公开(公告)号：US20180313217A1

公开(公告)日：2018-11-01

申请号：US15953524

申请日：2018-04-16

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

发明人： Jae Min Ju ,  Seok Jin Jang

IPC分类号： F01D5/30 ,  F01D5/32

CPC分类号： F01D5/3046 ,  F01D5/32 ,  F05D2260/30

摘要： A rotatable body includes a rotor and n buckets, each bucket being coupled to the rotor in a tangential entry manner. The rotor supports each of the n buckets coupled to the rotor, so the buckets may be stably coupled to the rotor, using a unified annular dovetail tenon that protrudes axially from the rotor. Each bucket includes a bucket dovetail mortise for engaging with the unified annular dovetail tenon in order to couple the bucket to the rotor. A method of manufacturing the rotatable body includes assembling first to (n−1)th buckets with the rotor wheel by successively inserting the first to (n−1)th buckets through the tangential entry; assembling the nth bucket with the adapter; assembling the adapter with the rotor wheel, by inserting the adapter assembled with the nth bucket into the tangential entry; and collectively moving all the buckets by one half pitch in the circumferential direction.

公开(公告)号：US09828866B2

公开(公告)日：2017-11-28

申请号：US14068544

申请日：2013-10-31

申请人： General Electric Company

发明人： David Orus Fitts ,  David Robert Schumacher ,  Laurence Scott Duclos ,  Anand Aravindrao Kulkarni ,  David Bruce Knorr

IPC分类号： F01D9/04 ,  F01D5/30 ,  F01D5/32

CPC分类号： F01D9/042 ,  F01D5/3046 ,  F01D5/32 ,  Y10T29/49321

摘要： A nozzle assembly includes at least one stationary nozzle and an outer ring having a predefined shape. The outer ring includes at least one groove defined therein configured to receive at least a portion of the at least one stationary nozzle. The nozzle assembly also includes an attachment member coupled between the stationary nozzle and the outer ring. The attachment member has a first configuration at a first nozzle assembly operating temperature a second configuration at a second nozzle assembly operating temperature.

公开(公告)号：US09422818B2

公开(公告)日：2016-08-23

申请号：US13698208

申请日：2011-06-21

申请人： Stephane Pierre Guillaume Blanchard ,  Laurent Pierre Joseph Ricou

发明人： Stephane Pierre Guillaume Blanchard ,  Laurent Pierre Joseph Ricou

IPC分类号： F01D5/30 ,  F01D5/28

CPC分类号： F01D5/3023 ,  F01D5/282 ,  F01D5/3046 ,  F01D5/3053 ,  F01D5/3069 ,  F05D2250/25 ,  Y02T50/672

摘要： A rotor wheel for a gas turbine engine, the wheel including: a metal holder disk including a plurality of teeth at its periphery, the teeth extending radially outwards from the disk; a plurality of composite material blades, each blade including a root engaged between two adjacent teeth of the holder disk and that is held against the teeth by a pivot connection; a clamp disk including a plurality of teeth at its periphery extending in an axial direction, the clamp disk being fastened against the holder disk and on the same axis, with each of its teeth taking up a circumferential position between a blade root and a tooth of the holder disk; and a mechanism exerting a clamping force in a circumferential direction urging the teeth of the clamp disk against the blade roots.

摘要翻译： 一种用于燃气涡轮发动机的转子轮，所述转轮包括：在其周边包括多个齿的金属保持盘，所述齿从所述盘径向向外延伸; 多个复合材料叶片，每个叶片包括接合在保持器盘的两个相邻齿之间的根部，并且通过枢转连接而保持抵靠齿; 夹持盘在其周边沿轴向延伸的多个齿，夹紧盘紧固在保持盘上并在相同的轴线上，其每个齿处于叶片根部与牙齿之间的圆周位置 保持盘; 以及在圆周方向上施加夹紧力的机构，其推动夹紧盘的齿抵靠叶片根部。

公开(公告)号：US20150040580A1

公开(公告)日：2015-02-12

申请号：US13963425

申请日：2013-08-09

申请人： General Electric Company

发明人： John Herbert Dimmick, III

IPC分类号： F04D29/32

CPC分类号： F04D29/322 ,  F01D5/303 ,  F01D5/3038 ,  F01D5/3046 ,  F02C3/04 ,  F02C3/055 ,  F02C3/06

摘要： A compressor blade mounting arrangement includes a compressor blade having an airfoil, a base attachment and a platform disposed between the airfoil and the base attachment. The base attachment includes a first root portion extending radially inwardly from the platform and a second root portion extending radially inwardly from the platform, the first root portion and the second root portion defining a hollow portion therebetween. The base attachment also includes a compression plate disposed within the hollow portion and in fitted engagement with the first root portion and the second root portion. The base portion further includes at least one tab protruding from at least one of the first root portion and the second root portion. The compressor blade mounting arrangement also includes a wheel including a channel extending from a base wall to a rim of the wheel, the channel having a varying opening width.

摘要翻译： 压缩机叶片安装装置包括具有翼型件的压缩机叶片，底座附件和设置在翼型件和底座附件之间的平台。 基座附件包括从平台径向向内延伸的第一根部部分和从平台径向向内延伸的第二根部部分，第一根部部分和第二根部部分在其间限定中空部分。 基座附件还包括设置在中空部分内并与第一根部部分和第二根部部分配合接合的压缩板。 基部还包括从第一根部部分和第二根部部分中的至少一个突出的至少一个突出部。 压缩机叶片安装装置还包括轮，该轮包括从底壁延伸到轮的轮缘的通道，该通道具有变化的开口宽度。

公开(公告)号：US20140271146A1

公开(公告)日：2014-09-18

申请号：US14184780

申请日：2014-02-20

申请人： DOUGLAS JAMES DIETRICH ,  KEVIN DAMIAN CARPENTER

发明人： DOUGLAS JAMES DIETRICH ,  KEVIN DAMIAN CARPENTER

IPC分类号： F04D29/64 ,  F04D29/08

CPC分类号： F04D29/644 ,  F01D5/3046 ,  F01D5/32 ,  F04D29/083 ,  F04D29/542 ,  Y10T29/49236

摘要： The present invention relates to a system and method for joining adjacent sections of a compressor diaphragm. A splitline jumper is positioned within a recessed portion of a seal ring segment of the adjacent compressor diaphragms. The splitline jumper is sized and oriented so as to prevent axial movement of the compressor diaphragms relative to each other and also to prevent rotational movement of the seal ring relative to the diaphragm.

摘要翻译： 本发明涉及一种用于连接压缩机隔膜的相邻部分的系统和方法。 分流跳线定位在相邻压缩机隔膜的密封环段的凹陷部分内。 分流式跳线的尺寸和取向是为了防止压缩机隔膜相对于彼此的轴向移动，并且还防止密封环相对于隔膜的旋转运动。

公开(公告)号：US20140219803A1

公开(公告)日：2014-08-07

申请号：US14168530

申请日：2014-01-30

申请人： Techspace Aero S.A.

发明人： Christophe Remy

IPC分类号： F01D5/06

CPC分类号： F01D5/066 ,  F01D5/02 ,  F01D5/06 ,  F01D5/3046 ,  F01D11/02 ,  F01D11/122 ,  F05D2250/38

摘要： The present application relates to the compressor drum of an axial turbomachine. The drum includes a wall of revolution that forms a hollow body. The wall includes two annular retaining surfaces of the blades which mate with corresponding retaining surfaces of the said blades. These surfaces are generally directed away from one another to form a profile which diverges as its distance radially from the outer surface of the wall increases. The retaining surfaces of the drum may be formed on an outer annular body or on inclined annular flanges.

摘要翻译： 本申请涉及轴向涡轮机的压缩机鼓。 鼓包括形成中空体的革命的墙壁。 该墙壁包括叶片的两个环形保持表面，其与所述叶片的对应的保持表面配合。 这些表面通常相互指向，以形成其距离壁的外表面径向延伸的距离增大的分布。 滚筒的保持表面可以形成在外部环形体上或倾斜的环形凸缘上。

公开(公告)号：US08662852B2

公开(公告)日：2014-03-04

申请号：US12909376

申请日：2010-10-21

申请人： Prashant Bhokardole ,  Prasad Mishrikotkar

发明人： Prashant Bhokardole ,  Prasad Mishrikotkar

IPC分类号： F04D29/34

CPC分类号： F01D5/3046 ,  F01D5/3007 ,  F01D5/3023 ,  F01D5/3053 ,  F05D2260/30

摘要： An arrangement and a method for mounting articulated turbine buckets in axial entry slots of rotor wheels. A curvature on a vertical plane may be incorporated on an axial male dovetail projection of the bucket root and the associated axial female dovetail slot of the rotor wheel. The curvature facilitates loading of buckets otherwise precluded by interferences, such as interlocking tip shrouds on adjacent buckets. Such loading may be provided by locating the shroud tip shroud in proximity to an adjacent tip shroud and pivoting the root end of the bucket around the location of the tip shroud such that the arc formed by the bucket allows the curvature of the axial male dovetail projection to swing into the axial female dovetail slot of the rotor wheel.

摘要翻译： 将铰接的涡轮机叶片安装在转子轮的轴向入口槽中的布置和方法。 垂直平面上的曲率可以结合在铲斗根部的轴向凸形燕尾形突起和转子轮的相关联的轴向雌性燕尾槽上。 曲率有利于装载铲斗，否则不会受到干扰，例如相邻铲斗上的互锁尖端护罩。 这种装载可以通过将护罩末端护罩定位在邻近的顶部护罩附近并使铲斗的根部端部围绕尖端护罩的位置枢转来提供，使得由铲斗形成的电弧允许轴向阳性燕尾形突起 摆动到转子轮的轴向雌性燕尾槽中。

公开(公告)号：US08651820B2

公开(公告)日：2014-02-18

申请号：US12836031

申请日：2010-07-14

申请人： Dmitriy Victorovich Krikunov ,  Amir Mujezinovic

发明人： Dmitriy Victorovich Krikunov ,  Amir Mujezinovic

IPC分类号： F01D5/30

CPC分类号： F01D5/3007 ,  F01D5/3023 ,  F01D5/303 ,  F01D5/3046 ,  F05D2250/231 ,  F05D2250/232

摘要： Swivel dovetail connections, such as a tangential entry, straight axial entry or curved axial entry dovetails, for connecting a blade and a rotor wheel in a turbomachine are disclosed. A modified shape of dovetail contact surfaces creates a swivel dovetail connection between blades and rotor wheels, and allows limited motion of blades relative to wheels, while still maintaining the structural connection between blades and wheels. The swivel dovetail connection is achieved by providing concave or convex dovetail contact surfaces between a rotor wheel and a blade such that the contact surfaces lie along a common substantially toroidal arc, an axially extending, substantially cylindrical arc, or a substantially frusto-conical arc.

摘要翻译： 公开了旋转燕尾连接，例如切向入口，直的轴向入口或弯曲的轴向入口燕尾，用于连接涡轮机中的叶片和转子轮。 燕尾形接触表面的改进形状在叶片和转子轮之间产生旋转燕尾连接，并允许叶片相对于轮子的有限运动，同时仍保持叶片和轮子之间的结构连接。 旋转燕尾连接通过在转子轮和叶片之间提供凹形或凸形的燕尾接触表面来实现，使得接触表面沿着共同的基本上环形的弧形，轴向延伸的大致圆柱形的弧形或基本截头圆锥形的弧形。

公开(公告)号：US20120301314A1

公开(公告)日：2012-11-29

申请号：US13116188

申请日：2011-05-26

申请人： Ioannis Alvanos ,  Gabriel L. Suciu ,  Christopher M. Dye ,  Glenn Levasseur

发明人： Ioannis Alvanos ,  Gabriel L. Suciu ,  Christopher M. Dye ,  Glenn Levasseur

IPC分类号： F01D5/14

CPC分类号： F01D5/3046 ,  C04B37/00 ,  C04B2235/5244 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/76 ,  F01D5/225 ,  F01D5/282 ,  F01D5/284 ,  F05D2240/12 ,  F05D2300/6033

摘要： A Ceramic Matrix Composite (CMC) airfoil for a gas turbine engine includes a CMC root section which extends to form a CMC airfoil section, the CMC root section defines a bore along a non-linear axis.

摘要翻译： 用于燃气涡轮发动机的陶瓷基体复合材料（CMC）翼型件包括延伸以形成CMC翼型部分的CMC根部，CMC根部沿着非线性轴线限定孔。

公开(公告)号：US08100657B2

公开(公告)日：2012-01-24

申请号：US12205941

申请日：2008-09-08

申请人： Muhammad Saqib Riaz ,  Qingxuan Michael Zhang

发明人： Muhammad Saqib Riaz ,  Qingxuan Michael Zhang

IPC分类号： B64C11/04

CPC分类号： F01D5/3046 ,  F01D5/225 ,  F05D2220/31 ,  F05D2250/314

摘要： A steam turbine rotating blade for a low pressure section of a steam turbine engine is disclosed. The steam turbine rotating blade includes an airfoil portion. A root section is attached to one end of the airfoil portion. A dovetail section projects from the root section, wherein the dovetail section includes a tangential entry dovetail. A tip section is attached to the airfoil portion at an end opposite from the root section. A cover is integrally formed as part of the tip section. The blade includes an exit annulus area of about 18.1 ft2 (1.68 m2) or greater.

摘要翻译： 公开了一种用于蒸汽涡轮发动机的低压部分的汽轮机旋转叶片。 蒸汽轮机旋转叶片包括翼型部分。 根部附接到翼型部分的一端。 燕尾部从根部突出，其中燕尾部包括切向进入燕尾。 尖端部分在与根部相对的端部处附接到翼型部分。 一体形成为顶端部分的一部分。 叶片包括约18.1ft2（1.68m2）或更大的出口环面积。