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    • 3. 发明申请
      WO2012152447A1 TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE 审中-公开
    • TURBO-ENGINE, PARTICULARLY INTERNAL COMBUSTION ENGINE
    • 涡轮发动机，特殊内燃机
    • WO2012152447A1
    • 2012-11-15
    • PCT/EP2012/002031
    • 2012-05-10
    • AELLA SA , TEPIC, Slobodan
    • TEPIC, Slobodan
    • F01D1/36 , F02C3/05 , F02C3/36 , F01D1/34
    • F01D1/34 , F01D1/36 , F02C3/05 , F02C3/365 , F04D5/001 , F04D17/161 , Y02T50/672
    • 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.
    • 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。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 5. 发明申请
      WO2018078350A1 GAS TURBINE ENGINE 审中-公开
    • GAS TURBINE ENGINE
    • 燃气涡轮发动机
    • WO2018078350A1
    • 2018-05-03
    • PCT/GB2017/053202
    • 2017-10-24
    • JIANG, Kyle
    • JIANG, Kyle
    • F02C3/05 , F02C3/14 , F23R3/42
    • A gas turbine engine (1) has a centrifugal compressor (4) and a radial turbine (14) mounted to a turbine shaft (2) for rotation with the shaft about the shaft axis Z. A number of combustion chambers (10) in the air/gas flow path between the compressor and the turbine are spaced circumferentially about the shaft axis. The combustion chambers (10) are elongate in the direction of air/gas flow and the longitudinal axis of each combustion chamber is skewed transversely relative to the axis Z of the turbine shaft. The combustion chambers (10) may be curved longitudinally about the shaft axis and may be aligned concentric about the axis. The engine may have a recuperator (8) radially outboard the compressor, the recuperator having radially directed flow passages through which air from the compressor is directed.
    • 燃气涡轮发动机（1）具有安装到涡轮轴（2）的离心式压缩机（4）和径向涡轮（14），用于与轴一起围绕轴轴线Z旋转。 在所述压缩机和所述涡轮之间的所述空气/气体流动路径中的燃烧室（10）的内部围绕所述轴线周向地间隔开。 燃烧室（10）在空气/气体流动的方向上是细长的，并且每个燃烧室的纵向轴线相对于涡轮轴的轴线Z横向地偏斜。 燃烧室（10）可以围绕轴线纵向地弯曲并且可以围绕轴线同心地对齐。 发动机可以在压缩机径向外侧具有换热器（8），换热器具有径向导向的流动通道，来自压缩机的空气通过该流动通道被导向。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 6. 发明申请
      WO2013189470A1 COMBUSTION ENGINE 审中-公开
    • COMBUSTION ENGINE
    • 内燃机
    • WO2013189470A1
    • 2013-12-27
    • PCT/CZ2013/000074
    • 2013-06-10
    • FESA s.r.o.
    • JANDA, Zdenek
    • F01D1/38 , F02C3/05 , F02C3/16
    • F01D1/38 , F02C3/05 , F02C3/16 , F05D2250/82
    • A combustion engine contains a mechanical rotor (4, 7) comprising at least one working tube (6) that is branched or unbranched, for supplying fuel into the mechanical rotor (4, 7), passing fuel through the working tube (6) and exhausting combustion products from the mechanical rotor (4, 7). The working tube (6) is spatially arranged in the mechanical rotor (4, 7) in such a way that each of its branches comprises a compressor section for compression of fuel until its ignition by the effect of the centrifugal force acting upon the fuel during rotation of the mechanical rotor (4, 7) around the rotation axis, an adjacent combustion section for burning of fuel and an expansion section, adjacent to combustion section, for expansion of fuel combustion products to reduce their pressure and temperature, where the mechanical work obtained by the expansion drives the mechanical rotor (4, 7).The combustion section is more distant from the rotation axis than the compressor section and the expansion section and each branch of the working tube (6) is, in the direction from the entrance of the working tube (6) to the mechanical rotor (4, 7), in its compression section routed in the mechanical rotor (4, 7) in such a way that besides getting farther away from the rotation axis it is also angled in or against the rotation direction of the mechanical rotor (4, 7) so that in the axial direction the part of the housing of the mechanical rotor (4, 7) that covers the combustion section can be as narrow as possible while the expansion section then returns to the rotation axis as well as to the direction of this axis.
    • 内燃机包括机械转子（4,7），该机械转子包括至少一个分支或不分支的工作管（6），用于将燃料供给机械转子（4,7），使燃料通过工作管（6）和 从机械转子（4,7）排出燃烧产物。 工作管（6）在空间上布置在机械转子（4,7）中，使得它的每个分支包括用于压缩燃料的压缩机部分，直到其通过作用在燃料上的离心力的作用而点燃 机械转子绕旋转轴线的旋转，邻近燃烧部分燃烧燃料的相邻燃烧部分和膨胀部分，用于扩展燃料燃烧产物以降低它们的压力和温度，其中机械加工 通过膨胀获得的驱动机械转子（4,7）。燃烧部分比压缩机部分更远离旋转轴线，并且工作管（6）的扩展部分和每个分支沿着从入口的方向 的工作管（6）连接到机械转子（4,7）上，在其在机械转子（4,7）中布置的压缩部分中，使得除了远离旋转轴线之外，它也是 在机械转子（4,7）的旋转方向上倾斜或抵抗机械转子（4,7）的旋转方向，使得在轴向方向上，覆盖燃烧部分的机械转子（4,7）的壳体的部分可以尽可能窄，而膨胀 部分然后返回到旋转轴以及该轴的方向。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 9. 发明申请
      WO2020041842A1 TESLA'S SUPER COMPRESSOR 审中-公开
    • TESLA'S SUPER COMPRESSOR
    • WO2020041842A1
    • 2020-03-05
    • PCT/BA2019/000001
    • 2019-08-27
    • VUJINOVIĆ, Zoran
    • VUJINOVIĆ, Zoran
    • F01D1/34 , F01D1/36 , F02C3/05
    • Tesla's super compressor belongs to the field of propulsion machinery for liquids and gases or vapors. It is based on the theoretical foundations of Tesla's concept of pump and energy transfer from a mechanical system to a fluid. The energy from the propulsion machine is transferred to the working fluid by the adhesive and viscous forces between the disks and the working fluid. The compressor itself consists of a rotor, a stator and an air tank with tubes. The technical problem has been solved by blowing the air from the rotor nozzle (8) at high speed into the air intake (7) and sucking air from the chamber (9). The energy transfer is carried out in the mixing chamber (6) and lasts until the particles equalize the energy, whereby the mixture formed is completely homogenized. In the diffuser (5), this mixture is slowed down to achieve at the end of the diffuser in the collecting duct (4) the pressure required for the operation of the device. This mixed and cooled compressed air is delivered to consumers or the central compressed air tank.
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 10. 发明申请
      WO2017212211A1 RADIAL FLOW TURBINE HEAT ENGINE 审中-公开
    • RADIAL FLOW TURBINE HEAT ENGINE
    • 径流式涡轮热力发动机
    • WO2017212211A1
    • 2017-12-14
    • PCT/GB2017/050843
    • 2017-03-24
    • HIETA TECHNOLOGIES LIMITED
    • JONES, Simon Lloyd , HISLOP, Drummond Watson , PULLEN, Keith Robert
    • F02C3/05 , F02C7/10 , F02C3/14
    • A radial flow turbine heat engine (2) includes a compressor (6), a recuperator (10), a combustor (12) and a turbine (8). A compressor outlet manifold (14) collects compressed gas from the compressor through a plurality of compressor outlets (18). A turbine inlet manifold supplies combustion gas to the turbine (8) through a plurality of turbine inlets (24). The compressor outlet manifold comprises a plurality of compressor outlet manifold ducts and the turbine inlet manifold comprises a plurality of turbine inlet manifold ducts. These manifold ducts are circumferentially interdigitated with respect of each other around the shaft (4) of the turbine to provide a flow path for compressed gas through the recuperator (10) located radially inwardly with respect to the rotation axis of the shaft compared to the flow path for the combustion gas in the hot side portion of the heat engine (2). Furthermore, a flow path for the combustion gas is provided to the turbine inlets which are radially inward with respect to the rotation axis of the shaft compared to flow paths for the compressed gas within the compressor outlet manifold (14) proximal to those turbine inlets (24).
    • 径流式涡轮机热力发动机（2）包括压缩机（6），换热器（10），燃烧器（12）和涡轮机（8）。 压缩机出口歧管（14）通过多个压缩机出口（18）从压缩机收集压缩气体。 涡轮机入口歧管通过多个涡轮机入口（24）将燃烧气体供应到涡轮机（8）。 压缩机出口歧管包括多个压缩机出口歧管导管，并且涡轮机入口歧管包括多个涡轮机入口歧管导管。 这些歧管导管在涡轮的轴（4）周围相对于彼此在周向上相互交叉指向，以提供压缩气体通过相对于轴的旋转轴线径向向内定位的回流换热器（10）的流动路径， 用于热机（2）的热侧部分中的燃烧气体的路径。 此外，相比于压缩机出口歧管（14）内靠近那些涡轮入口的压缩气体的流动路径，将燃烧气体的流动路径提供给相对于轴的旋转轴线径向向内的涡轮入口（ 24）。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
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