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1. 发明申请

US20180036831A1 METHOD OF JOINING BY ELECTRON BEAM OR LASER WELDING A TURBOCHARGER TURBINE WHEEL TO A SHAFT; CORRESPONDING TURBOCHARGER TURBINE WHEEL 审中-公开
公开(公告)号：US20180036831A1
公开(公告)日：2018-02-08
申请号：US15549286
申请日：2016-01-22
申请人： BorgWarner Inc.
发明人： Silvio KOCH , Stefan EISINGER
IPC分类号： B23K15/00 , F01D5/06 , F01D5/02 , B23K26/28 , B23K26/32
CPC分类号： B23K15/0053 , B23K15/0093 , B23K26/28 , B23K26/282 , B23K26/32 , B23K33/006 , B23K33/008 , B23K2101/001 , B23K2101/003 , B23K2101/006 , F01D5/025 , F01D5/063 , F05D2220/40 , F05D2230/233 , F05D2230/234 , F16D1/027
摘要： A turbocharger wheel (4) and shaft (1) assembly exhibits a frustoconical geometry of welding zone contact surfaces extending to the outer circumference of the shaft (1). This frustoconical geometry not only allows continuous centering of the parts (1, 4) during joining, it also eliminates the problem of stress propagation along a plane. The location of the electron beam is shifted so that only the radially outer segment of the frustoconical contact surface is joined by welding, leaving a radially inner unmelted and unfused zone for maintaining firm contact of the oblique surfaces.

2. 发明授权

US09797256B2 Turbine rotor 有权
公开(公告)号：US09797256B2
公开(公告)日：2017-10-24
申请号：US14380603
申请日：2013-02-26
申请人： MITSUBISHI HEAVY INDUSTRIES, LTD.
发明人： Hitomi Otsubo , Takashi Arai , Motoki Ebisu
IPC分类号： F01D5/02 , B23K15/00 , B23K26/70 , C21D9/50 , F01D5/06 , C21D9/00 , B23K101/00 , C21D1/09 , C21D1/30
CPC分类号： F01D5/025 , B23K15/0006 , B23K15/0026 , B23K15/0053 , B23K26/702 , B23K2101/001 , C21D1/09 , C21D1/30 , C21D9/0068 , C21D9/50 , F01D5/063 , F05D2220/40 , F05D2230/234 , F05D2230/40 , F05D2240/60
摘要： To provide a turbine rotor which enables mass production with a low-cost apparatus and which capable of suppressing leaning of the rotor shaft after welding to improve the yield, while a turbine blade rotor 12 and the rotor shaft 14 are fit to each other with concave and convex portions 12a and 14a and are permitted to be rotated, laser beam L from a laser beam generating device 30 is applied to a joint face 16 along the circumferential direction to weld the welding portion. Then, laser beam L is polarized to temper a region X on the rotor shaft side containing the welding portion with laser beam L. In contrast to residual stress R1 having a local angular distribution generated during the welding, residual stress R2 is permitted to be generated over the entire circumference by tempering. Leaning of the rotor shaft 14 after cooling is thereby be suppressed.

3. 发明授权

US09784110B2 Steam turbine rotor 有权
公开(公告)号：US09784110B2
公开(公告)日：2017-10-10
申请号：US14453782
申请日：2014-08-07
申请人： Mitsubishi Hitachi Power Systems, Ltd.
发明人： Kunio Asai , Masahiko Arai , Kenichi Murata
IPC分类号： F01D5/06 , C22C38/08 , C22C38/18
CPC分类号： F01D5/063 , C22C38/001 , C22C38/08 , C22C38/18 , C22C38/44 , C22C38/46 , C22C38/48 , F05D2220/31 , F05D2230/235 , F05D2300/171 , F05D2300/175 , F05D2300/177
摘要： It is an objective of the invention to provide a steam turbine rotor that is capable of both reducing SCC susceptibility and improving LCF life thereof. There is provided a steam turbine rotor, comprising a rotor disk in a low pressure final stage L-0, and another rotor disk in a plurality of stages including a stage L-1 positioned closer to a high pressure side than the low pressure final stage L-0, the rotor disk in the low pressure final stage L-0 and the rotor disk in a plurality of stages including the stage L-1 being joined by welding, wherein a material of both the rotor disk in the low pressure final stage L-0 and the rotor disk in a plurality of stages including the stage L-1 is a 12Cr steel and has a tensile strength of 900 to 1200 MPa.

4. 发明申请

US20160376890A1 TURBINE 审中-公开
标题翻译：涡轮
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。

5. 发明授权

US09388697B2 First stage compressor disk configured for balancing the compressor rotor assembly 有权
标题翻译：用于平衡压缩机转子组件的第一级压缩机盘
公开(公告)号：US09388697B2
公开(公告)日：2016-07-12
申请号：US13551517
申请日：2012-07-17
申请人： Dover M. Fernandez , Cory Patrick Muscat , Gary Paul Vavrek , James Eric Miller
发明人： Dover M. Fernandez , Cory Patrick Muscat , Gary Paul Vavrek , James Eric Miller
IPC分类号： F01D5/02 , F01D5/06
CPC分类号： F01D5/027 , F01D5/063 , Y10T29/49321
摘要： A first stage compressor disk of a gas turbine engine includes a body. The body includes a forward end, an aft end, and an outer surface. The body also includes a plurality of forward balancing holes through the outer surface. The forward balancing holes align circumferentially about the body. The body further includes a plurality of aft balancing holes through the outer surface. The aft balancing holes align circumferentially about the body and are located aft of the forward balancing holes. The first stage compressor disk also includes a radial flange at the aft end of the body. The radial flange extends radially outward from the body. The radial flange includes slots for mounting airfoils.
摘要翻译：燃气涡轮发动机的第一级压缩机盘包括主体。主体包括前端，后端和外表面。主体还包括穿过外表面的多个前平衡孔。前向平衡孔围绕身体圆周对准。主体还包括穿过外表面的多个后平衡孔。后平衡孔沿着本体周向对准并位于前平衡孔的后方。第一级压缩机盘片还包括在身体后端的径向凸缘。径向凸缘从主体径向向外延伸。径向凸缘包括用于安装翼型件的槽。

6. 发明申请

US20160076377A1 TURBOCHARGER SHAFT AND WHEEL ASSEMBLY 有权
标题翻译：涡轮增压器轴和轮组件
公开(公告)号：US20160076377A1
公开(公告)日：2016-03-17
申请号：US14488067
申请日：2014-09-16
申请人： Honeywell International Inc.
发明人： Brent ZOLLINGER , Maurizio BARBONE , Didier HORLAVILLE , Andrei MINCULESCU , Nicolas VAZEILLE
IPC分类号： F01D5/06 , F02C6/12
CPC分类号： F01D5/063 , B23K26/032 , B23K26/034 , B23K26/044 , B23K26/0619 , B23K26/123 , B23K26/28 , B23K2101/001 , B23K2103/04 , B23K2103/26 , F01D5/025 , F02C6/12 , F05D2220/40 , F05D2230/232
摘要： A unit for a turbocharger can include a turbine wheel portion that includes a turbine wheel material and a turbine wheel axis; a shaft portion that includes a shaft material and a shaft axis where the shaft material includes a molybdenum content less than 0.5 percent by weight; and a weld that includes a nail shape in cross-section where a head portion of the nail shape includes an axial dimension of approximately 1 mm or less and wherein a shank portion of the nail shape includes an axial dimension of approximately 0.4 mm or less.
摘要翻译：用于涡轮增压器的单元可以包括涡轮机叶轮部分，其包括涡轮机叶轮材料和涡轮机叶轮轴线; 轴部，其包括轴材料和轴线，其中所述轴材料包含小于0.5重量％的钼含量; 以及焊钉，其包括指甲形状的横截面，其中指甲形状的头部包括大约1mm或更小的轴向尺寸，并且其中指甲形状的柄部分包括大约0.4mm或更小的轴向尺寸。

7. 发明申请

US20150306713A1 A METHOD OF FABRICATING A ROTOR OF A TURBOFAN ENGINE 审中-公开
标题翻译：一种制造涡轮发动机转子的方法
公开(公告)号：US20150306713A1
公开(公告)日：2015-10-29
申请号：US14646801
申请日：2013-12-02
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Steve A. McLeod , Daryl A. Baker
IPC分类号： B23P15/00 , F01D5/02
CPC分类号： B23P15/006 , F01D5/02 , F01D5/026 , F01D5/063 , F05D2220/30 , F05D2230/00 , F05D2230/10 , F05D2230/233 , F05D2230/60
摘要： A method of fabricating a disk assembly for a turbofan engine is disclosed and includes the steps of forming a first and second disk and welding the second disk to the first disk to form a weld joint. A portion of the first disk and the second disk are removed along the weld joint on at least one surface to reduce a size of a heat affected zone and substantially reduce possible formation of material inconsistencies.
摘要翻译：公开了一种制造用于涡轮风扇发动机的盘组件的方法，包括形成第一和第二盘并将第二盘焊接到第一盘以形成焊接接头的步骤。第一盘和第二盘的一部分沿着至少一个表面上的焊接接头去除以减小热影响区域的尺寸并且基本上减少材料不一致的可能形成。

8. 发明申请

US20150267542A1 ROTOR SHAFT WITH COOLING BORE INLETS 审中-公开
标题翻译：带冷却孔的转子轴
公开(公告)号：US20150267542A1
公开(公告)日：2015-09-24
申请号：US14661220
申请日：2015-03-18
申请人： ALSTOM Technology Ltd.
发明人： Steffen Holzhaeuser , Carlos Simon-Delgado , Carl Berger
IPC分类号： F01D5/18 , F01D25/12 , F01D5/02
CPC分类号： F01D5/18 , F01D5/02 , F01D5/063 , F01D5/087 , F01D25/12 , F05D2220/31 , F05D2220/32 , F05D2230/10 , F05D2240/60 , F05D2260/232 , F05D2260/941
摘要： The invention relates to a rotor shaft adapted to rotate about a rotor axis thereof. The rotor shaft includes a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft, and a plurality of cooling bores extending radially or quasi-radially outward from the inside to an outside of the rotor shaft. Each cooling bore having a bore inlet location and a distal bore outlet portion, the respective bore inlet location being adapted to abut on the rotor cavity. At least one side or part-side of the cooling bore inlet location is provided with an asymmetric edge fillet in order to maximize the wall thickness between two adjacent cooling bores.
摘要翻译：本发明涉及适于围绕其转子轴线旋转的转子轴。转子轴包括与转子轴内的转子轴同心或准同心配置的转子腔，以及从转子轴的内侧向外径向或半径向外延伸的多个冷却孔。每个冷却孔具有孔入口位置和远端孔出口部分，相应的孔入口位置适于邻接转子腔。冷却孔入口位置的至少一侧或部分侧设置有不对称边缘，以使两个相邻冷却孔之间的壁厚最大化。

9. 发明授权

US09039365B2 Rotor, a steam turbine and a method for producing a rotor 有权
标题翻译：转子，汽轮机和转子的制造方法
公开(公告)号：US09039365B2
公开(公告)日：2015-05-26
申请号：US13344677
申请日：2012-01-06
申请人： Thomas Joseph Farineau , Robin Carl Schwant
发明人： Thomas Joseph Farineau , Robin Carl Schwant
IPC分类号： F01D5/02 , F01D5/06
CPC分类号： F01D5/06 , F01D5/022 , F01D5/023 , F01D5/026 , F01D5/063 , Y10T29/49327
摘要： A rotor, a steam turbine having a rotor, and a method of producing a rotor are disclosed. The rotor disclosed includes a shaft high pressure section. The high pressure section includes a first high pressure section, a second high pressure section, the second high pressure section being joined to the first pressure section, and a third high pressure section, the third high pressure section being joined to the second high pressure section. At least a portion of the second high pressure section is formed of a high-chromium alloy steel comprising 0.1-1.2 wt % of Mn, up to 1.5 wt % of Ni, 8.0-15.0 wt % of Cr, up to 4.0 wt % of Co, 0.5-3.0 wt % of Mo, 0.05-1.0 wt % of V, 0.02-0.5 wt % of Nb, 0.005-0.15 wt % of N, up to 0.04 wt % of B, up to 3.0 wt % of W, and balance Fe and incidental impurities.
摘要翻译：公开了一种转子，具有转子的汽轮机和制造转子的方法。所公开的转子包括轴高压部分。高压部包括第一高压部，第二高压部，与第一压力部接合的第二高压部和第三高压部，第三高压部与第二高压部接合。第二高压部分的至少一部分由高铬合金钢形成，其包含0.1-1.2重量％的Mn，至多1.5重量％的Ni，8.0-15.0重量％的Cr，至多4.0重量％的 Co，0.5-3.0重量％的Mo，0.05-1.0重量％的V，0.02-0.5重量％的Nb，0.005-0.15重量％的N，至多0.04重量％的B，至多3.0重量％的W，并平衡Fe和杂质。

10. 发明授权

US08932012B2 Reduced monobloc multistage drum of axial compressor 有权
标题翻译：减少轴向压缩机的整体多级鼓
公开(公告)号：US08932012B2
公开(公告)日：2015-01-13
申请号：US13045115
申请日：2011-03-10
申请人： Michel Wlasowski
发明人： Michel Wlasowski
IPC分类号： F04D29/54 , F01D5/34 , F01D5/06 , F01D5/30 , F04D29/053 , F04D29/32
CPC分类号： F01D5/34 , F01D5/063 , F01D5/3061 , F04D29/053 , F04D29/321 , F04D29/329
摘要： An axial turbomachine compressor drum rotor stage includes an axis of rotation, a wall generally symmetrical in revolution about the axis of rotation. The wall forms a hollow body and includes a veil and an annular area integrally formed with the veil for supporting a row of vanes. The annular area includes a central part raised in relation to that of the veil.
摘要翻译：轴向涡轮机压缩机鼓转子级包括旋转轴线，围绕旋转轴线大致对称的壁。壁形成中空体，其包括面纱和与面纱一体形成的用于支撑一排叶片的环形区域。环形区域包括相对于面纱的中心部分凸起的中心部分。

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