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1. 发明授权

EP3620243B1 FORGING ASSEMBLY HAVING CAPACITANCE SENSORS, AND METHOD OF ANALYZING PERFORMANCE OF SUCH ASSEMBLY 有权转让
公开(公告)号：EP3620243B1
公开(公告)日：2022-04-27
申请号：EP19188131.7
申请日：2019-07-24
发明人： REBBECCHI, Thomas A. , THOMAS, Jean Philippe
IPC分类号： B21J13/02 , B21J13/03 , B21K3/04

2. 发明公开

EP3974081A1 TIAL ALLOY PRODUCTION METHOD AND TIAL ALLOY 审中-公开
公开(公告)号：EP3974081A1
公开(公告)日：2022-03-30
申请号：EP20810725.0
申请日：2020-03-18
申请人： IHI Corporation
发明人： KUBUSHIRO, Keiji
IPC分类号： B21J1/06 , B21J5/00 , B21K3/04 , C22C14/00 , C22C1/00 , C22F1/00 , C22F1/18
摘要： A method of manufacturing a TiAl alloy includes a casting step of melting and casting a TiAl alloy raw material which contains 42 at% or more and 45 at% or less of Al, 3 at% or more and 6 at% or less of Nb, 3 at% or more and 6 at% or less of V, 0.1 at% or more and 0.3 at% or less of B, and the balance being Ti and inevitable impurities, a hot forging step of hot forging the cast TiAl alloy by heating the cast TiAl alloy to a temperature range between 1200 °C or higher and 1350 °C or lower, and a thermal treatment step of holding the hot-forged TiAl alloy at a temperature range between 1220 °C or higher and 1300 °C or lower for a hour range between 1 hour or longer and 5 hours or shorter, applying a first thermal treatment to the hot-forged TiAl alloy, cooling the TiAl alloy subjected to the first thermal treatment to a temperature range between 1000 °C or higher and 1100 °C or lower at a cooling rate of 400 °C/hour or more, holding the TiAl alloy subjected to the first thermal treatment at a temperature range between 1000 °C or higher and 1100 °C or lower for a hour range between 1 hour or longer and 4 hours or shorter, applying a second thermal treatment to the TiAl alloy subjected to the first thermal treatment, and rapidly cooling the TiAl alloy subjected to the second thermal treatment.

3. 发明授权

EP3302874B1 PROCÉDÉ DE FABRICATION D'UNE AUBE DE TURBOMACHINE EN TIAL 有权
公开(公告)号：EP3302874B1
公开(公告)日：2021-10-13
申请号：EP16733637.9
申请日：2016-05-26
发明人： LECONTE, Gilbert , FRANCHET, Jean-Michel , SALLOT, Pierre
IPC分类号： B23P13/04 , B23P15/02 , B22F3/17 , B22F3/20 , B21C23/00 , B21C23/14 , B21C23/16 , B21C35/02 , B21K3/04 , B22F5/04

4. 发明授权

EP3281719B1 HOT FORGING DIE AND HOT FORGING METHOD 有权
公开(公告)号：EP3281719B1
公开(公告)日：2020-09-23
申请号：EP16776474.5
申请日：2016-03-31
申请人： Hitachi Metals, Ltd.
发明人： MITSUNAGA, Hisashi , FUKUI, Tsuyoshi , TERAMAE, Toshiya , NONOMURA, Toshiaki , MATSUMOTO, Hideki , SHIMOHIRA, Eiji , KOHIKI, Satoshi
IPC分类号： B21J13/02 , B21J5/00 , B21K3/04 , B21J7/14 , B21J9/06 , B21J1/04

5. 发明公开

EP3623100A1 WROUGHT ROOT BLADE MANUFACTURE METHODS 审中-公开
公开(公告)号：EP3623100A1
公开(公告)日：2020-03-18
申请号：EP19195215.9
申请日：2019-09-03
申请人： United Technologies Corporation
发明人： SHAH, Dilip M. , CETEL, Alan D. , SEETHARAMAN, Venkatarama K.
IPC分类号： B23P15/02 , B21J5/02 , B21K3/04 , C22F1/00 , F01D5/14 , B21H7/16 , F01D5/30 , C21D9/00 , B23H9/10
摘要： A method for manufacturing a blade, the method includes casting a nickel alloy blade precursor having an airfoil (122) and a root (124). The airfoil (122) and the root (124) are solution heat treated differently from each other. After the solution heat treating, the root (124) is wrought processed. After the wrought processing, an exterior of the root (124) is machined.

6. 发明公开

EP3584334A1 VERFAHREN ZUR HERSTELLUNG EINES GESCMIEDETEN BAUTEILS AUS EINER TIAL-LEGIERUNG UND DADURCH HERGESTELLTES BAUTEIL 审中-公开
公开(公告)号：EP3584334A1
公开(公告)日：2019-12-25
申请号：EP19180148.9
申请日：2019-06-14
申请人： MTU Aero Engines AG
发明人： Schloffer, Martin
IPC分类号： C22C14/00 , B21K3/04 , C22F1/18 , F01D5/00 , F01D5/28
摘要： Die Erfindung betrifft eine Verfahren zur Herstellung eines Bauteils aus einer TiAl-Legierung durch zweistufiges isothermes Schmieden und ein dadurch hergestelltes Bauteil. Das Verfahren umfasst ein erstes isothermes Schmieden einer Bauteil-Vorstufe bei einer Temperatur von mindestens 1180°C, ein Zwischenglühen der geschmiedeten Vorstufe bei einer Temperatur im Bereich von 1130°C bis 1170°C für 1 bis 8 Stunden und ein anschliessendes zweites isothermes Schmieden bei einer Temperatur von mindestens 1180°C mit einem Umformungsgrad, der niedriger ist als der Umformungsgrad beim ersten isothermen Schmieden.

7. 发明授权

EP2465622B1 A clipping die for clipping a component 有权
公开(公告)号：EP2465622B1
公开(公告)日：2019-01-23
申请号：EP11189312.9
申请日：2011-11-16
申请人： Rolls-Royce plc
发明人： McBain, John
IPC分类号： B21K3/04 , B21J5/02

8. 发明授权

EP2423340B1 Process and system for fabricating gamma tial turbine engine components 有权转让
公开(公告)号：EP2423340B1
公开(公告)日：2018-07-18
申请号：EP11179093.7
申请日：2011-08-26
申请人： United Technologies Corporation
发明人： Das, Gopal
IPC分类号： C22C14/00 , C22F1/18 , B21K3/04 , B23H7/00 , B26D1/00 , B26F3/00 , B30B11/00 , F01D5/00 , B23P15/02
CPC分类号： C22C14/00 , B21J1/00 , B21J1/02 , B21J1/06 , B21J5/002 , B21K3/04 , B23H1/00 , B23P15/02 , C22B9/04 , C22B9/20 , C22B34/1295 , C22F1/183
摘要： A process for manufacturing a turbine engine component (10) comprises the steps of: casting ingots made of a gamma TiAl material using a double vacuum arc remelting casting technique; subjecting the cast ingots to a hot isostatic pressing to close porosity; forming at least one pancake of the gamma TiAl material by isothermally forging the hot isostatic pressed ingots; sectioning each pancake into a plurality of blanks; heat treating the blanks to produce a desired microstructure and mechanical properties; and machining the blanks into finished turbine engine components (10). A system for performing the process is also disclosed.

9. 发明公开

EP3081319A4 HOLLOW FAN BLADE PREPARATION METHOD 审中-公开
标题翻译： HERSTELLUNGSVERFAHRENFÜRHOHLEGEBLÄSESCHAUFEL
公开(公告)号：EP3081319A4
公开(公告)日：2017-08-23
申请号：EP14870491
申请日：2014-12-11
申请人： INST FOR METALS SUPERPLASTICITY PROBLEMS OF THE RUSSIAN ACAD OF SCIENCES , OPEN JOINT STOCK COMPANY AVIADVIGATEL , JOINT STOCK COMPANY UFA ENGINE IND ASS
发明人： INOZEMTSEV ALEXANDER ALEXANDROVICH , MULYUKOV RADIK RAFIKOVICH , PAVLINICH SERGEY PETROVICH , ARTYUKHOV ALEXANDER VIKTOROVICH , SAFIULLIN RINAT VLADIKOVICH , TRIFONOV VADIM GENNADIEVICH , KHARIN SERGEY ALEXANDROVICH , MANAPOV IREK USMANOVICH , MOROZOV MIKHAIL ALEXANDROVICH
IPC分类号： B21D53/78 , B21D26/02 , B21K3/04 , B23P15/04
CPC分类号： B21D53/78 , B21D26/055 , B23P15/04
摘要： The invention relates to metal forming using diffusion welding and superplastic forming. Stop-off material is preliminarily applied in a predetermined screen pattern to areas where surfaces of skin and core preforms come into contact. Skin preforms are provided with a groove, and core preform is provided with a slot for mounting at least one tube. A stack is sealed along edges with the exception of where at least one tube is to be mounted. A tube is mounted to be connected to a collector zone, and oxygen and binder of the stop-off material are removed from cavities in the stack. The stack is fully sealed, heated, and the preforms are diffusion-welded in predetermined areas, also along an entrance edge, an exit edge and a peripheral edge. An integral structural preform is given an airfoil shape and subjected to superplastic forming by supplying working fluid into cavities between the skin and core preforms through also at least one tube. The collector zone is disposed on the side of the stack, which corresponds to the peripheral edge of the blade. For mounting one or more tubes for supplying working fluid at superplastic forming, the groove in the skin preforms and the slot in the core preform are provided at a distance from the outer boundary of the entrance edge or exit edge less than L/3, where L is the length of the blade chord along the peripheral edge. It is thus possible to eliminate risk of defects during blade forming without compromising performance characteristics of the blade and increase in labor intensity of producing same.
摘要翻译：本发明涉及使用扩散焊接和超塑性成形的金属成形。阻挡材料预先以预定的屏幕图案施加到表皮和芯预制件的表面接触的区域。蒙皮预制件设置有凹槽，并且芯预制件设有用于安装至少一个管的狭槽。除了要安装至少一个管子的地方以外，堆栈沿着边缘密封。安装管以连接到收集器区域，并且停止材料的氧气和粘合剂从堆叠中的空腔移除。叠层完全密封，加热，并且预成型件也沿着入口边缘，出口边缘和外围边缘扩散焊接在预定区域中。整体结构预成型件被赋予翼型形状并且通过还通过至少一个管道将工作流体供应到表层和型芯预成型件之间的腔体中而经受超塑性成形。收集器区域设置在堆叠的一侧上，其对应于叶片的外围边缘。为了在超塑成形中安装一个或多个用于供应工作流体的管道，预成型件中的凹槽和芯预成型件中的槽设置成距入口边缘或出口边缘的外边界小于L / 3，其中 L是沿着外围边缘的叶片弦的长度。因此可以在叶片成形期间消除缺陷的风险，而不损害叶片的性能特性并增加生产叶片的劳动强度。

10. 发明公开

EP2623229A4 MANUFACTURING METHOD FOR BLADE MATERIAL AND MANUFACTURING DEVICE FOR BLADE MATERIAL 有权转让
标题翻译： HERSTELLUNGSVERFAHRENFÜREIN KLINGENMATERIAL UND HERSTELLUNGSVORRICHTUNGFÜREIN KLINGENMATERIAL
公开(公告)号：EP2623229A4
公开(公告)日：2017-07-26
申请号：EP11828931
申请日：2011-09-22
申请人： HITACHI METALS LTD
发明人： SATO KOJI , TOGA TAKASHI , WAKAZONO YOSHIHIRO , MATSUMOTO HIDEKI , SHIGIHARA YUSUKE
IPC分类号： B21K3/04 , B21D11/14 , B21D53/78 , B21J13/10
CPC分类号： B21K3/04 , B21D53/78 , B21D53/92 , B21J13/10 , Y10T29/49336 , Y10T29/53996
摘要： Provided are a manufacturing method for a blade material and a manufacturing device for a blade material, by which a long blade material can be manufactured without using a large-sized press forging machine. A manufacturing method for a blade material, in which hot forging is sequentially performed by molds from the root side to a blade (vane) tip, wherein when a root-side portion is grasped and a material to be forged is restrained by a mold, twisting is performed on a region between the grasped portion and the restrained portion. A manufacturing method for a blade material, in which hot forging and twisting are repeated, is preferable, and a manufacturing method for a blade material, in which hot forging is performed while molds are sequentially changed, is more preferable.
摘要翻译：本发明提供一种叶片材料的制造方法以及叶片材料的制造装置，能够不使用大型压锻机来制造长叶片材料。一种叶片材料的制造方法，其中，通过模具从根侧向叶片（叶片）前端依次进行热锻造，其中，在掌握了根部侧部分并利用模具来限制锻造材料的情况下，在抓握部分和限制部分之间的区域执行扭转。优选重复进行热锻和扭转的叶片材料的制造方法，更优选在模具依次变更的同时进行热锻造的叶片材料的制造方法。

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