Gearturbine - Atypical Thermodynamic Technology Submission

[gearturbine]

Gearturbine - Atypical Thermodynamic Technology Submission

http://gearturbine.260mb.com

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

http://www.youtube.com/watch?v=0cPo9Lf44TE

GEARTURBINE -Atypical Combustion Turbine Engine, -State of the Art, -New Thermodynamic Technology, -With Retrodynamic "Dextrogiro vs Levogiro" Effect, is when the inflow direction moves is against [VS] of the circular rotary dynamic, When the inflow have more velocity the rotor have more RPM / because push the single turbine with the planetary gear, (an a example is like to move the head to the side of the strike hit) / RPM Rotor Move VS Inflow Conduits Way /ACTION VS REACTION / Front to Front / Velocity vs Velocity, making in a simple way a very strong concept of power thrust, a unique technical quality. -Wide cylindrical shape dynamic mass (continue Inertia cinetic positive tendens motion / all the motor weight is goin with the power thrust direction), -Non Waste, parasitic losses form-function engine system for; cooling, lubrication & combustion; -Lubrication & Combustion inside a conduit radial position, out way direction, activated by centrifugal force Fueled Injected, -Cooling in & out; In by Thermomix flow & Out by air Thermo transference, activated by the dynamic rotary move, -Increase the first compression by going of reduction of one big circumference fan blades going to, -2two very long distance captive compression inflow propulsion conduits (like a digestive system) (long interaction) in perfect equilibrium well balanced start were end like a snake bite his own tale, -Inside active rotor with 4 pairs of retrodynamic turbos (complete regeneration power system), -Mechanical direct "Planetary Gear" power thrust like a Ying Yang (very strong torque) (friendly loose friction) 2two small gears in polar position inside a bigger shell gear, wide out the rotor circumference were have much more lever power thrust, lower RPM in a simple way solution, to make possible for a some innovative work application (cars/land). -3 Stages of inflow turbo compression before the combustion. -3 points united of power thrust; 1- Rocket Flames, 2-Planetary Gear & 3-Exhaust Propulsion, all in one system. -2two continuous circular moving inside combustion (rocket flames) like two dragons trying to bite the tail of the opposite other. -Hybrid flow system different kind of aerolasticity thermoplastic inflow propulsion types; single, action & reaction turbines applied in one same system, -Military benefits, No blade erosion by sand & very low heat target profile. -Power thrust by barr (tube); air sea land & generation application, -A pretender of very high % porcent efficient power plant engine. -Patent; Dic 1991 IMPI Mexico #197187