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Novel Rotary-InFlow Technology / Gearturbine Project – Featured Development


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#1 Carlos Barrera

Carlos Barrera

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  • Country:Mexico
  • Engineering Discipline (Branch):Design
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  • Designation:Dessigner

Posted 27 February 2012 - 10:18 PM

 *GEARTURBINE PROJECT:


Atypical InFlow Thermodynamic


Technology Proposal Submission


Innovative [TURBO-ROTARY]


Novel (Fueled) Motor Engine Type


-The Gearturbine comes from the contemporary ecological essential global needs of an efficient power plant fueled motor engine. -Power thrust by bar (tube); air, sea, land and power generation, work use application.


*Have the similar simple basic system of the "Aelopilie" Heron´s Steam Turbine device from Alexandria, [10-70 AD] one thousand nine hundred years ago. Because; the circular dynamic motion, with 2/Two Opposites power [polar position] lever, and is feeds from his axis center.


YouTube Video/10.30 min; * Atypical New · GEARTURBINE / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type - Non Waste Looses


http://www.youtube.c...h?v=0cPo9Lf44TE


-Desirable Contemporary Innovation, With the Possible [Efficient] Invention. -Mechanical [Thermodynamic] Universal Human History Evolution. [Unlike] Epic Technology Revelation. -Next Step Power-plant New Design Form Function Device Change.


 


*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


 


*Innovation Technology Break Barrier / Paradigm [Broken-Seal] Solution. State of the art. Innovative Turbo-Rotary concept Top system.


-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. A very strong Novel concept of torque power thrust. At field explanatory example with a metaphor is like if a sailboat take the wind from his prow front to move; wind/inflow + knots/rpm + wind/inflow + knots/rpm + wind/inflow + knots/rpm + etc... = Acceleration x Acceleration = Exponential Acceleration. Whereas it has more movements forwards, it receives a frontal impulse still but to move more forwards. A present example of the implementation of the Retrodynamic effect is in the application in the accelerator (and collider) of particles that this in the border of Switzerland and France.


-Shape-Mass + Rotary-Motion = Inertia-Dynamic / Form-Function Wide [Flat] Cylindrical shape + positive dynamic rotary mass = continue Inertia kinetic positive tendency motion / all the complete Rotary motor mass weight is going with the power thrust move circular direction.


-Non-waste parasitic looses system for cooling, lubrication & combustion; -Lubrication & Combustion, inside a conduit radial position, out way direction, activated by Centrifugal Force-Fueled Injected. -Cooling; a) IN-Thermomix flow, & B) OUT-Air Thermo transference.


-Combustion 2Two [Inside-Rotary-Dynamic] continue circular [Rockets] flames. Like two dragons trying to bite the tail of the [ying yang] opposite other.-Increase the first compression by going of flow reduction of one big circumference blades going pass to 2TWO reduced, very long distance (total captive compression) INFLOW [inside propulsion] CONDUITS [long flow interaction] [like a digestive system] Start were ends, in perfect shape balance in perfect equilibrium well balanced, like a snake bite his own tale. -4 TURBOS Rotary [inside-rotary-active] [In-Flow, Out-Flow] Total Thrust-Power Regeneration [Complete] Power System. -Mechanical direct 2two [Small] "Planetary Gears" at polar position. Like the Ying Yang Symbol/Concept. Wide out the Rotor circumference were have much more lever [HIGH Torque] POWER THRUST. -Military benefits, No blade erosion by sand & very low heat target profile.-3 stages of inflow turbo compression before combustion; 1)1-Turbine, 2)2-Turbos 3)2-Turbos. -And 3 points of power thrust; 1-flow way, 2-gear, 3-turbine.


*The most innovative power plant motor engine project today. Higher efficient % percentage. Next trend wave toward global technological coming change.


Patent; Dic. 1991 IMPI Mexico #197187 - Carlos Barrera. - Individual Designer - Inventor and project owner. / All Rights Reserved. - Monterrey NL Mexico.








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