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51. 发明申请

WO2006001855A2 GAS FLOW ENHANCER FOR COMBUSTION ENGINES 审中-公开
标题翻译：用于燃烧发动机的气体流量增强器
公开(公告)号：WO2006001855A2
公开(公告)日：2006-01-05
申请号：PCT/US2005007971
申请日：2005-03-07
申请人： CUMMINGS CRAIG D
发明人： CUMMINGS CRAIG D
IPC分类号： F01D1/36
CPC分类号： F01N1/088 , F01N3/0892 , F01N3/36 , F01N3/38 , Y02T10/20
摘要： A gas flow enhancer for a combustion engine includes a housing, configured to receive an inlet flow of gas at an inlet pressure, and enclosing an expansion chamber. Disposed within the expansion chamber are a set of inner vanes and outer vanes, and a flow separator. The outer vanes are disposed outside the flow separator and produce an outer helical flow of the gas. The inner vanes are disposed within the flow separator and produce an inner helical flow of the gas, the inner helical flow having a higher velocity and lower pressure than the outer helical flow. The outer helical flow and inner helical flow are recombined at an outlet of the expansion chamber so as to produce an outlet laminar flow profile having a lower average pressure than the inlet pressure.
摘要翻译：用于燃烧发动机的气体流动增强器包括壳体，其构造成在入口压力下接纳气体的入口流，并且包围膨胀室。在膨胀室内设置有一组内叶片和外叶片以及一流分离器。外部叶片设置在流动分离器的外部并产生气体的外部螺旋流。内叶片设置在流动分离器内并产生气体的内螺旋流，内螺旋流具有比外螺旋流更高的速度和更低的压力。外螺旋流和内螺旋流在膨胀室的出口处重新组合，以产生具有比入口压力更低的平均压力的出口层流轮廓。

52. 发明申请

WO2003027444A1 DUPLEX SHEAR FORCE ROTOR 审中-公开
标题翻译：双面剪力转子
公开(公告)号：WO2003027444A1
公开(公告)日：2003-04-03
申请号：PCT/US2002/030502
申请日：2002-09-26
申请人： SHEAR FORCE, LTD.
发明人： PACELLO, John , TYBOR, Frank, J.
IPC分类号： F01D1/36
CPC分类号： F04D29/2255
摘要： A single (110) or multi-stage (510) centrifugal pump or mixer duplex shear force rotor consisting of two non-parallel shrouds (17, 18). The driven shroud (18) contains a center opening (19). The rotor has an open, unobstructed entrance section (7) and includes a protrusion (22) designed to force-feed the discharge section in a smooth laminar flow pattern. The discharge section incorporates a series of raised ribs (1). The raised ribs (1) begin at the peripheral edge (28) of the shrouds (17, 18) and extend to approximately 50 % of the distance from the peripheral edge towards the center of the rotor (32). Cast-in place spacers (23) space the drive (17) and driven (18) shrouds. Alternatively, the rotor (710) can include no raised ribs. In addition, the raised ribs (812, 814) can have a cross-section that includes a tapered trailing edge to reduce wear. Alternatively, neither the drive (617) nor driven (618) shrouds are perpendicular to the axis of rotation (42).
摘要翻译：由两个非平行罩（17,18）组成的单（110）或多级（510）离心泵或混合器双相剪切力转子。从动护罩（18）包含一个中心开口（19）。转子具有开放的，无障碍的入口部分（7），并且包括设计成以平滑层流模式强制供给排出部分的突出部（22）。排放部分包括一系列凸起的肋（1）。升高的肋（1）从护罩（17,18）的周边边缘（28）开始并且延伸到从周向边缘朝向转子（32）的中心的距离的大约50％。嵌入式垫片（23）将驱动器（17）和驱动（18）护罩空间。或者，转子（710）可以不包括凸起肋。此外，凸起的肋（812,814）可以具有包括锥形后缘的横截面以减少磨损。或者，驱动器（617）或驱动（618）护罩都不垂直于旋转轴线（42）。

53. 发明申请

WO02055883A2 TURBO-MOLECULAR PUMP HAVING ENHANCED PUMPING CAPACITY 审中-公开
标题翻译：具有增强泵送能力的涡轮分子泵
公开(公告)号：WO02055883A2
公开(公告)日：2002-07-18
申请号：PCT/US2001/048903
申请日：2001-12-13
IPC分类号： F04D19/04 , F01D1/36 , F04D19/00
CPC分类号： F01D1/36 , F04D19/042
摘要： In one aspect, a vacuum processing system comprising a vacuum processing chamber and a turbo-molecular pump disposed on the vacuum processing chamber is provided. The turbo-molecular pump comprises a casing having an inlet port and an outlet port, a stator disposed on an inner wall of the casing, a rotor disposed in the stator, and a motor extending coaxially with the rotor, wherein at least the first stage of the pump is enlarged with no correspondingly larger pump components other than the corresponding upper portion of the housing.
摘要翻译：在一个方面，提供一种真空处理系统，其包括真空处理室和设置在真空处理室上的涡轮分子泵。涡轮分子泵包括具有入口和出口的壳体，设置在壳体的内壁上的定子，设置在定子中的转子和与转子同轴地延伸的电动机，其中至少第一级的泵被扩大，没有相应较大的泵构件而不是壳体的相应上部。

54. 发明申请

WO02004788A1 TURBINE, POWER GENERATION SYSTEM THEREFOR AND METHOD OF POWER GENERATION 审中-公开
标题翻译：发电机，发电系统及其发电方法
公开(公告)号：WO02004788A1
公开(公告)日：2002-01-17
申请号：PCT/AU2001/000813
申请日：2001-07-06
IPC分类号： F01D1/36 , F01D15/00 , F25B11/00 , F25B27/00 , F25B40/00 , H01L35/00 , F01D1/08 , F01D5/04 , F01D9/02 , F01D17/14
CPC分类号： F01D15/005 , F01D1/36 , F05D2210/14 , F25B11/00 , F25B27/00 , F25B40/00 , H01L35/00
摘要： A turbine includes a rotor (2) rotatable within a rotor chamber including a plurality of blades (5) about its periphery. Drag surfaces are created by the plurality of disc surfaces in the rotor (2), five discs being shown, and these receive a working fluid which is caused to flow spirally towards a central aperture (7) in the rotor (2). The working fluid may be provided at hypersonic or lower speeds and may be provided by a fuel burning means. A thermoelectric generator utilising the turbine is also disclosed.
摘要翻译：涡轮机包括在包括围绕其周边的多个叶片（5）的转子室内可旋转的转子（2）。通过转子（2）中的多个盘表面产生拖动表面，示出了五个盘，并且这些盘接收工作流体，螺旋地朝向转子（2）中的中心孔（7）流动。工作流体可以以超音速或低速提供，并且可以由燃料燃烧装置提供。还公开了一种利用涡轮机的热电发电机。

55. 发明申请

WO00042292A1 SEPARATION APPARATUS COMPRISING A FRICTION MACHINE 审中-公开
标题翻译：包含摩擦机的分离装置
公开(公告)号：WO00042292A1
公开(公告)日：2000-07-20
申请号：PCT/CA2000/000014
申请日：2000-01-06
IPC分类号： A47L5/22 , A47L9/10 , A47L9/16 , B01D45/14 , B01D47/16 , B04C9/00 , F01D1/36 , F04D17/16
CPC分类号： F04D17/161 , A47L5/22 , A47L9/122 , A47L9/16 , A47L9/1625 , A47L9/1641 , A47L9/1666 , B01D45/14 , B01D47/16 , B04C9/00 , B04C2009/004 , F01D1/36
摘要： A prandtl layer turbine has a longitudinally extending housing (14) having a fluid inlet port (60); a plurality of spaced apart members (12) rotatably mounted in the housing to transmit motive force between fluid introduced through the fluid inlet port and the members and to separate the fluid into at least two fluid streams; and, a fluid outlet port positioned on the housing for receiving each fluid stream. The prandtl layer turbine may be used in conjunction with a cyclone separator (94, 96) either to provide the motive force to draw a fluid through the cyclone separator or to both provide the motive force and to provide a second stage separation. The cyclone separator and turbine may be housed in a vacuum cleaner. A fan may be provided to assist in fluid flow through the turbine. Two turbines may be connected together whereby a first fluid is used to drive the first turbine and the first turbine is used to drive the second turbine which in turn provides motive force to a second fluid.
摘要翻译：普朗特层涡轮机具有具有流体入口（60）的纵向延伸的壳体（14）; 多个间隔开的构件（12），可旋转地安装在壳体中以在通过流体入口端口引入的流体和构件之间传递动力并将流体分离成至少两个流体流; 以及定位在所述壳体上用于接收每个流体流的流体出口。普朗特层涡轮机可以与旋风分离器（94,96）一起使用，以提供通过旋风分离器抽取流体的动力或者提供动力并提供第二级分离。旋风分离器和涡轮可以容纳在真空吸尘器中。可以提供风扇以帮助流体流过涡轮机。两个涡轮机可以连接在一起，由此使用第一流体来驱动第一涡轮机，并且第一涡轮机用于驱动第二涡轮机，而涡轮机又向第二流体提供动力。

56. 发明申请

WO2020093952A1 一种斜击式针状涡轮审中-公开
公开(公告)号：WO2020093952A1
公开(公告)日：2020-05-14
申请号：PCT/CN2019/115121
申请日：2019-11-01
申请人：时剑
发明人：时剑
IPC分类号： F01D1/36 , F03B5/00
摘要：一种斜击式针状涡轮，包括喷嘴（3），壳体（2）和盘状转子（1），其中，盘状转子（1）上密集地布满针状突起（6），盘状转子（1）的圆周上有环形挡墙（8），喷嘴（3）的喷气方向与盘状转子（1）的盘面呈5至45度夹角。

57. 发明申请

WO2020002702A1 SCHEIBENLÄUFERTURBINE, VERFAHREN ZUM BETRIEB EINER SCHEIBENLÄUFERTURBINE, EINRICHTUNG ZUR UMWANDLUNG THERMISCHER ENERGIE IN MECHANISCHE ENERGIE, VERFAHREN ZUR UMWANDLUNG THERMISCHER ENERGIE IN MECHANISCHE ENERGIE SOWIE VERFAHREN ZUR UMWANDLUNG THERMISCHER ENERGIE IN ELEKTRISCHE ENERGIE 审中-公开
公开(公告)号：WO2020002702A1
公开(公告)日：2020-01-02
申请号：PCT/EP2019/067570
申请日：2019-07-01
申请人： ERK ECKROHRKESSEL GMBH
发明人： HELLWIG, Udo
IPC分类号： F03G7/00 , F01D1/36
摘要： Die Erfindung betrifft eine Scheibenläuferturbine (10) zur Umwandlung der Enthalpie eines Gasvolumenstroms (17) in mechanische Energie, sowie ein Verfahren zum Betrieb der erfindungsgemäßen Scheibenläuferturbine (10). Ferner betrifft die Erfindung eine Einrichtung zur Umwandlung thermischer Energie in mechanische Energie sowie ein Verfahren zur Umwandlung thermischer Energie in mechanische Energie und ein Verfahren zur Umwandlung thermischer Energie in elektrische Energie. Dabei umfasst die Scheibenläuferturbine (10) wenigstens eine auf einer Rotationsachse (50) angeordnete Scheibe (11), welche bei im Wesentlichen tangentialer Anströmung mit einem Gasvolumenstrom (17) in Rotation versetzbar ist, sodass mechanische Energie an einer mit der Scheibe (11) gekoppelten Welle (51) abnehmbar ist. Dabei weist ein die Scheibe (11) ausbildende Scheibenkörper (13) zumindest einen Hohlraum (14) auf, in dem zwecks Kühlung des Scheibenkörpers (13) ein Kühlmedium (16), insbesondere eine Kühlflüssigkeit, aufgenommen oder aufnehmbar ist. Ferner weist die Scheibenläuferturbine (10) wenigstens einen Gasaufnahmeraum (12) zur Aufnahme und Ausbringung des zumindest teilweise tangential die Scheibe (11) anströmenden Gasvolumenstroms (17) auf.

58. 发明申请

WO2018184078A3 TESLA THREEE PHASE HYBRID ROTARY INTERNAL COMBUSTION ENGINE 审中-公开
公开(公告)号：WO2018184078A3
公开(公告)日：2018-10-11
申请号：PCT/BA2018/000001
申请日：2018-04-02
申请人： VUJINOVIĆ, Zoran
发明人： VUJINOVIĆ, Zoran
IPC分类号： F01D1/36 , F23R3/00
摘要： Tesla's three-phase hybrid rotary internal combustion engine is based on theoretical essentials of Tesla's concept of internal combustion engines and the principles of transforming kinetic fluid energy into mechanical work applied on Tesla's turbine. The technical field is Mechanical engineering. It is positioned on a completely new so-called three-phased phase of currents and usage of fluid energy into mechanical work with reversible thermo-dynamic processes relied on one energetic releaser (23). It is thermically isolated (19), without sliding surfaces, it does not use motor oil, it has two bearing-supported movable engine parts, outer shaft (24) and exhaust valve (12). It is projected in a way that it can use waste heat for work on the outer shaft. It can work as an internal combustion engine, as pneumatic engine or combined. The usage of aggregates is possible in every field of appliance, with a great strength range, on earth, water or air.

59. 发明申请

WO2018047018A3 BOUNDARY LAYER TURBOMACHINE 审中-公开
公开(公告)号：WO2018047018A3
公开(公告)日：2018-03-15
申请号：PCT/IB2017/001528
申请日：2017-09-08
申请人： GREEN FROG TURBINES (UK) LIMITED
发明人： JONES, Mark, W. , HELTON, Billy, W.
IPC分类号： F01D1/36
摘要： A boundary layer turbomachine can include a housing (10) defining an interior space and having an inlet opening and an outlet opening to facilitate movement of a fluid through the housing (10). The boundary layer turbomachine can also include a rotor assembly (20) disposed in the rotor chamber and configured to rotate about an axis of rotation (1). The rotor assembly (20) can have a plurality of disks (21) spaced apart along the axis of rotation (1) to provide gaps (54) between the disks (21). The plurality of disks (21) can also define an interior opening (26) along the axis of rotation (1). The rotor assembly (20) can have a disk carrier (46) disposed at least partially in the interior opening (26) in support of the plurality of disks (21). The disk carrier (46) can have a fluid passageway (47) exposed to two or more of the gaps (54) between the disks (21). The fluid can pass through gaps (54) between the disks (21) and the interior opening (26) as the fluid moves through the housing (10).

60. 发明申请

WO2018047018A2 BOUNDARY LAYER TURBOMACHINE 审中-公开
标题翻译：边界层涡轮机
公开(公告)号：WO2018047018A2
公开(公告)日：2018-03-15
申请号：PCT/IB2017/001528
申请日：2017-09-08
申请人： GREEN FROG TURBINES (UK) LIMITED
发明人： JONES, Mark, W. , HELTON, Billy, W.
IPC分类号： F01D1/36
摘要： A boundary layer turbomachine can include a housing (10) defining an interior space and having an inlet opening and an outlet opening to facilitate movement of a fluid through the housing (10). The boundary layer turbomachine can also include a rotor assembly (20) disposed in the rotor chamber and configured to rotate about an axis of rotation (1). The rotor assembly (20) can have a plurality of disks (21) spaced apart along the axis of rotation (1) to provide gaps (54) between the disks (21). The plurality of disks (21) can also define an interior opening (26) along the axis of rotation (1). The rotor assembly (20) can have a disk carrier (46) disposed at least partially in the interior opening (26) in support of the plurality of disks (21). The disk carrier (46) can have a fluid passageway (47) exposed to two or more of the gaps (54) between the disks (21). The fluid can pass through gaps (54) between the disks (21) and the interior opening (26) as the fluid moves through the housing (10).
摘要翻译：边界层涡轮机械可包括限定内部空间并具有入口开口和出口开口的外壳（10），以促进流体通过外壳（10）的移动。边界层涡轮机还可以包括布置在转子室中并且构造成围绕旋转轴线（1）旋转的转子组件（20）。转子组件（20）可具有多个沿旋转轴线（1）间隔开的圆盘（21），以在圆盘（21）之间提供间隙（54）。多个盘（21）也可以限定沿旋转轴线（1）的内部开口（26）。转子组件（20）可以具有至少部分地设置在内部开口（26）中以支撑多个盘（21）的盘载体（46）。盘架（46）可具有暴露于盘（21）之间的两个或更多个间隙（54）的流体通路（47）。随着流体移动通过壳体（10），流体可以穿过圆盘（21）和内部开口（26）之间的间隙（54）。

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