公开(公告)号：EP1329592A1

公开(公告)日：2003-07-23

申请号：EP02001348.8

申请日：2002-01-18

申请人： SIEMENS AKTIENGESELLSCHAFT

发明人： Bast, Ulrich, Dr. ,  Hermann, Wolfgang, Dr.

IPC分类号： F01D5/28 ,  F01D25/00 ,  F01D5/30 ,  B23P15/04

CPC分类号： F01D5/284 ,  F01D5/147 ,  F01D5/288 ,  F01D5/3084 ,  F05D2240/80 ,  F05D2300/15 ,  F05D2300/21 ,  F05D2300/2118 ,  F05D2300/22 ,  F05D2300/603 ,  Y02T50/67

摘要： Nach dem Stand der Technik bereiten Laufschaufeln in der vierten Stufe einer Gasturbine, die eine Länge von 50cm überschreiten, Probleme bezüglich der mechanischen Festigkeit, weil beim Rotieren der Laufschaufeln zu große Fliehkräfte auftreten.
Eine erfindungsgemäße Laufschaufel (16) in der vierten Reihe (V4) einer Gasturbine (41) weist durch einen hohen Keramikanteil eine geringere Dichte auf, so dass die Fliehkräfte reduziert sind.

摘要翻译： 涡轮机至少有四个阶段。 如果第四阶段的叶片长于50厘米，离心力对其机械强度有不利影响。 如果通过在其制造中使用较高比例的陶瓷材料，轴向燃气轮机的第四排（V4）中的转子叶片（16）的密度降低，则可以减轻这一点。

公开(公告)号：EP1092485A3

公开(公告)日：2003-07-16

申请号：EP00308659.2

申请日：2000-10-02

申请人： ROLLS-ROYCE PLC

发明人： Launders, Paul David

IPC分类号： B21D26/02 ,  B23K20/02 ,  B21D53/78 ,  B23P15/04

CPC分类号： B21D53/78 ,  B23K20/023 ,  B23K20/18 ,  B23P15/04 ,  Y10T29/49318 ,  Y10T29/49336 ,  Y10T29/49339

摘要： A method of manufacturing an article (10) from two metal workpieces (30,32), the first and second metal workpieces (30,32) define the outer profile of the article (10). The second workpiece (32) is thicker than the first workpiece (30). The first workpiece (30) has two flat surfaces (34,36) and the second workpiece has one flat surface (38) and one machined (42) surface (40). Stop of is applied to surface (34) to prevent diffusion bonding at preselected areas. The workpieces (30,32) are assembled into a stack (58) so that the flat surfaces (34,38) are in abutment. Heat and pressure are applied to diffusion bond the workpieces (30,32) together to form an integral structure (60). The integral structure (60) is placed in a die such that the first workpiece (30) faces a convex surface of the die. The integral structure (60) is heated to cause the integral structure (60) to be hot creep formed on the convex surface of the die. The integral structure (62) is hot formed in a superplastic forming die by heating and internally pressurising the integral structure (62) to cause a preselected area of the second workpiece to be hot formed to produce the article (10).

公开(公告)号：EP1216785A3

公开(公告)日：2003-05-02

申请号：EP01128579.8

申请日：2001-11-30

申请人： ALSTOM (Switzerland) Ltd

发明人： Beeck, Alexander, Dr. ,  Fernihough, John

IPC分类号： B23P15/04 ,  F01D5/18

CPC分类号： B23P15/04 ,  B33Y80/00 ,  F01D5/147 ,  F01D5/18 ,  F05D2230/13 ,  F05D2230/21 ,  F05D2230/23 ,  F05D2230/90 ,  Y10T29/49339 ,  Y10T29/49796

摘要： Die vorliegende Erfindung betrifft ein Verfahren zur schnellen Herstellung von hohlen Komponenten von Strömungsmaschinen, insbesondere Turbinenschaufeln, für die Fertigungsentwicklung. Bei dem Verfahren wird die herzustellende Turbinenschaufel (1) in zwei oder mehrere Teilstücke (5, 6, 10, 11) derart unterteilt, dass keines der Teilstücke einen Hohlraum aufweist. Die zwei oder mehreren Teilstücke (5, 6, 10, 11) werden einzeln mittels eines Rapid-Prototype-Verfahrens gegossen und anschließend zur Bildung der hohlen Komponente (1) zusammengefügt. Das Verfahren ermöglicht die einfache und kostengünstige Herstellung von Turbinenschaufeln für die Fertigungsentwicklung, insbesondere für die Entwicklung der Kühlsysteme.

公开(公告)号：EP1049562A2

公开(公告)日：2000-11-08

申请号：EP98963749.1

申请日：1998-10-27

申请人： Siemens Westinghouse Power Corporation

发明人： BURKE, Michael, A. ,  FREYER, Paula, D. ,  HEBBAR, Mohan, A. ,  SETH, Brij, B. ,  SWARTZBECK, Gary, W. ,  ZAGAR, Thomas, Walter

IPC分类号： B23P15/04 ,  C22F1/10 ,  F01D5/12

CPC分类号： F01D5/28 ,  B23H9/10 ,  B23K20/023 ,  B23K20/16 ,  B23K35/3033 ,  B23K35/304 ,  B23K2201/001 ,  B23P15/04 ,  C22C19/057 ,  C22F1/10 ,  C30B11/00 ,  C30B29/52 ,  F01D5/147 ,  F01D5/18 ,  F01D5/184 ,  F05D2230/23 ,  F05D2230/40 ,  F05D2300/607 ,  Y02T50/67 ,  Y02T50/671 ,  Y02T50/673 ,  Y02T50/676 ,  Y10T428/12271 ,  Y10T428/12347 ,  Y10T428/12431 ,  Y10T428/12944

摘要： Large gas turbine blades made from separate cast segments of superalloys are disclosed. The turbine blade is designed such that bond lines between adjacent segments are placed in low stress regions of the blade. The cast superalloy segments of the blades are aligned and fitted together with specified tolerances. The turbine blade segments are then joined by transient liquid phase bonding, followed by a controlled heat treatment which produces the desired microstructure in the bond region. The method allows for the production of large, high quality turbine blades by joining small, high quality cast superalloy sections, in comparison with prior attempts to cast large turbine blades as single pieces which have produced very low yields and high individual component costs.

公开(公告)号：EP0837220A3

公开(公告)日：1999-12-15

申请号：EP97117117.8

申请日：1997-10-02

申请人： MTU MOTOREN- UND TURBINEN-UNION MÜNCHEN GMBH

发明人： Richter, Karl-Hermann, Dr. ,  Knott, Ulrich, Dr.

IPC分类号： F01D5/00 ,  B23P15/04 ,  B23K26/00 ,  B23K1/00 ,  B23K1/002 ,  B23K1/008

CPC分类号： B23P6/005 ,  B23K1/002 ,  F01D5/005 ,  F05D2230/80 ,  Y10T29/49318 ,  Y10T29/4973 ,  Y10T29/49737 ,  Y10T29/49748

摘要： Es wird ein Verfahren zur Instandsetzung verschlissener Schaufelspitzen von Turbinenschaufeln beschrieben, bei dem die verschlissene Schaufelspitze entfernt wird, so daß die Höhe des verbleibenden Restschaufelblatts (2) einer standardisierten Höhe h entspricht, die Ist-Geometrie des Endes des Restschaufelblatts (2) in der Höhe h gemessen wird, ein Reparaturprofil (4) mit einer der Differenz zwischen einer Soll-Höhe H des instandgesetzten Schaufelblatts (1) und der standardisierten Höhe h des Restschaufelblatts (2) entsprechenden Dicke aus einem Reparaturmaterial mit einer der Ist-Geometrie des Endes des Restschaufelblatts entsprechenden Kontur geformt wird, und das Reparaturprofil (4) am Ende des Restschaufelblatts (2) angebracht wird.

公开(公告)号：EP0547219B1

公开(公告)日：1995-07-19

申请号：EP92917464.7

申请日：1992-06-04

申请人： SECRETARY of STATE for DEFENCE in HER BRITANNIC MAJESTY'S GOV. of the UNITED KINGDOM of GREAT BRITAIN and NORTHERN IRELAND

发明人： PARTRIDGE, Peter, George ,  WISBEY, Andrew

IPC分类号： B23P15/04 ,  F01D5/30

CPC分类号： F01D5/20 ,  B23K20/023 ,  B23K35/005 ,  Y10T29/49318 ,  Y10T29/49337

摘要： A titanium or titanium based alloy compressor blade (1) is given a wear-resistant portion such as a tip portion (2) by producing an interfitting male/female joint between the blade and the wear-resistant portion in which the joint portion of the latter is produced with inwardly directed corrugations and the former is pressed at elevated temperature after assembly of the two parts so as to cause the material of the blade to flow into and conform to the shape of the latter and to produce a diffusion bond between the two parts. Interlayers (7, 8) may be used to improve chemical compatibility between the respective parts.

公开(公告)号：EP0305113B1

公开(公告)日：1993-10-13

申请号：EP88307666.3

申请日：1988-08-18

申请人： IMI TITANIUM LIMITED ,  ROLLS-ROYCE plc

发明人： Neal, Donald Francis ,  Kearns, Michael William ,  Fox, Stephen Peter ,  Melville, James Entwistle ,  Wright, Kenneth Wilfred ,  Wood, Philip Steven ,  Pinder, John Timothy ,  Clark, Stephen Craig

IPC分类号： B23P15/04 ,  F01D5/28

CPC分类号： F01D5/288 ,  B23P15/04 ,  F01D5/20 ,  Y10T29/49337

公开(公告)号：EP0266954A3

公开(公告)日：1990-01-24

申请号：EP87309488.2

申请日：1987-10-27

申请人： AIRFOIL TEXTRON INC.

发明人： Doble, Gordon S.

IPC分类号： F01D5/18 ,  F01D5/14 ,  B23P15/04 ,  B21K3/04

CPC分类号： F01D5/18 ,  B23K20/02 ,  B23P15/04 ,  F01D5/147 ,  Y10T29/49337

摘要： A transversely twisted hollow airfoil member is provided by diffusion bonding together airfoil components each having a skin or shell (32) in the form of a partial airfoil twisted transversely along its length (L) and one or more internal support ribs (50, 52, 54) having bonding surfaces (50a, 52a, 54a) which are not twisted transversely along their length. Each support rib extends substantially normal to a bonding plane (T) defined by bonding surfaces on the supporting ribs. As a result of the rib and bonding surface orientation, the airfoil components can be forged and the components bonded together at elevated temperature in short times between dies movable by high pressure toward one another normal to the bonding surfaces.

摘要翻译： 横向扭曲的空心翼型构件通过将翼型构件扩散接合在一起而提供，翼型构件各自具有沿其长度（L）横向扭绞的局部翼型形式的蒙皮或壳体（32）以及一个或多个内部支撑肋（50,52,53） 54）具有不沿其长度横向扭曲的结合表面（50a，52a，54a）。 每个支撑肋基本垂直于由支撑肋上的结合表面限定的结合平面（T）延伸。 由于肋和粘合面的取向，翼型件可以锻造，并且零件之间在较短时间内在高温下粘合在一起，这两个零件之间可以通过高压朝向彼此垂直于粘合表面移动。

公开(公告)号：EP0266954A2

公开(公告)日：1988-05-11

申请号：EP87309488.2

申请日：1987-10-27

申请人： AIRFOIL TEXTRON INC.

发明人： Doble, Gordon S.

IPC分类号： F01D5/18 ,  F01D5/14 ,  B23P15/04 ,  B21K3/04

CPC分类号： F01D5/18 ,  B23K20/02 ,  B23P15/04 ,  F01D5/147 ,  Y10T29/49337

摘要： A transversely twisted hollow airfoil member is provided by diffusion bonding together airfoil components each having a skin or shell (32) in the form of a partial airfoil twisted transversely along its length (L) and one or more internal support ribs (50, 52, 54) having bonding surfaces (50a, 52a, 54a) which are not twisted transversely along their length. Each support rib extends substantially normal to a bonding plane (T) defined by bonding surfaces on the supporting ribs. As a result of the rib and bonding surface orientation, the airfoil components can be forged and the components bonded together at elevated temperature in short times between dies movable by high pressure toward one another normal to the bonding surfaces.

摘要翻译： 提供横向扭转的中空翼片构件，其通过将各自具有沿着其长度（L）横向扭转的部分翼型形式的皮肤或壳体（32）和一个或多个内部支撑肋（50,52,52）扩散粘合在一起， 54）具有不沿其长度横向绞合的接合表面（50a，52a，54a）。 每个支撑肋基本上垂直于由支撑肋上的接合表面限定的接合平面（T）延伸。 作为肋和接合表面取向的结果，可以锻造翼型部件，并且组件在短时间内在升高的温度下结合在一起，两个模具可以通过高压朝着接合表面方向彼此高速地相互移动。

公开(公告)号：EP0018806B1

公开(公告)日：1986-07-30

申请号：EP80301376.2

申请日：1980-04-28

申请人： TRW INC.

发明人： Gerken, John M.

IPC分类号： B23P15/04 ,  F01D9/04

CPC分类号： B23P15/006 ,  F01D9/042 ,  F01D25/005