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1. 发明授权

EP3068976B1 BLADE WEDGE ATTACHMENT LAY-UP 有权转让
公开(公告)号：EP3068976B1
公开(公告)日：2018-11-21
申请号：EP14854284.8
申请日：2014-09-26
申请人： United Technologies Corporation
发明人： LUCZAK, Blake J.
IPC分类号： F01D5/32 , F01D5/28
CPC分类号： F01D5/3007 , F01D5/147 , F01D5/282 , F01D5/288 , F01D5/3092 , F01D5/32 , F01D5/323 , F01D5/326 , F05D2220/32 , F05D2260/30 , F05D2300/6032
摘要： A blade for a gas turbine engine includes composite layers including neck plies and tooth plies that are flared relative to the neck plies. The neck plies and tooth plies respectively provide a neck and a root. The root includes a tooth. A Wedge is provided by wedge plies adhered over the root and the tooth.

2. 发明授权

EP2687729B1 ROTOR STRUCTURE 有权转让
公开(公告)号：EP2687729B1
公开(公告)日：2018-09-12
申请号：EP12757839.1
申请日：2012-01-31
申请人： Mitsubishi Hitachi Power Systems, Ltd.
发明人： HIRATA, Tomoyuki , HIROKAWA, Kazuharu , TAKAOKA, Yoshimasa
IPC分类号： F04D29/34 , F01D5/30
CPC分类号： F04D29/322 , F01D5/3038 , F01D5/32
摘要： This rotor structure (R c ) is provided with: a rotation shaft body (10) in which a blade groove (11) extending in the circumferential direction of the axis is formed on an outer circumference section (10A) which rotates around said axis, and in which the width dimension of the blade groove (11) on the side of a groove opening (11a) is less than the width dimension of the blade groove (11) on the side of the groove bottom (11b); and multiple blade bodies arrayed in the circumferential direction on the outer circumference section (10A) of the rotation shaft body (10), wherein each of the blade bodies has a blade base fitted into the blade groove (11). A blade retaining piece (30) is provided positioned between at least one pair of two blade bodies neighboring in the aforementioned circumferential direction in the blade groove (11). Protrusions (33d, 33d) are formed on either the blade retaining piece (30), or on an opening wall portion (13, 13) of the blade groove (11) on the side of the groove opening (11a), and depressions (14, 14) engaging with said protrusion (33d, 33d) are formed on the other of said blade retaining piece (30) or said opening wall portion (13, 13).

3. 发明授权

EP3167163B1 RADSCHEIBENANORDNUNG 有权
公开(公告)号：EP3167163B1
公开(公告)日：2018-07-11
申请号：EP15778914.0
申请日：2015-10-08
申请人： Siemens Aktiengesellschaft
发明人： HOELL, Harald , KAMPKA, Kevin , KOLK, Karsten , LANGE, Marc , SCHRÖDER, Peter , VEITSMAN, Vyacheslav
IPC分类号： F01D5/30
CPC分类号： F01D11/006 , F01D5/02 , F01D5/3015 , F01D5/32 , F05D2220/32 , F05D2230/64 , F05D2260/30 , F05D2260/36

4. 发明公开

EP3239040A1 PROPELLER BLADES 有权转让
标题翻译：螺旋桨叶片
公开(公告)号：EP3239040A1
公开(公告)日：2017-11-01
申请号：EP16305487.7
申请日：2016-04-27
申请人： Ratier-Figeac
发明人： Andrzejewski, Arnaud , Delmas, Catherine , Seminel, Bruno
IPC分类号： B64C11/04
CPC分类号： F01D5/32 , B64C11/04 , F01D5/02 , F01D5/12 , F05D2230/60 , F05D2300/121 , F05D2300/43
摘要： A propeller blade assembly comprises a propeller blade (2) having a blade root (6) for attaching the propeller blade (2) to a hub (8). The blade root (6) has a radially outer surface (32). The assembly further comprises a collar (14) mounted to the blade root (6). The collar (14) comprises at least two collar segments (20, 22) assembled around the radially outer surface (32) of the blade root (6). Each collar segment (20, 22) has a radially inner surface (26, 30), an opposed radially outward surface (24, 28) and first and second circumferential end lugs (36, 38, 42, 44). The lugs (36, 38, 42, 44) receive fasteners (48) for coupling the collar segments (20, 22) together to form the collar (14). The collar segments (20, 22) are formed from a flexible plastics material and the radially inner surface (26, 30) of each collar segments (20, 22) engages the radially outer surface (32) of the blade root (6) only over a limited circumferential extent of the collar segment (30, 32).
摘要翻译：一种螺旋桨叶片组件包括螺旋桨叶片（2），该螺旋桨叶片具有用于将螺旋桨叶片（2）连接到轮毂（8）的叶片根部（6）。叶根（6）具有径向外表面（32）。该组件还包括安装到叶片根部（6）的轴环（14）。套环（14）包括围绕叶根（6）的径向外表面（32）组装的至少两个套环段（20,22）。每个套环段（20,22）具有径向内表面（26,30），相对的径向向外表面（24,28）以及第一和第二圆周端凸耳（36,38,42,44）。凸耳（36,38,42,44）接收紧固件（48），用于将套环段（20,22）连接在一起以形成套环（14）。轴环段（20,22）由柔性塑料材料形成，并且每个轴环段（20,22）的径向内表面（26,30）仅接合叶片根部（6）的径向外表面（32）在轴环段（30,32）的有限的周向范围内。

5. 发明公开

EP3225786A2 LOAD ABSORPTION SYSTEMS AND METHODS 审中-公开
标题翻译：负载吸收系统和方法
公开(公告)号：EP3225786A2
公开(公告)日：2017-10-04
申请号：EP17153922.4
申请日：2017-01-31
申请人： General Electric Company
发明人： BISHOP, Michael Jason , KELKAR, Rajendra Madhukar , YUEN, Alex , WOODFIELD, Andrew Philip
IPC分类号： F01D11/24 , F01D5/32
CPC分类号： F04D29/34 , B22F3/04 , B22F3/1055 , B22F3/15 , B22F3/225 , B22F5/009 , B33Y80/00 , F01D5/3007 , F01D5/3015 , F01D5/32 , F01D5/323 , F01D5/326 , F02K3/06 , F04D29/322 , F04D29/329 , F05D2220/323 , F05D2220/36 , F05D2230/31 , F05D2250/283 , F05D2260/30 , F05D2300/133 , Y02T50/671 , Y02T50/673
摘要： A load absorbing system that may include a rotor blade retention system (52) is provided. The load absorbing system may include a block (56), a first retainer plate (62A), and a deformable core (54). The block (56) may be selectively positioned alongside a dovetail groove (50). The block (56) may have a first face (66) directed away from the blade root (44) and an axially-spaced second face (68) directed toward the blade root (44). The first retainer plate (62A) may be attached to the second face (68) of the block (56) and axially positioned between the block (56) and the axially-directed surface of the blade root (44). The deformable core (54) may be positioned between the block (56) and the first retainer plate (62A).
摘要翻译：提供了一种可包括转子叶片保持系统（52）的负载吸收系统。负载吸收系统可以包括块体（56），第一保持板（62A）和可变形芯体（54）。块（56）可以选择性地与燕尾槽（50）并排放置。块56可以具有远离叶片根部44的第一面66和朝向叶片根44的轴向间隔开的第二面68。第一保持板（62A）可以附接到块体（56）的第二面（68）并且轴向定位在块体（56）和叶根（44）的轴向指向的表面之间。可变形芯部（54）可以定位在块体（56）和第一保持板（62A）之间。

6. 发明公开

EP3068976A4 BLADE WEDGE ATTACHMENT LAY-UP 有权转让
标题翻译： AUFLAGEFÜRKLINGENKEILBEFESTIGUNG
公开(公告)号：EP3068976A4
公开(公告)日：2017-08-23
申请号：EP14854284
申请日：2014-09-26
申请人： UNITED TECHNOLOGIES CORP
发明人： LUCZAK BLAKE J
IPC分类号： F01D5/32 , F01D5/28
CPC分类号： F01D5/3007 , F01D5/147 , F01D5/282 , F01D5/288 , F01D5/3092 , F01D5/32 , F01D5/323 , F01D5/326 , F05D2220/32 , F05D2260/30 , F05D2300/6032
摘要： A blade for a gas turbine engine includes composite layers including neck plies and tooth plies that are flared relative to the neck plies. The neck plies and tooth plies respectively provide a neck and a root. The root includes a tooth. A Wedge is provided by wedge plies adhered over the root and the tooth.
摘要翻译：用于燃气涡轮发动机的叶片包括复合层，所述复合层包括相对于颈层张开的颈层和齿层。颈层和齿层分别提供颈部和根部。根包含一颗牙齿。楔形物由粘附在根部和牙齿上的楔形层提供。

7. 发明授权

EP2397654B1 Vane assembly and method for assembling the same 有权
标题翻译：叶片组件和组装定子叶片组件的方法
公开(公告)号：EP2397654B1
公开(公告)日：2016-05-18
申请号：EP11250589.6
申请日：2011-06-15
申请人： Rolls-Royce Corporation
发明人： Rivers, Jonathan M. , Scott, Matthew A.
IPC分类号： F01D9/04 , F01D25/28 , F01D25/24 , F01D5/32
CPC分类号： F01D9/041 , F01D5/32 , F01D9/042 , F05D2230/64 , F05D2230/644 , F05D2250/411 , F05D2260/30

8. 发明公开

EP2873809A1 Rotor einer Strömungsmaschine 失效
标题翻译：涡轮机转子
公开(公告)号：EP2873809A1
公开(公告)日：2015-05-20
申请号：EP14193326.7
申请日：2014-11-14
申请人： MTU Aero Engines AG
发明人： Klötzer, Alexander , Hofmann, Dieter
IPC分类号： F01D5/30 , F01D5/32
CPC分类号： F01D5/3038 , F01D5/32
摘要： Die Erfindung betrifft einen Rotor einer Strömungsmaschine. Der Rotor umfasst mindestens eine Schaufel (4, 6, 8), die ein Schaufelblatt (20) und einen Schaufelfuß (54, 55, 58) aufweist, und einen Rotorgrundkörper (2), insbesondere eine Scheibe (2), die eine nach außen geöffnete Umfangsnut (12) zur Aufnahme des Schaufelfußes (54, 55, 58) aufweist. Dabei sind die Umfangsnut (12) und der Schaufelfuß (54, 55, 58) derart geformt, dass durch Drehen der Schaufel (4, 6, 8) um eine Achse (A r , A T ) der Schaufelfuß (54, 55, 58) in der Umfangsnut (12) sicherbar ist.
摘要翻译：本发明涉及一种涡轮机的转子。该转子包括至少一个叶片（4,6，8）具有翼型件（20）和叶片根部（54，55，58）和一个转子基体（2），特别是盘（2），其具有一个向外用于接收叶根（54，55，58）打开周向槽（12）。在此，周向槽（12）和所述叶片（54，55，58）成形为使得由（8 4,6）围绕叶片轴线（A R，AT）的旋转刀片（54，55，58）在所述周向槽（12）被固定。

9. 发明公开

EP2867478A1 SCHAUFELKRANZ FÜR EINE TURBOMASCHINE 有权
标题翻译：铲花圈叶轮机FOR
公开(公告)号：EP2867478A1
公开(公告)日：2015-05-06
申请号：EP13745035.9
申请日：2013-07-29
申请人： Siemens Aktiengesellschaft
发明人： ZELMER, Dimitri
IPC分类号： F01D5/32
CPC分类号： F01D5/32 , F01D5/14 , F01D5/3007 , F01D5/323 , F04D29/322
摘要： The invention relates to a blade ring (44) for an axial turbomachine, comprising a blade carrier (46) with a number of retaining grooves (21) and with a corresponding number of blades (27), the blade roots of which are inserted into the retaining grooves (21), wherein the blades (27), on the underside (33) thereof facing toward a groove base (35) of the retaining groove (21), have a recess (37), the base (59) of which recess is at least partially obliquely inclined relative to the groove base (35) of the retaining groove (21) and in which recess there is arranged in each case one wedge-shaped clamping element (47) for pressing the blade root against the support flanks (23). To enable the blade (27) to be mounted in the retaining groove (21) without a preload and to provide a blade ring (44) which can be used in operation without a screw connection, it is provided that a spring element (55) is provided in each recess (37), the spring force of which spring element acts on the respective wedge-shaped clamping element (47) along the retaining groove (21), and that means are provided with which the wedge-shaped clamping element (47) can, for the mounting of the blade (27) in the retaining groove (21) without a preload, be displaced temporarily into a position in which the blade root (31) is seated in the retaining groove (21) with play.

10. 发明授权

EP2614221B1 AUBE DE TURBOREACTEUR 有权
标题翻译：舀一涡轮发动机
公开(公告)号：EP2614221B1
公开(公告)日：2015-04-15
申请号：EP11751613.8
申请日：2011-09-05
申请人： Messier-Bugatti-Dowty , Aircelle
发明人： MASSON, Richard , DUNLEAVY, Patrick , DESJOYEAUX, Bertrand
IPC分类号： F04D29/54 , F01D5/32 , F01D5/12 , F01D5/28 , F01D5/14 , F01D5/24 , F01D9/04 , F01D25/24
CPC分类号： F01D5/12 , F01D5/147 , F01D5/282 , F01D5/32 , F01D9/042 , F01D25/246 , F04D29/542 , F05D2230/60 , F05D2240/12 , F05D2260/30 , Y02T50/672

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