* More than 10 years of know-how, new kind of power plant, hybrid turbine = action & reaction system. I have grant patent, power trust by a bar = air,sea,land & generation aplications, two very long cautive compression conduit= (like a digestive system or similar to the propulsion by pulse exaust pipe), with an inside active rotor with four pairs of dynamic turbos, with the unique technical cuality of; "Dextrogiro vs Levogiro" Effect- is when the rotor move is against the inside rotor flow making a very strong dynamic new effect.
Two gears for a direct mechanical thrust push, in a planetary move conecting on a inside gear at the shell in a simple circular rotor movement for a new concept of turbine engine.
The strong centrifugal force of the circular rotor movement is used for combustion and the lubrication system to get at the aplication points and to to work well. No waste cooling because the inside active rotor is moving, and it is cooled by air transference / not the air pass at the engine - the engine pass at the air, (inside has a critical heat point, reserved to ceramics), inside the cavity in the point of flame is a circular clear space know as a tovera, to make a inside a coold system. So are two coold systems; outside and inside.
The gearturbine for his form-function, can have a fast changes of RPM and good for a turbine on a land aplication (a very big global change)
The two gears of the rotor are at the end limit of the rotor circunference and is were have more power, and are the smallest of the inside internal shell gear were moves, and that is a simple way to reduce the extreme RPM, additionaly it's technical quality is efficient enough to make fast changes in RPM for land applications like I say before.
To calculate the percent of efficiency of this engine, you've got to
take into account a few very efficient parts know well like four pairs of dynamics turbos (with superchargers on the next evolution/see draws), compression and exhaust with an action turbine, two singles turbines receptors (I make an improvement with the "Imploturbocompressor"on this efficient positions), the two polar positions flames are going inside with the rotor (like a YING-YANG), the inside flow is going front to front vs-against the rotor move, making dextrogiro vs levogiro effect, direct mechanical trust push by gear, no waste energy for extra system.Lubrication and combustion are provided by the free centrifugal force of the rotor movement. Taking this into account to make an "Overunit Engine".
You can adapt a dynamo to generate electricity, and make an efficient "Electrolysis" to break the molecule of water (H2O=H,H,O) and use the hydrogen for fuel in a clean and cheap way. It's technical quality
make this engine a good option to be used as a power plant in the colonization
of other planets with water, like Mars for example, and the circular moves of the rotor are good to work like a giroscope for a space vehicle aplication.
The "Gear Turbine" is similar of nature of the first human dynamic mechanical device - "Heron's Well from Alexandria"(1900 years back) because is refueled and provide from the center and the points of flame are moving one versus the other on the same simple circular way (like a YING-YANG), Coming back again to the beginning basics of the human mechanical creation, start with an efficiency concept of a simple circular move.
Heron's Well / similar concept.
Fig IV-Out side front view./Simple.
Fig III- Front cut at the middle.
See the gear contact, the flame 32.
The inside active rotor moves counter clockwise.
Fig II - Lateral cut at the middle.
Check the turbo 14, and all details.
Fig I- all the pieces fiting on A,B,C,D stepts.
The rotor complete on the right side.
-Drawings fo the next step evolution. It is possible easily to make a plus mechanical superchargers blowers on the same turbo positions, a very strong power thrust.
And the tornado flow, a new radical power concept.
The lubrication system is on by the strong centrifugal force
and going back by the centripetal force of the rotor move by a directional conducting.
Flows - The cavities inside inside the active rotor
Check the four pairs of turbo, and the cavities start were finish.
FLOW STEPS:
1- First air compression ( tornado flow on the evolution ).Compression
front side of an
action turbine
2- Second compression, first turbo, side cool (hot 7) Reaction turbine.
3-Third compression, second turbo, side cool (hot 6).The point were
the cavities cross.
4-Point of flame./ The flame have a circular move inside the active
rotor. The point of
flame have a free space between the cavities for a inside
cooling system.
5-Point of direct mechanical thrust push by gear. On the drawings
is a part like a Pelton
well, but the evolution or next step on this point are
gone a change for the
"Imploturbocompressor" ( the other project #2).
6-Hot side of turbo (cool 3). The point were the cavities croos.reaction
turbine.
7-Hot side of turbo (cool 2). The point were the hot gas exhaust outside
the
rotor. Reaction turbine.
8-last point of interaction of gas exhaust compression. Exhaust,
back side of action
turbine.
Direction flows by steps
Compression :1,2,3
Thrust: 4,5,8
Reaction turbine 2,7 & 3,6
Action turbine 1,8.
-Inside the rotor
comparison of the cavities with two snakes. bites his tales.
Ends were starts.
El Norte - Newspaper very well international recognized,
From saturday 20 Feb. 1993. Monterrey Mexico.
Muy Interesante 1. from year IX no.10 / 1992
Scientific magazine.
