE CONVERT INTO HOT EXHAUST GASES 20.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE THIS HOT EXHAUST GASES 20 FI RST STRIKE ON HIGH PRESSURE TU RBI NE 128 WITH BIGEER PRESSURE AND KINETIC ENERGY SO RESULT IN HIGH PRESSURE TURBINE 128 START ROTATING AND PRESSU RE AND TEMPRETURE OF HOT EXHAUST GASES 20 GET REDUCE AND THEN AGAIN THIS HOT EXHAUST GASES 20 STRIKE ON LOW PPRESSURE TURBINE 127 WITH PRESSURE AND KINETIC ENERGY SO RESULT IN

PRESSURE AND TEM PRETURE OF HOT EXHAUST GASES 20 GET

.V. : .

REDUCE AGAIN AND LOW PRESSURE TURBINE 127 START ROTATE AND. HOT EXHAUST GASES 20 TRAVEL IN EXHAUST PIPE 5 AND MIX THROUGH ATMOSPHERE AND BIG THRUST .

REFERRING TO FIGURE 1 CAN BE SEEN THAT TH E WHEN HIGH PRESSURE TURBINE 128 AND LOW PRESSURE TURBINE 127 ROTATE DUE TO STRIKE OF HOT EXHAUST GASES 20 THEN HIGH PRESSURE COMPRESSOR 126 AND LOW PRESSURE COMPRESSOR 125 ALSO ROTATE BECAUSE HIGH PRESSURE COMPRESSOR 126 AND HIGH PRESSURE TURBINE 128 INSTALLED OR MOUNTED ON SHAFT 130 AND LOW PRESSURE TURBINE 127 AND LOW PRESSURE COMPRESSOR 125 INSTALLED ON SHAFT 129 . THIS CYCLE CONTINUE AGAIN AND AGAIN.

REFERRING TO FIGURE 1 CAN BE SEEN THAT THE I N TURBOFAN JET ENGINE 113 HOT EXHAUST GASES 20 ARE ALSO USE TO ROTATE AXIAL FAN \ 115 WHICH IS ATTACHED TO THE SHAFT 129 FOR INCREASE THRUST AND FU EL ECONOMY.

FOLLOWING IS LIST OF TH E JET ENGINE IN WHICH MY INVENTION USE FOR REDUCE ELECTRICITY AND INFRARED VISIBILITY OF HOT EXHAUST GASES 20 OF IC ENGINE -

1. TU RBO JET ENGINE

Ί

2. TURBO JET ENGINE WITH AFTER BURNER.

3. TU RBOPROP JET ENGINE 4.TURBOPROP JET ENGINE WITH AFTER BURNER.

5.TURB0FAN JET ENGINE WITH AFTER BURNER.

6.SMALL BY PASS TURBOFAN JET ENGINE . 7.HIGH BY PASS TURBO FAN JET ENGINE.

IN THIS INVENTION CURRENT REPRESENTED BY LETTER I AND ANGLE OF ROTATION OF ARMATURE COIL 12 OR ARMATURE COIL 75 OR COIL AB REPRESENT BY Θ.

REFERRING TO FIGURE 2 TO FIGURE 6 CAN BE SEEN THAT THE

MAGNET 10 AND MAGNET 11, ACCORDING TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION, AN E.M.F. IS PRODUCE IN THEM WHICH IS CAUSES CURRENT TO FLOW THROUGH THE EXTERNAL CIRCUITE. TH E MAGNITUDE OF THIS E.M.F. IS DEPENDENT ON SELECTED POSITION OF THE ARMATUR COIL 12 IN RELATION TO THE MAGNETIC FIELD.

REFERRING TO FIGURE 2 CAN BE SEEN THAT THE ANGLE OF ROTATIO Θ OF ARMATUR COIL 12 IS O DEGREE.

REFERRING TO FIGURE 2 CAN BE SEEN THAT THE THIS IS INITIAL POSITION-1 OF ARMATUR COIL 12 AND ARMATUR COIL 12 IS PERPENDICULAR TO THE MAGNETIC FIELD THE CONDUCTOR A AND CONDUCTOR B OF THE COIL MOVE PARALLEL TO THE MAGNETIC FIELD . SINCE THERE IS NO FLUX CUTTING , NO E.M.F. GENERATED IN THE CONDUCTORS AND THEREFORE , NO CURRENT FLOW THROUGH THE EXTERNAL CIRCUITE.

REFERRING TO FIGURE 3 CAN BE SEEN THAT THE FIGURE 3 INDICATE POSITION-2 OF THE ARMATURE COIL 12.

REFERRING TO FIGURE 3 CAN BE SEEN THAT THE ANGLE OF ROTATION Θ OF ARMATUR COIL 12 IS 90 DEGREE.

REFERRING TO FIGURE 2 AND FIGURE 3 AND CAN BE SEEN THAT THE ARMATURE COIL 12 ROTATE FROM POSITION -1 TO POSITION -2 ,MORE AND MORE LINES OF FORCE ARE CUT BY THE CONDUCTORS. IN THE POSITION -2 CONDUCTOR A AND CONDUCTOR B OF ARMATURE COIL 12 MOVE AT RIGHT ANGLE TO THE MAGNETIC FIELD AND CUT THROUGH A MAXIMUM NUMBER OF LINES OF FORCE , SO THE E.M.F. INDUCED IN THEM IS ALSO MAXIMUM . IN OTHER WORDS,BETWEEN ZERO TO 90 DEGREE , THE E.M.F. IN BOTH CONDUCTORS BEING IN SERIES, THE RESULTANT ARMATURE COI L 12 E.M.F. IS THE SUM OF THE TWO CONDUCTOR E. M.F. .IT IS THEREFORE /TWICE THAT OF ONE OF THE CONDUCTORS , SINCE THE VOLTAGE ARE EQUAL. THE CURRENT THROUGH THE CIRCUITE VARIES JUST AS THE E.M.F. VARIES ,BEING ZERO fT 0 DEGREE AND TO A MAXIMUM AT 90 DEGREE . IN POSITION - 2 OF THE ARMATU RE COIL 12 , ACCORDING FLEMING'S RIGHT HAND RULE JHE DIRECTION OF THE INDUCED CURRENT IN CONDUCTOR A IS TOWARD THE OBSERVER AND IN CONDUCTOR B, IT IS AWAY FROM THE OBSERVERAS INDICATED.THERFORE, THE CURRENT FLOWS TH ROUGH EXTERNAL RESISTER FROM THE TERMINAL C TO THE TERMINAL D.

REFERRING TO FIGURE 4 CAN BE SEEN THAT THE ANGLE OF ROTATION Θ OF ARMATUR COIL 12 IS 180 DEGREE.

REFE ING TO FIGURE 4 CAN BE SEEN THAT THE FIGURE 4 INDICATE POSITION-3 OF THE ARMATURE COIL 12.

REFERRING TO FIGURE 3 AND FIGURE 4 CAN BE SEEN THAT THE ARMATURE COIL 12 CONTINUES TO ROTATE FU RTHER FROM POSITION -2 TO ; POSITION -3 , THE LINES OF FORCE CUT BY THE CONDUCTORS GRADUALLY REDUCE THIS DECREASES THE GENERATED E.M.F. IN THEM

REFERRING TO FIGURE 4 CAN BE SEEN THAT TH E IN POSITON-3, THE CONDUCTOR A AND CONDUCTOR B OF ARMATURE COIL 12 AGAIN PARALLEL TO TH E FIELD AND HENCE NO E.M.F. IS INDUCED IN THEM. TH EREFORE, THE CURRENT THROUGH THE EXTERNAL RESISTOR IS ALSO ZERO.

REFERRING TO FIGURE 2 AND FIGURE 4 CAN BE SEEN THAT THE DURING THE ROTATION OF THE ARMATURE COIL 12 FROM 0 DEGREE TO 180 DEGREE, TH E CONDUCTOR A AND CONDUCTOR B OF THE ARMATURE COIL 12 MOVE IN THE SAME DIRECTION THROUGH THE MAGNETIC FIELD . TH ERFORE , THROUGHOUT THIS PERIOD , THE POLARITY OF THE GENERATED E.M.F. REMAINS SAM E AND CURRENT FLOWA THROUGH THE EXTERNAL RESISTOR FROM C TO D ONLY.

REFERRING TO FIGURE 5 CAN BE SEEN THAT THE FIGURE 5 INDICATE POSITION-4 OF THE ARMATURE COIL 12.

REFERRING TO FIGURE 6 CAN BE SEEN THAT THE ANGLE OF ROTATION Θ OF ARMATUR COIL 12 IS 360 DEGREE.

REFERRING TO FIGURE 2 TO FIGURE 6 CAN BE SEEN THAT THE ARMATURE COIL 12 ROTATE FROM POSITION -1 TO POSITION -4. REFERRING TO FIGURE 4 CAN BE SEEN THAT THE AS THE ARMATURE COIL 12 ROTATES BEYOND POSITION - 3 THE DIRECTION OF THE CUTTING ACTION OF THE CONDUCTORS THROUGH THE MAGNETIC FIELD REVERSES. NOW THE CONDUCTOR A OF THE ARMATURE COIL 12 CUTS UP THROUGH THE FIELD AND THE CONDUCTOR B OF THE ARMATURE COIL 12 CUTS DOWN THROUGH THE FIELD . IN CONSEQUENCE BOTH, THE POLARITY OF THE GENERATED E.M.F. AND THE CURRENT FLOW REVERSE.TO MAKE IT MORE CLEAR , CONCIDER THE COIL POSITION - 4 BY APPLYING FLEMING'S RIGHT HAND RULEJT IS SEEN THAT DIRECTION OF THE INDUCED CURRENT IN CONDUCTOR A OF ARMATURE COIL 12 IS AWAY FROM THE OBSERVER AND IN CONDUCTOR B, IT IS TOWARD THE OBSERVER.AS SUCH , CURRENT FLOWS THROUGH THE EXTERNAL RESISTOR R FROM D TO C. THUS , DURING THE ENTIRE SECOND HALF REVOLUTION I.E. WHEN THE ARMATURE COIL 12 ROTATES FROM POSITION -3 TO POSITION -4 AND BACK TO THE POSITION -1 , THE CURRENT FLOWS IN THE OPPOSITE DIRECTION TO THAT IN THE FIRST HALF REVOLUTIONS . ALSO SIMILAR TO POSITION -2 , E.M.F. IN THE ARMATURE COIL 12 IS MAXIMUM IN POSITION -4. IN GENERAL , THE VARIATIONS IN THE MAGNITUDE OF E.M.F. OF THE ALTERNATOR 6 WHEN THE ARMATURE COIL 12 ROTATES FROM 180 DEGREE TO 360 DEGREE , ARE EXACTLY SIMILAR TO THOSE IN THE FIRST HALF REVOLUTION.

REFERRING TO FIGURE 7 CAN BE SEEN THAT THE UNIT 88 CONTAIN THE TRANSFORMER 63 AND FULL WAVE BRIDGE RECTIFIER 13 AND VOLTAGE REGULATOR 65 AND BATTERY 14 AND FILTER CAPACITOR 64.

REFERRING TO FIGURE 7 CAN BE SEEN THAT THE IN THE UNIT 88

VOLTAGE REGULATOR 65 AND OUTPUT TERMINAL OF THE VOLTAGE REGULATOR 65 IS CONNECTED TO THE INPUT TERMINAL OF THE BATTERY 14 .

REFERRING TO FIGURE 8 CAN BE SEEN THAT THE U NIT 116 CONTAIN THE TRANSFORMER 63 AND FULL WAVE BRIDGE RECTIFIER 13 AND VOLTAGE REGULATOR 65 AND FILTER CAPACITOR 64 .

REFERRING TO FIGURE 7 AND FIGURE 8 CAN BE SEEN THAT THE MAIN DIFFRENCE IN TH E UNIT 116 AND U NIT 88 IS THAT IN UNIT 116 NOT INCLUDE BATTERY 14 AND REMAINING CONSTRUCTION OF UNIT 116 IS EXACTLY SIMILAR TO THE UNIT 88.

REFERRING TO FIGURE 9 AND FIGURE 10 CAN BE SEEN THAT THE A STEP DOWN TRANSFORMER 63 IS USED TO REDUCE THE AC MAINS VOLTAGE TO AN ADEQUATELY SMALL VALUE AND TH E TURNS RATIO OF THE TRANSFORMER 63 IS ADJUSTED TO OBTAINED A STEPPED DOWN AC VOLTAGE.

REFERRING TO FIGURE 9 AND FIGURE 10 CAN BE SEEN THAT THE FULL WAVE BRIDGE RECTIFIER 13 CONVERTING THE ALTERNATING VOLTAGE OR CURRENT INTO A U NIDIRECTIONAL VOLTAGE OR CURRENT AND THE FULL WAVE BRIDGE RECTIFIER 13 CONSISTS OF FOUR DIODES CONNECTED TO FORM A BRIDGE AND CENTER TAPPED INPUT TRANSFORMER IS NOT REQUIRED.

REFERRING TO FIGURE 9 AND FIGURE 10 CAN BE SEEN THAT THE FULL WAVE BRIDGE RECTIFIER 13 OFFERS FULL WAVE RECTIFICAION AND TH E DIODES CONDUCT IN PAIRS.

REFERRING TO FIGU RE 9 AND FIGURE 10 CAN BE SEEN THAT THE ALTERNATOR 6 PRODUCE AC TURBOELECTRICITY AND TRANSFORMER 63 REDUCE IT VALU E AT DESIRE LEVEL .

REFERRING TO FIGURE 9 CAN BE SEEN THAT THE OPERATION OF THE FULL WAVE BRIDGE RECTIFIER 13 IN POSITIVE HALF CYCLE OF AC TURBO ELECTRICITY WHICH IS PRODUCE BY ALTERNATOR 6 BY USING POWER OF THE EXHAUST GASES 20 OF IC ENGINE 113 . REFERRING TO FIGURE 9 CAN BE SEEN THAT THE I N POSITIVE HALF CYCLE OF AC TURBOELECTRICITY SUPPLY TH E SECONDARY VOLTAGE VAB IS POSITIVE , THEREFORE DIODE Di AND DIODE D2 ARE FORWARED BIASED WHEREAS DIODE Ds AND DIODE D4 ARE REVERSE BIASED .

REFERRING TO FIGURE 9 CAN BE SEEN THAT THE I N POSITIVE HALF CYCLE OF AC TURBOELECTRICITY SUPPLY AND THE EQUIVALENT CIRCUITE FOR THIS INTERVAL SHOWN IN FIGURE 9.

REFERRING TO FIGURE 9 CAN BE SEEN THAT THE IN POSITIVE HALF CYCLE OF AC TU RBOELECTRICITY REVERSE BIASED DIODE D3 AND DIODE! D4 ARE ACT AS OPEN SWITCHES.

REFERRING TO FIGURE 10 CAN BE SEEN THAT THE OPERATION OF THE FULL WAVE BRIDGE RECTIFIER 13 IN NEGATIVE HALF CYCLE OF AC TURBO ELECTRICITY WHICH IS PRODUCE BY ALTERNATOR 6 BY USING POWER OF THE EXHAUST GASES 20 OF ENGINE 113 .

REFERRING TO FIGURE 10 CAN BE SEEN THAT THE OPERATION OF THE FULL WAVE BRIDGE RECTIFIER 13 IN NEGATIVE HALF CYCLE OF AC TURBOELECTRICITY OF ALTERNATOR 6.

REFERRING TO FIGURE 10 CAN BE SEEN THAT THE IN NEGATIVE HALF CYCLE OF AC TURBOELECTRICITY SUPPLY THE SECONDARY VOLTAGE VAB IS NEGATIVE, THEREFORE DIODE D3 AND DIODE D4 ARE FORWARED BIASED WHEREAS DIODE Di AND DIODE D2 ARE REVERSE BIASED .

REFERRING TO FIGURE 10 CAN BE SEEN THAT THE IN NEGATIVE HALF CYCLE OF AC TU RBOELECTRICITY SUPPLY AND TH E EQUIVALENT CIRCUITE FOR THIS INTERVAL SHOWN IN FIGURE 10.

REFERRING TO FIGURE 10 CAN BE SEEN THAT TH E IN NEGATIVE HALF CYCLE OF AC TURBOELECTRICITY REVERSE BIASED DIODE Di

AN D D IO DE D2 AR E ACT AS OPEN SWITCH ES.

i ^'

REFERRING TO FIGU RE 7 TO FIGURE 10 CAN BE SEEN THAT THE INPUTj; TERMINALS OF THE FILTER CAPACITOR 64 CONNECTED TO THE OUTPUT TREMINAL OF THE FULL WAVE BRIDGE RECTIFIER 13 BECAUSE TO REDUCE THE RIPPLE CONTENTS IN THE OUTPUT OF A FULL WAVE BRIDGE RECTIFIER 13 TO OBTAIN PURE DC VOLTAGE.

REFERRING TO FIGURE 7 TO FIGURE 9 CAN BE SEEN THAT THE WE CAN CONNECT THE FILTER CAPACITOR 64 ACROSS THE OUTPUT TREMINAL OF THE FULL WAVE BRIDGE RECTIFIER 13 .

REFERRING TO FIGURE 9 TO FIGU RE 10 CAN BE SEEN THAT THE OUTPUT TREMINAL OF THE FILTER CAPACITOR 64 CONNECTED TO THE VOLTAGE REGULATOR 65 AND VOLTAGE REGULATOR 65 IS LAST STEP IN TH E DC TURBOELECTRICITY ; VOLTAGE REGULATOR 65 IS CIRCUITE WHICH WILL TRY T O MAINTAIN OUTPUT VOLTAGE CONSTANT UNDER ALL THE OPERATING CONDITION ; SO RETSULT IN WHEN FULL CYCLE OF AC TURBOELECTRICITY TRAVEL IN THE EQUIVALENT CIRCUITE MENTIONED IN FIGU RE 9 AND FIGURE 10 THEN WE GET RIPPLE FREE PURE DC VOLTAGE OR PURE DC TURBOELECTRICITY AT OUTPUT TERMINAL OF VOLTAGE REGULATOR 65 AND THIS OUTPUT TERMINAL OF VOLTAGE REGULATOR 65 IS CONNECTED TO THE BATTERY 14 SO RESULT IN BATTERY GET CHARGE AND INPUT TERMINAL OF THE BATTERY 14 IS CONNECTED THE OUTPUT TERMINAL OF THE LOAD OR BU LE 29.

REFERRING TO FIGURE 11 CAN BE SEEN THAT THE FIGURE 11 SHOW THE DETAIL ATOM STUCTURE OF ELEMENT AND COMPOUND OF BATTERY 14 WHEN THE BATTERY 14 GET THE CHARGING ON TURBOELECTRICITY PRODUCE BY OF ALTERNATOR 6 .

REFERRING TO FIGURE 11 CAN BE SEEN THAT THE FIGURE 11 SHOW THE CHEMICAL REACTION DONE IN BATTERY 14 WHEN BATTERY 14 GET CHARGING ON TU RBOELECTRICITY PRODUCE BY OF ALTERNATOR 6 .

REFERRING TO FIGURE 11 CAN SEEN THAT THE POTENTIAL OR VOLTAGE DIFFRENCE CREATED BETWEEN TWO METALS , WHICH ARE IMMERSED IN AN ELECTROLYTE ,IS CALLED CELL VOLTAGE . A BATTERY 14 CONVERT CHEMICAL ENERGY OF METALS SUBMERGED IN

ELECTROLYTE INTO ELECTRICAL ENERGY BY MEANS OF AN ELECTRO

ί.

CHEMBOAL OXIDATION -REDUCTION PROCESS.

^{■ '} Mir? REFERRING TO FIGURE 11 CAN SEEN THAT WHEN THE BATTERY 14 TERMINAL ARE CONNECTED Tl AN EXTERNAL LOADJHE SULPHATE IRON IN THE ELECTROSLYTE COMBINE W ITH THE POSITIVE AND NEGATIVE PLATES ^'". FORMING LEAD SULPHATE AND ELECTRIVAL ENERGY IS RELEASEb .

REFERRING TO FIGURE 11 CAN SEEN THAT OXYGEN IN THE ACTIVE MATERIAL OF THE POSITIVE PLATES COMBINES WITH HYDROGEN FROM THE SULPHURIC ACID TO FORM WATER , WHICH REDUCES THE CONCENTRATION OF THE ACID IN ELETRCOLYTE.AS THE DISCHARGE CONTINUOUS , THE ACTIVE ELEMENTS OF BOTH PLATES BECOME MORE ALIKE, I. E. LEAD SULPHATE AND THE ELECROLYTE BECOME WEAKER.

REFERRING TO FIGURE 11 CAN SEEN THAT THEREFORE THE VOLTAGE BECOMES LOWER A CONCENTRATION OF ACID REDUCES. EVENTUALLY THE BATTERY LOSSES ITS POWER OF DELIVERING ELECTRICALY AT AN IMPRESSIVE INTENSITY OF VOLTAGE AND IS SAID TO BE DISCHARGED.

REFERRING TO FIGURE 11 CAN SEEN THAT THE ACTIVE CHEMICALS CAN BE RESTOREDTO THE CHARGED BY PASSING CURRENT IN OPPOSITE DIRECTION .

REFERRING TO FIGURE 11 CAN SEEN THAT THIS IS SAID TO BE THE CHARGED CONDITION OF THE BATTERY 14.THE HEAVIEST DEMAND IS MADE ON A BATTERY 14 WHEN ENGINE 1 IS STARTED. IN MOST MODERN CARS ONCE ENGINE 1 IS RUNNING , THE DYNAMO PROVIDE A FLOW OF CURRENT TO THE BATTERY 14 TO RECHARGE IT AND KEEP IT CHARGED AND IN MOST MODERN CARS THE NEGATIVE TERMINAL OF BATTERY 14 IS EARTHED BY CONNECTING TO CHASSIS OR BODY.

REFRRING TO FIGURE 12 CAN BE SEEN THAT THE EQUATION OF THE CHEMICAL REACTION OF BATTERY 14 WHEN IT GET CHARGING AND DISCHARGING.

REFRRING TO FIGURE 13 CAN BE SEEN THAT THE DETAIL PART OF ELECTROLYTE UNIT 18 IN WORKING POSITION.

REFERRING TO FIGURE 15 CAN BE SEEN THAT THE ; THE FIGURE 15 INDICATE THAT CONVENTIONAL TURBOFAN ENGINE 113 GET START IT PRODUCE CONVENTIONAL HOT TOXIC EXHAUST GASES 20 .

REFERRING TO FIGURE 2 TO FIGURE 6 CAN BE SEEN THAT THE BASIC CONCEPT OF " TURBO ELECTRICITY."

REFERRING TO FIGURE 2 TO FIGURE 6 AND FIGURE 15 CAN BE SEEN THAT THE IN THIS INVENTION WHEN INTRNAL COMBUSTION ENGI NE

113^! GET START IT PRODUCE EXHAUST GASES 20 WHICH CAME OUT IN THROUGH EXHAUST PIPE 5 AND STRIKE ON TU RBINE WHEEL 7 AND THEN THIS EXHAUST GASES 20 MIX IN TH E ATMOSPERE VIA THROUGH TURBINE EXHAUST GAS OUTLET 8 . TURBINE WHEEL 7 PLACE IN TURBINE HOUSING 9.

REFERRI NG TO FIGURE 2 TO FIGURE 6 AND FIGURE 15 CAN BE SEEN THAT TH E SO ; WHEN OF EXHAUST GASES 20 OF OF INTERNAL COMBUSTION ENGINE 113 GET STRIKE ON TURBINE WHEEL 7 AND TURBINE WHEEL 7 GET START ROTATE DUE TO KINETIC ENERGY AND PRESSURE CONTAIN IN EXHAUST GASES 20 ANY TYPE INTERNAL COMBUSTION ENGINE 1 ; SO RESU LT IN; TEMPRETURE AND PRESSURE OF EXHAUST GASES 20 OF ANY TYPE OF INTERNAL COMBUSTION ENGINE 1 GET REDUCE .WE CAN CONVERT THE PRESSURE AND KI NETIC ENERGY CONTAIN IN EXHAUST GASES 20 OF ANY TYPE OF INTERNAL COMBUSTION ENGINE 1 INTO MECHANICAL WORK BY USI NG TURBINE WHEEL 7.

LET SEE FIRST PRINCIPLE OF GENERATOR OR ALTERNATOR 6 AND ALTERNATOR 55:- WHEN CONDUCTOR IS MOVED I N MAGNETIC FIELD OR MAGNETIC FIELD IS MOVED WITH RESPECT TO THE CONDUCTOR ACCORDI ND TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION , AN ELECTROMOTIVE FORCE IS SET UP IN CONDUCTOR .TH US AS LONG AS THERE IS RELATIVE MOTION BETWEEN CONDUCTOR AND MAGNETIC FIELD., A VOLTAGE WILL ALWAYS BE GENERATED I N THE CONDUCTOR.

REFERRING TO FIGURE 2 TO FIGURE 6 CAN BE SEEN THAT THE WORKING OF ALTERNATOR 6 ACCORDING TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION AS FOLLOW :-

IN THIS INVENTION ; SO WHEN ANY TYPE OF IC ENGINE 1 GET START IT PRODUCE THE EXHAUST GASES 20 STRIKE ON TURBINE WHEEL 7 AND ARMATURE 12 ROTATE IN MAGNETIC FIELD OF MAGNET 10 AND MAGNET 11 ; SO MAGNETIC FLUX CUT BY ARMATURE 12 THEN ACCORDING TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION , AN E.M.F. PRODUCE IN THEM WHICH CAUSES A CURRENT TO FLOW THROUGH THE EXTERNAL CIRCUITE AND MAGNITUDE OF THIS E.M.F. IS DEPEND UPON THE POSITION OF ARMATURE COIL 12 IN RELATION TO THE MAGNETIC FI ELD OF MAGNET 10 AND MAGNET 11.

END OF THE ARMATURE COIL 12 CONNECTED TO THIS SLIP RINGS 23 AND SUP RING 24 WHICH ARE ROTATE WITH THE ARMATURE 12. THE BRUSH 25 PRESSED AGAINST TH E SLIP RI NG 23 AND BRUSH 26 PRESSED AGAINST THE SLIP RING 24. THE CURRENT GENERATED BY ARMATURE 12 FLOW TOWARD SUP RING 23 AND SLIP RING 24 AND AGAIN THIS CURRENT COLLECT BY BRUSH 25 AND BRUSH 26.

THE BRUSH 25 AND BRUSH 26 ALREADY CONNECTED TO UNIT 88 THIS ALTERNATING CURRENT CONVERT INTO DIRECT CURRENT BY THE UNIT 88 . THIS UNIT 88 ALREADY CONNECTED TO THE BATTERY 14 AND BATTERY 14 IS CONNECTED TO THE ELECTROLYTE UNIT 18 SO RESULT IN BATTERY 14 GET CHARGED .

REFERRING TO FIGURE 2 TO FIGURE 6 CAN BE SEEN THAT THE ALTERNATOR 6 DRIVE OR RUN BY THE POWER OF EXHAUST GASES 20 OF I NTERNAL COMBUSTION ENGINE 113 BUT NOT DRIVE ON POWER OF INTERNAL COMBUSTION ENGINE 113 ; SO RESULT IN INTERNAL COMBUSTION ENGINE 113 FREE FROM ALTERNATOR 6 LOAD ; SO I GAVE NAME TO THIS PROCESS OF GENERATION OF THE ELECTRICITY IS " TURBO ELECTRICITY ".

HERE IS END OF THE WORKING OF ALTERNATOR 6 ACCORDING TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION

REFERRING TO FIGURE 15 AND FIGURE 16 CAN BE SEEN THAT THE UNIT 88 CONNECTED TO THE ELECTOROLYTE UNIT 18 SO RESULT IN START THE PROCESS OF ELECTROLYSIS.

REFERING TO FIGURE 15 AND FIGURE 16 CAN BE SEEN THAT THE EQUATIONS OF ELECTROLYSIS PROCESS OF ELECTROLYSIS UNIT 18 AND IN THIS ELECTROLYSIS PROCESS THE "H" LETTER INDICATE THE HYDROGEN GAS AND "0" LETTER INDICATE THE OXYGEN GAS .

REFERING TO FIGURE 15 AND FIGURE 16 CAN BE SEEN THAT THE DETAIL DESCRIPTION AND WORKING OF EQUATIONS OF ELECTROLYSIS PROCESS OF ELECTROLYSIS UNIT 18 AS FOLLOW : -

IN PURE WATER AT THE NEGATIVELY CHARGED CATHODE 15 , A REDUCTION REACTION TAKES PLACE, WITH ELECTRONS (E^") FROM THE CATHODE 15 BEING GIVEN TO HYDROGEN CATIONS TO FORM HYDROGEN GAS H2 (THE HALF REACTION BALANCED WITH ACID):

REDUCTION AT CATHODE 15 : 2 H⁺(AQ) + 2E^~ -> H₂(G)

AT THE POSITIVELY CHARGED ANODE 16 , AN OXIDATION REACTION OCCURS, GENERATING OXYGEN GAS O2 AND GIVING ELECTRONS TO THE ANODE 16 TO COMPLETE THE CIRCUIT:

OXIDATION AT ANODE 16 : 2 H₂0(L) -> 0₂(G) + 4 H⁺(AQ) + 4E^~

THE SAME HALF REACTIONS CAN ALSO BE BALANCED WITH BASE AS LISTED BELOW. NOT ALL HALF REACTIONS MUST BE BALANCED WITH ACliD OR BASE. MANY DO, LIKE THE OXIDATION OR REDUCTION OF WATER LISTED HERE. TO ADD HALF REACTIONS THEY MUST BOTH BE BALANCED WITH EITHER ACID OR BASE.

CAlHi E 15 (REDUCTION): 2 H₂0(L) + 2E^~ -> H₂(G) + 2 OH (AQ) ANODE 16 (OXIDATION): 4 OH^" (AQ) -> 0₂(G) + 2 H₂0(L) + 4 E^" HALF REACTION PAIR YIELDS TH E SAME OVERALL WATER INTO OXYGEN GAS O2 AND HYDROGEN

OVERALL REACTION :- 2 H₂0(L) ^ 2 H₂(G) + 0₂(G)

THE NUMBER OF HYDROGEN GAS H2 MOLECULES PRODUCED IS THUS TWICE THE NUMBER OF OXYGEN GAS O2 MOLECULES. ASSUMING EQUAL TEMPERATU RE AND PRESSURE FOR BOTH GASES, THE PRODUCED HYDROGEN GAS H2 HAS THEREFORE TWICE TH E VOLUME OF THE! PRODUCED OXYGEN GAS O2 . TH E NUMBER OF ELECTRONS PUSHED THROUGH THE WATER IS TWICE THE NUMBER OF GENERATED HYDROGEN GAS H2 MOLECU LES AND FOUR TIMES THE NUMBER OF GENERATED OXYGEN GAS H2 MOLECULES .

THERMODYNAMICS OF TH E PROCESS OF ELECTROLYSIS UNIT 18 : -

DECOMPOSITION OF PURE WATER I NTO HYDROGEN GAS H2 AND OXYGEN GAS O2 AT STANDARD TEMPERATURE AND PRESSURE IS NOT FAVORABLE I N TH ERMODYNAMIC TERMS.

ANODE 16 (OXIDATION): 2 H₂0(L) 0₂(G) + 4 H⁺(AQ) + 4E^" EO OX = -1.23 V (EO

RED = 1.23 )^l5])

CATHODE 15 (REDUCTION): 2 H⁺(AQ) + 2E^~ -> H₂(G) EO RED = 0.00 V.

THUS, THE STANDARD POTENTIAL OF THE WATER ELECTROLYSIS CELL IS - 1.23 V AT 25 °C AT PH 0 (H⁺ = 1.0 M). AT 25 °C WITH PH 7 (H⁺ = l.OxlO^"7 M), TH E POTENTIAL IS UNCHANGED BASED ON THE NERNST EQUATION. HOWEVER, ELECTROLYSIS WILL NOT GENERALLY PROCEED AT THESE VOLTAGES, AS THE ELECTRICAL INPUT MUST PROVIDE TH E FULL AMOUNT OF ENTHALPY OF THE H₂-0₂ PRODUCTS (286 KJ PER MOL). THIS TAKES THE TH EORETICAL AND REAL OBSERVED THRESHOLD OF ELECTROLYSIS TO (-J1.48 V. THIS IS A STANDARD VALUE DERIVED FROM BASIC ENERGY CONSERVATION FOR H₂ WITH A KNOWN MOLAR ENTHALPY VALUE OF 286 KJ, (DIATOMIC H₂ HAVING 2 FARADAY UNITS OF CHARGE PER MOL), THEREFORE THE IDEAL VOLTAGE BECOMES 286,000/(2*96485) = 1.48 V.

THE NEGATIVE VOLTAGE INDICATES THE GIBBS FREE ENERGY FOR ELECTROLYSIS OF WATER 17 IS GREATER THAN ZERO FOR THESE REACTIONS. THIS CAN BE FOUND USING THE G = -NFE EQUATION FROM CHEMICAL KINETICS, WHERE N IS THE MOLES OF ELECTRONS AND F IS THE FARADAY CONSTANT. THE REACTION CANNOT OCCUR WITHOUT ADDING NECESSARY ENERGY, USUALLY SUPPLIED BY AN EXTERNAL ELECTRICAL POWER SOURCE OR BATTERY 14 .

REFERRING TO FIGURE 15 TO FIGURE 16 CAN SEE THAT THE ANY TYPE I NTERNAL COMBUSTION ENGINE 113 GET START THEN IT PRODUCE EXHAUST GASES 20 WHICH IS DRIVE THE ALTERNATOR 6 OR IT MEAN EXICUTE THE " TURBOELECTRICITY PROCESS " AND

ELECTROLYTE UNIT 18 START PRODUCE HYDROGEN GAS H2 AND OXYGEN GAS O2.

REFERRING TO FIGURE CAN SEE THAT THE FIGURE 14 TO FIGURE 16 SHOW THE PRINCIPLE OF ELECTROLYSIS UNIT 18 FOLLOW AS : -

REFERRING TO FIGU RE 15 TO FIGURE 16 CAN BE SEEN THAT THE AN ELECTRICAL POWER SOURCE BATTERY 14 IS CONNECTED TO TWO ELECTRODES , OR TWO PLATES (TYPICALLY MADE FROM SOME INERT METAL SUCH AS PLATINUM, STAINLESS STEEL OR IRIDIUM) WHICH ARE PLACED IN THE WATER.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE HYDROGEN GAS H2 WILL APPEAR AT THE CATHODE 15 (THE NEGATIVELY CHARGED ELECTRODE, WHERE ELECTRONS ENTER THE WATER), AND OXYGEN GAS O2 WILL APPEAR AT THE ANODE 16 (THE POSITIVELY CHARGED ELECTRODE).

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE ASSUMING IDEAL FARADAIC EFFICIENCY, THE AMOUNT OF HYDROGEN H2 leNERATED IS TWICE THE NUMBER OF MOLES OF OXYGEN GAS

O2 • m ISL AND BOTH ARE PROPORTIONAL TO THE TOTAL ELECTRICAL CHARGE CONDUCTED BY TH E SOLUTION 17 ; HOWEVER, IN MANY CELLS fOMPETING SIDE REACTIONS DOMINATE, RESULTING IN DIFFERENT PRODUCTS AND LESS THAN IDEAL FARADAIC EFFICIENCY. ONE WAY PRESSURE RELIEF VALVE 31 CONNECTED TO OUTLET OF OXYGEN GAS 02 AND ANOTHER ONE WAY PRESSURE RELIEF VALVE 32 CONNECTED TO OUTLET OF HYDROGEN GAS H2.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE ELECTROLYSIS OF PURE WATER REQUIRES EXCESS ENERGY IN THE FORM OF OVERPOTENTIAL TO OVERCOME VARIOUS ACTIVATION BARRIERS.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE WITHOUT THE EXCESS ENERGY THE ELECTROLYSIS OF PURE WATER OCCURS VERY SLOWLY OR NOT AT ALL.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE THIS IS IN PART DUE TO THE LIMITED SELF-IONIZATION OF WATER. PURE WATER HAS AN ELECTRICAL CONDUCTIVITY ABOUT ONE MILLIONTH THAT OF SEAWATER.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE MANY ELECTROLYTIC CELLS MAY ALSO LACK TH E REQUISITE ELECTROCATALYSTS. TH E EFFICIENCY OF ELECTROLYSIS IS INCREASED THROUGH THE ADDITION OF AN ELECTROLYTE (SUCH AS A SALT, AN ACID OR A BASE) AND THE USE OF ELECTROCATALYSTS.

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE ELECTROLYSIS 17 MADE UP BY COMBINATION OF THE PURE WATER AND SALT AND ELECTROLYSIS UNIT 18 CONTAIN WATER WITH SOLUBLE SALT 17 OR ELECTROLYSIS 17 , ANODE 16 , CATHODE 15 AN D HYDROGEN GAS H2 OUTLET 27 AND OXYGEN GAS O2 OUTLET 28 ANQ THIS BOTH OUTLET 27 AND OUTLET 28 OF HYDROGEN GAS H2 AND OXYGEN GAS O2 INSERTED INTO INTAKE MANI FOLD 2 OF INTERNAL COMBUSTION ENGINE 113.

REFHERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE TO AV0_}(,l| SUCTION OF ELECTROLYTE LIQUID INTO THE I NTAKE MANIFOLD PIFjfjJ OF ENGINE 113 THE ONE WAY PRESSURE RELI EF VALVE 32 OXYGEN GAS O2 AND ANOTHER ONE WAY

CONNECTED TO OUTLET OF HYDROGEN

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE AS CURRENT FLOW THROUGH ELECTROLYSIS UNIT 18 THEN HYDROGEN GAS H^;2 AND OXYGEN GAS O2 GET SEPARATE AND THIS HYDROGEN GAS H2 . AND OXYGEN GAS O2 GET SUCK INTO ANY TYPE OF INTERNAL COMBUSTION ENGINE 113 .

REFERRING TO FIGURE 15 TO FIGURE 16 CAN BE SEEN THAT THE ELECTROLYSIS UNIT 18 CONSUME POWER OF BATTERY 14 AND BATTERY 14 CHARGED ON POWER OF EXHAUST GASES 20 OF INTERNAL COMBUSTION ENGINE 113; SO INDIRECTLY ELECTROLYSIS UNIT 18 RUN ON POWER OF EXHAUST GASES 20 OF INTERNAL COMBUSTION ENGINE 113 ; SO THIS IS SECOND HOLE PROCESS OF PRODUCTION OF HYDROGEN GAS H2 AND OXYGEN GAS O2 IS CALLED AS " TURBO ELECTROLYSIS " PROCESS.

REFERRING TO FIGURE 16 CAN BE SEEN THAT TH E ; THE FIGURE 16 INDICATE HYBRIDE STAGE OF TURBOFAN ENGINE 113 AND IN HYBRIDE STAGE OF TURBOFAN ENGINE 113 HYDROGEN GAS H2 USE AS FUEL INSTEAD OF CONVENTIONAL PETROLIUM FUEL 136 SO RESULT IF CONVENTIONAL PETROLIUM FUEL 136 GET OVER OR WE CUT OFF SUPPLY OF CONVENTIONAL PETROLIUM FUEL 136 THEN ALSO TURBOFAN ENGINE 113 CONTINUOUSLY WORK BECAUSE OUTPUT OF TURBOELECTROLYSIS PROCESS HYDROGEN GAS H2 BURN WITH COMBINATION OF THE AIR 22 AND OXYGEN 02 OF ELECTROLYTE UNIT 18 .

REFERRING TO FIGURE 16 CAN BE SEEN THAT THE ; THE FIGURE 16 INDICATE THE FUEL INJETCOR 131 OF TURBOFAN ENGINE 113 STOP INJECTING THE CONVENTIONAL PETROLIUM FUEL 136 INTO COMBUSTION CHAMBER 135 OF TURBOFAN ENGINE 113 .

REFERRING TO FIGURE 16 CAN BE SEEN THAT THE ;IN THE FIGURE 16 WHEN HYBRIDE TURBOFAN ENGINE 113 GET START IT PRODUCE HOT EXHAUST GASES 20 AND WHEN TURBOFSN ENGINE .113 RUN ON HYBRIDE STAGE THEN TURBODFAN ENGINE 113 PRODUCE THE HOT EXHAUST GASES 20 INFROM OF NON TOXIC AND LESS HARMFUL HOT GASES WITH SOME WATER VAPOUR AND THIS HOT EXHAUST GASES 20 STRIKE ON TURBINE 7 AND; RUN ALTERNATOR 6 AND ALTERNATOR 6 PRODUCE ALTERNATING CURRENT WHICH CONVERT INTO DIRECT CURRENT BY UNIT 88 AND AGAIN EXICUTE TURBOELECTOLYSIS PROCESS AND AGAIN HYDROGEN GAS H2 AVAILABLE AS FUEL TO JET ENGINE 113.

REFERRING TO FIGURE 17 CAN BE SEEN THAT THE ; THE FIGURE 17 SHOW THE UNIT 33 AND UNIT 33 CONTAIN BATTERY 14 AND VOLTAGE REGULATOR 65 AND CAPACITOR FILTER 64.

REFERRING TO FIGURE 17 CAN BE SEEN THAT THE ; IN THE FIGURE 17 OUTPUT TERMINAL OF THE CAPACITOR FILTER 64 IS CONNECTED TO THE INPUT TERMINAL OF THE VOLTAGE REGULATOR 65 AND OUTPUT TERMINAL OF THE VOLTAGE REGULATOR 65 IS CONNECTED TO THE INPUT TERMINAL OF THE BATTERY 14.

REFERRING TO FIGURE 18 AND FIGURE 19 CAN BE SEEN THAT THE 3D VIEW OF DC TURBOELECTRICITY PRODUCE BY DC GENERATOR 72 BY USING POWER OF EXHAUST GASES 20 OF IC ENGINE 113.

REFERRING TO FIGURE 18 AND FIGURE 19 CAN BE SEEN THAT THE FIGURE 18 AND FIGURE 19 SHOW THE DETAILS PART OF THE DC GENERATOR 72.

REFERRING TO FIGURE 18 AND FIGURE 19 CAN BE SEEN THAT THE ELEMENTARY TWO POLES D.C. GENERATOR 72.

THE GENERAL PRINCIPLE OF ELECTRICAL GENERATOR AND THE WORKING OF AN ELEMENTARY ALTERNATOR 6 HAS ALREADY DISCUSSED IN FIGURE - 61 TO FIGURE - 69 ; SO CURRENT SUPPLIED BY SUCH ALTERNATOR IS NECESSARILY ALTERNATING. IF A DIRECT CURRENT OR UNIDIRECTIONAL CURRENT IS DESIRED , THEN THIS ALTERNATING CURRENT MUST BE RECTIFIED OR COMMUTATED AS IT ENTE THE EXTERNAL CIRCUITE OR BATTERY 14. THIS RECTIFICATION CANii¾E ACCOMPLISHED BY REPLACING THE SLIP RING SLIP RINGS 23 AND SLI P RING 24 OF THE ELEM ENTARY ALTERNATOR 6 IN FIGURE 18 TO. FIGURE 19 BY A SINGLE SPLIT RING M GENERALLY KNOWN AS A CO ivj MUTATOR 76. THIS RINGIS MADE BY CUTTI NG A CYLINDRICAL PI¾|j |jSOME CONDUCTING MATERIAL SUCH AS COPPER INTO TWO HALVES OR SEGMENT AND THESE SEGMENT ARE INSU LATED FROM ^;EACH OTHER BY A THIN SHEET OF MICA OR SOME OTHER INSULATING MATERIAL 85 .

REFERRI G TO FIGURE 18 AND FIGURE 19 CAN BE SEEN THAT TH E COIL AB OR ARMATUR COIL 75 IS PLACED INBETWEEN MAGNET 73 AND MAGNET 74. TURBINE 7 AND THE COIL AB OR ARMATURE 75 INSTALLED ON SHAFT 21 . END OF THE COIL AB OR ARMATURE 75 CONNECTED OR JOINED TO COMMUTATOR 76. BRUSH 77 AND BRUSH 78 CONNECTED TO THE COMMUTATOR 76.THE END OF THE BRUSH 77 AN D, BRUSH 78 IS CONNECTED TO TH E LOAD OF EXTERNAL CIRCUITE OR BATTERY 14. IF WE WANT DC TURBOELECTRICITY THEN AC TURBOELECTRICITY MUST BE RECTIFIED OR COMMUTATAED AS IT ENTERS THE EXTERNAL CIRCUITE AND THIS RECTIFICATION DONE BY SINGLE SPLIT RING M GENERALLY KNOW AS A COMMUTATOR 76.

REFERRING TO FIGURE 18 CAN BE SEEN THAT TH E CONDITION WHEN THE COIL AB OR ARMATURE 75 IS UNDERGOING THE FIRST HALF REVOLUTION AND IN THIS CASE THE CURRENT FLIOWS THROUGH THE LOAD RESISTER R FROM C TO D.

REFERRING TO FIGURE 19 CAN BE SEEN THAT THE CONDITION WH EN TH E COIL AB OR ARMATURE 75 IS U NDERGOING THE SECOND HALF REVOLUTION , THE DIRECTION OF CURRENT IN TH E COIL REVERSES AS ILLUSTRETED IN FIGURE 19 BUT AT SAME TIME THE POSITION OF THE SEGMENT 83 AND 84 ALSO REVERSE . THEREFORE THE CURRENT THROUGH THE LOAD RESISTER R AGAIN FLOWS FROM C TO D THUS EVEN THOUGH THE CURRENT INDUCED IN THE ARMATURE COIL AB OR ARMATUTRE 75 IS ALTERNATING DU E TO RECTIFYI NG ACTION OF COMMUTATOR THE DIRECTION OF THE CURRENT SUPPILED TO. TH E EXTERNAL CIRCUITE IS ALWAYS TH E SAME. IN THIS INVENTION CURRENT REPRESENTED BY LETTER I AND ANGLE OF ROTATION OF ARMATURE COIL 12 OR ARMATURE COIL 75 OR COIL AB REPRESENT BY Θ.

REFERRING TO FIGURE 20 CAN BE SEEN THAT THE ; THE FIGURE 20 SHOW THE CHARGING OF BATTERY 14 ON TURBOELECTRICITY OF SHOW DYNAMO 72 BY USING EXHAUST GASES 20 OF ENGINE 113.

REFERRING TO FIGURE 21 CAN BE SEEN THAT THE ; THE FIGURE 21 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING DYNAMO 72 WHICH IS RUN ON EXHAUST GASES 20 OF TURBOFAN JET ENGINE 113.

REFERRING TO FIGURE 22 CAN BE SEEN THAT THE ; THE FIGURE 22 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING ALTERNATOR 6 WHICH IS RU N ON EXHAUST GASES 20 OF TURBOPROP ENGINE 112.

REFERRING TO FIGURE 23 CAN BE SEEN THAT THE ; THE FIGURE 23 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING ALTERNATOR 6 WHICH IS RUN ON EXHAUST GASES 20 OF TURBOJET ENGINE 111.

REFERRING TO FIGURE 24 CAN BE SEEN THAT THE ; THE FIGU RE 24 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING ALTERNATOR 6 WHICH IS RUN ON EXHAUST GASES 20 OF INTERNAL COMBUSTION SINGLE FOUR STROKE

GASES 20 OF INTERNAL COMBUSTION SINGLE TWO STROKE COMPRESSION IGNITION ENGINE 170.

REFERRING TO FIGURE 27 CAN BE SEEN THAT THE ; THE FIGURE 27

SHOW THE TURBOELECTRICITY PROCESS AND TURBO ELECTRO LYSIS

PRC ss BY USING ALTERNATOR 6 WHICH IS RUN ON EXHAUST

GA¾E11O OF INTERNAL COMBUSTION SINGLE TWO STROKE SPARK

'j ¾&< i '

IGNITIO ENGINE 171.

REFERRING TO FIGURE 28 CAN BE SEEN THAT THE ; THE FIGURE 28 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING DYNAMO 72 WHICH IS RUN ON EXHAUST GASES 20 OF INTERNAL COMBUSTION SINGLE FOUR STROKE COMPRESSION IGNITION ENGINE 168.

RERERRING TO FIGURE 2 AND FIGURE 19 AND FIGURE 29 CAN BE SEEN THAT THE SHAFT 21 MADE UP OF NON CONDUCTIVE OR FULLY ELECTRICALY RESISTIVE MATERIAL TO AVOID CURRENT FLOW TOWARD TURBINE 7 FROM ARMATURE 12 OR ROTOR 47 OR COIL 75.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE ALTERNATOR 55 CONSISTS OF FOLLOWIN MAIN PART :-

STATOR - STATOR 34 CONSIST OF SOFT IRON CORE ON WHICH WINDING ARE WOUND . A POSITIVE DIODE RECTIFIER AND NEGATIVE DIODE RECTIFIER IS CONNECTED TO EACH OF ITS END TO CONVERT AC TO DC .

ROTOR - MAGNETISED ROTOR 47 TURNS INSIDE STATOR 34.THE MAIN PARTS OF TH ROTOR ARE ROTOR COIL, INTER LOCKING FINGERS FROM EACH END OF ROTOR 47 AND SLIP RING 45 AND SLIP RING 46.

RECTIFIER- RECTIFIER 13 CONVERT AC TO DC. BRUSH ES - BRUSH 56 AND BRUSH 57 USE TO MAKE THE CONTACT WITH SLIP RING 45 AND SLIP RING 46.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE IN CASE OF ALTERNATOR 55 , IN THIS INVENTION SHAFT 21 MADE UP OF NON CONDUCTIVE OR FULLY ELECTRICALY RESISTIVE MATERIAL TO AVOID CURRENT FLOW TOWARD TURBINE 7 FROM ROTOR 47 AND IN THIS INVENTION, IN CASE OF ALTERNATOR 55 THE TURBINE WHEEL 7 INSTALL ON SAME SHAFT 21 OF THE ROTOR 47 OF THE ALTERNATOR 55. j

REFERRING TO FIGU RE 29 CAN BE SEEN THAT TH E ROTOR 47 PLACED INSIDE THE STATOR 34.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE IN CASE OF ALTERNATOR 55 ; WHEN EXHAUST GASES 20 OF THE ALL TYPE INTERNAL COMBUSTION ENGINE 1 STRIKE ON TURBINE WHEEL 7 WITH KI NETIC ENERGY SO TURBINE WHEEL 7 GET ROTATE AND ROTOR 47 OF THE ALTERNATOR 55 ALSO GET ROTATE IN SAME DIRECTION OF THE TURBIN E WHEEL 7.

RERERRI NG TO FIGURE 29 CAN BE SEEN THAT THE IT SHOW DETAIL PART OF ALTERMNATOR 6 .

REFERRI NG TO FIGURE 29 CAN BE SEEN THAT THE WORKING OF ALTERNATOR 55 ACCORDING TO FARADAY'S LAW OF ELECTROMAGNETIC INDUCTION AS FOLLOW :-

REFERRING TO FIGU RE 29 CAN BE SEEN THAT THE IN CASE OF ALTENATOR 55 , ALTERNATOR 55 HAS STATIONARY SOFT IRON RING KNOWS AS STATOR 34 AND ARMATURE. ROTOR 47 IS MOUNTED ON BEARING INSIDE THE STATOR 34 DRIVEN BY BELT 69. ARMATURE CONTAINS ONE WINDING OF COIL HAVING ITS END CONNECTED TO SLIP RING 45' AND SLIP RING 46. CURRENT IS FED TO TH IS SLIP RING 45 AND SLIP RING 46 THROUGH STATIONARY CARBON BRUSH 56 AND BRUSH 57 RESPECTIVELY. THE STATIONARY CARBON BRUSHES ASSEMBLY 36 ATTACHED TO SLIP RING 45 AND SLIP RING 46. IN I HIS _; INVENTION ;SO WHEN IC ENGINE 113 GET START IT

PRODUCED THE EXHAUST GASES 20 STRIKE ON TURBINE WHEEL 7 AND ROTOR, 47 START ROTATE .

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE CURRENT IS FED TO SUP RING 56 AND SLIP RING 57 THROUGH STATIONARY CARBON BRUSH AND WHEN CURRENT FLOW THROUGH THE ARMATURE COIL

47 IT GET MAGNETIZED FORMING ONE NORTH POLE AND OTHER SOUTH POLE. ITS TURNING MAGNET GENERATES CURRENT IN

ALTERNATORS 55 STATIONARY WINDING ; AS THE ARMATURE OR ROTOR 47 ROTATES THE CURRENT PRODUCE IS ALTERNATING CURRENT.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE OUTPUT TERMINAL OF THE STATOR 34 CONNECTED TO THE UNIT 88.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE UNIT 88 CONVERT ALTERNATING CURRENT INTO DIRECT CURRENT AND BULB 29 GET SWITCH ON.

REFERRING TO FIGURE 29 CAN BE SEEN THAT THE ; THE FIGURE 29 SHOW THE TURBOELECTRICITY PROCESS AND TURBOELECTROLYSIS PROCESS BY USING ALTERNATOR 55 WHICH IS RUN ON EXHAUST GASES 20 OF INTERNAL COMBUSTION TURBOFAN JET ENGINE 113.

THE MAIN OBJECT OF MY INVENTION IS THAT BEST USE OF EXHAUST GASES POWER FOR GENERATING ELECTRICITY AND COMPLETE ELECTROLYSIS CHEMICAL PROCESS FOR PRODUCTION OF THE HYDROGEN GAS H2 AND OXYGEN GAS 02 AND CHARGING OF BATTERY 14 A!ND DRIVE OTHER ELECTRICAL ACCESSORIES OF VEHICLE AND

REDUCE INFRARED LOSSES AND VISIBILITY. BY USING MY INVENTION WE CAN 'PRODUCE MORE OXYGEN GAS O2 AND HYDROGEN GAS H2 GET

AVAII ABLE FOR ALL TYPE OF INTERNAL COMBUSTION ENGINE; SO WE IET VERY AND VERY BEST MILEAGE AND FUEL ECONOMY. SO RESI IN REDUCE TOXIC HARMFUL EXHAUST GASES PRODUCE BY

INC ilPLETE COMBUSTION OF PETROLEUM FUEL SUCH AS PETROL, DIESEL, KEROSENE. SO REDUCE INDIRECTLY POLLUTION AND GLOBAL WAjilNG.

ΤΗΐΙΚίΝ OBJECT OF MY INVENTION IS THAT ACHIEVE EASY STEP OF OBTAIN 'HYDROGEN GAS AND OXYGEN GAS BY SAFE METHOD WITH LOW COST.

THE MAIN OBJECT OF MY INVENTION IS THAT BEST USE OF POWER

^'■· ,: ^"-I ^■■ -

OF EXHAUST GASES 20 ALL TYPE OF INTERNAL COMBUSTION ENGINE FOR GENERATING ELECTRICITY AND COMPLETE ELECTROLYSIS CHEMICAL PROCESS FOR PRODUCTION OF THE HYDROGEN GAS H2 AND OXYGEN GAS O2 ELECTROLYSIS UNIT 18.

THE MAIN PROFIT OF MY INVENTION IS THAT ANY TYPE OF INTERNAL COMBUSTION ENGINE CONVERT INTO FUEL EFFICIENT HYBRID ENGINE. MY INVENTION GENERATE THE ELECTRICITY WHICH IS USE TO CHARGE THE BATTERY 14 AND FOR THE DRIVE THE ELECTROLYSIS UNIT 18 , STARTER ,BULB 29, AIR CONDITIONER , FM, FAN, INDICATOR , BREAK LIGHT, HEAD LIGHT OF VEHICLE.

THIS MY INVENTION GIVE STATEMENT THAT THE WE CAN PRODUCE ELECTRICITY AND CHARGE THE BATTERY 14, REDUCE OR HIDE INFRARED VISIBILITY AND LOSSES OF ALL TYPE INTERNAL COMBUSTION ENGINE AND ALL TYPE EXTERNAL COMBUSTION ENGINE AND DRIVE THE ELECTROLYSIS UNIT 18 BY USING THE EXHAUST GASES 20 OF ALL INTERNAL COMBUSTION ENGINE AND REDUCE POLLUTION AND GLOBAL WARMING .

ANOTHER PROFIT OF MY INVENTION IS THAT THERE IS NO ANY MECHANICAL POWER CONSUMPTION TO DRIVE THE ALTERNATOR 6 AND DYNAMO 72 AND ALTERNATOR 55 AND FOR PRODUCE ELECTRICITY AND FOR CHARGING BATTERY 14 AND FOR DRIVE THE ELECTROLYSIS UNIT 18 BECAUSE THEIR NO ANY ACTUAL MECHANICAL CONTACT IN BETWEEN ALTERNATOR 6 AND ALL TYPE OF INTERNAL COMBISION ENGINE ; SO RESULT IN REDUCE FRICTION AND BELT TENSION IN-BETWEEN PULLEY OF ALTERNATOR 6 AND PULLEY OF CRANKSHAFT OF ALL TYPE OF INTERNAL COMBUSTION ENGINE . NO NEED OF BELT , PULLEY TO DRIVE THE ALTERNATOR 6 VIA THROUGH BELT BY THE ALL TYPE OF INTERNAL COMBUSTION ENGINE ; SO REDUCE COST OF THE ALL TYPE OF INTERNAL COMBUSTION ENGINE .

Claims

I CLAIM ,

1. MY INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR GENERATE THE ELECTRICITY AND FOR EXECUTE THE ELECTROLYSIS PROCESS TO OBTAIN HYDROGEN GAS H2 AND OXYGEN GAS O2 BY USING POWER OF EXHAUST GASES 20 OF ANY TYPE OF INTERNAL

COM USTION ENGINE .

5. lylY INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR CONVERT ANY TYPE OF INTERNAL COMBUSTION ENGINE INTO FUEL EFFICIENT ECO FRIENDLY HYBRID ENGINE.

6. MY INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR

I

TO_j'jREDUCE TOTAL FRICTION AND BELT TENSION IN BETWEEN ANY TY$E OF, INTERNAL COMBUSTION ENGINE AND ALTERNATOR 6

ANjJ DYNAMO 72 AND ALTERNATOR 55; SO NEED OF BELT , PULLEY TO DRI E ALTERNATOR 6 AND TO DRIVE DYNAMO 72 AND TO DRIVE

ALTERNATOR 55.

7. MY l:liiVENTION"USES OF EXHAUST GASES OF JET ENGINE" USE IN AUTOMOBILE ENGINEERING , MECHANICAL ENGINEERING, POWER ENGINEERING ELECTRICAL ENGINEERING , HYBRID

ENGINEERING AND IN ELECTRICAL OR BATTERY POWERED VEHICLE.

8. ^: . MY INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR REDUCE, THE LOSSES OF EXHAUST GASES 20 OF ANY TYPE OF INTERNAL COMBUSTION ENGINE .

9. INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR REDUCE AIR , WATER , AND ALL TYPE ATMOSPHERIC POLLUTION PRODUCE DUE TO HARMFUL TOXIC GASES 20 OF INCOMPLETE COMBUSTION OF PETROLEUM FUEL SUCH LIKE AS PETROL DIESEL KEROSENE ETC SO THIS MY INVENTION HELP TO REDUCE GLOBAL WARMING.

lOL MY INVENTION "USES OF EXHAUST GASES OF JET ENGINE" USE FOR PRODUCE HYDROGEN GAS H2 AND OXYGEN GAS O2 WHICH IS USE IN ANY TYPE OF INTERNAL COMBUSTION ENGINE AS ECO FRIENDLY FUEL WITH AIR, SO THIS IS ALTERNATIVE OPTION OF FUEL INSTEAD OF PETROLEUM FUEL AND USE FOR REDUCE INFRARED VISIBILITY OF ENGINE .