公开(公告)号：EP4225527B1

公开(公告)日：2024-09-11

申请号：EP21798422.8

申请日：2021-09-30

IPC分类号： B23K20/18 ,  B23P15/04 ,  B21D53/78 ,  B23K20/02 ,  F01D5/14 ,  F04D29/02 ,  F04D29/32

CPC分类号： B23P15/04 ,  F01D5/147 ,  F04D29/023 ,  F04D29/324 ,  B23K2101/00120180801 ,  B23K2103/1420180801 ,  B23K2103/1820180801 ,  B23K2103/2620180801 ,  B23K20/02 ,  B23K20/233 ,  Y02T50/60

公开(公告)号：EP2969293B1

公开(公告)日：2024-04-17

申请号：EP13878459.0

申请日：2013-12-16

IPC分类号： B23P15/04 ,  F04D29/32 ,  F01D5/14 ,  B21K3/04 ,  B21H7/00 ,  B21D53/78

CPC分类号： B21D53/78 ,  B21K3/04 ,  B21H7/00 ,  F04D29/324 ,  F05D2240/30320130101 ,  B23P15/04

公开(公告)号：EP4313480A1

公开(公告)日：2024-02-07

申请号：EP22717217.8

申请日：2022-03-21

申请人： SAFRAN AIRCRAFT ENGINES

发明人： TUREL, Arnaud ,  VOIRON, Mickaël

IPC分类号： B23P15/00 ,  B23P15/04 ,  B23P15/02 ,  B33Y40/20 ,  B22F10/60 ,  B23B31/00 ,  B24B31/06

公开(公告)号：EP4288658A1

公开(公告)日：2023-12-13

申请号：EP22750367.9

申请日：2022-02-03

申请人： TPI Composites, Inc.

发明人： SALIMI, Amir ,  RAINE, Christopher

IPC分类号： F03D1/06 ,  B29L31/08 ,  B23P15/04 ,  B29B11/14 ,  B29C70/54

公开(公告)号：EP4225527A1

公开(公告)日：2023-08-16

申请号：EP21798422.8

申请日：2021-09-30

申请人： SAFRAN AIRCRAFT ENGINES

发明人： SALMON, Jérôme ,  GIMEL, Alexandre ,  GLEIZE, Christophe ,  PEREIRA, Axel ,  RICHARD, Jean-François

IPC分类号： B23K20/18 ,  B23P15/04 ,  B21D53/78 ,  B23K20/02 ,  F01D5/14 ,  F04D29/02 ,  F04D29/32

公开(公告)号：EP4127407A1

公开(公告)日：2023-02-08

申请号：EP21716517.4

申请日：2021-03-22

申请人： Safran Ceramics

发明人： GIMAT, Matthieu, Arnaud ,  BOUILLON, Eric ,  CARLIN, Maxime, François, Roger

IPC分类号： F01D5/14 ,  B23P15/04 ,  F01D5/28 ,  F01D9/04 ,  F01D9/06 ,  F04D29/38

公开(公告)号：EP3964326A1

公开(公告)日：2022-03-09

申请号：EP21196974.6

申请日：2012-11-01

申请人： Raytheon Technologies Corporation

发明人： WEISSE, Michael A.

IPC分类号： B23P15/04 ,  B64C11/24 ,  F04D29/32 ,  F01D5/14 ,  F01D5/16

摘要： An airfoil (10) comprises an airfoil body (12) with an internal cavity (16) and inner and outer covers (32,34). The airfoil body defines a first major surface of the airfoil, and a rib (18) extends along the internal cavity. The inner cover (32) is bonded to the airfoil body (12) over the internal cavity (16), and includes a coupling element (20) extending along the internal cavity in cooperative engagement with the rib. The outer cover (34) is bonded to the airfoil body (12) over the inner cover (32), and defines a second major surface of the airfoil.

公开(公告)号：EP3498971B1

公开(公告)日：2022-01-05

申请号：EP18206187.9

申请日：2018-11-14

发明人： Harding, Adrian

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

公开(公告)号：EP3888822A1

公开(公告)日：2021-10-06

申请号：EP21163010.8

申请日：2021-03-16

申请人： General Electric Company

发明人： TAXACHER, Glenn Curtis ,  LANG, Claire Fridtjof

IPC分类号： B22F5/10 ,  B22F10/47 ,  B22F10/66 ,  B29C64/40 ,  B22F7/02 ,  B22F10/43 ,  B22F10/62 ,  B29C64/153 ,  F01D5/00 ,  B23P15/04 ,  B33Y10/00 ,  B33Y80/00 ,  F01D5/18 ,  F01D5/28 ,  B22F5/00 ,  B22F5/04

摘要： A protective mask (100) for a part (102), the part (102) including a plurality of openings (104) in a surface (106) thereof, is provided. The protective mask (100) includes a mounting member (120) at least partially within each of at least two of the plurality of openings (104). Each mounting member (120) includes a water soluble material (160). A masking member (130) couples the at least two mounting members (120). The masking member (130) includes a non-water soluble material (162). Each mounting member (120) includes a first plurality of integral layers of the water soluble material (160), and the masking member (130) includes a second plurality of integral layers of the non-water soluble material (162). The protective mask (100) can be made by a two material additive manufacturing system (150). A related method is also provided.

公开(公告)号：EP2469027B1

公开(公告)日：2021-09-22

申请号：EP11194046.6

申请日：2011-12-16

发明人： Barlow, Simon Mark ,  Wallis, Michael James

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