公开(公告)号：EP4138073B1

公开(公告)日：2024-10-09

申请号：EP22190343.8

申请日：2022-08-15

IPC分类号： G10K11/168 ,  G10K11/172 ,  B29C73/00 ,  B29C73/04 ,  B29C73/10 ,  B32B3/12 ,  B32B5/02 ,  B32B5/26 ,  B32B7/12 ,  B32B15/04 ,  B32B15/09 ,  B32B15/10 ,  B32B15/12 ,  B32B15/14 ,  B32B21/06 ,  B32B21/08 ,  B32B21/10 ,  B32B27/10

CPC分类号： G10K11/168 ,  G10K11/172 ,  B29C73/04 ,  B29C73/10 ,  B32B7/12 ,  B32B5/024 ,  B32B2260/02120130101 ,  B32B15/092 ,  B32B2262/06220130101 ,  B32B2262/026920130101 ,  B32B5/2795 ,  B32B2307/10220130101 ,  B32B5/026 ,  B32B15/10 ,  B32B29/005 ,  B32B15/098 ,  B32B27/42 ,  B32B15/14 ,  B32B2262/027620130101 ,  B32B21/08 ,  B32B27/38 ,  B32B2260/04620130101 ,  B32B2262/10120130101 ,  B32B2262/024620130101 ,  B32B2262/0820130101 ,  B32B29/02 ,  B32B2605/1820130101 ,  B32B21/10 ,  B32B27/36 ,  B32B3/12 ,  B32B27/10 ,  B32B2262/10620130101 ,  B32B27/12 ,  B32B21/06 ,  B32B2255/0220130101 ,  B32B2262/0420130101 ,  B32B15/12 ,  B32B15/09 ,  B32B15/043 ,  B64C1/40 ,  B64C1/066 ,  B64D11/003 ,  B64D11/00

公开(公告)号：EP3831585B1

公开(公告)日：2024-09-11

申请号：EP19858816.2

申请日：2019-07-23

IPC分类号： B29C73/10 ,  B29C70/30 ,  B29C70/54

CPC分类号： B29C73/10 ,  B29C2793/003620130101 ,  B29C70/542 ,  B29C70/30

公开(公告)号：EP4392239A1

公开(公告)日：2024-07-03

申请号：EP22769109.4

申请日：2022-08-22

申请人： Faserverbund Innovations UG (haftungsbeschränkt)

发明人： DIERKES, Dominik

IPC分类号： B29C70/30 ,  B29C70/44 ,  B29C70/54 ,  B29C73/10 ,  B32B37/10

CPC分类号： B29C73/10 ,  B29C70/546 ,  B29C70/544 ,  B29C70/30 ,  B29C70/44 ,  B29B11/16

公开(公告)号：EP2254750B1

公开(公告)日：2018-07-04

申请号：EP08730446.5

申请日：2008-02-22

申请人： Compagnie Générale des Etablissements Michelin

发明人： CHEBLI, Adib, Tony ,  IKONOMOV, Metodi, Lubenov

IPC分类号： B29C73/12 ,  B29C73/10 ,  B29L30/00

CPC分类号： B29C73/12 ,  B29C73/10 ,  B29L2030/00

摘要： Methods, computer program products, and apparatus for stitching the interior surface of a tire, the steps of the method including rotating the tire about a central rotational axis, applying a force to maintain the tire in a substantially radial fixed position relative to a stitching wheel; applying a predetermined force to the interior surface of the tire with the stitching wheel, the stitching wheel contacting the interior surface of the tire while the tire is rotating; and, mechanically translating the stitching wheel laterally across the interior of the tire during tire rotation.

公开(公告)号：EP2361742B1

公开(公告)日：2018-06-27

申请号：EP09827583.7

申请日：2009-11-18

申请人： Mitsubishi Heavy Industries, Ltd.

发明人： KANEMASU Masayuki ,  NISHIYAMA Shigeru ,  HORIZONO Hideki

IPC分类号： B29C73/02 ,  B29C70/44 ,  B29K101/10 ,  B29K105/08 ,  B29C43/12

CPC分类号： B29C43/3642 ,  B29C43/12 ,  B29C73/025 ,  B29C73/10 ,  B29C2043/3644 ,  B29K2105/0002 ,  B29K2105/0872

摘要： In manufacturing composite material by curing fluid, strength deterioration of the composite material due to repair before the fluid is cured is reduced. A suction hole is formed in a bag film (3) for sealing a space for fibers being impregnated with resin, after start of impregnation. The suction hole is covered by a plate (56) with holes (57). The resin is sucked from the space through the plate (56). According to such composite material manufacturing method, a defect, which occurs during fibers are impregnated with resin, can be repaired before the resin is cured without causing disorder and damage in the fibers. In a composite material formed from one repaired in the above way, the repaired portion is strong, namely, there is no strength deterioration due to repair after curing, and thus, the material is preferred as compared with a composite material which is repaired after resin is cured.

公开(公告)号：EP3325262A1

公开(公告)日：2018-05-30

申请号：EP15739266.3

申请日：2015-07-17

申请人： LM Wind Power International Technology II ApS

发明人： DRACHMANN HAAG, Michael

IPC分类号： B29D99/00 ,  F03D1/06

CPC分类号： F03D1/0675 ,  B29C73/10 ,  B29D99/0025 ,  B29K2055/02 ,  B29K2067/00 ,  B32B5/02 ,  B32B27/08 ,  B32B27/12 ,  B32B27/302 ,  B32B27/308 ,  B32B27/365 ,  B32B37/02 ,  B32B37/06 ,  B32B37/1018 ,  B32B37/24 ,  B32B2250/03 ,  B32B2250/24 ,  B32B2255/10 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2270/00 ,  B32B2305/076 ,  B32B2305/72 ,  B32B2307/554 ,  B32B2355/02 ,  B32B2367/00 ,  B32B2369/00 ,  B32B2603/00 ,  F03D80/50 ,  F05B2230/90 ,  F05B2240/2022 ,  F05B2240/30 ,  F05B2280/6003 ,  Y02E10/721 ,  Y02P70/523

摘要： The invention relates to a wind turbine blade having a leading edge erosion shield. The erosion shield comprises an inner layer of a first thermoplastic material, the inner layer being an integral part of the shell body of the wind turbine blade. The erosion shield further comprises an outer layer of a second thermoplastic material attached to the inner layer.

公开(公告)号：EP3261834A1

公开(公告)日：2018-01-03

申请号：EP15883635.3

申请日：2015-12-21

申请人： Sikorsky Aircraft Corporation

发明人： DEW, Nathaniel ,  DENAVIT, Paul H. ,  GARHART, Jonathan K. ,  CAWTHRA, Neil W.

IPC分类号： B32B3/12

CPC分类号： B29C73/10 ,  B29C33/0016 ,  B29C35/02 ,  B29C35/0227 ,  B29C37/0075 ,  B29C70/00 ,  B29C73/04 ,  B29C2035/0827 ,  B29C2791/001 ,  B29K2105/0872 ,  B29K2307/04 ,  B29L2031/3082

摘要： A method of repairing a composite structure or forming a component of a part is provided. The method includes releasably laying up of a first member that is curable at a first temperature at or above a constrained temperature limit of the composite structure or part, releasably laying up of a second member on the first member that is curable at a second temperature below the constrained temperature limit, curing the second member into a scaffold at the second temperature at the composite structure or part, transferring the first member and the scaffold remotely from the composite structure or part for first member curing and removing the cured first member from the scaffold for bonding of the cured first member to the composite structure or part.

公开(公告)号：EP2920009B1

公开(公告)日：2018-01-03

申请号：EP12888379.0

申请日：2012-11-15

申请人： Compagnie Générale des Etablissements Michelin

发明人： WESTON, David, Alan ,  HODGKINSON, Raymond, Leslie

IPC分类号： H01L41/053

CPC分类号： H01L41/047 ,  B23K1/0016 ,  B23K31/02 ,  B29C73/10 ,  B29L2030/00 ,  B60C19/00 ,  B60C23/0411 ,  B60C23/0493 ,  B60C99/00 ,  H01L41/293 ,  H01L41/313 ,  H05K1/18 ,  H05K3/34 ,  H05K2203/04 ,  H05K2203/1194 ,  Y10T29/42

摘要： A conductive terminal structure for a piezoelectric device used as part of a tire mountable apparatus is provided. Unlike known electrical connection structures which include a plurality of conductive terminals that are all exposed through a single insulating layer of the piezoelectric device, such as a top layer of the piezoelectric device, the electrical connection structure can be arranged in a one up, one down configuration. In this configuration, at least one conductive terminal is exposed through a top insulating layer of the piezoelectric device. In addition, at least one conductive terminal of a piezoelectric component is exposed through a bottom insulating layer of the piezoelectric device. The electrical connection structure can be used in combination with a connector assembly design to preserve the integrity of the electrical connection between the electrical and mechanical connection structure and a printed circuit board.

公开(公告)号：EP2750974B1

公开(公告)日：2017-10-04

申请号：EP12753212.5

申请日：2012-08-07

申请人： Airbus Operations Limited

发明人： TIGHE, David

IPC分类号： B64F5/00 ,  B29C73/10 ,  B64C1/06

CPC分类号： G01M5/0016 ,  B29C73/10 ,  B64C1/064 ,  B64C3/00 ,  B64C3/182 ,  B64C3/187 ,  B64C3/26 ,  B64F5/00 ,  B64F5/60 ,  Y10T29/49732 ,  Y10T29/49826

摘要： The present invention provides an aircraft structure comprising a structural component and a set of reinforcing straps for reinforcing the structural component, wherein the set comprises a first reinforcing strap having an inner and outer surface, wherein the inner surface is attached to a first surface of the structural component such that the first reinforcing strap extends longitudinally along the structural component and a second reinforcing strap having an inner and outer surface, wherein the inner surface is attached to the outer surface of the first reinforcing strap such that the second reinforcing strap extends longitudinally along the first reinforcing strap. The invention also provides an aircraft, a method of reinforcing an aircraft structure and a method of inspecting an aircraft structure.

摘要翻译： 本发明提供了一种飞机结构，其包括结构部件和用于加强结构部件的一组加强带，其中该组包括具有内表面和外表面的第一加强带，其中内表面附接到 使得所述第一加强带沿着所述结构部件纵向延伸，以及具有内表面和外表面的第二加强带，其中所述内表面附接到所述第一加强带的外表面，使得所述第二加强带沿着所述结构部件纵向地 第一条增强带。 本发明还提供了一种飞机，一种加强飞机结构的方法以及一种检查飞机结构的方法。

公开(公告)号：EP3209489A1

公开(公告)日：2017-08-30

申请号：EP15790192.7

申请日：2015-10-22

申请人： Short Brothers Plc

发明人： MCKIBBIN, Andrew

IPC分类号： B29C73/02 ,  B29C70/44

CPC分类号： B29C73/025 ,  B29C70/443 ,  B29C73/02 ,  B29C73/10 ,  B29K2063/00 ,  B29K2105/0872 ,  B29K2307/04

摘要： Apparatus and methods for manufacturing and repairing fibre-reinforced composite materials are disclosed. In various embodiments, the apparatus and methods disclosed herein use a resin retaining/releasing device comprising resin having a viscosity that is temperature dependent for infusion into a region of a part. The resin retaining/releasing device may include a first sheet and an opposite second sheet at least partially enclosing the quantity of resin. The first sheet and the second sheet may be gas-permeable. The second sheet may be substantially resin-impermeable when the viscosity of the resin is above a threshold viscosity and resin-permeable when the viscosity of the resin is below the threshold viscosity.

摘要翻译： 披露了用于制造和修复纤维增强复合材料的设备30和方法。 在各种实施例中，本文公开的设备和方法使用树脂保持/释放装置14，树脂保持/释放装置14包括树脂16，树脂16具有取决于温度的粘度以便灌注到部件的区域中。 树脂保持/释放装置可以包括第一片材18和至少部分地包围一定量的树脂的相对的第二片材20。 第一片和第二片可以是透气的。 当树脂的粘度高于阈值粘度时，第二片基本上可以是树脂不可渗透的，并且当树脂的粘度低于阈值粘度时，第二片可以是树脂可渗透的。 真空屏障40可以覆盖注入区域32或部分34; 在屏障40和部分34之间的密封可以通过密封构件42实现。真空口44可以与第一体积41流体连通。加热毯46可以设置在第二体积54内。树脂的量可以从 输液区域。