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Thermodynamic pressure generator

a generator and thermodynamic technology, applied in the field of turbine engines, can solve the problems of near ambient temperature, release of exhaust gases into the atmosphere that are not combustible, etc., and achieve the effects of less fuel consumption, high horsepower, and great torqu

Inactive Publication Date: 2006-02-02
TAFOYA SAMUEL BARRAN
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The solution results in a cost-effective, fuel-efficient turbine engine with reduced environmental impact, producing non-combustible exhaust at ambient temperature, lower rotor speeds, and fewer components, enabling simpler manufacture and maintenance.

Problems solved by technology

Cooling chambers positioned adjacent to the oil reservoir, and oil cooling fins, reduce exhaust heat and cooling heat as an energy loss, resulting in the release of exhaust gases to the atmosphere that are not combustible and near ambient temperature.

Method used

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Examples

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Embodiment Construction

[0017]FIGS. 1-3 show the most preferred embodiment of the present invention turbine engine having an oscillating valve M that allows a premixed fuel mixture (fuel mixture flow is shown by the arrows with solid arrowheads in FIG. 2) to enter a combustion chamber C in turbulence, until it comes into contact with the lips of two annular spoilers A1 and A2, which then convert a portion of the fuel / air mixture into laminar flow in the form of two Karmon vortex rings VR1 and VR2, for delayed ignition. When the remaining turbulent flow is ignited by a continuous spark from igniter B1, a rapid pressure rise occurs that simultaneously kills both vortex rings VR1 and VR2, and the fuel mixture therein goes from laminar to turbulence, adding fuel to the already burning charge E to supercharge it and permit near total ignition. Thus the exhaust gases of the present invention contain no combustible or environmentally polluting by-products. In addition, since the present invention turbine engine a...

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PUM

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Abstract

A thermodynamic pressure generator having an oscillating valve that allows premixed fuel to enter a combustion chamber in turbulence, until it comes into contact with an annular spoiler, which converts a portion of the fuel into a Karmon vortex ring for delayed ignition. A continuous spark then ignites the remaining fuel with rapid pressure rise that kills the vortex. The fuel in the vortex goes from laminar to turbulence, adding fuel to the already burning charge, super charging it and permitting total ignition. Thus, present invention exhaust contains no polluting by-products and only sensible heat is released into the environment. Exhaust gases are released radially through turbine vanes having a shape that permits a relatively low rotational speed, with sufficient peripheral speed to create torque of considerable degree. Applications include, but are not limited to, land transportation vehicles, propeller-driven airplanes, and marine vessels.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS [0001] None BACKGROUND OF THE INVENTION [0002] 1. Field of the Invention [0003] This invention relates to the field of turbine engines, specifically to a thermodynamic pressure generator that has an oscillating valve allowing a premixed fuel charge to enter a combustion chamber in turbulence, until it comes into contact with two annular spoilers that convert a portion of the mixture into two Karmon vortex rings having laminar flow for delayed ignition. A continuous spark ignites the turbulent air / fuel mixture with rapid pressure rise that kills the formation of the vortex rings. The fuel mixture in the rings then goes from laminar to turbulence, adding fuel to the already burning charge, super charging it and permitting near total ignition. Thus, exhaust from the present invention contains no combustible gases or environmentally polluting by-products. The engine also provides its own cooling system, therefore releasing only sensible heat into ...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): F02C3/16
CPCF01D15/02F02C5/12F02C5/02F02C3/16
Inventor TAFOYA, SAMUEL BARRAN
Owner TAFOYA SAMUEL BARRAN
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