http://rdf.ncbi.nlm.nih.gov/pubchem/patent/GR-20100100340-A

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publicationDate 2012-01-31^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber GR-20100100340-A
titleOfInvention STROVILOANTIDRASTIRAS DUAL FLOW, VARIABLE CYCLE WITH STROVILOUS reverse TAXES WITH COMBUSTION CHAMBER AREA WITHOUT DILUTION WITH cooled turbine HIGH PRESSURE WITHOUT FINS FIXED COVER WITH thermodynamic cycle VERY HIGH TEMPERATURE AND THERMAL DECOMPOSITION CATALYST HYDROCARBONS AND / OR WATER IN HYDROGEN
abstract Dual-flow turbine reactor, wherein the high-pressure turbine (7) is the turbine that drives the fan (2) and the low-pressure turbine (8) is the turbine that drives the compressor (4). The rotation times of these turbines are reversed, with no guide blades arranged in the housing. Variable blade guides (1) are provided at the fan inlet (2) and variable blade guides (3) at the compressor inlet (4). In the pure (simple) version of the turbocharger, the nozzle (9) of the inner housing is variable by fluctuating the nozzle surface. In the mixed (composite) version of the turbocharger, the common nozzle (9) of the inner and outer casing is variable by fluctuating the nozzle surface. In both cases, changing the parameters of the thermodynamic cycle and / or optimizing the turbocharger characteristics through the variable nozzle is possible.
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