公开(公告)号：EP2629963A2

公开(公告)日：2013-08-28

申请号：EP11831792.4

申请日：2011-09-12

申请人： MTU Aero Engines GmbH

发明人： HESS, Thomas ,  BAYER, Erwin ,  EISEN, Markus ,  BROICHHAUSEN, Klaus ,  SATZGER, Wilhelm ,  SIKORSKI, Siegfried ,  DUSEL, Karl-Heinz ,  MELZER, Hans-Christian

IPC分类号： B29C73/00 ,  B29C67/00 ,  B22F3/105 ,  B28B1/00

CPC分类号： F01D5/141 ,  B22F3/1055 ,  B22F2003/1056 ,  B29C64/153 ,  B29C73/00 ,  B29C73/34 ,  B29C2035/0838 ,  B29D99/0025 ,  B33Y80/00 ,  Y02P10/295 ,  Y10T428/20

摘要： The invention relates to a device for producing, repairing and/or replacing a component, especially an aircraft component, by means of a powder that can be solidified by energy radiation of an energy radiation source, characterized in that the device comprises an application unit that is designed such that the powder can be applied onto an uneven surface by means of the application unit.

摘要翻译： 本发明涉及一种设备，用于制造，修复和/或更换部件，特别是在飞机部件，通过粉末的手段也可以通过能量辐射源的能量辐射固化，其特征在于DASS模具装置包括应用单元的做 设计审查做的粉末可以走上不平整的表面上由应用单元来施加。

公开(公告)号：EP2606238A1

公开(公告)日：2013-06-26

申请号：EP11750019.9

申请日：2011-08-17

申请人： MPC Inc.

发明人： PARRY, William, W. ,  BURACHINSKY, Erik

IPC分类号： F04D13/08 ,  F04D29/02 ,  F04D29/22 ,  F04D29/44 ,  B29C70/00 ,  B29C70/48 ,  B29C33/52

CPC分类号： F01D5/282 ,  B29C33/3842 ,  B29C33/40 ,  B29C33/52 ,  B29C70/06 ,  B29C70/30 ,  B29C70/46 ,  B29C70/48 ,  B29D99/0025 ,  B29K2031/00 ,  B29K2063/00 ,  B29K2105/06 ,  B29K2309/08 ,  B29K2995/0063 ,  B29K2995/007 ,  B29L2031/08 ,  B29L2031/7504 ,  F01D5/147 ,  F01D9/041 ,  F04D13/08 ,  F04D29/026 ,  F04D29/2227 ,  F04D29/448 ,  F05C2253/04 ,  F05D2220/30 ,  F05D2230/21 ,  F05D2260/95 ,  F05D2300/43 ,  F05D2300/44 ,  F05D2300/603

摘要： A non-metallic vertical turbine pump and a method of manufacturing same are provided. In accordance with one embodiment, the vertical turbine pump can include a motor, and a drive shaft coupled to the motor for rotation, a casing with a mixed flow diffuser including a diffuser hub and diffuser vanes that project out from the diffuser hub, and a mixed flow impeller configured to rotatably fit inside the casing, having an impeller hub, impeller vanes, extending from the hub, and a front and a back shroud connected to opposing ends of the impeller vanes. At least one of the mixed flow impeller and the mixed flow diffuser can be made of a non-metallic material and is a singular homogenous component.

公开(公告)号：EP2599715A1

公开(公告)日：2013-06-05

申请号：EP11306587.4

申请日：2011-11-30

申请人： Ratier-Figeac SAS ,  Hamilton Sundstrand Corporation

发明人： Seminel, Bruno ,  Grimal, Stéphane ,  Nagle, David P. ,  Carvalho, Paul A.

IPC分类号： B64C11/26

CPC分类号： F01D5/147 ,  B29D99/0025 ,  B64C11/26

摘要： A propeller blade (100) includes a foam core (104) and a structural layer (106) that surrounds at least a portion of the foam core (104) and includes a face side (107) and a camber side (109). The propeller blade (100) also includes an insert (105) disposed in the foam core (104) in operable contact with the face side (107) and the camber side (109) of the structural layer (106).

摘要翻译： 螺旋桨叶片（100）包括泡沫芯（104）和围绕泡沫芯（104）的至少一部分并且包括面侧（107）和外倾侧（109）的结构层（106）。 推进器叶片（100）还包括设置在泡沫芯（104）中的可与结构层（106）的表面侧（107）和外倾侧（109）可操作接触的插入件（105）。

公开(公告)号：EP2347889B1

公开(公告)日：2013-05-29

申请号：EP11250081.4

申请日：2011-01-26

申请人： United Technologies Corporation

发明人： Naik, Rajiv A.

IPC分类号： B29C70/24 ,  B29D99/00 ,  B29B11/16 ,  D03D25/00 ,  F01D5/28 ,  D03D13/00 ,  B29L31/08

CPC分类号： F01D5/147 ,  B29B11/16 ,  B29C70/24 ,  B29D99/0025 ,  B29L2031/08 ,  D03D11/00 ,  D03D13/004 ,  D03D25/005 ,  D10B2505/02 ,  F01D5/282 ,  F05D2250/20 ,  F05D2300/6012 ,  Y10T29/49337 ,  Y10T29/49801 ,  Y10T442/3195

公开(公告)号：EP2527128A2

公开(公告)日：2012-11-28

申请号：EP12003739.5

申请日：2012-05-10

申请人： Gamesa Innovation & Technology, S.L.

发明人： Velez Oria, Sergio ,  Zugasti Paramo, Amaia ,  Marin Martinez, Francisco Javier ,  Rodriguez Saiz, Emilio ,  Arocena De La Rua, Ion ,  Sanz Pascual, Eneko

IPC分类号： B29C65/00 ,  F03D1/06 ,  F16B11/00

CPC分类号： F03D1/0675 ,  B29C65/4835 ,  B29C65/5035 ,  B29C65/5057 ,  B29C65/52 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/131 ,  B29C66/232 ,  B29C66/3452 ,  B29C66/54 ,  B29C66/543 ,  B29C66/636 ,  B29C66/9141 ,  B29C66/919 ,  B29C66/929 ,  B29C66/98 ,  B29D99/0025 ,  B29L2031/085 ,  F16B11/006 ,  Y02E10/721 ,  Y02P70/523

摘要： A method for bonding a first and a second prefabricated parts of a wind turbine blade comprising the steps of: disposing bands (45, 55, 65) of an adhesive material in a manageable uncured state following traces (43, 53, 63) signaled on a bonding area of one of said parts, said adhesive material being able to flow in a curing stage in a controlled way, the width (W) and height (H) of said bands (45, 55, 65) and the separation (S1) between said traces (43, 53, 63) being determined so that a predetermined separation (S2) between said bands (45, 55, 65) comprised between 0-300 mm remains after the bonding; bonding both parts under predetermined conditions of pressure and temperature. The invention also refers to a wind turbine blade having prefabricated parts bonded using said method.

摘要翻译： 一种用于接合风力涡轮机叶片的第一和第二预制部件的方法，包括以下步骤：在发出信号的痕迹（43,53,63）之后，将粘合剂材料的带（45,55,65）布置在可管理的未固化状态 所述粘合材料能够以受控的方式在固化阶段中流动，所述带（45,55,65）的宽度（W）和高度（H）和分离（S1 确定所述迹线（43,43,63）之间的距离，使得在所述接合之后仍保留在0-300mm之间的所述带（45,55,65）之间的预定分离（S2） 在预定的压力和温度条件下粘合两部分。 本发明还涉及具有使用所述方法结合的预制部件的风力涡轮机叶片。

公开(公告)号：EP2286983B1

公开(公告)日：2012-03-14

申请号：EP10172116.5

申请日：2010-08-06

申请人： Rolls-Royce plc

发明人： Roberts, David Vaughan ,  McMillan, Alison Jane ,  Booth, Stephen John

IPC分类号： B29C70/88 ,  F01D5/28 ,  F01D17/02

CPC分类号： F01D25/24 ,  B29C70/882 ,  B29D99/0025 ,  B29L2031/08 ,  B29L2031/7504 ,  F01D5/282 ,  F01D17/02 ,  F05D2300/507 ,  Y02T50/672 ,  Y02T50/673

公开(公告)号：EP2241432A3

公开(公告)日：2011-06-22

申请号：EP10250389.3

申请日：2010-03-04

申请人： United Technologies Corporation

发明人： Parkin, Michael ,  Klinetob, Carl Brian ,  Alexander, Phillip ,  Clarkson, Steven

IPC分类号： B29D99/00 ,  B29C70/86 ,  B29C70/08 ,  B29C70/48 ,  F01D5/28

CPC分类号： B29C66/721 ,  B29C65/4835 ,  B29C65/5057 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/73752 ,  B29C66/73754 ,  B29C66/73941 ,  B29C66/742 ,  B29C70/088 ,  B29C70/24 ,  B29C70/48 ,  B29C70/865 ,  B29D99/0025 ,  B29K2105/24 ,  B29K2105/243 ,  B29K2705/00 ,  B29L2031/082 ,  F01D5/282 ,  F02K3/04 ,  B29K2063/00 ,  B29K2307/04

摘要： An intermediate-manufactured composite airfoil (10) includes first and second composite skins (12,14) each having a plurality of fibers (16) in a polymer matrix (18). A composite core (20) is removably located between the first and second composite skins (12,14). The composite core (20) includes a dry, three-dimensional, woven fiber network (22) or, alternatively, a three-dimensional, woven fiber network (22) in a fully cured polymer matrix (24).

公开(公告)号：EP2326488A1

公开(公告)日：2011-06-01

申请号：EP09781870.2

申请日：2009-08-14

申请人： LM GLASFIBER A/S

发明人： GRABAU, Peter

IPC分类号： B29C70/54 ,  B29C33/16 ,  B29C70/44 ,  B29C70/48 ,  B29C70/88 ,  B29C65/16 ,  F03D1/06

CPC分类号： B29C70/543 ,  B29C33/16 ,  B29C70/443 ,  B29C70/48 ,  B29C70/541 ,  B29C70/88 ,  B29D99/0025 ,  B29K2305/00 ,  B29K2305/12 ,  B29L2031/082 ,  B29L2031/085 ,  B32B37/10 ,  F03D1/065 ,  F05B2280/6013 ,  F05B2280/6015 ,  F05C2253/16 ,  F05C2253/20 ,  Y02E10/721 ,  Y02P70/523

摘要： A method of manufacturing a wind turbine blade shell part comprising fibre material impregnated with cured resin is described. The method comprises the steps of : a) providing a first mould part (110) having a first forming surface (112) with a contour that defines at least a part of an outer surface of turbine blade shell part, b) arranging fibre material in the first mould part, the fibre material comprising fibres of a magnetisable material, c) providing a resin in the first mould part simultaneous with and/or subsequent to step b), and d) curing the resin in order to form the wind turbine blade shell part or wind turbine blade (150). The fibre material is retained against the first forming surface by use of magnet means (114, 116, 118) during step b) and/or step c). A mould part comprising magnet means (114, 116, 118) and a wind turbine blade are also described.

公开(公告)号：EP2113358B1

公开(公告)日：2011-03-16

申请号：EP09004605.3

申请日：2009-03-30

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Schreiber, Karl

IPC分类号： B29D99/00 ,  B29C45/14

CPC分类号： B29C45/1418 ,  B29D99/0025 ,  B29K2705/00 ,  B29L2031/082 ,  Y10T29/49336

公开(公告)号：EP2288488A2

公开(公告)日：2011-03-02

申请号：EP09768913.7

申请日：2009-06-11

申请人： REpower Systems AG

发明人： KULENKAMPFF, Jens ,  FAULKNER, Benn

IPC分类号： B29C70/84 ,  B29C65/00

CPC分类号： F03D1/065 ,  B29C33/30 ,  B29C33/34 ,  B29C65/483 ,  B29C65/5042 ,  B29C66/54 ,  B29C66/543 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C69/004 ,  B29C70/443 ,  B29C70/48 ,  B29D99/0025 ,  B29L2031/082 ,  B29L2031/085 ,  Y02E10/721 ,  Y02P70/523 ,  B29K2307/04 ,  B29K2309/08

摘要： The invention relates to a method for producing a rotor blade for a wind energy plant, which, in the operationally -ready state runs from a blade root region, for connecting to the rotor hub of the wind energy plant, to a blade tip and is divided into at least two pieces for production thereof. According to the invention, the production of the rotor blade, in particular serial production, may be facilitated and accelerated, wherein the rotor blade is segmented into more than two segments for production, at least for some of said segments, separate moulds for simultaneous separate use are provided and the segments for final production of the rotor blade are joined outside a production mould to give a rotor blade or rotor blade part.