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1. 发明授权

US10052826B2 Bulk resin infusion 有权
公开(公告)号：US10052826B2
公开(公告)日：2018-08-21
申请号：US13279308
申请日：2011-10-23
申请人： Robert Dennis Hawkins
发明人： Robert Dennis Hawkins
IPC分类号： B29C45/14 , B29C70/34 , B29C70/44 , B29C70/46 , B29L31/00
CPC分类号： B29C70/342 , B29C70/443 , B29C70/465 , B29L2031/779
摘要： A method for performing resin infusion into a dry reinforcement on a layup mandrel comprises placing resin at a resin zone on the mandrel; bagging the reinforcement and the resin with a bagging film; heating the resin while applying compaction pressure to the bagging film to cause the resin to be infused into the reinforcement; and creating a pressure differential outside of the bagging film over the resin zone to control rate and pressure at which the resin is infused into the reinforcement. As a result, the resin pressure and infusion rate are controlled independently of the compaction pressure on the reinforcement.

2. 发明申请

US20180162073A1 TAPE-SHAPED PREPREG AND FIBER-REINFORCED MOLDED OBJECT 审中-公开
公开(公告)号：US20180162073A1
公开(公告)日：2018-06-14
申请号：US15574893
申请日：2016-05-18
申请人： KABUSHiKI KAISHA KOBE SEIKO SHO (KOBE STEEL, LTD.)
发明人： Takayasu FUJIURA , Naoyuki TASHIRO
IPC分类号： B29C70/38 , B29B15/12 , B29B15/14 , C08J5/04 , B29C70/34
CPC分类号： B29C70/388 , B29B15/122 , B29B15/14 , B29C69/008 , B29C70/345 , B29C70/465 , C08J5/041 , C08J5/24
摘要： An aspect of the present invention is a tape-shaped prepreg which includes a plurality of unidirectionally oriented fibers and a binder infiltrated into these fibers. The tape-shaped prepreg is characterized by having an average thickness of 50 μm to 150 μm and a content percentage of these fibers of 30 vol % to 60 vol %. The prepreg is further characterized in that: a fractal dimension D of a coefficient of variation Cv(n) is 0.4 to 1.5; and a degree of orientation P, expressed by the following equation, is 0.8 or greater and less than 1.0: Degree of orientation P=1−((minor-axis length of approximate ellipse)/(major-axis length thereof)).

3. 发明申请

US20180162019A1 IMPROVEMENTS IN OR RELATING TO THREE DIMENSIONAL MOULDINGS 审中-公开
公开(公告)号：US20180162019A1
公开(公告)日：2018-06-14
申请号：US15579276
申请日：2016-06-23
申请人： Hexcel Reinforcements SASU
发明人： Mayeul Ducrot
IPC分类号： B29C43/02 , B29C33/42
CPC分类号： B29C43/021 , B29C33/42 , B29C70/465 , B29C2043/026 , B29C2793/0081 , B29K2105/0863 , B29K2105/12 , B29K2105/256 , B29L2031/30
摘要： This invention relates to a moulding compound blank, a method for compression moulding the same and the resulting product. The blank comprises a moulding compound comprising a fibrous reinforcement material and a resin material wherein the moulding compound comprises a flow guide (6, 7, 8) located at the surface of the blank for directing flow of the moulding compound within the cavity of the compression mould during compression moulding.

4. 发明授权

US09981429B2 Press moulding method 有权
公开(公告)号：US09981429B2
公开(公告)日：2018-05-29
申请号：US14404664
申请日：2013-05-30
申请人： Gurit (UK) Ltd.
发明人： Daniel Thomas Jones , Stephen Patrick Main , Martin James Starkey , Peter Jennings , Gregory Aratoon
IPC分类号： B29C70/46 , B29C43/18 , B29C70/34 , B29C70/66 , B29C70/08 , B29C43/00 , B29C70/44 , B29C43/20 , B29C43/56 , B29K63/00 , B29K105/08 , B29K307/04 , B29K309/08 , B29L9/00 , B29L31/30
CPC分类号： B29C70/465 , B29C43/00 , B29C43/18 , B29C43/20 , B29C43/203 , B29C70/086 , B29C70/345 , B29C70/443 , B29C70/46 , B29C70/467 , B29C70/66 , B29C2043/563 , B29K2063/00 , B29K2105/0872 , B29K2105/0881 , B29K2307/04 , B29K2309/08 , B29L2009/00 , B29L2031/3005
摘要： A method of press molding a molding material to form a molded part of fiber-reinforced resin matrix composite material, the method comprising the steps of:i. providing a mold tool having a lower mold part and an upper mold part, the upper mold part having a first molding surface for molding a first molded surface of the molded part and the lower mold part having a second molding surface for molding a second molded surface of the molded part; ii. providing a multilaminar panel of molding material comprising at least one layer of fibers and at least one layer of resin, the multilaminar panel having first and second opposite major surfaces; iii. locating the molding material in the mold tool; iv. progressively closing the mold tool to define a substantially closed mold cavity containing the molding material, the closing step including: a. a preliminary closing phase to achieve mutual engagement between the lower and upper mold parts, b. a secondary closing phase after engagement between the lower and upper mold parts with the mold tool partially closed to define a closed intermediate cavity containing the molding material, the closed intermediate cavity being larger than the molded part and the first molding surface of the upper mold part being spaced from the first major surface by a spacing distance, in the secondary phase air being at least partially evacuated from the closed intermediate cavity while the first molding surface of the upper mold part is spaced from the first major surface to provide a vacuum pressure, and c. a tertiary closing phase after the vacuum pressure has been provided in the closed intermediate cavity, the tertiary phase having: I. a first stage prior to both the first molding surface contacting the first major surface and the second molding surface contacting the second major surface, and II. a second compression stage after both the first molding surface has contacted the first major surface and the second molding surface has contacted the second major surface, the closure speed of relative movement between the lower and upper mold parts being higher in the first stage than in the second compression stage; v. applying pressure to the molding material in the mold cavity to configure the molding material in a fully molded shape; and vi. substantially fully curing the resin to form a molded part from the molding material.

5. 发明授权

US09889612B2 Automated resin and fiber deposition for resin infusion 有权
公开(公告)号：US09889612B2
公开(公告)日：2018-02-13
申请号：US14521455
申请日：2014-10-22
申请人： The Boeing Company
发明人： Michael D. Silcock , Christopher A. Howe , Brice A. Johnson
IPC分类号： B29C70/38 , B29C70/44 , B29C70/46 , B29C65/00 , B29C70/54 , B29K105/08
CPC分类号： B29C70/386 , B29C66/9241 , B29C70/388 , B29C70/465 , B29C70/545 , B29C2793/0027 , B29K2105/0872 , Y10T156/1007 , Y10T156/1378 , Y10T156/17
摘要： A composite structure is fabricated by laying up at least one ply of fiber reinforcement and at least one layer of resin on a tool. The resin film layer is formed by laying strips of resin film. The fiber reinforcement is infused with resin from the resin layer.

6. 发明申请

US20170151769A1 METHODS OF FORMING A THINNED PREPREG SHEET 审中-公开
公开(公告)号：US20170151769A1
公开(公告)日：2017-06-01
申请号：US15429867
申请日：2017-02-10
申请人： THE BOEING COMPANY
发明人： Keith Daniel Humfeld
IPC分类号： B32B37/08 , B32B38/08
CPC分类号： B32B37/08 , B29C70/465 , B29C70/506 , B32B38/08 , B32B2038/0024 , B32B2305/076 , C08J5/24
摘要： A method of forming a thinned prepreg sheet is disclosed. The method comprises providing a first precursor sheet comprising reinforcement fibers impregnated with a matrix resin in a first state. The method also comprises forming a second precursor sheet having a first thickness by cooling the first precursor sheet until the matrix resin is transformed from the first state to a second state. The method further comprises forming a crushed sheet comprising interstices having an average size by crushing the second precursor sheet, where the crushed sheet has a second thickness. The method also comprises forming the thinned prepreg sheet by heating the crushed sheet until the matrix resin is transformed from the second state to a third state. The thinned prepreg sheet has a third thickness less than the first thickness of the second precursor sheet.

7. 发明授权

US09662854B2 Sandwich composite component and production process therefor 有权
公开(公告)号：US09662854B2
公开(公告)日：2017-05-30
申请号：US14388304
申请日：2012-12-21
申请人： DAIMLER AG
发明人： Benno Stamp , Tobias Blumenstock , Roman Wittig
IPC分类号： B32B3/12 , B29C70/46 , B32B27/06 , B32B27/10 , B29C70/08 , B32B37/14 , B29C43/20 , B29C43/52 , B32B3/04 , B32B37/04 , B29L31/60 , B29L31/30 , B29K1/00 , B29K23/00 , B29K101/12 , B29K105/04 , B29K105/06 , B29K105/00 , B29K309/08
CPC分类号： B32B3/12 , B29C43/206 , B29C43/52 , B29C70/086 , B29C70/088 , B29C70/465 , B29K2001/00 , B29K2023/12 , B29K2101/12 , B29K2105/045 , B29K2105/06 , B29K2105/253 , B29K2309/08 , B29L2031/30 , B29L2031/608 , B32B3/04 , B32B27/065 , B32B27/10 , B32B37/04 , B32B37/146 , B32B2250/05 , B32B2250/24 , B32B2305/022 , Y10T428/236
摘要： A sandwich component (10) having a honeycomb core layer (4) and at least one fiber-reinforced thermoplastic outer layer (3) and the corresponding production method. The outer layer (3) is connected to the honeycomb core layer (4) by a thermoplastic material. At least one side of the sandwich component (10 has a decorative layer (1,1′), which is arranged on the outer layer (3). The sandwich component (10) furthermore has at least one foam layer (2), which is arranged between the outer layer (3) and the decorative layer (1,1′), and which is connected to the outer layer (3) and the decorative layer (1,1′).

8. 发明申请

US20170144389A1 MANUFACTURING METHOD FOR THERMOFORMING A FIBER-REINFORCED COMPOSITE LAMINATE 审中-公开
公开(公告)号：US20170144389A1
公开(公告)日：2017-05-25
申请号：US15351793
申请日：2016-11-15
申请人： Airbus Operations GmbH
发明人： Benjamin Ehring
IPC分类号： B29C70/46 , B29C65/00 , B29C65/02 , B29C70/54 , B29C35/08
CPC分类号： B29C70/467 , B29C35/0805 , B29C65/02 , B29C66/721 , B29C70/465 , B29C70/545 , B29C70/56 , B29C2035/0822 , B29K2105/105 , B29L2031/3076
摘要： A manufacturing method for thermoforming a fiber-reinforced composite laminate with fiber rovings embedded within a thermoplastic matrix includes: mounting fiber rovings to a transport frame, the mounted rovings being arranged to form a support grid layer laterally framed by the transport frame, each roving being mounted on both ends under tension to the transport frame; placing a matrix material layup of thermoplastic material on top of the support grid layer, wherein the tension of the rovings and a density of the support grid layer are configured such that the support grid layer supports the matrix material layup; softening the matrix material layup by heating the support grid layer together with the matrix material layup within a heating station; forming a semi-finished composite laminate by pressing the support grid layer together with the softened matrix material layup; and consolidating the semi-finished composite laminate to form the fiber-reinforced composite laminate.

9. 发明授权

US09643363B2 Manufacture of a structural composites component 有权
公开(公告)号：US09643363B2
公开(公告)日：2017-05-09
申请号：US13127960
申请日：2009-11-05
申请人： Ken Kendall
发明人： Ken Kendall
IPC分类号： B29C70/46 , B29C43/18 , B29C33/04 , B29C33/10 , B29C43/58 , B29K105/06
CPC分类号： B29C70/465 , B29C33/04 , B29C33/10 , B29C43/18 , B29C2043/5816 , B29K2105/06
摘要： A method of manufacturing a structural composites component in a mold comprising first and second mold halves is provided. The method comprises the steps of providing a fiber or fabric preform, providing a resin layer that is separate from the preform, inserting one of the preform or the resin layer into the first mold half of the mold, then separately inserting the other of the preform or the resin layer into the first mold half such that the one of the preform or the resin layer is disposed on top of the other of the preform or the resin layer in the first mold half. The second mold half is then closed over the first mold half and the mold is pressurized in a compression press to cause the resin film to impregnate the preform, the mold being maintained at a constant temperature throughout the method of manufacture.

10. 发明申请

US20170066201A1 Method for Producing a Sandwich Component and Sandwich Component 审中-公开
标题翻译：三明治成分和三明治成分的制备方法
公开(公告)号：US20170066201A1
公开(公告)日：2017-03-09
申请号：US15113746
申请日：2014-12-16
申请人： Daimler AG
发明人： Hubert BIEDER , Tobias BLUMENSTOCK , Benno STAMP , Roman WITTIG
IPC分类号： B29C70/08 , B32B5/24 , B32B27/32 , B32B27/12 , B32B27/36 , B29C70/48 , B32B5/06
CPC分类号： B29C70/086 , B29C45/14008 , B29C45/1418 , B29C45/14336 , B29C45/14786 , B29C51/145 , B29C70/465 , B29C70/48 , B29C2045/0093 , B29D99/0021 , B29L2031/3005 , B29L2031/3014 , B32B5/06 , B32B5/245 , B32B27/12 , B32B27/32 , B32B27/36 , B32B37/0076 , B32B37/04 , B32B37/1027 , B32B37/203 , B32B38/0004 , B32B2038/008 , B32B2305/022 , B32B2305/07 , B32B2305/18 , B32B2305/70 , B32B2307/738 , B32B2309/02 , B32B2309/12 , B32B2605/003
摘要： A method for producing a sandwich component, in particular an inner trim component for a motor vehicle, is disclosed. The method begins with a core layer made from a foamed plastic and a cover layer which includes reinforcing fibers and plastic fibers. The plastic of the core layer has a first melting temperature which is higher than the second melting temperature of the plastic fibers of the cover layer. By the core layer being arranged on the cover layer, a multilayer composite is created. This multilayer composite can be further processed into a semi-finished product. The multilayer composite or the semi-finished product is then heated in a heating device to a temperature which is lower than the first melting temperature but therefore higher than the second melting temperature. Then the heated multilayer composite or the semi-finished product is formed in a forming tool in order to produce the sandwich component.
摘要翻译：公开了一种用于制造三明治组件的方法，特别是用于机动车辆的内饰件。该方法开始于由发泡塑料制成的芯层和包括增强纤维和塑料纤维的覆盖层。芯层的塑料具有比覆盖层的塑料纤维的第二熔融温度高的第一熔融温度。通过芯层布置在覆盖层上，形成多层复合材料。该多层复合材料可以进一步加工成半成品。然后将多层复合材料或半成品在加热装置中加热到低于第一熔融温度但因此高于第二熔融温度的温度。然后，在成形工具中形成加热的多层复合材料或半成品，以制造夹层组件。

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