BladesAre All Rotor Blades That Aims for Output 220 to 530 Times an ExistingGas Turbine
RotaryEngine That Aims for Electric Power Generation 224 to 536 Times an ExistingGas Turbine(1)
ReciprocatingEngine That Aims for Zero CO2 Emission, Power Output 124 to 136 Times anExisting Gasoline Engine, and Low Cost (1)
Fully AutomaticProcess with Monobloc Casting for Each Turbine Stage: Steam Turbine Whose
BladesAre All Rotor Blades That Aims for Output 220 to 530 Times an ExistingGas Turbine
RotaryEngine with Enormous Hope for the Future (1)
After receiving an e-mailmessage that suggested I should reduce emission of combustion gases tozero, all the methods I could think about required huge amount of water.One example is mixing combustion gases with water vapors more radicallythan cumulonimbus clouds to dissolve combustions gases into the water throughvaporization-condensation process. Luckily, however, it turned out my inventionproduces the maximum amount of water, which makes it most suitable forreducing emission of combustion gases to zero. Further carelessness ofmine was revealed as I found that in the steam condenser vacuum in thefinal stage the output increases significantly when the gravitational powerexceeds 10,000 times that of an existing steam turbine while driving attwice the recovered heat value of an existing boiler, but I had missedthis point in my calculation.
(Summaryof the Fundamental Researches)
To summarize my criticism of theexisting technology, none of the existing gas turbines or steam turbinesutilize heat effectively at all. The meaning of the words "adiabatic expansion"is to not utilize heat effectively. If heat is effectively used, the gasturbine exhaust-gas temperature approaches -273oC and a heat exchanger for exhaust heat recovery will be reversed to aheat exchanger for low temperature heat recovery. In a steam turbine thetemperature velocity containing an enormous amount of vaporization latentheat of superheated steam at a supercritical pressure is energy convertedto velocity power of a vast water mass at around 20oC which does not require cooling. In the steam condenser vacuum in thefinal stage the output increases significantly (thermal value of superheatedsteam output = (10,000 times the gravitational power of existing technology)/ α x (2 times the recovered thermal value) x (5 times the pressure difference)= output 220 to 530 times an existing gas turbine). The rise of the coolingsea water temperature diminishes to approximately 1/100.
Gas TurbineWhose Blades Are All Rotor Blades and Which Is Used for Low TemperatureHeat Recovery Driven by Very Low-Temperature Nitrogen Gas as a Medium ofVelocity and for Other Special Purposes As Well
(ATypical Error)
An article headlined "1,700oC Class Turbine Shows Prospect" was introduced in the April 18, 2001 issueof the Nikkan Kogyo Shimbun news paper which described technology intendedto improve jet engine performances by raising the temperature of combustiongases at the turbine entrance. A typical example of an error is found here.If you try to expand the volume and the speed of combustion gases for improvementand increase of thermal efficiency and specific output by raising the temperatureof combustion gases at the turbine inlet, since temperature and volumeof combustion gases are bad design issues, it will require turbines towithstand higher critical temperature and an increase of volume will callfor an increase of rotor blade area to correspond to a decrease of unitgravitational power, which, if not compensated, will cause a deficiencyin the cross-sectional area of flow path to be balanced by an increaseof velocity. In other words, an increase of speed without an increase ofpressure difference results in an increase of loss, which by typical deceptionis said to be a gain. A rise and increase in thermal efficiency and specificoutput as well come from an increase of specific mass of combustion gases.
(ATypical Improvement)
By reversing the typical errorabove, if the combustion chamber which doubles as a heat exchanger limitlesslyexchanges heat of combustion to bring the temperature of combustion gasesat the entrance to the lowest level, the gas turbine exhaust-gas temperatureapproaches -273oC. The problems of temperature and volume of combustion gases are minimized,the compression pressure can be increased more than twofold to above 10MPa without a limit, and the fuel combustion mass can be increased fourfoldto the theoretical air fuel ratio, therefore (air compressed to the samevolume for ((doubled pressure difference) x (quadrupled fuel mass) = (morethan octupled output at zero consumption of fuel thermal value) can begained. Thermal value of combustion gases obtained through heat exchangeproduces superheated steam at a supercritical pressure having approximatelytwice the recovered heat value of an existing boiler including all thethermal value with reference to -273oC contained in the compressed air, which results in ((thermal output valueof superheated steam 200 to 500 times an existing gas turbine) + (20- to30-fold mass output of superheated steam)) = (thermal output value of combustiongases 220 to 530 times an existing gas turbine).
(ExistingGas Turbines Do Not Use Heat at All)
Now the combustion chamber whichdoubles as a heat exchanger for a gas turbine whose blades are all rotorblades, illustrated in FIG 40, limitlessly exchanges heat of combustionto bring the temperature of combustion gases at the entrance to the lowestlevel and cause it to approach -273oC. The lowest temperature combustion gases produced by heat exchange havethe lowest barriers of temperature and volume, and the compression pressurecan be raised 2 to 3 times the existing technology to more than 10 to 15MPa, and the fuel combustion mass can be increased 4 times to the theoreticalair fuel ratio, realizing an increase of the output to (2 times the pressuredifference x 4 times the fuel mass) = 8 times that of an existing gas turbineof the same compressed air volume. The low temperature heat of the entirecombustion gases is recovered as, for example, very low-temperature nitrogengas and can be used effectively to, for instance, cool an entire urbanarea. The thermal value of combustion gases gained by heat exchange is(the total thermal value of the compressed air above -273oC + the total heat output of fuel) = approximately 2 times the recoveredheat value of an existing boiler. By use of a heated, high-temperatureturbine whose blades are all rotor blades, the mechanical efficiency israised 2 to 3 times, and the mass output of combustion gases by a gas turbinehaving all blades as rotor blades at zero consumption of fuel thermal valuefor the same fuel volume is (2 times the pressure difference x 2 to 3 timesthe mechanical efficiency) = 4 to 6 times the output of an existing gasturbine.
Steam TurbineWhose Blades Are All Rotor Blades That Aims for Output 220 to 530 Timesan Existing Gas Turbine Using the Same Fuel Volume
(ExistingSteam Turbines Make No Use of Heat As Well)
Now, thermal value gained throughheat exchange amounting to approximately 2 times that of an existing boileris supplied as superheated steam at a supercritical pressure into the uppermoststream of a steam turbine whose blades are all rotor blades, as shown inFIG 43, and, throughout the process of output generation, by cooling waterjet superheated steam which has a temperature around 20oC that does not require to be cooled, temperature velocity of superheatedsteam containing an enormous amount of vaporization latent heat is energyconverted to water mass velocity power which is more than 10,000 timesthe gravitational power in the final stage vacuum of the existing technology.This produces (5 times the pressure difference x 2 times the thermal valuex 10,000 times the power) / α = (200 to 500 times the thermal output valueof superheated steam). The heated, high-temperature turbine having allblades as rotor blades raises the mechanical efficiency 2 to 3 times andbrings about (5 times the pressure difference x 2 times the steam massx 2 to 3 times the mechanical efficiency) = (20 to 30 times the mass outputvalue of superheated steam) and (200 to 500 times the thermal output valueof superheated steam + 20 to 30 the mass output value of superheated steam)= (220 to 530 times the thermal output value of combustion gases of anexisting gas turbine).
(RotaryEngine with Zero Emission of Combustion Gases Such as CO2)
Combining a steam turbine whoseblades are all rotor blades that aims for water mass velocity power 500times an existing gas turbine using the same fuel volume and a gas turbinewhose blades are all rotor blades that is driven by very low-temperaturecombustion gases into a steam gas turbine whose blades are all rotor blades,as shown in FIG 41, that makes combustion gases dissolve into water with500-fold mass for discharge. However, since reducing the emission of combustiongases such as CO2 is a loss, a steam turbine having all blades as rotorblades is jointly used with the steam gas turbine. Thermal value gainedthrough heat exchange amounting to approximately 2 times that of an existingboiler is supplied as superheated steam at a supercritical pressure, atan optimal volume rate, into the uppermost stream of a steam turbine havingall blades as rotor blades and, throughout the process of output generation,by cooling water jet superheated steam which has a low temperature thatdoes not require to be cooled, gravitational power in the final stage vacuumas well as temperature velocity of superheated steam containing an enormousamount of vaporization latent heat is energy converted to water mass velocitypower which is more than 10,000 times the existing technology.
In a vigorous agitation-vaporization-condensationprocess where the lowest temperature combustion gases resulted from heatexchange in output generation are supplied into an optimal intermediatestage according to the pressure, by condensing an optimal amount of waterwith particles of very low-temperature combustion gases as the cores andby lowering the temperature to minimum level to cause separation in theform of hails, the low temperature heat recovery value is maximized andheat exchange expansion is caused even in the steam condenser vacuum wherethere is zero emission of combustion gases so that the steam gas turbinehaving all blades as rotor blades produces 224 to 536 times output of anexisting gas turbine. Further, in order to leave the finite fuel resourcesto our descendants, low cost pulverized coal fuel will be used for fuelspecific burning to generate electricity where gravitational power of coalis added to double the mass output of combustion gases for 8- to 12-foldgeneration of electric power, which can be further improved to gain 228-to 542-fold generation of electric power, to recover a vast amount of lowtemperature heat value, and to emit zero combustion gases including CO2.
RotaryEngine Aircraft That Aims for Zero CO2 Emission, 124- to 136-Fold Output,Supersonic Speed, and Very Little Exhaust Gas and Sound
RotaryEngine Airplane That Aims for Zero CO2 Emission, 124- to 136-Fold Output,and Instantaneous Acceleration to a Supersonic Speed Over Mach 10
(FullyAutomatic Process with Monobloc Casting for Each Turbine Stage Is Preferred)
For example, in a steam gas turbineas shown in FIG. 41 whose blades are all rotor blades, by using water jetto cool superheated steam, temperature velocity of superheated steam containingan enormous amount of vaporization latent heat is energy converted to watermass velocity power which is more than 10,000 times the gravitational powerin the final stage vacuum of the existing technology. A small part or largepart of the rotor blade area can be reduced to 1/10,000 in the final stageand to 1/1,700 in the atmospheric pressure section to provide for rationaldesign of the rotor blade area. Also by making all the blades movable,therefore the blade profiles those of rotor blades, and compressing theair in a wavy pattern with linear sections, the most efficient air compressioncan be achieved and at the same time annular monobloc casting and fullyautomatic process of compressor blades (wheel) at each stage is possible.In the same manner, i.e. by jetting out superheated steam or combustiongases in a wavy pattern with linear sections, evaporation membranes canbe created among the blades of the heated, high-temperature turbine forthe most efficient output. At the same time, in performing annular monobloccasting of turbine blades in each stage, realization of casting by a high-temperatureheating method and a water jet cooling method, facilitated by thermal insulation,and execution of fully automatic process reduce manufacturing cost to 1/10,as low as the limit, and help accelerate prevention of global warming.
(100Times Larger Output Than the Existing Technology Brings Height of Prosperityto Air Transportation and Movement)
For example, a bypass air blastpropulsion steam turbine as shown in FIG. 44 whose blades are all rotorblades, by completely using the given heat, (water mass output with 1,700times more atmospheric pressure gravitational power) /α x (2 times morerecovered thermal value) x (5 times more pressure difference) = (thermaloutput value of superheated steam 100 times the output of an existing gasturbine) is obtained, which can be combined with (mass output value ofsuperheated steam 20 to 30 times the output of an existing gas turbine)for a total output 120 to 130 times more than an existing gas turbine.A significant increase of the output reduces the fuel combustion mass to1/100 and help achieve a safety level of zero fire hazard easily. For instance,in the case of a space shuttle mother ship that accelerates instantaneouslyto a supersonic speed over Mach 10, a part of the superheated steam issupplied to the uppermost stream of the steam turbine having all bladesas rotor blades which provides a constant blast propulsion force. Bypassair blasting devices, each of which has a simple structure and utilizesthe principle of spray, further increase the efficiency of blast propulsion.Mass output of combustion gases at the lowest temperature is used as aconstant blast propulsion force to provide (power 124 to 136 times an existinggas turbine). The superheated steam is used as appropriate or stored formultiplication and, when necessary, a vast volume of the steam is instantaneouslyblasted to reach a supersonic speed over Mach 10 in an instant. This methodallows an easy launch of a satellite using a solid propellant rocket spendingzero expendable parts.
RotaryEngine Aircraft That Aims for Zero CO2 Emission, 124- to 136-Fold Output,Supersonic Speed, and Very Little Exhaust Gas and Sound
For example, a bypass air blastpropulsion steam turbine as shown in FIG. 44 whose blades are all rotorblades can be used as a constant blast propulsion force in, for instance,a supersonic jet airliner, a supersonic passenger vessel, a vertical take-offand landing passenger airplane, or an atomic passenger airplane which usessurfaces of sea water or roofs of buildings as airports and brings heightof prosperity to air transportation and movement. Bypass air blasting devices,each of which has a simple structure and utilizes the principle of spray,further increase the efficiency of blast propulsion. The total of combustiongases bypass blast at the lowest temperature is used as a constant blastpropulsion force and the remainder of superheated steam bypass blast isused as appropriate or stored mainly for hazards or crises under the conceptof "safety first." Using all of the existing airports and surfaces of seaas departure and arrival points for long distance transport vessels andsupplementing it with roofs of buildings as airports as well help reducefuel efficiency to around 1/100, which brings height of prosperity to supersonicflights, air transportation and movement. Blasting very low-temperaturecombustion gases for propulsion provides a safety level of zero fire hazardand reduce noise level to as little as 1/10.
(100Times Larger Output Than the Existing Technology Brings Height of Prosperityto Super High-Speed Water Transportation)
For example, a bypass water blastpropulsion steam turbine as shown in FIG 45 whose blades are all rotorblades can be used in, for instance, various kinds of super high-speedpassenger vessels and various kinds of super high-speed freight vesselsthat depart from and arrive at harbors and bring height of prosperity tomaritime transportation and movement. A steam turbine having all bladesas rotor blades is driven by a part of superheated steam as a constantblast propulsion force where air is taken in and steam that includes watermass is ejected for lifting and propelling the vessel. Bypass water blastingdevices, each of which has a simple structure and utilizes the principleof spray, further increase the efficiency of blast propulsion and the remainderof bypass blast superheated steam is used as appropriate or stored foruse in emergency situations. The total of combustion gases at the lowesttemperature is used as a constant bypass blast propulsion. In the processof blast propulsion in which water is taken in from the front, the combustiongases are transferred to heat exchange expansion very low-temperature combustiongases. In the process where sea water is drawn in and cooled and then ejectedfor propulsion and finally supplied toward the seabed, substances necessaryfor marine lives are drawn in and ejected to help fish, shellfish, andmicroorganisms to breed and grow in numbers, which is how the suggestedtechnology can help increase food production.
RotaryEngine Automobile That Aims for Zero CO2 Emission and 124- to 136-FoldOutput
(RotaryEngine Automobile That Provides Zero Emission of CO2 and Other CombustionGases While Operating at 100 Times More Output Than the Existing Technology)
If used in transportation vehiclessuch as large, medium, and small size automobiles whose total individualoutput is used in a form of rotating power, by completely using the givenheat output is extraordinarily increased and noise level becomes exceptionallylow. A steam gas turbine (SGT) whose blades are all rotor blades (FIG 31)(FIG41) = (steam gas turbine whose blades are all rotor blades to output 124to 136 times an existing gas turbine) can be achieved. Therefore, a totalthermal value of combustion gases is supplied to the uppermost stream ofa steam gas turbine (STG) having all blades as rotor blades as superheatedsteam with about 2 times the recovered heat value of an existing boilerand mass of combustion gases at the lowest temperature is supplied to anoptimal stage in the intermediate steam according to the pressure. By coolingwater jet superheated steam which has a temperature around 20oC that does not require to be cooled, temperature velocity of superheatedsteam containing an enormous amount of vaporization latent heat is energyconverted to water mass velocity power which is 1,700 times the gravitationalpower in the final stage atmosphere section of the existing technology.This produces (pressure difference 5 times an existing gas turbine x 2times the thermal value x 1,700 times the power) / α = (100 times thethermal output value of superheated steam). The heated, high-temperatureturbine having all blades as rotor blades raises the mechanical efficiency2 to 3 times and brings about (5 times the pressure difference x 2 timesthe steam mass x 2 to 3 times the mechanical efficiency) = (20 to 30 timesthe mass output value of superheated steam) and (100 times the thermaloutput value of superheated steam + 20 to 30 the mass output value of superheatedsteam) = (120 to 130 times the thermal output value of combustion gasesof an existing gas turbine). In the latter stage of output generation,by condensing water with particles of very low-temperature combustion gasesas the cores to cause separation in the form of hails, combustion gasesare dissolved into relatively large amount of water with 100 times themass of combustion gases for discharge. Thus, emission of CO2 and othercombustions gases can be reduced to zero or very little even for smallsize cars to prevent global warming.
(Absurdityof the Current Rotary Engine Technology Gives a Premonition for SomethingExtraordinary)
Since export of the existing seedsof profit continued while hollowing out of industry was spoken loudly of,the process of decline in seeds of profit and the money-scattering politicsled to the increase of Japanese government bonds by 200 trillion yen withinless than 10 years. The failure of economic policy unprecedented in theworld history brought down the asset value below 1 quadrillion yen, whichis still decreasing. In the situation where seeds for profit have beenlost, only around 10 years remain until the day to lose foreign currencies.The debts by regional governments and businesses continue to grow, andplunges of the stock market, the yen, and the Japanese bonds are approaching.Now new seeds for profit are required to replace the old seeds for profit.In case Japan goes bankrupt, it will no longer be able to import food andsuffer from starvation and hyperinflation of an unprecedented scale inhuman history. Businesses will no longer function. Companies like Toyotaand Honda are wasting no time to prepare for escape from Japan expandingtheir overseas manufacturing bases. Technologies of Toyota and Honda nolonger have any significant advantages over the competitors and cannoteven survive in Japan, not to mention save it from bankruptcy. In orderfor Japan to avoid bankruptcy, we need new seeds of profit that by farexcel Toyota and Honda. For this reason, I have made Japanese patent applicationsfor over 7,000 claims that can pull the country out of the situation andam waiting for national level cooperation.
ReciprocatingEngine That Aims for Zero CO2 Emission, Power Output 124 to 136 Times anExisting Gasoline Engine, and Low Cost (1)
The first collaborator in Japanis a professor of the engineering department of a university and becausehe is a thermodynamics believer, he says he cannot comprehend my inventionsin any other forms than experimental results. However, he thinks my inventionsare interesting and has been researching and developing an energy conservationcycle engine that seems to be most suitable for automotive applications,spending the money out of his own pocket since July, 2000. As an inventorof the 21st century, I need to keep monopolizing inventions that hold overwhelmingadvantages against others so that my collaborators can receive the highestcompensations. Thus, as they have to be priority claim inventions, I amplanning to further expand the current inventions of 7,354 claims infinitely,even though some of them may overlap with one another. My plan is to avoidthe hyperinflation unprecedented in human history by securing a profitratio to suit the world's highest cost of labor. Offers to support thefees for world-wide patent application activities are appreciated.
FIG 1:Different Types of Engines and Their Thermal Efficiencies
(Description1) With regard to reciprocating engines, a laboratory of a universitywhich has published many papers concerning researches on combustion inclosed containers has volunteered to experiment my energy conservationcycle for verification. While approaching complete combustion in a closedcontainer at a theoretical air fuel ratio, if the maximum pressure of combustionis brought near to 8 times the compression pressure without combustion,I define the process as cooling and combustion within a reduced diametermain combustion chamber doubling as a heat exchanger. In order to maximizethe (superheated steam pressure difference x mass), exhaust-gas temperatureis minimized by an exhaust heat recovery heat exchanger. The recoveredheat capacity is supplied to the reduced diameter main combustion chamber-heatexchanger to realize an energy conservation cycle engine having a thermalefficiency of approximately 70%.
Summary:{In none of school textbooks or merchandised books on reciprocating engines,there is no mention about the loss equivalent to the non-rotational releasethermal energy loss of about 40% or the kinetic energy reduction loss ofabout 30% on which I spent half a century to research. However, concerningthe kinetic energy reduction loss of approximately 30%, Dr. Felix Wankelsuggested that by bringing the loss down to near 0% the thermal efficiencycan be doubled. This suggestion was agreed by and receiving cooperationfrom many large companies in the world. Almost all Japanese auto-makersplus some other companies have been involved in the development of therotary engines based on the suggestion. They do know very well about this,better than an amateur like myself.}
Summary:{Concerning the non-rotational release thermal energy loss of about 40%,one of merchandised books on reciprocating engines contains a graph asshown in FIG 1 that indicates different types of engines and their thermalefficiencies. This is an indication that they know about this kind of lossbetter than I do, but there is no explanation about the loss equivalentto the non-rotational release thermal energy loss. A small size gasolineengine (GS) which takes the maximum value of thermal energy release rationear the top dead point and has a non-rotational release thermal energyloss of about 50% shows the worst thermal efficiency of 15% or so. However,a large size vessel diesel engine which takes the minimum thermal energyrelease ratio near the top dead point, by delaying the combustion and increasingthe ratio between piston stroke and its external diameter by 4 times torealize a super-long stroke, and has a reduced non-rotational release thermalenergy loss of about 20% shows a very good thermal efficiency of 55%.}
Whatsuccessful industrialists fear the most is loosing large amounts of businessto brilliant follow-on patents, so they would strictly prohibit providingany explanation that may aid such follow-on patents. Instead, they brainwashedscientists and engineers with thermodynamics, and consequently their mindsdo not function any more.
Summary:{I thing in applications like automobiles which require small size, lightweight, and large output engines, delaying combustion timing causes unburneddiesel particles due to insufficient combustion time, which are sourcesof environmental pollution. In other words, delaying combustion timingmeans intentionally polluting the environment. I think they are takingadvantage, with a false intention, of the theories of thermodynamics thathave nothing to do with the existing reciprocating engines and using athermal efficiency calculation method that is considered under a semi-staticchange condition with no loss in the constant-volume combustion cycle toemphasize that what is presented is the optimal configuration or construction,thereby terminate scientists thinking on the global level and prevent newcomers in the market.}
Summary:{To be more specific, FIG 1 "Different Types of Engines and Their ThermalEfficiencies" shows very precise thermal efficiency of each type of existingreciprocating engines. Therefore, to obtain a high performance reciprocatingengine, calculation of thermal efficiency must naturally be done with existingreciprocating engines. In other words, in order to design and invent ahigh performance reciprocating engine, a thermal efficiency calculationmethod for existing reciprocating engines is essential. However, the emergenceof a high performance reciprocating engine will pose threat to the vestedinterests and provides great opportunity for newcomers.}
Summary:{Most of the textbooks and other books make thermal efficiency calculationvery difficult to understand by adopting a thermodynamic thermal efficiencycalculation method that is fantasized under a semi-static change conditionwith no loss such as a constant-volume combustion cycle. This method hasnothing to do with the existing reciprocating engines (FIG 33). In a semi-staticchange condition with no loss, thermal energy is lost by the amount itworked toward outside and the thermal efficiency is 100%. However, thiswould be very difficult to comprehend if expressed in a diagram, whichprobably facilitated the brainwash, and a diagram of constant-volume combustioncycle suggests something of that sort. Therefore, "in the constant-volumecombustion cycle, when the total thermal energy of the fuel is releasedat the top dead point, the thermal efficiency takes the maximum value,"which is quite the opposite of the thermal efficiency of the existing reciprocatingengine mentioned above. It is natural for companies to try to block newentries in the business.}
(Description2) The biggest lessen came from Wankel's rotary engine. Dr.Wankel thought and proposed that the thermal efficiency can be increasedby 2 times and both the specific volume and the specific weight can bereduced by 1/2 by lowering the kinetic energy reduction loss of about 30%to near 0% in a 4 cycle gasoline engine. This suggestion is agreed by andreceiving cooperation from many major companies in the world. They succeededto reduce the kinetic energy reduction loss to around 5% and lower boththe specific volume and the specific weight to almost 1/2. However, asthe thermal efficiency decreased instead of increasing, the attempt wasa failure. This means that however large power may be released for howeverlong time at the dead point, no rotating power is generated because thenon-rotational release thermal energy loss is 100%. In other words, inthis rotary engine, the non-rotational release thermal energy loss actssimultaneously on the dead point of the rotor and the dead point of thecrank. Thus, the ratio of the thermal energy that is released at the deadpoint increases and the non-rotational release thermal energy loss roseto 65% to 70%, which made further research and development very difficult.So, it was found that reduction of the non-rotational release thermal energyloss was the most important issue as well as reduction of the kinetic energyreduction loss, leaving the attempt as a failure just like many other examplesof failures.
EnergyConservation Cycle Engine Which Will be Used in a Medium Size High SpeedVessel That Aims for Zero CO2 Emission, Power Output 124 to 136 Times anExisting Gasoline Engine, and Low Cost
EnergyConservation Cycle Engine Which Will be Used in Different Types of VesselsThat Aims for Zero CO2 Emission, Power Output 24 to 36 Times an ExistingGasoline Engine, and Low Cost
EnergyConservation Cycle Engine Which Will be Used in Different Types of AutomobilesThat Aims for Zero CO2 Emission, Power Output 24 to 36 Times an ExistingGasoline Engine, and Low Cost
EnergyConservation Cycle Engine Which Will be Used in Different Types of PowerEquipment and Machines That Aims for Zero CO2 Emission, Power Output 24to 36 Times an Existing Gasoline Engine, and Low Cost
(Description3) Concerning reduction of the non-rotational release thermalenergy loss, it was successfully reduced to as low as about 20% by delayingthe combustion timing in a diesel engine. However, because pollution isworsened by increase of exhaust particles including soot due to insufficientburning time when combustion is delayed, it is inevitable that the ratiobetween piston stroke and its external diameter is increased by 4 timesto effect a super-long stroke. This is not normally usable in applicationssuch as automobiles which require light weight and large output engines.An energy conservation cycle is such an engine that reduces the non-rotationalrelease thermal energy loss near to 0% without delaying the combustiontiming but by delaying the timing of thermal energy release only. It isdreadful that all of it is hidden under the cover of thermodynamics ofconstant-volume combustion cycle in textbooks and other well known books.
(Description4) In (FIG 25), an energy conservation cycle is introduced inorder to bring down the non-rotational release thermal energy loss nearto 0%. The kinetic energy reduction loss is lowered near to 0% by adoptingperfect elastic collision reciprocating motion. In an energy conservationcycle engine, considering isolated combustion as shown in the area of the(right dead point colored in red) within a reduced diameter main combustionchamber-heat exchanger 2 which has a diameter reduced to, for example,1/5 of the expanded diameter piston (green), if isolation is broken atabout 70oto 80o followingthe right dead point, the thermal energy release value and the non-rotationalrelease thermal energy loss in the vicinity of the dead point will be loweredto 1/25. The total combustion time of the existing technology + α correspondsto the constant-volume combustion multiplied by 25 (the maximum pressureof combustion is brought near to 8 times the compression pressure withoutcombustion while approaching complete combustion in a closed containerat a theoretical air fuel ratio). The compression pressure without combustionof a gasoline engine (2 MPa) corresponds to the maximum pressure of combustionof a diesel engine (16 MPa).
Long-time isolated combustion thatrequires jetting a vast amount of high pressure, high temperature watercan raise the maximum pressure of combustion to 20 MPa by jetting superheatedsteam at a supercritical pressure. Release of almost all steam and combustiongases including exhaust heat value is completed instantaneously by dynamicpressure at the position 90ofollowing the dead point where friction loss is minimum so that the non-rotationalrelease thermal energy loss is lowered near to 0% under the condition ofa large pressure difference, large mass, an large dynamic pressure. Thecrank shaft is directly driven with the piston by adopting an expandeddiameter piston (green color). Kinetic energy reduction loss is broughtdown near to 0% due to perfect elastic collision reciprocating motion whichis realized by 2 cycle explosion process at both the right dead point andthe left dead point.
Then,after receiving an e-mail message that suggested I should reduce emissionof combustion gases to zero, the output soared to 24 to 36 times the outputof an existing gasoline engine that uses the same amount of fuel at a volumeat which combustion gas emission can be reduced to zero.
(ReducingEmission of Combustion Gases to Zero) As a method to reduceemission of combustion gases to zero, I have adopted a method to dissolveall of combustion gases into a vast amount of water using chemical substances,which should result in a dissolved gas concentration exceeding acid rains.As shown in (FIG 25), an exhaust heat recovery heat exchanger 2a is providedto recover the exhaust heat value. Heat is recovered from exhaust-gas temperatureat about 500oC including the enormous amount of vaporization latent heat and the temperatureis lowered as much as possible to about 50oC. The recovered heat capacity is more than 400oC per cycle. Since recovered heat capacity of 400oC accumulates after each cycle if the same amount of fuel is combusted,it totals to 400oC x 100 cycles = 40000oC after 100 cycles. Thus, it can limitlessly grow.
Making use of the greatest advantagethat is isolated combustion within a reduced diameter main combustion chamber-heatexchanger 2 and setting the conditions to obtain the maximum pressure ofcombustion of a diesel engine (16 MPa) from the compression pressure withoutcombustion of a gasoline engine (2 MPa), if preparation for combustionis started from about 75obefore the dead point and continue burning until about 75oafter the dead point, a reduced diameter main combustion chamber with avolume larger than a certain level can have combustion which allows jettinga vast amount of water. Combustion with hot water jet using superheatedsteam at a supercritical pressure can increase the output to a maximumpressure of combustion higher than 20 MPa. Combustion with cold water jetcan expand the water mass to 1,700 times more atmospheric pressure gravitationalpower than steam. With water jet having a large pressure difference of20 MPa, 1,700 times more gravitational power, and large mass, the expandeddiameter piston (colored in green in FIG 25) is moved by hydrostatic driveand dynamic reaction. (20 MPa pressure difference x 1,700 timer more power/ α) = (100 times the output of an existing gasoline engine) is achievedin a large sized energy conservation cycle engine and (24 to 36 times morethan the ideal output) in a medium sized energy conservation cycle engine.
Because the process of isolatedcombustion within a reduced diameter main combustion chamber-heat exchanger2 involves agitation and combustion while jetting water with 100 timesmore mass than the high pressure high temperature combustion gases, combustiongases can be dissolved into water in ideal ambient air. Through the processwhere the expanded diameter piston (green color) is driven by dynamic reactionwhile jetting cold water with 100 times more mass than the combustion gasesby superheated steam with a pressure difference more than 20 MPa, the wateris vigorously vaporized and condensed by super high-speed agitation andcombustion and reacts with the remaining combustion gases thus an enormousamount of combustion gases is dissolved into water having 100 times moremass and drained. This makes possible zero emission of combustion gasesincluding CO2. Ventilation and drain are performed during the exhaust strokethrough the ventilation hole provided in the lower section. The remainingwater is drained as pressurized water through the safety valve during thesecond half of the compression stroke. A reduced diameter main combustionchamber energy conservation cycle engine having a volume larger than acertain level emits no combustion gases and one with a volume smaller thana certain level emits very little amount of combustion gases.
If an engine, integrated with asteam gas turbine having all blades as rotor blades, that lowers the combustiongases exhaust temperature near to -273oC and raises the recovered heat value to about 2 times more than an existingboiler is compared with a large size energy conservation cycle engine thatincreases recovered heat value by 400oC per rotation up to an astronomical value of recovered heat and increasessuperheated steam at a supercritical pressure so that the maximum pressureof combustion approaches limitlessly to a supercritical pressure, the energyconservation cycle engine has an overwhelming advantage. However, if anengine, integrated with a steam gas turbine having all blades as rotorblades, that produces output 120 to 530 times more than an existing gasturbine from thermal output value of combustion gases is compared to theenergy conservation cycle engine same as above, the engine integrated witha steam gas turbine having all blades as rotor blades has an overwhelmingadvantage. Therefore, it is very difficult to decide which of the two isbetter than the other. However, since a small size energy conservationcycle engine ends up being similar to an existing gasoline engine, advantagesare found with a medium size energy conservation cycle engine that has24 to 36 times more output than an existing gasoline engine using the samefuel volume.
Themost urgently required research for the sake of human beings is the areaof research that has been hidden by thermodynamics.
Let’seliminate profit-oriented applied researches. Help us in our efforts toreduce pollution and prevent global warming so that all human beings canlive together.
Invitingpeople who want to partner with us to invest money to reduce pollutionand prevent global warming.
A university professor has beenresearching and developing an energy conservation cycle engine, financingthe project out of his own pocket since July, 2000 and needs more fundfor his activities. What is anticipated to happen is great decompositionof methane hydrate, rapid rise of carbon dioxide density, and extinctionof human beings, therefore prevention of global warming driven by the marketmechanism is a common hope of all humans. To this end, I have looked tocompanies in different countries, asking for contributions for more than100 million yen necessary for fees to file PCT international applicationsoverseas. It s my hope to sell from lawn mowers to space shuttle motherships under Tanigawa LLC brand together with companies in the collaboratingcountries and contribute to prevention of global warming, while I concentrateon expanding inventions.
Our business model will be suchas the following; fully utilizing existing manufacturing facilities anddoor-to-door delivery services, it will include IT-based advertisements,sales and marketing, IT-based sales upon receipt of orders, IT-based outsourcing(for parts selection and production), IT-based outsourcing (for manufacturingand assembly), and IT-based outsourcing (for delivery). Once all proposalsare made through the Internet, positions will be filled, maybe by the first-come-first-servedbasis. They will be all entrepreneurs and work out of their homes. (Noquestions will be asked on nationality, occupation, age, or sex) Proposalsfor financial resources, parts designs, verification tests, and selectionof door-to-door delivery services are adopted and executed within the groupof research and development entrepreneurs. I will dominate with patentsso that collaborators can receive the highest remuneration.Let us monopolizethe sales of large, medium and small size power generating installationsin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small scale electricity, heat,and cold in the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size cars in the worldwith the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size ships in the worldwith the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size high-speed shipsin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size super high-speedships in the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size airplanes in theworld with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size supersonic airplanesin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size power equipmentin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size power vehiclesin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size outboard enginesin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size general purposeengines in the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size lawn mowers inthe world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size propeller airplanesin the world with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size satellites in theworld with the patents. (We invite partnering proposals.)
Letus monopolize the sales of large, medium and small size space shuttle motherships in the world with the patents. (We invite partnering proposals.)
The degree of contributionto humanity by energy conservation cycle engines is expected to be 1,000times more than Bill Gates. The professor of the engineering departmentof a university is expected to contribute to humanity more than Bill Gates,which will result in more remuneration than the one Bill Gates receives.I will do my best to dominate with my invention. The principle of the engineseach integrated with a steam gas turbine whose blades are all rotor bladesis the most sophisticated one and the degree of their contribution to humanityis also 1,000 times more than Bill Gates. We should elevate it to nationallevel collaboration on research and development so that we can put brakeon the ever-increasing unemployment rate and to regain world's number onecompetitive position.
詳細 For further details,please follow the link to: http://ww1.tiki.ne.jp/~tanigawa/
For questions and contacts,please call or send fax to Hiroyasu Tanigawa at 81-86-277-9417 (voice andfax).