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    • 1. 发明授权
    • Convex sealing bottom for a twin-shaft turbine
    • 双轴涡轮机的凸形密封底部
    • US07874790B2
    • 2011-01-25
    • US11575426
    • 2005-09-14
    • Mario PecchioliDino Bianchi
    • Mario PecchioliDino Bianchi
    • F04D29/40
    • F02C7/28F01D5/08F01D9/023F01D11/00F01D25/14F01D25/145
    • Convex sealing bottom (10) for a twin-shaft turbine of the type comprising a series of convex disks constrained to each other by means of a series of pins, each disk of said disks comprises an outer shaped edge which is engaged with a corresponding annular surface (71) of an inner grooved surface (72) of a ring (70) for obtaining an axial seal.The series of disks comprises three disks, a first disk (12), a second disk (13) and a third disk (14) respectively.The three disks are fixed to each other centrally by means of a series of spokes (30) and are constrained in pairs respectively by means of a series of pins which are arranged orthogonally to the three disks to minimize the relative movements of the three disks in an axial direction at the same time allowing the radial dilatations of the three disks themselves.
    • 用于双轴涡轮机的凸密封底部(10),其包括通过一系列销彼此约束的一系列凸盘,所述盘的每个盘包括外形边缘,其与相应的环形 用于获得轴向密封的环(70)的内槽表面(72)的表面(71)。 一系列磁盘分别包括三个磁盘,第一磁盘(12),第二磁盘(13)和第三磁盘(14)。 三个磁盘通过一系列辐条(30)在中心彼此固定,并且通过与三个磁盘正交配置的一系列销对成对约束,以最小化三个磁盘的相对运动 轴向同时允许三个盘自身的径向扩张。
    • 6. 发明授权
    • Methods and systems for oil free low voltage conduits
    • 无油低压管道的方法和系统
    • US08978243B2
    • 2015-03-17
    • US13480563
    • 2012-05-25
    • Luciano MeiFabrizio FranciDino Bianchi
    • Luciano MeiFabrizio FranciDino Bianchi
    • H01R4/02F04D25/06F04D13/10F04D29/058
    • F04D25/0693F04D13/10F04D17/122F04D29/058H01R4/023H01R4/029Y10T29/49117
    • A turbomachine is provided. The turbomachine comprises a compressor, at least two magnetic bearings provided at opposite ends of a compressor shaft, a motor having a motor shaft, a first electrical cable having a first end, a second end, an internal core section and an outer sheath section with the internal core section and the outer sheath section extending from the first end to the second end, a first connector configured to connect the first end to the first magnetic bearing, wherein the first connector is welded or brazed to the first end to both the internal core section and the outer sheath section, and a second connector configured to connect the second end to the first external connection, wherein the second connector is welded or brazed to the second end to both the internal core section and the outer sheath section.
    • 提供涡轮机。 涡轮机包括压缩机,设置在压缩机轴的相对端处的至少两个磁性轴承,具有电动机轴的电动机,具有第一端部的第一电缆,第二端部,内部芯部分以及具有 所述内部芯部分和所述外部护套部分从所述第一端延伸到所述第二端;第一连接器,被配置为将所述第一端连接到所述第一磁性轴承,其中所述第一连接器被焊接或钎焊到所述第一端部, 芯部和外护套部,以及第二连接器,其被配置为将第二端连接到第一外部连接,其中第二连接器被焊接或钎焊到内芯部和外护套部的第二端。
    • 7. 发明申请
    • METHODS AND SYSTEMS FOR OIL FREE LOW VOLTAGE CONDUITS
    • 无油低压电路的方法和系统
    • US20120299412A1
    • 2012-11-29
    • US13480563
    • 2012-05-25
    • Luciano MeiFabrizio FranciDino Bianchi
    • Luciano MeiFabrizio FranciDino Bianchi
    • H02K7/09H01R43/00H02K11/00
    • F04D25/0693F04D13/10F04D17/122F04D29/058H01R4/023H01R4/029Y10T29/49117
    • A turbomachine is provided. The turbomachine comprises a compressor, at least two magnetic bearings provided at opposite ends of a compressor shaft, a motor having a motor shaft, a first electrical cable having a first end, a second end, an internal core section and an outer sheath section with the internal core section and the outer sheath section extending from the first end to the second end, a first connector configured to connect the first end to the first magnetic bearing, wherein the first connector is welded or brazed to the first end to both the internal core section and the outer sheath section, and a second connector configured to connect the second end to the first external connection, wherein the second connector is welded or brazed to the second end to both the internal core section and the outer sheath section.
    • 提供涡轮机。 涡轮机包括压缩机,设置在压缩机轴的相对端处的至少两个磁性轴承,具有电动机轴的电动机,具有第一端部的第一电缆,第二端部,内部芯部分以及具有 所述内部芯部分和所述外部护套部分从所述第一端延伸到所述第二端;第一连接器,被配置为将所述第一端连接到所述第一磁性轴承,其中所述第一连接器被焊接或钎焊到所述第一端部, 芯部和外护套部,以及第二连接器,其被配置为将第二端连接到第一外部连接,其中第二连接器被焊接或钎焊到内芯部和外护套部的第二端。
    • 8. 发明申请
    • Convex Sealing Bottom for a Twin-Shaft Turbine
    • 双轴涡轮凸轮密封底部
    • US20070257440A1
    • 2007-11-08
    • US11575426
    • 2005-09-14
    • Mario PecchioliDino Bianchi
    • Mario PecchioliDino Bianchi
    • F02F11/00
    • F02C7/28F01D5/08F01D9/023F01D11/00F01D25/14F01D25/145
    • Convex sealing bottom (10) for a twin-shaft turbine of the type comprising a series of convex disks constrained to each other by means of a series of pins, each disk of said disks comprises an outer shaped edge which is engaged with a corresponding annular surface (71) of an inner grooved surface (72) of a ring (70) for obtaining an axial seal. The series of disks comprises three disks, a first disk (12), a second disk (13) and a third disk (14) respectively. The three disks are fixed to each other centrally by means of a series of spokes (30) and are constrained in pairs respectively by means of a series of pins which are arranged orthogonally to the three disks to minimize the relative movements of the three disks in an axial direction at the same time allowing the radial dilatations of the three disks themselves.
    • 用于双轴涡轮机的凸密封底部(10),其包括通过一系列销彼此约束的一系列凸盘,所述盘的每个盘包括外形边缘,其与相应的环形 用于获得轴向密封的环(70)的内槽表面(72)的表面(71)。 一系列磁盘分别包括三个磁盘,第一磁盘(12),第二磁盘(13)和第三磁盘(14)。 三个磁盘通过一系列辐条(30)在中心彼此固定,并且通过与三个磁盘正交配置的一系列销对成对约束,以最小化三个磁盘的相对运动 轴向同时允许三个盘自身的径向扩张。