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Found results for
patents
1.
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IMPROVED CONVERSION OF SOLAR HEAT TO ELECTRICITY
Application Number |
EP2022080551 |
Publication Number |
2023/078929 |
Status |
In Force |
Filing Date |
2022-11-02 |
Publication Date |
2023-05-11 |
Owner |
AELLA SA (Switzerland)
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Inventor |
Tepic, Slobodan
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Abstract
A solar heat powerplant comprising: a first heat reservoir which is a cold reservoir (3), a second heat reservoir which is a hot reservoir (1), at least one heat exchanger (5) adapted for radiative dry cooling of the cold reservoir (3) and/or for radiative heating of the hot reservoir (1) by absorbing solar irradiation, and a power generator (8) which operates by extracting heat from the hot reservoir (1) and transferring residual heat into the cold reservoir (3).
IPC Classes ?
- F24S 10/50 - Solar heat collectors using working fluids the working fluids being conveyed between plates
- F24S 60/10 - Arrangements for storing heat collected by solar heat collectors using latent heat
- F24S 60/30 - Arrangements for storing heat collected by solar heat collectors storing heat in liquids
- F24S 90/00 - Solar heat systems not otherwise provided for
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2.
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Turbo-engine, particularly internal combustion engine
Application Number |
14116830 |
Grant Number |
09759067 |
Status |
In Force |
Filing Date |
2012-05-10 |
First Publication Date |
2014-04-17 |
Grant Date |
2017-09-12 |
Owner |
AELLA SA (Switzerland)
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Inventor |
Tepic, Slobodan
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Abstract
The invention is directed to a turbo-engine, particularly internal combustion engine, comprising a housing and therein a bladeless turbine section (30; 42; 67) of the stacked disc- or Tesla-type construction, wherein the turbine section (30; 42; 67) has a plurality of closely spaced discs (32; 49; 61) arranged for common rotation about a rotation axis in the housing, said turbine section (30; 42; 67) is adapted for passing with tangential flow components a working fluid stream from a radially inner region to a radially outer region of said turbine section (30; 42; 67) while adopting energy from said working fluid stream for rotating the discs (30; 49; 61). Preferably, the turbo-engine further comprises a compressor section (40; 66) of the stacked disc- or Tesla-type construction having a plurality of closely spaced discs (45; 61) arranged for common rotation about said rotation axis and a combustion zone (41; 64), wherein said compressor section (40; 66) being arranged coaxially with—and radially inwardly of the turbine section (30; 42; 67) with the combustion zone (41; 64) provided radially between the compressor section and the turbine section.
IPC Classes ?
- F01D 1/34 - Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
- F01D 1/36 - Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
- F02C 3/05 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor the compressor and the turbine being of the radial flow type
- F04D 5/00 - Pumps with circumferential or transverse flow
- F04D 17/16 - Centrifugal pumps for displacing without appreciable compression
- F02C 3/36 - Open cycles
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3.
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Generating electrical power utilizing surface-level hot air as the heat source, high atmosphere as the heat sink and a microwave beam to initiate and control air updraft
Application Number |
13865556 |
Grant Number |
09049752 |
Status |
In Force |
Filing Date |
2013-04-18 |
First Publication Date |
2013-09-05 |
Grant Date |
2015-06-02 |
Owner |
Aella SA (Switzerland)
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Inventor |
Tepic, Slobodan
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Abstract
The invention describes a method of generating electrical power utilizing hot surface air as the heat source, high atmosphere as the heat sink and a microwave beam aimed upward providing updraft to initiate and control the large-scale air circulation. The frequency of the microwave beam is centered at approximately 60 GHz, within the absorption band of molecular oxygen, so as to result in beam penetration to an altitude of several kilometers. The power plant comprises a high-power microwave source, e.g. a bank of gyrotrons, one or more turbine-generator sets, and—optionally—a condenser/cyclone (if on a floating platform). The plant can also provide clean water from condensation out of humid, sea level air. The plant could also be used to remove atmospheric carbon dioxide from large quantities of air. The dynamic chimney produced by the microwave beam could alternatively be deployed in conjunction with a solar heat power plants, industrial chimneys, and cooling towers of conventional power plants to increase their effective height.
IPC Classes ?
- F03B 13/00 - Adaptations of machines or engines for special useCombinations of machines or engines with driving or driven apparatusPower stations or aggregates
- H02P 9/04 - Control effected upon non-electric prime mover and dependent upon electric output value of the generator
- H05B 6/64 - Heating using microwaves
- F03D 1/04 - Wind motors with rotation axis substantially parallel to the air flow entering the rotor having stationary wind-guiding means, e.g. with shrouds or channels
- F03D 9/00 - Adaptations of wind motors for special useCombinations of wind motors with apparatus driven therebyWind motors specially adapted for installation in particular locations
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4.
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TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE
Application Number |
EP2012002031 |
Publication Number |
2012/152447 |
Status |
In Force |
Filing Date |
2012-05-10 |
Publication Date |
2012-11-15 |
Owner |
AELLA SA (Switzerland)
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Inventor |
Tepic, Slobodan
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Abstract
The invention is directed to a turbo-engine, particularly internal combustion engine, comprising a housing and therein a bladeless turbine section (30; 42; 67) of the stacked disc- or Tesla-type construction, wherein the turbine section (30; 42; 67) has a plurality of closely spaced discs (32; 49; 61 ) arranged for common rotation about a rotation axis in the housing, said turbine section (30; 42; 67) is adapted for passing with tangential flow components a working fluid stream from a radially inner region to a radially outer region of said turbine section (30; 42; 67) while adopting energy from said working fluid stream for rotating the discs (30; 49; 61). Preferably, the turbo-engine further comprises a compressor section (40; 66) of the stacked disc- or Tesla-type construction having a plurality of closely spaced discs (45; 61 ) arranged for common rotation about said rotation axis and a combustion zone (41; 64), wherein said compressor section (40; 66) being arranged coaxially with- and radially inwardly of the turbine section (30; 42; 67) with the combustion zone (41; 64) provided radially between the compressor section and the turbine section.
IPC Classes ?
- F01D 1/36 - Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
- F02C 3/05 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor the compressor and the turbine being of the radial flow type
- F02C 3/36 - Open cycles
- F01D 1/34 - Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
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