公开(公告)号：EP4431268A1

公开(公告)日：2024-09-18

申请号：EP24163594.5

申请日：2024-03-14

Applicant: Spirit AeroSystems, Inc.

Inventor： MEYER, Andi ,  WADSWORTH, Mark Anthony ,  JONES, Ronald

IPC: B29C70/44

CPC classification number: B29D99/0003 ,  B29D99/0005 ,  B29C70/545 ,  B29C70/44 ,  B29D99/0014 ,  B64C1/064 ,  B64C3/26 ,  B29C70/34

Abstract: A method for manufacturing a composite part includes forming an initial radius filler on a composite panel. The initial radius filler is formed from a plurality of plies of composite material stacked on the composite panel. The method includes forming a radius of curvature on at least one side of the initial radius filler, positioning a composite stiffener on the composite panel, wherein the composite stiffener is contoured to define a radius gap when joined with the composite panel, positioning the composite stiffener against the at least one side of the initial radius filler, compressing the composite stiffener, composite panel, and initial radius filler via vacuum bag, and heating the initial radius filler to at least one of a cure temperature, a melting temperature, or a fusing temperature to form, from the initial radius filler, a radius gap filler in the radius gap.

公开(公告)号：EP3705282B1

公开(公告)日：2024-09-11

申请号：EP20170894.8

申请日：2019-01-04

IPC: B29C70/54 ,  B29C70/20

CPC classification number: B29C70/202 ,  B29C70/545 ,  Y02T50/40

公开(公告)号：EP4168245B1

公开(公告)日：2024-09-04

申请号：EP21736638.4

申请日：2021-06-10

IPC: B29D99/00 ,  B29C70/24 ,  B29C70/48 ,  B29C37/00 ,  B29C70/54 ,  B29C65/00

CPC classification number: B29D99/0025 ,  B29C70/24 ,  B29C70/48 ,  B29C37/0025 ,  B29C70/545 ,  B29L2031/0820130101 ,  B29L2031/750420130101 ,  B29C70/086

公开(公告)号：EP3593990B1

公开(公告)日：2024-08-21

申请号：EP17899723.5

申请日：2017-03-10

IPC: B32B3/26 ,  B32B5/26 ,  B32B5/28 ,  B32B27/12 ,  B29C45/14 ,  B29C39/10 ,  B29C45/37 ,  B29C33/42

CPC classification number: B26F1/12 ,  B26F1/26 ,  B29C39/10 ,  B29C43/02 ,  B32B38/04 ,  B32B5/26 ,  B32B2260/02120130101 ,  B32B2260/02320130101 ,  B32B2260/04620130101 ,  B32B3/08 ,  B32B3/06 ,  B32B3/266 ,  B32B5/02 ,  B32B7/00 ,  B32B27/12 ,  B32B2250/4020130101 ,  B32B2250/4420130101 ,  B32B2605/0820130101 ,  B29C70/74 ,  B29C45/14786 ,  B29C45/14336 ,  B29C2045/005820130101 ,  B29C70/545 ,  B29C70/48

公开(公告)号：EP4414150A1

公开(公告)日：2024-08-14

申请号：EP24151929.7

申请日：2024-01-15

Applicant: The Boeing Company

Inventor： Spalding, John F. ,  Matsen, Marc R. ,  Janda, Gwendolyn Marie

IPC: B29B11/16

CPC classification number: B29B11/16 ,  B29C70/342 ,  B29C70/44 ,  B29C70/545

Abstract: Methods of forming a composite structure from a preform (400) with a vent (411) are presented. A preform comprises a plurality of sets of full length plies (406), a plurality of sets of partial plies ((408) alternating with the plurality of sets of full length plies, and a vent extending through the plurality of sets of partial plies.

公开(公告)号：EP4408728A1

公开(公告)日：2024-08-07

申请号：EP22857025.5

申请日：2022-09-21

Applicant: PIAGGIO & C. S.p.A.

Inventor： AGUGGIARO, Andrea

IPC: B62K19/16 ,  B62K25/28 ,  B29C70/00

CPC classification number: B62K19/16 ,  B62K25/283 ,  B29C70/46 ,  B29C70/12 ,  B29C70/86 ,  B29C70/081 ,  B29C70/545 ,  B29C2793/00920130101 ,  B29C43/36 ,  B29C43/02 ,  B29C65/48 ,  B29C66/53 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29L2031/309120130101 ,  B29C66/71 ,  B29C65/483 ,  B29C66/1122

公开(公告)号：EP3473416B1

公开(公告)日：2024-06-26

申请号：EP18185680.8

申请日：2018-07-26

IPC: B29C70/54 ,  B29D99/00 ,  B64C1/06

CPC classification number: B29C70/545 ,  B29D99/0014 ,  B64C3/34 ,  B64C3/182 ,  B64C1/064

公开(公告)号：EP4093668B1

公开(公告)日：2024-06-12

申请号：EP21700804.4

申请日：2021-01-08

IPC: B64C1/14 ,  B64C1/06 ,  B64C39/02 ,  B64C39/04 ,  B64F5/10 ,  B29C70/54 ,  B29D99/00 ,  B32B38/10 ,  B64C39/00

CPC classification number: B64C1/061 ,  B64C2001/004520130101 ,  B64C1/14 ,  B29C70/545 ,  B64F5/10 ,  B64U10/25 ,  B64U20/73 ,  B64U10/10

公开(公告)号：EP4357090A1

公开(公告)日：2024-04-24

申请号：EP23198789.2

申请日：2023-09-21

Applicant: Rolls-Royce plc

Inventor： World, Kevin ,  Groves, Simon ,  Wasinski, Wojciech ,  Wright, Neal

IPC: B26F1/24 ,  B29C70/54 ,  B29C70/24

CPC classification number: B29C70/24 ,  B29C70/545 ,  B29C2793/004520130101 ,  B26F1/24

Abstract: A needle apparatus (70) for making a pinning hole in a composite material comprising a needle (14) having a longitudinal axis, a collar (32) fixed about the needle, a motor (16) having an axis of rotation, and being fixed to the needle such that the needle can be rotated by the motor, the motor and the collar being situated within a motor housing (50), the motor housing having a first bush (34), and a second bush (36), wherein the collar is positioned between the first bush and second bush so as to prevent the needle from moving away from or towards the motor, but allow the needle to rotate freely around its longitudinal axis, wherein each needle apparatus further comprises a linear actuator (40) connected to the motor such that the motor can be moved along the axis of rotation of the motor by the linear actuator.

公开(公告)号：EP3441219A1

公开(公告)日：2019-02-13

申请号：EP18187298.7

申请日：2018-08-03

Applicant: TOYOTA JIDOSHA KABUSHIKI KAISHA

Inventor： IWANO, Yoshihiro

IPC: B32B5/02 ,  B32B5/12 ,  B32B5/28 ,  B32B3/14 ,  B44C3/02

CPC classification number: B32B5/12 ,  B29C70/222 ,  B29C70/443 ,  B29C70/545 ,  B29K2105/0836 ,  B29K2105/089 ,  B29K2307/04 ,  B29L2031/3058 ,  B32B3/14 ,  B32B5/02 ,  B32B5/026 ,  B32B5/142 ,  B32B5/145 ,  B32B5/245 ,  B32B5/28 ,  B32B2250/44 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/106 ,  B32B2307/40 ,  B32B2451/00 ,  B32B2605/08 ,  B62D29/04 ,  B62D35/007

Abstract: A resin structure (10) includes a first structural portion (20) and a second structural portion (30). The first structural portion (20) includes a characteristic design surface (10S) and structures an end portion at a side of the resin structure (10) at which the characteristic design surface (10S) is disposed. An orientation direction of fibers in a first pattern portion (22) of the first structural portion (80) differs from an orientation direction of fibers in a second pattern portion (24, 26). The second structural portion (30) includes a region disposed at the opposite side of the first structural portion (20) to the side at which the characteristic design surface (10S) is disposed. Fibers contained in the second structural portion differ in fiber width from the fibers contained in the first structural portion (20). A portion of the fibers contained in a region of the second structural portion (30) superposed with the first structural portion (20) are configured to be visible through the resin of the first structural portion (20).