公开(公告)号：US09828861B2

公开(公告)日：2017-11-28

申请号：US14428706

申请日：2013-09-17

申请人： SNECMA ,  HERAKLES

发明人： Son Le Hong

IPC分类号： F01D5/28 ,  F01D5/30 ,  F01D11/00 ,  F01D5/14

CPC分类号： F01D5/282 ,  F01D5/147 ,  F01D5/3038 ,  F01D5/3084 ,  F01D11/008 ,  F05D2220/30 ,  F05D2230/30 ,  F05D2230/60 ,  F05D2240/24 ,  F05D2300/20 ,  F05D2300/2261 ,  F05D2300/437 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

摘要： A turbine engine blade made of composite material including fiber reinforcement obtained by three dimensionally weaving yarns and densified with a matrix, the blade including an airfoil and a blade root forming a single part. The blade root includes two opposite lateral flanks that are substantially plane and that are clamped between two independent pads made of composite material, which pads are fastened against the lateral flanks of the blade root to form a blade root that is bulb-shaped.

公开(公告)号：US09765637B2

公开(公告)日：2017-09-19

申请号：US14466044

申请日：2014-08-22

申请人： SNECMA

发明人： Damien Merlot ,  Remi Sers

IPC分类号： F01D5/30 ,  F01D5/12 ,  F01D5/14 ,  F01D11/00 ,  F01D5/34 ,  F01D5/02

CPC分类号： F01D5/3069 ,  F01D5/021 ,  F01D5/12 ,  F01D5/143 ,  F01D5/3038 ,  F01D5/3061 ,  F01D5/34 ,  F01D11/008 ,  F05D2220/323 ,  F05D2240/24 ,  Y02T50/671 ,  Y02T50/673

摘要： An assembly for an aircraft turbine engine including an integral element including a disk and a plurality of blades is provided. Each blade has a connection zone connecting the blade to the disk, the connection zone including a first part arranged at the external flowpath delimitation surface provided on the disk, and at least one second end part arranged at a recess formed in the disk along the axial extension of the external surface, the average fillet radius defined by the second end part being larger than the fillet radius defined by the first part. The assembly further includes a flowpath reconstruction part formed in the aerodynamic continuity of the external surface, so as to cover the recess.

公开(公告)号：US09695698B2

公开(公告)日：2017-07-04

申请号：US14451690

申请日：2014-08-05

申请人： ROLLS-ROYCE PLC

发明人： Mark John Knight

IPC分类号： F01D5/30 ,  F01D5/14 ,  F01D11/16

CPC分类号： F01D5/3038 ,  F01D5/141 ,  F01D5/30 ,  F01D11/16 ,  F05D2230/60 ,  F05D2240/24 ,  F05D2240/30

摘要： A turbomachine aerofoil blade has an aerofoil body portion and a dovetail root fixing at the base of the aerofoil body portion which slides, in use, into a correspondingly shaped slot of a rotor of the turbomachine. The dovetail root fixing has a neck portion, and support flanks engage with matching angled surfaces of the slot under centrifugal loading of the aerofoil blade to support the aerofoil blade on the rotor. The neck portion is shaped such that a rotational adjustment of the aerofoil blade relative to its angular position when supported under centrifugal loading is needed to provide adequate clearance at the neck portion to allow the dovetail root fixing to slide into the slot. On centrifugal loading the engagement of the support flanks with the matching angled surfaces of the slot forces a reversal of the rotational adjustment and reduces the clearance at the neck portion.

公开(公告)号：US09689271B2

公开(公告)日：2017-06-27

申请号：US14118436

申请日：2012-05-14

申请人： Luc Henri Chatenet ,  John Le Quellec

发明人： Luc Henri Chatenet ,  John Le Quellec

IPC分类号： F01D5/32 ,  F01D5/30 ,  F04D29/02 ,  F04D29/32 ,  B23P15/00

CPC分类号： F01D5/326 ,  B23P15/006 ,  F01D5/3038 ,  F01D5/3092 ,  F01D5/323 ,  F04D29/023 ,  F04D29/322 ,  F05D2260/30 ,  F05D2300/505 ,  Y02T50/671 ,  Y10T29/49332

摘要： A turbine engine rotor wheel including a disk including at least one slot formed in its outer periphery for mounting roots of blades, a presser being mounted between each blade root and a bottom of the slot. The presser is bistable in position and is capable of occupying a first stable position for assembly and disassembly in which it does not exert a force on the blade root, and a second stable position in which it exerts a radial force on the blade root to hold the blade stationary and to stabilize the blade in a final position.

公开(公告)号：US20170002669A1

公开(公告)日：2017-01-05

申请号：US15113062

申请日：2014-11-03

申请人： General Electric Technology GmbH

发明人： Jaroslaw Leszek SZWEDOWICZ ,  Andreas BAUER ,  Jonas BOETTCHER ,  Marcus NEUBAUER

IPC分类号： F01D5/30 ,  F01D25/24 ,  F01D9/04

CPC分类号： F01D5/3038 ,  F01D9/042 ,  F01D11/008 ,  F01D25/246 ,  F05D2220/32 ,  F05D2260/30 ,  F05D2300/171 ,  F05D2300/501 ,  F05D2300/505 ,  F05D2300/603

摘要： A mechanical fastening system for rotating or stationary components such as turbine or compressor blades on a rotor or a shaft or a casing, respectively, is disclosed. The system includes a circumferential mounting groove adapted for receiving root sections of the rotating or stationary components as well as intermediate fastening components for fixation of the components in equidistance positions. The intermediate fastening components comprise at least an upper platform and at least a side plate having a groove for mounting on said rotor. The intermediate fastening components are made of a plurality of distinct parts of different materials from which at least one clamping part is made of or comprises a shape memory alloy or similar material having a pseudo-elasticity behavior.

摘要翻译： 公开了一种用于分别在转子或轴或壳体上的旋转或静止部件如涡轮机或压缩机叶片的机械紧固系统。 该系统包括适于容纳旋转或静止部件的根部的圆周安装凹槽以及用于将部件固定在等距位置的中间紧固部件。 中间紧固部件包括至少一个上部平台和至少一个具有用于安装在所述转子上的凹槽的侧板。 中间紧固部件由不同材料的多个不同部分制成，至少一个夹紧部分由其形成或包括具有假弹性行为的形状记忆合金或类似材料。

公开(公告)号：US09382805B2

公开(公告)日：2016-07-05

申请号：US13751810

申请日：2013-01-28

申请人： ROLLS-ROYCE PLC

发明人： Alexander Lewis Shaw

IPC分类号： F01D5/30 ,  F04D29/32 ,  F01D5/02 ,  F04D29/66

CPC分类号： F01D5/30 ,  F01D5/027 ,  F01D5/303 ,  F01D5/3038 ,  F04D29/321 ,  F04D29/662 ,  Y10T29/49316

摘要： A balanced rotor comprising a circumferential slot and a plurality of aerofoils each secured in the slot by a respective root, the root having a root block having circumferentially facing flanks and a seal wing extending circumferentially from one of the flanks, characterized in that the seal wing has a notch engaging a balance weight positioned between adjacent roots.

摘要翻译： 平衡转子，其包括周向狭槽和多个翼型件，每个翼型件分别通过相应的根部固定在所述槽中，所述根部具有根部块，所述根部具有周向面向的侧面和从所述侧面中的一个周向延伸的密封翼，其特征在于，所述密封翼 具有接合位于相邻根之间的平衡重的凹口。

公开(公告)号：US09382801B2

公开(公告)日：2016-07-05

申请号：US14190759

申请日：2014-02-26

申请人： General Electric Company

发明人： Paul James Cassidy ,  Engelbert John Paauwe ,  Michael James Tessier

IPC分类号： F01D5/32 ,  F01D5/00 ,  F01D5/30 ,  F01D25/28

CPC分类号： F01D5/005 ,  F01D5/3038 ,  F01D5/32 ,  F01D25/285 ,  F05D2230/68 ,  Y10T29/49318

摘要： A method of removing a bucket from a turbomachine rotor wheel includes exposing a base portion of the bucket, positioning a pulling device radially outwardly of the base portion, connecting the base portion of the bucket to the pulling device through a linking rod, exerting an axially outwardly directed force on the linking rod through the pulling device, and removing the base portion from the rotor wheel.

摘要翻译： 从涡轮机转子轮移除铲斗的方法包括使铲斗的基座部分露出，将拉动装置定位在基部的径向外侧，通过连杆将铲斗的基部连接到牵引装置， 通过拉动装置在连杆上产生向外的力，以及从转子轮移除基部。

公开(公告)号：US09341071B2

公开(公告)日：2016-05-17

申请号：US14055124

申请日：2013-10-16

申请人： General Electric Company

发明人： Michael James Healy ,  Brian Denver Potter

IPC分类号： F01D5/30 ,  F01D5/32

CPC分类号： F01D5/303 ,  F01D5/3038 ,  F01D5/32

摘要： Locking spacer assemblies and turbomachines are provided. In one embodiment, a locking spacer assembly includes a spacer, the spacer including a platform and a plurality of legs extending generally radially inward from the platform. The locking spacer assembly further includes a clamp configured to contact and cause elastic deformation of each of the plurality of legs in a generally axial direction towards each other. The locking spacer assembly further includes a locking lug configured to contact and impart a force against each of the plurality of legs in an opposite generally axial direction.

摘要翻译： 提供了锁定间隔件组件和涡轮机。 在一个实施例中，锁定间隔件组件包括间隔件，间隔件包括平台和从平台大致径向向内延伸的多个腿。 锁定间隔件组件还包括夹具，该夹具构造成使多个腿中的每一个在大致轴向方向上彼此接触并引起弹性变形。 锁定间隔件组件还包括锁定凸耳，所述锁定凸耳构造成在相反的大致轴向方向上接触并向所述多个支腿中的每一个施加力。

公开(公告)号：US20160084260A1

公开(公告)日：2016-03-24

申请号：US14830367

申请日：2015-08-19

申请人： ROLLS-ROYCE PLC

发明人： Paul Dennis CLARKE

IPC分类号： F04D29/32

CPC分类号： F04D29/323 ,  F01D5/3007 ,  F01D5/303 ,  F01D5/3038 ,  F04D29/324 ,  F05D2250/70

摘要： A compressor disc for a compressor of a gas turbine engine includes a circumferentially extending groove for receiving blade roots of a plurality of compressor blades. The circumferentially extending groove includes a planar surface offset into the groove.

摘要翻译： 一种用于燃气涡轮发动机的压缩机的压缩机盘包括用于容纳多个压缩机叶片的叶片根部的周向延伸的槽。 周向延伸的凹槽包括偏移到凹槽中的平坦表面。

公开(公告)号：US09255483B2

公开(公告)日：2016-02-09

申请号：US13668996

申请日：2012-11-05

申请人： General Electric Company

发明人： Thomas Joseph Farineau ,  Timothy Scott McMurray

IPC分类号： F03B3/12 ,  F01D5/30 ,  F01D5/32 ,  F01D5/22

CPC分类号： F01D5/3038 ,  F01D5/225 ,  F01D5/32

摘要： A locking blade for a rotor can include an airfoil portion with a root from which a tongue extends. Opposed bucket segments can engage the tongue and can be retained in a longitudinal direction of the blade by a fastener, such as a pin, that can extend through holes in the segments and tongue. Tines parallel to and on opposite sides of the tongue can extend from the root and include holes through which the fastener can extend, the bucket segments extending between respective tines and the tongue. The structure can eliminate an assembly gate in a rotor.

摘要翻译： 用于转子的锁定刀片可以包括具有舌部的根部的翼型部分。 相对的铲斗段可以接合舌部并且可以通过诸如销的紧固件保持在刀片的纵向方向上，该紧固件可以延伸穿过节段和舌头中的孔。 舌头平行于舌片和相对侧上的齿可以从根部延伸，并且包括紧固件可以延伸穿过的孔，铲斗段在相应的尖齿和舌部之间延伸。 该结构可以消除转子中的组装门。