公开(公告)号：US20180320547A1

公开(公告)日：2018-11-08

申请号：US15969895

申请日：2018-05-03

申请人： ROLLS-ROYCE plc

发明人： Martin T. BENTLEY ,  Stephen J. BENDALL

IPC分类号： F01D25/12 ,  F16C3/02

CPC分类号： F01D25/12 ,  F05D2220/32 ,  F05D2240/61 ,  F05D2260/20 ,  F16C3/02 ,  F16C2360/23

摘要： A shaft (21) for use as a rotating shaft in a gas turbine engine has an axis (X), an outer surface, an inner surface (28), an upstream end and a downstream end. The shaft (21) is arranged, in use, to rotate in a circumferential direction (R) about the axis (X). The inner surface (28) includes a radially inwardly protruding flange (22), a circumferential array of radially extending apertures (26) provided in the flange (22) and an array of channels (24) extending from an upstream side to a downstream side of the flange (22). The channels arranged circumferentially between adjacent apertures (26) of the circumferential array of apertures (26).

公开(公告)号：US20180320543A1

公开(公告)日：2018-11-08

申请号：US16002620

申请日：2018-06-07

申请人： Jay HASKIN

发明人： Jay HASKIN

IPC分类号： F01D15/12 ,  F01D5/22 ,  F01D25/16 ,  F01D25/24 ,  F04D25/02

CPC分类号： F01D15/12 ,  F01D5/225 ,  F01D25/162 ,  F01D25/24 ,  F04D25/02 ,  F05D2220/32 ,  F05D2220/40 ,  F05D2240/14 ,  F05D2240/50 ,  F05D2240/61 ,  F05D2260/4031

摘要： A power transmission system for use with a turbine, a turbocharger, or a compressor has a housing, a first shaft mounted within the housing, a second shaft rotatably mounted within the housing and positioned exterior of the first shaft, a second set of blades affixed to the first shaft, and a second set of blades affixed to the second shaft. The first set of blades is positioned adjacent to the second set of blades. The first set of blades are rotatable in a direction opposite to the second shaft and the second set of blades. A shroud is affixed to an outer periphery of one of the sets of blades so as to have a portion overlying at least a portion of an outer periphery of the other of the first and second sets of blades. A power receiver is driven by the second shaft so as to convert rotational energy of the second shaft into energy or motion.

公开(公告)号：US10082037B2

公开(公告)日：2018-09-25

申请号：US14874831

申请日：2015-10-05

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Gideon Venter

IPC分类号： F01D11/00 ,  F01D25/16 ,  F01D25/18 ,  F01D3/04 ,  F01D11/02 ,  F01D11/04 ,  F02C7/28

CPC分类号： F01D11/005 ,  F01D3/04 ,  F01D11/02 ,  F01D11/04 ,  F01D25/16 ,  F01D25/162 ,  F01D25/183 ,  F02C7/28 ,  F05D2220/32 ,  F05D2240/50 ,  F05D2240/52 ,  F05D2240/55 ,  F05D2240/56 ,  F05D2240/57 ,  F05D2240/61 ,  F05D2260/15 ,  F05D2270/3015

摘要： The present invention describes a gas turbine having two shafts, which are rotatably mounted using bearing devices in the area of a casing. An intermediate shaft sealing device is arranged between the bearing devices, which includes a sealing element connected to a first shaft, in which a further sealing element connected to the second shaft radially engages. An operating pressure is applied, in the area limited by the shafts in the axial direction of the shafts, to facing effective areas of the sealing elements, while the pressure prevailing in the area outside the shafts in the axial direction acts on effective areas of the sealing elements facing away from one another. A ratio between the outer diameters limiting the facing effective areas and the inner diameters likewise limiting these effective areas is in each case greater than or equal to 1.25.

公开(公告)号：US20180266274A1

公开(公告)日：2018-09-20

申请号：US15458305

申请日：2017-03-14

申请人： PRATT & WHITNEY CANADA CORP.

发明人： Ian A. MACFARLANE

IPC分类号： F01D25/16 ,  F01D25/18 ,  F16C19/26 ,  F16C27/04

CPC分类号： F01D25/16 ,  F01D25/164 ,  F01D25/18 ,  F05D2220/32 ,  F05D2240/61 ,  F16C19/26 ,  F16C27/045 ,  F16C33/6659 ,  F16C2360/23

摘要： A sleeve is provided for supplying lubricant to an inter-shaft bearing mounted between co-axially mounted inner and outer shafts of a gas turbine engine. The sleeve has a sleeve annular outer surface and a sleeve annular inner surface. At least one lubricant supply connecting member extends from the sleeve outer surface for connection to a lubricant supply. At least one sleeve channel fluidly links the sleeve annular inner surface to the lubricant supply connecting member.

公开(公告)号：US20170107822A1

公开(公告)日：2017-04-20

申请号：US15293618

申请日：2016-10-14

申请人： DOOSAN HEAVY INDUSTRIES CONSTRUCTION CO., LTD.

发明人： Kyung Kook KIM

IPC分类号： F01D5/08 ,  F04D29/58 ,  F04D29/32

CPC分类号： F01D5/085 ,  F01D5/026 ,  F01D5/08 ,  F01D25/12 ,  F02C7/18 ,  F04D29/321 ,  F04D29/582 ,  F05D2220/32 ,  F05D2240/61 ,  F05D2260/20

摘要： Disclosed herein is a cooling apparatus of a gas turbine including a compressor disk unit mounted in a gas turbine and provided with compressor cooling passages; the torque tube units provided in an adhering state to each other while being adjacent to the compressor disk unit and provided with a cooling air supply passage communicating with the compressor disk cooling passage; and a turbine disk unit provided with a turbine disk cooling passage communicating with the cooling air supply passage of the torque tube unit, in which the torque tube units are disposed between the compressor disk unit and the turbine disk unit and coupled therewith in an adhering state to each other along an axial direction of a rotation shaft mounted in the gas turbine and the cooling air supply passage is open in horizontal direction along the axial direction from an edge of the torque tube unit.

公开(公告)号：US20160376890A1

公开(公告)日：2016-12-29

申请号：US15259218

申请日：2016-09-08

申请人： Kabushiki Kaisha Toshiba

发明人： Asako INOMATA ,  Iwataro SATO ,  Hideyuki MAEDA ,  Satoru SEKINE ,  Kazutaka TSURUTA ,  Takeo SUGA

IPC分类号： F01D5/08 ,  F01D5/06

CPC分类号： F01D5/08 ,  F01D5/06 ,  F01D5/063 ,  F01D5/081 ,  F01D5/085 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/61 ,  F05D2260/20 ,  F05D2270/3062

摘要： A turbine 10 includes: a turbine rotor having a rotor main body including a hollow part into which a cooling fluid flows, and a plurality of rotor wheels arranged in an axial direction of the rotor main body and protruding from the rotor main body. A cooling-fluid introducing passage extending from the hollow part in a direction intersecting with the axial direction of the rotor main body is formed in the rotor main body so as to allow the cooling fluid in the hollow part to flow through the cooling-fluid introducing passage and then to flow around the rotor wheel to be conducted to the working-fluid flow passage. A flow-rate control plug regulating a flow rate of the cooling fluid flowing through the cooling-fluid introducing passage is disposed in the cooling-fluid introducing passage.

摘要翻译： 涡轮10包括：涡轮转子，具有转子主体，该转子主体包括冷却流体流过的中空部分，以及沿转子主体的轴向布置并从转子主体突出的多个转子轮。 在与转子主体的轴向交叉的方向上从中空部延伸的冷却流体导入通道形成在转子主体中，以使中空部分中的冷却流体流过冷却流体导入 通过，然后围绕转子轮流动以被传导到工作流体流动通道。 调节冷却流体导入通道的冷却流体的流量的流量控制插头配置在冷却流体导入通路内。

公开(公告)号：US09322293B2

公开(公告)日：2016-04-26

申请号：US13636802

申请日：2011-03-28

申请人： Michel Gilbert Roland Brault ,  Philippe Pierre Vincent Bouiller

发明人： Michel Gilbert Roland Brault ,  Philippe Pierre Vincent Bouiller

IPC分类号： F01D25/18 ,  F16L37/14 ,  F16L21/08

CPC分类号： F01D25/18 ,  F05D2230/64 ,  F05D2230/642 ,  F05D2240/61 ,  F05D2260/30 ,  F05D2260/602 ,  F05D2260/6022 ,  F16L21/08 ,  F16L37/14 ,  Y10T29/49826

摘要： A venting pipe used to guide a gas stream in a turbojet including at least one hollow rotary shaft inside which the pipe is mounted, the pipe extending generally along an axis. The pipe includes at least two pipe segments configured to be aligned longitudinally and assembled to one another while retaining a degree of freedom in relative translation thereof, at least one of the segments including a deformable mechanism configured to deform radially as the pipe segments are tightened against one another in the shaft of the turbojet, to bear on the shaft. The pipe structure facilitates mounting of the pipe.

摘要翻译： 用于引导涡轮喷气机中的气流的排气管，其包括至少一个中空旋转轴，管内安装有管，管通常沿轴线延伸。 管道包括至少两个管段，其构造成纵向对齐并且彼此组装，同时保持其相对平移的自由度，所述段中的至少一个包括可变形机构，所述可变形机构构造成随着管段被紧固而径向变形 在涡轮喷气发动机的轴上彼此相依，承担在轴上。 管道结构便于安装管道。

公开(公告)号：US20160097292A1

公开(公告)日：2016-04-07

申请号：US14874831

申请日：2015-10-05

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Gideon VENTER

IPC分类号： F01D11/00 ,  F01D25/18 ,  F01D25/16

CPC分类号： F01D11/005 ,  F01D3/04 ,  F01D11/02 ,  F01D11/04 ,  F01D25/16 ,  F01D25/162 ,  F01D25/183 ,  F02C7/28 ,  F05D2220/32 ,  F05D2240/50 ,  F05D2240/52 ,  F05D2240/55 ,  F05D2240/56 ,  F05D2240/57 ,  F05D2240/61 ,  F05D2260/15 ,  F05D2270/3015

摘要： The present invention describes a gas turbine having two shafts, which are rotatably mounted using bearing devices in the area of a casing. An intermediate shaft sealing device is arranged between the bearing devices, which includes a sealing element connected to a first shaft, in which a further sealing element connected to the second shaft radially engages. An operating pressure is applied, in the area limited by the shafts in the axial direction of the shafts, to facing effective areas of the sealing elements, while the pressure prevailing in the area outside the shafts in the axial direction acts on effective areas of the sealing elements facing away from one another. A ratio between the outer diameters limiting the facing effective areas and the inner diameters likewise limiting these effective areas is in each case greater than or equal to 1.25.

摘要翻译： 本发明描述了一种具有两个轴的燃气轮机，它们使用轴承装置可旋转地安装在壳体的区域中。 中间轴密封装置设置在轴承装置之间，其包括连接到第一轴的密封元件，其中连接到第二轴的另一个密封元件径向接合。 在轴的轴向限制的区域中施加操作压力，以面对密封元件的有效区域，而在轴向方向外侧的区域中的压力作用在有效区域上 密封元件彼此背离。 限制面对有效面积的外径与同样限制这些有效面积的内径之间的比率在每种情况下大于或等于1.25。

公开(公告)号：US09217463B2

公开(公告)日：2015-12-22

申请号：US14076834

申请日：2013-11-11

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Ruediger Oessenich ,  Andreas Freund ,  Mirko Filler ,  Ole Renner ,  Alexander Pabst

IPC分类号： F16C3/00 ,  F16C3/02 ,  F01D5/06 ,  F01D5/28

CPC分类号： F16C3/026 ,  B29C70/462 ,  F01D5/06 ,  F01D5/282 ,  F05D2240/61 ,  F05D2300/603 ,  F05D2300/6034 ,  F05D2300/614 ,  F16C2360/23 ,  Y02T50/672 ,  Y02T50/673

摘要： A radial shaft of a gas-turbine engine which is made up of +/−45° layers, zero layers and +/−30° layers of carbon fiber composite and connected to load-input end pieces via sinusoidal connecting areas.

摘要翻译： 燃气涡轮发动机的径向轴，其由+/- 45°层，零层和+/- 30°层的碳纤维复合材料组成并通过正弦连接区域连接到负载输入端部件。

公开(公告)号：US20150330243A1

公开(公告)日：2015-11-19

申请号：US14760894

申请日：2013-12-12

申请人： SNECMA

发明人： Jonathan Boris BAPTISTA

IPC分类号： F01D11/00 ,  F16J15/44

CPC分类号： F01D11/003 ,  F05D2240/55 ,  F05D2240/58 ,  F05D2240/60 ,  F05D2240/61 ,  F05D2250/14 ,  F05D2250/36 ,  F16J15/44

摘要： A sealing device for sealing between coaxial shafts of a turbomachine, the sealing device including an elastic ring having a circular central opening allowing a sliding connection with an internal shaft, an external surface configured to engage with an internal surface of a portion of an external shaft, two retaining components situated one on either side of the elastic ring and allowing the elastic ring an axial clearance, wherein the elastic ring is a profile section.

摘要翻译： 一种用于在涡轮机的同轴轴之间进行密封的密封装置，所述密封装置包括具有允许与内轴滑动连接的圆形中心开口的弹性环，外表面构造成与外轴的一部分的内表面接合 ，两个保持部件位于弹性环的任一侧上，并且允许弹性环具有轴向间隙，其中弹性环是轮廓部分。