State of the Art Novel InFlow Tech ·1-Gearturbine: Reaction Turbine, ·Rotary-Turbo, Similar to the Aeolipile

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Featured Project Development - State of the Art Novel InFlow Technology:
·1-Gearturbine, Rotary-Turbo:

*Wordpress Blog State of the Art Novel InFlow Gearturbine Imploturbocompressor:

http://stateoftheartnovelinflowtech.blogspot.com

*1-GEARTURBINE PROJECT,
Reaction-Turbine System Type,
Rotary-Turbo-InFlow Tech,
Atypical InFlow Thermodynamic,
Technology Proposal Submission,
Novel Fueled Motor Engine Type:

*1-GEARTURBINE BEHANCE Images Gallery Portafolio:

https://www.behance.net/gallery/21019191/Novel-Rotary-Turbo-InFlow-Tech-Gearturbine-Project

·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. Next trend wave toward global technological coming change.

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

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

-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.

-Non waste parasitic looses for; friction, cooling, lubrication & combustion. -Shape-Mass + Rotary-Motion = Inertia-Dynamic.

-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.

-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.

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  • ABOUT THE ENTRANT

  • Name:
    Carlos Barrera
  • Type of entry:
    individual
  • Software used for this entry:
    CAD
  • Patent status:
    patented