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1. 发明申请

WO2023078929A1 IMPROVED CONVERSION OF SOLAR HEAT TO ELECTRICITY 审中-公开
公开(公告)号：WO2023078929A1
公开(公告)日：2023-05-11
申请号：PCT/EP2022/080551
申请日：2022-11-02
申请人： AELLA SA
发明人： TEPIC, Slobodan
IPC分类号： F24S10/50 , F24S60/10 , F24S60/30 , F24S90/00
摘要： 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).

2. 发明申请

WO2012152447A1 TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE 审中-公开
标题翻译：涡轮发动机，特殊内燃机
公开(公告)号：WO2012152447A1
公开(公告)日：2012-11-15
申请号：PCT/EP2012/002031
申请日：2012-05-10
申请人： AELLA SA , TEPIC, Slobodan
发明人： TEPIC, Slobodan
IPC分类号： F01D1/36 , F02C3/05 , F02C3/36 , F01D1/34
CPC分类号： F01D1/34 , F01D1/36 , F02C3/05 , F02C3/365 , F04D5/001 , F04D17/161 , Y02T50/672
摘要： 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.
摘要翻译：本发明涉及涡轮发动机，特别是内燃机，其包括壳体和其中堆叠的盘式或特斯拉式结构的无叶涡轮部分（30; 42; 67），其中所述涡轮部分（30; 42 ; 67）具有多个紧密间隔的盘（32; 49; 61），其布置成围绕所述壳体中的旋转轴线共同旋转，所述涡轮部分（30; 42; 67）适于通过切向流分量传递工作流体同时从所述工作流体流采取能量以旋转盘（30; 49; 61），从所述涡轮部分（30; 42; 67）的径向内部区域流向径向外部区域。优选地，涡轮发动机还包括堆叠的盘式或特斯拉型结构的压缩机部分（40; 66），其具有多个紧密间隔的盘（45; 61），其布置成围绕所述旋转轴线共同旋转，并且燃烧区（41; 64），其中所述压缩机部分（40; 66）与涡轮部分（30; 42; 67）同轴并且径向向内设置，其中燃烧区域（41; 64）径向地设置在压缩机部分和涡轮部分。

3. 发明公开

EP2522808A1 Turbo-engine, particularly internal combustion engine 审中-公开
标题翻译：涡轮机，不动床动力驱动器
公开(公告)号：EP2522808A1
公开(公告)日：2012-11-14
申请号：EP11170776.6
申请日：2011-06-21
申请人： Aella SA
发明人： Tepic, Slobodan
IPC分类号： F01D1/36 , F02C3/05 , F02C3/36 , F01D1/34
CPC分类号： F01D1/34 , F01D1/36 , F02C3/05 , F02C3/365 , F04D5/001 , F04D17/161 , Y02T50/672
摘要： 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.
摘要翻译：本发明涉及涡轮发动机，特别是内燃机，其包括壳体和其中堆叠的盘式或特斯拉型结构的无叶涡轮部分（30; 42; 67），其中涡轮部分（30; 42 ; 67）具有多个紧密间隔的盘（32; 49; 61），其布置成围绕所述壳体中的旋转轴线共同旋转，所述涡轮部分（30; 42; 67）适于通过切向流分量传递工作流体同时从所述工作流体流采取能量以旋转盘（30; 49; 61），从所述涡轮部分（30; 42; 67）的径向内部区域流向径向外部区域。优选地，涡轮发动机还包括堆叠的盘式或特斯拉型结构的压缩机部分（40; 66），其具有多个紧密间隔的盘（45; 61），其布置成围绕所述旋转轴线共同旋转，并且燃烧区（41; 64），其中所述压缩机部分（40; 66）与涡轮部分（30; 42; 67）同轴并且径向向内设置，其中燃烧区域（41; 64）径向地设置在压缩机部分和涡轮部分。

4. 发明授权

EP2707574B1 TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE 有权转让
公开(公告)号：EP2707574B1
公开(公告)日：2018-07-25
申请号：EP12725616.2
申请日：2012-05-10
申请人： Aella SA
发明人： TEPIC, Slobodan
IPC分类号： F01D1/36 , F02C3/05 , F02C3/36 , F01D1/34
CPC分类号： F01D1/34 , F01D1/36 , F02C3/05 , F02C3/365 , F04D5/001 , F04D17/161 , Y02T50/672
摘要： 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.

5. 发明公开

EP4177536A1 IMPROVED CONVERSION OF SOLAR HEAT TO ELECTRICITY 无效
公开(公告)号：EP4177536A1
公开(公告)日：2023-05-10
申请号：EP21206240.0
申请日：2021-11-03
申请人： Aella SA
发明人： TEPIC, Slobodan
IPC分类号： F24S10/50 , F24S60/10 , F24S60/30 , F24S90/00
摘要： The present invention discloses a solar heat powerplant utilizing the full cycle of potential radiative heat exchange between the Sun, the Earth, and deep space. Utilization of radiative cooling during night hours combined with irradiation during the day provides approximately doubling of theoretical efficiency when compared with conventional solar power capture schemes without light concentration.

6. 发明公开

EP2707574A1 TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE 有权转让
标题翻译：涡轮机，绝缘子VERBRENNUNGSMOTOR
公开(公告)号：EP2707574A1
公开(公告)日：2014-03-19
申请号：EP12725616.2
申请日：2012-05-10
申请人： Aella SA
发明人： TEPIC, Slobodan
IPC分类号： F01D1/36 , F02C3/05 , F02C3/36 , F01D1/34
CPC分类号： F01D1/34 , F01D1/36 , F02C3/05 , F02C3/365 , F04D5/001 , F04D17/161 , Y02T50/672
摘要： 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.
摘要翻译：本发明涉及涡轮发动机，特别是内燃机，其包括壳体和其中堆叠的盘式或特斯拉型结构的无叶涡轮部分（30; 42; 67），其中涡轮部分（30; 42 ; 67）具有多个紧密间隔的盘（32; 49; 61），其布置成围绕所述壳体中的旋转轴线共同旋转，所述涡轮部分（30; 42; 67）适于通过切向流分量传递工作流体同时从所述工作流体流采取能量以旋转盘（30; 49; 61），从所述涡轮部分（30; 42; 67）的径向内部区域流向径向外部区域。优选地，涡轮发动机还包括堆叠的盘式或特斯拉型结构的压缩机部分（40; 66），其具有多个紧密间隔的盘（45; 61），其布置成围绕所述旋转轴线共同旋转，并且燃烧区（41; 64），其中所述压缩机部分（40; 66）与涡轮部分（30; 42; 67）同轴并且径向向内设置，其中燃烧区域（41; 64）径向地设置在压缩机部分和涡轮部分。

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