18-10-2016, 12:40 PM
State of the Art Novel Rotary-Turbo-InFlow Tech - Gearturbine Project - Featured Development - Atypical Motor Engine Type
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-This innovative concept consists of hull and core where are held all 8 bteps 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.
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
= continue Inertia positive tendency motion. Kinetic Rotating Mass.
-Combustion 2Two continue 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. -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.
Benefits Summary
State of the Art / Novel Rotary-Turbo-InFlow Tech / Featured Development - GEARTURBINE PROJECT Have the similar basic
system of the Aeolipile 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. Higher efficient
percent. No blade erosion by sand & very low heat target signature Pat:197187IMPI MX Dic1991 Atypical Motor Engine Type
Offer Features
Global
Development Status Summary
Project
Potential Applications
Power-Plant Motor Engine; Air, Sea, Land and Generation