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Aeronautical Engineering/Atypical InFlow Thermodynamic Technology Submission - Gearturbine Project

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Question
What do you think, about this Gearturbine project, its viable?

Information about; GEARTURBINE PROJECT
Atypical InFlow Thermodynamic Technology Submission
Innovative New Turbo-ROTARY Fueled Motor Engine Type

*The Gearturbine comes from the contemporary ecological essential global needs of a efficient power plant fueled motor engine.
-Power thrust by bar (tube); air, sea, land, power generation, work application.
-Have the same simple basic system of the "Aelopilie" Heronīs 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.

http://gearturbine.260mb.com
YouTube Video/10.30 min.; Atypical New * GEARTURBINE / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type - Non Waste Looses
http://www.youtube.com/watch?v=0cPo9Lf44TE

*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-Turbo1 hot
8)1-Turbine / bigger

Gearturbine; atypical fueled turbine engine, state of the art. New thermodynamic technology. Turbo-Rotary / Top system.
-With Retrodynamic dextrogiro vs levogiro phenomenon effect. / Rotor-RPM VS InFlow / front to front "Collision-interaction Type" - inflow vs blades surface/(gear). Technical unique dynamic motion mode.
-Form-function (flat) wide cilindrical shape / continue kinetic inertia, positive tendence dynamic mass motion. The rotary motor weight is going with the the circular motion power thrust.
-Non-waste parasitic looses system for: cooling, lubrication & combustion.
-Combustion 2Two (Inside dynamic) continue circular flames (like 2two opposite rockets, (at the same axis)).
-2 Two (very) long captive compression inflow propulsion conduits. start at were ends, in perfect shape balance.
-4 Turbos (rotary & translation motion) inside active.
-Mechanical direct 2two planetary gears thurst, inside in a bigger shell, total lever, polar position. (Big torque) (like the Ying Yang simbol concept).
-3 stages of inflow turbo compression before combustion; 1)1-Turbine, 2)2-Turbos 3)2-Turbos.

*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.

Answer
I don't know. I don't speak Spanish so I couldn't understand the video. Generally, a new propulsion device must be tested in a laboratory, and the results published in a recognized technical journal.  Then people can see how it performs relative to other systems. See the Tesla websites for comparisons. Good luck.
Paul

Aeronautical Engineering

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Paul Soderman

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Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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