State of the Art-Roman InFlow Tech: 1-Gearturbine RotaryTurbo, 2-Imploturbocompressor One CompressionStep

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State of the Art-Roman InFlow Tech: 1-Gearturbine RotaryTurbo, 2-Imploturbocompressor One CompressionStep




by retrodynamic » 09/12/16, 01:21

Novel Technologie State of the Art Novel InFlow Tech featured Development project 1Gearturbine 2Imploturbocompressor

* Wordpress Blog State of the Art Novel InFlow Gearturbine Imploturbocompressor


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* 1-GEARTURBINE BEHANCE Images Gallery Portafolio
1 Gearturbine Novel Rotary Turbo InFlow Project Gearturbine Tech Development Featured
Atypical Gearturbine Retrodynamic Dextrogiro VS Levogiro Effect Ying Yang Thrust Waste Loses State Way Type No Art Innovative Concept Top System Percent Most Effective
Its similar simple system of Heron Aeolipile Steam Turbine Alexandria Device 10 70 AD
Atypical YouTube New GEARTURBINE Retrodynamic DextroRPM VS LevoInFlow Ying Yang Thrust Way Way Waste Loses No
8XY thermodynamic cycle track steps
New FormFunction MOTOR Device Type
Retrodynamic RotorRPM VS InFlow Way Collision type of interaction
No pest loses for cooling of combustion lubrication systems
Mass form rotational movement continue dynamic inertia tendence positive motion like a freewheel
Opposite thrust force like Ying Yang Simbol
Pat 197187 IMPI MX Dic 1991

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* 2-IMPLOTURBOCOMPRESSOR BEHANCE Images Gallery Portafolio
2 Imploturbocompressor
A move Part Design Excellence System
InFlow's interaction comes from Macroflow and goes to MicroFlow by Implossion
One-stage Compressive Influx Compression and Output to a Single Circular Dynamic Movement New Concept
To see an animation Imploturbocompressor is posible on a simple way just to check a hurricane satellite view and is the same implo way of influx nature

tags; power, energy, technology, engineering, innovation,

: Arrow: :!: : Idea: : roll:

* Traduccion al Español: Estado del Arte - Novel InFlow Tech - Desarrollo de Proyectos Destacados; 1-Turbina de Engrane, 2-Imploturbocompressor:

1-Engrane Turbina; Sistema Turbo Rotativo, Tecnología de Flujo Termodinamico / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type - Non Waste Looses / Es similar en su simple función básica a la Turbina de Herón de Alexandria 10-70AD. / * 8-X / Y Etapas de Ciclo Termodinámico / Patente; Dic. 1991 IMPI México # 197187 / Con un muy elevado porcentaje de eficiencia.

2-Imploturbocompressor; a concepto perfecto esto debido a que el sistema Solamente consta de una sola peza en movimiento, excelencia de ingeniería mecánica aplicada. Consecuentemente Ademas solamente un paso para aplicar compression de flujo, compression y salida de flujo in a solo movimiento circular. El flujo goes from Macro-flujo hacia Micro-flujo, consuiguiendo una aceleración de flujo. Para ver una animación del sistema del Imploturbocompressor, es muy sencillo, solamente viendo la vista satelital de une huracán.

* English Translation: State of the Art - Novel InFlow Tech - Featured Project Development; 1-Gearturbine, 2-Imploturbocompressor:

*Introduction; State of the Art - Novel InFlow Tech - Featured Project Development; | / · 1; Rotary-Turbo-InFlow Tech / - GEARTURBINE PROJECT Have the similar basic system of the Aeolipilie Heron Steam Turbine device from Alexandria 10-70 AD * With Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Way Power Type - Non Waste Looses * 8X / Y Thermodynamic CYCLE Way Steps. 4 Turbos, Higher efficient percent. No blade erosion by sand & very low heat target signature Pat: 197187IMPI MX Dic1991 Atypical Motor Engine Type. | / · 2; Imploturbocompressor; One Moving Part System Excellence Design - The InFlow Interaction comes from Macro-Flow and goes to Micro-Flow by Implossion - Only One Compression Step; Inflow, Compression and outflow at one simple circular dynamic motion / New Concept. To see a Imploturbocompressor animation, is possible on a simple way, just to check an Hurricane Satellite view, and is the same implo inflow way nature.

* Abstract; * State of the Art - Novel InFlow Tech - Featured Project Development;
1-Gearturbine, 2-Imploturbocompressor

* 1-GEARTURBINE PROJECT
Rotary-Turbo-InFlow Tech
Atypical InFlow Thermodynamic
Technology Proposal Submission
Novel Fueled Motor Engine Type

State of the art Innovative concept Top system Higher efficient percent. * Power by bar, for Air-Planes, Sea-Boats, Land-Transport & Dynamic Power-Plant Generation.
-Have similar system of the Aeolipile Heron Steam device from Alexandria 10-70 AD. -New Form-Function Motor-Engine Device. Next Step, Epic Design Change, Broken-Seal Revelation. -Desirable Power-Plant Innovation.

-Youtube; * Atypical New • GEARTURBINE / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type - No Waste Looses

The present invention relates to a compression and pushing motor characterized in that it is composed of a housing, said housing accommodates a rotor rotating in its internal space supported by a pair of gears whose passage coincides with the inner surface of the rotor; A rotor (or core) that internally has flow ducts presented in reverse of another, balanced these, begin at the point where they end; It has several cavity points for reaction turbines, as well as two combustion chambers isolated by a system of nozzles and presented in the manner of poles, which are on opposite sides of one another, but with the same circular direction of the rotor when It rotates; The rotor also has several fluid conduits radially presented; A hollow power transmission rod arranged and traversing in the center of the rotor, which in its interior flows the lubricant and fuel with movement of the ends towards the center, at this point by means of the centrifugal force of the rotor parts of the rotor; In the bar of air intake, it is possible to use a rotary air compressor, which can be used in conjunction with an air compressor. activates the current necessary for combustion; A center of the nucleus in which the formation of the internal ducts of the rotor begins and ends (in and out); Said center of the core of a pair of semi-cylindrical cavities housing two pairs of turbochargers said core of the core is diagonally traversed by fluid ducts exiting from the bar to the combustion bed and lubrication points and by the centrifugal force of the rotation of the rotor sends the fluids to the required points to their radial direction; Exhaust blades are the exit point of the exhaust gases that leave the internal ducts of the rotor and contrareaccionan with the fixed blade in the last point of use of the propulsion of the motor; Two combustion chambers are contained in the rotor blade when they are joined together, and they are joined to the rotor blade by a common rotor blade. internal gear of the housing; A starter motor which means a gear engages the starter gear attached to the bar.

-This innovative concept consists of hull and core where are held all 8 Steps of the work-flow which make the concept functional. The core has several gears and turbines which are responsible for these 8 steps (5 of them are dedicated to the turbo stages). The first step is fuel compression, followed by 2 cold turbo levels. The fourth step is where the fuel starts burning - combustion stage, which creates thrust for the next, 5th step - thrust step, which provides power to the planetary gears and turbines and moves the system. This step is followed by two hot turbo steps and the circle is enclosed by the final 8th step - bigger turbine. All this motion in a retrodynamic circumstance effect, wich is plus higher RPM speed by self motion. The Reaction at front of the action.

8-X / Y Thermodynamic CYCLE - Way Steps:
1) 1-Compression / bigger
2) 2-Turbo 1 cold
3) 2-Turbo 2 cold
4) 2-Combustion - circular motion flames / opposites
5) 2-Thrust - single turbo & planetary gears / ying yang
6) 2-Turbo 2 hot
7) 2-Turbo 1 hot
8)1-Turbine / bigger

-With Retrodynamic Dextrogiro vs Levogiro Phenomenon Effect. / Rotor-RPM VS InFlow / front to front; "Collision-Interaction Type" - inflow vs blades-gear-move. Technical unique dynamic innovative motion mode. [Retrodynamic Reaction = When the inflow have more velocity the rotor have more RPM Acceleration, with high (XY Position) Momentum] Which the internal flow (and rotor) duplicate its speed, when activated being in a rotor (and inflow) with [inverse ] opposite Turns. The Reaction at front of the action. A very strong Novel torque power concept. -Non waste parasitic looses for; friction, cooling, lubrication & combustion.

-Shape-Mass + Rotary-Motion = Inertia-Dynamic / Form-Function Wide [Flat] Cylindrical shape + positive dynamic rotary mass = continuous Inertia positive tendency motion. Kinetic Rotating Mass. Tendency of matter to continue to move. Like a Free-Wheel.

-Combustion 2Two continuous circular [Rockets] flames. [ying yang] opposite one to the other. - With 2TWO very long distance INFLOW [inside propulsion] CONDUITS. -4 TURBOS Rotary Total Thrust Power Regeneration Power System. -Mechanical direct 2two [Small] Planetary Gears at polar position. -Like the Ying Yang Symbol / Concept.

-The Mechanical Gear Power Thrust Point Wide out the Rotor circumference were have much more lever [HIGH Torque] POWER THRUST. -No blade erosion by sand & very low heat target signature profile. -3 points of power thrust; 1-flow way, 2-gear, 3-turbine. *Patent; Dic. 1991 IMPI Mexico # 197187 All Rights Reserved. Carlos Barrera.

· 2-IMPLOTURBOCOMPRESSOR; One Moving Part System Excellence Design - The InFlow Interaction comes from Macro-Flow and goes to Micro-Flow by Implossion - Only One Compression Step; Inflow, Compression and outflow at one simple circular dynamic motion Concept.

* · “Excellence in Design" because is only one moving part. Only one unique compression step. Inflow and out flow at the same one system, This invention by its nature a logic and simple design in the dynamics flow mechanics area. The invention is a wing made of one piece in a rotating motion, contained in a pair cavity system connected by implocavity, and interacting dynamically with a flow, that passes internally "Imploded" through its simple mechanism. This flow can be gas (air) or liquid ( water). And have two different applications, in two different form-function; this one can be received (using the dynamic flow passage, as a receiver). Or it can be generated (with a power plant, generating a propulsion).

An example cut be, as a Bike needs a chain to work from motor to wheel. And for the Imploturbocompressor application, cut be as; in a circumstance at the engine, as an A-activate flow, and with a tube for a conduit going to the wheel as a B-receiving-flow the work use.

To see a Imploturbocompressor animation, is posible on a simple way, just to check the Hurricane Satellite view, and is the same implo inflow way nature.

And when the fact that it is intended to be used, it does not necessarily need to be exhausted, but it must be a dynamic passing gas or liquid flow. This could be possible at the passing and interacting period when it passes through its simple mechanism. This can be in any point of the work flow trajectory.

In case the flow that is received is a water falling by gravity, and a dynamo is placed on the rotary bar, the Imploturbocompressor can profit an be obtained by generating? electricity such as obtained by the pelton well, like I say before. The "Imploturbocompressor", is a good option to pump water, or a gas flow, and all kinds of pipes lines dynamic moves.

Or only receive the air-liquid flow, because of this flow through the simple mechanism of a rotating mechanism of one-to-one interaction within the implocavities system. And this flow can be made of a horizontal wind, which can be used in the construction industry, and it can be used in the construction industry. 180 grades view. The above mentioned information relates to this invention refers to technical applications, such as a dynamic flow receiver. (whether being gas or liquid).

With the appropriate power plant and the appropriate dimensioning and number of RPM this invention is also feasible to generate an atmospheric air propulsion and the auto-propulsion of an aircraft. Being an effective and very simple system that implodes and compresses the atmospheric air permits the creation of a new concept of propulsion for aircrafts, due to its simple mechanism and innovative nature. At the place of the aircraft were the system appears and the manner how the propulsion direction can be oriented with a vectorial flow (no lobster tail) with I call "yo-yo system" (middle cut (at the shell) to move, one side loose), guided and balanced is feasible to create a new concept of TOVL-vertical take-off landing, Because the exhaust propulsion can going out radial in all the 360 ​​vectorial positions, going out direct all the time in all the vectors direction. With his rotor cover for an better furtive fly, like going down of a bridge for example.

Likewise, with the due form and dimensioning, and considering the liquid density and the due revolutions for this element there could be generated a propulsion (water) in order to move an aquatic ship, whether on surface or under water. Also can be a good option to pump liquid combustion for a rocket propulsion.

Making a metaphoric comparison with the intention to make it easier to understand this new technical detail, it would be similar to the trajectory a knot (without obstructing the flow), so the complete way of the flow of the imploturbocompresor system have three different ways; direct way (entrance) - turn - direct way (implocavity) - turn - direct way (exit), all this in a 1 simple circular move system concept.

Its prudent to mention that the curves and the inclinations of the blades of a rotating wing of this invention, is conferred by its shape and function to structural rigidity allowing it to conduct and alter appropriately the dynamic flow through its system.
Attachments
Imploturbocompressor Other side A and B.% 22A% 22 as a receiver, and% 22B% 22 as a generator.jpg
IMPLOTURBOCOMPRESSOR
Imploturbocompressor Other side A and B.% 22A% 22 as a receiver, and% 22B% 22 as a generator.jpg (14.48 KB) Viewed 5323 times
Imploturbocompressor A and B.% 22A% 22 as a receiver, and% 22B% 22 as a generator.jpg
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Imploturbocompressor A and B.% 22A% 22 as a receiver, and% 22B% 22 as a generator.jpg (14.21 KB) Consulted 5323 times
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Gearturbine Inside Rotor Ducts Turbo Compression Steps.jpg
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State of the Art-Tech InFlow Novel Project Development; · 1-Gearturbine RotaryTurbo Rétrodynamique = Dextro RPM VS Levo InFlow + Ying Yang Way power-No waste Type loses similar system Aeolipile 10-70 AD Pat197187IMPI MX Dic1991 / · 2-Imploturbocompressor A MovingPart Excellence System Design A step similar compression the hurricane satellite view, is the same way Implo InFlow flow goes to macroflow MicroFlow
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Re: State of the Art-Roman InFlow Tech: 1-Gearturbine RotaryTurbo, 2-Imploturbocompressor One CompressionStep




by Christophe » 10/12/16, 16:04

retrodynamic wrote:Novel Technologie State of the Art Novel InFlow Tech featured Development project 1Gearturbine 2Imploturbocompressor



This is a very technical first message as I like them! :!:

Do you have a summary in French?

Who would at least give the advantages, disadvantages ...?
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izentrop
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Re: State of the Art-Roman InFlow Tech: 1-Gearturbine RotaryTurbo, 2-Imploturbocompressor One CompressionStep




by izentrop » 13/12/16, 15:30

Hello,
I did not see Romanesque art like that ??
What is circulating in this turbine, water, air?

3 rotors in the machine ?? Does it seem complicated and energy consuming?

Characteristics: power, efficiency?
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