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51. 发明申请

US20120196083A1 PROCESS AND APPARATUS FOR PRODUCING BEAM MEMBER 有权
标题翻译：生产光束成员的工艺和设备
公开(公告)号：US20120196083A1
公开(公告)日：2012-08-02
申请号：US13500521
申请日：2010-10-13
申请人： Tatsuya Hanawa , Tamotsu Suzuki
发明人： Tatsuya Hanawa , Tamotsu Suzuki
IPC分类号： B32B3/04 , B32B38/08 , B32B37/12 , B32B38/00
CPC分类号： B29C70/50 , B29B11/16 , B29C70/865 , B29D99/0003 , B29D99/0007 , B29L2031/008 , Y10T156/1051 , Y10T428/24264
摘要： A process for producing a beam member formed by a reinforcing fiber base material which has a web portion and at least a pair of flange portions extending to both sides via at least a branching point from the web portion, at a cross-sectional surface orthogonal to a longitudinal direction of the beam member, and by a shaped filler which fills a gap having a wedge shape formed at the branching point, is provided. The shaped filler is produced by: (A) a filler supply process for supplying a filler member configured by reinforcing fibers; (B) a preshaping process for providing a preshaped filler having at least a wedge projection portion, by pressurizing the filler member by a preshaping mold; and (C) a filler deforming process for providing a shaped filler by deforming the preshaped filler.
摘要翻译：一种用于制造由增强纤维基材形成的梁构件的方法，所述加强纤维基材具有腹板部分和至少一对凸缘部分，所述至少一对凸缘部分在与所述腹板部分的至少一个分支点延伸到两侧的横截面处，提供了梁构件的纵向方向，以及填充在分支点处形成有楔形的间隙的成形填料。成形填料是通过以下方法制造的：（A）用于供给由增强纤维构成的填料构件的填料供给工序; （B）预成型方法，用于提供具有至少楔形突出部分的预成型填料，通过预成型模具对填料构件加压; 和（C）通过使预成形填料变形来提供成形填料的填料变形过程。

52. 发明授权

US08142583B2 Method for production of several fibre composite components 有权
标题翻译：多种纤维复合材料的生产方法
公开(公告)号：US08142583B2
公开(公告)日：2012-03-27
申请号：US12375828
申请日：2007-07-03
申请人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
发明人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
IPC分类号： B29C70/54 , B29C70/30
CPC分类号： B29C70/443 , B29C70/086 , B29C70/50 , B29C70/545 , B29C70/865 , B29C2793/009 , B29L2031/003 , Y02T50/43 , Y10T156/10 , Y10T428/24628
摘要： A method for production of fiber composite components, particularly suitable for the production of profiles of complicated shape with varying profile cross-section and/or with at least parts with curved lines, such as used for the production of aircraft, for example. The method (a) produces plural core components, (b) separates application of a first fiber material to each of the core components, (c) assembles the core components provided with the first fiber material to form a sequence of core components, (d) applies a second fiber material common to the core component sequence along at least one side of the core component sequence, provided with the first fiber material, (e) impregnates and hardens the first and second fiber materials to form a fiber-reinforced component body, and (f) separates the component body into plural sections as represented by the fiber composite components.
摘要翻译：一种生产纤维复合材料组件的方法，特别适用于生产具有不同轮廓横截面的复杂形状的轮廓和/或至少具有弯曲线的部件，例如用于生产飞行器的轮廓。方法（a）产生多个核心部件，（b）将第一纤维材料应用于每个核心部件，（c）组装具有第一纤维材料的芯部件以形成核心部件序列（d ）沿着核心部件序列的至少一侧施加第一纤维材料，所述第二纤维材料沿核芯部件序列的至少一侧施加第一纤维材料，（e）浸渍并硬化第一和第二纤维材料以形成纤维增强部件体，和（f）将组分体分成如纤维复合组分所表示的多个部分。

53. 发明申请

US20120049000A1 Composite Aircraft Joint 有权
公开(公告)号：US20120049000A1
公开(公告)日：2012-03-01
申请号：US12868886
申请日：2010-08-26
申请人： Kirk Ben Kajita , Douglas Allen Frisch
发明人： Kirk Ben Kajita , Douglas Allen Frisch
IPC分类号： B64C1/26 , B32B15/00 , B32B37/24 , B64C3/00 , B32B37/02
CPC分类号： B64C3/26 , B29C70/088 , B29C70/865 , B29K2705/00 , B29L2031/3085 , B64C1/26 , Y02T50/43 , Y10T156/10 , Y10T428/24612
摘要： A method and apparatus comprises a first number of layers of a composite material for a wing, a second number of layers of the composite material for the wing, and a metal layer located between the first number of layers and the second number of layers in the wing. The metal layer has a first thickness at a first area configured to receive a number of fasteners and a second thickness at a second area.

54. 发明申请

US20120018075A1 Hockey Blade with Wrapped, Stitched Core 有权
标题翻译：曲棍球包裹，缝线芯
公开(公告)号：US20120018075A1
公开(公告)日：2012-01-26
申请号：US13189026
申请日：2011-07-22
申请人： Adam Gans
发明人： Adam Gans
IPC分类号： B32B7/08
CPC分类号： A63B59/70 , A63B59/20 , A63B2102/24 , A63B2209/023 , B29C70/086 , B29C70/30 , B29C70/347 , B29C70/54 , B29C70/543 , B29C70/86 , B29C70/865 , B29K2105/04 , B29K2105/0854 , B29K2105/253 , B29K2667/00 , B29K2707/04 , B29K2715/003 , B29L2031/52
摘要： A construct for a hockey blade that includes a foam core. The foam core includes a first core face, a second core face, and a core edge. A first layer of resin preimpregnated tape is wrapped continuously around the first core face, the core edge and the second core face. A thread is stitched along the first layer of preimpregnated tape. A second layer of resin preimpregnated tape wrapped continuously around the first layer of resin preimpregnated tape.
摘要翻译：包括泡沫芯的曲棍球刀的构造。泡沫芯包括第一芯面，第二芯面和芯边。树脂预浸胶带的第一层被连续包裹在第一芯面，芯边缘和第二芯面上。沿着第一层预先浸渍的胶带缝合线。第二层树脂预浸渍的条带围绕第一层树脂预浸胶带连续缠绕。

55. 发明申请

US20110318513A1 METHOD FOR MAKING A FORM PARTY BY 3D WEAVING, AND RESULTING FORM PART 审中-公开
标题翻译：通过3D制作制作形式的方法，以及形成部分
公开(公告)号：US20110318513A1
公开(公告)日：2011-12-29
申请号：US13141852
申请日：2009-12-22
申请人： David Marsal , Xavier Millier
发明人： David Marsal , Xavier Millier
IPC分类号： B32B1/08 , B29C70/40
CPC分类号： B29C70/865 , B29B11/16 , B29C33/505 , B29C70/24 , B29C70/48 , B29L2031/3067 , D03D3/02 , D03D11/02 , D03D25/005 , D10B2505/02 , Y10T428/1352
摘要： A hollow part is obtained by 3D weaving and by impregnation. A preform is made by three-dimensional weaving and by ensuring partial non-interlinking during the weaving, thereby subsequently making it possible to define a cavity within the woven mass, and then to stabilize a shape of the preform during an impregnation stage.
摘要翻译：通过3D编织和浸渍获得中空部分。通过三维织造制造预成型件，并且通过在织造期间确保部分非互连，由此随后可以在织造物质内限定空腔，然后在浸渍阶段期间稳定预成型件的形状。

56. 发明申请

US20110311172A1 COMPONENT AND METHOD FOR THE PRODUCTION THEREOF 审中-公开
标题翻译：组件及其生产方法
公开(公告)号：US20110311172A1
公开(公告)日：2011-12-22
申请号：US13203783
申请日：2010-02-24
申请人： Egon Frank
发明人： Egon Frank
IPC分类号： F16C19/00 , B32B37/16
CPC分类号： F16C33/34 , B29C70/025 , B29C70/086 , B29C70/32 , B29C70/865 , B29L2031/045 , B32B1/08 , B32B5/024 , B32B5/18 , B32B5/22 , B32B5/245 , B32B5/30 , B32B9/005 , B32B9/045 , B32B9/046 , B32B9/047 , B32B9/048 , B32B27/065 , B32B27/08 , B32B27/12 , B32B27/14 , B32B27/18 , B32B2260/021 , B32B2260/025 , B32B2260/046 , B32B2262/0269 , B32B2262/0276 , B32B2262/065 , B32B2262/10 , B32B2262/101 , B32B2262/106 , B32B2264/06 , B32B2264/105 , B32B2264/107 , B32B2307/308 , B32B2307/50 , B32B2307/56 , B32B2307/714 , B32B2307/718 , B32B2597/00 , F16C19/52 , F16C33/12 , F16C33/122 , F16C33/14 , F16C33/62 , F16C33/64 , F16C2223/42 , F16C2300/14
摘要： The invention relates to a component (1) with an axis (A) consisting of at least a first layer (2) in the form of a tubular body and at least a second layer (3) which is arranged outside and/or inside of the tubular body (2) and which is firmly connected with the first layer (2). To make the element lightly and abrasive resistant simultaneously, the first layer (2) consists of a composite material, wherein the second layer (3) consists of a hard material. Furthermore, the invention relates to a method for the production of such an element.
摘要翻译：本发明涉及一种具有轴线（A）的部件（1），该轴线（A）至少包括管状体形式的第一层（2）和至少第二层（3），所述第二层（3）布置在管状体（2）并与第一层（2）牢固连接。为了使元件同时轻轻地耐磨，第一层（2）由复合材料组成，其中第二层（3）由硬质材料组成。此外，本发明涉及一种用于生产这种元件的方法。

57. 发明申请

US20110278761A1 METHOD OF PRODUCING A PANEL AND A CORE THEREFOR 有权
标题翻译：生产面板及其核心的方法
公开(公告)号：US20110278761A1
公开(公告)日：2011-11-17
申请号：US13130162
申请日：2009-11-19
申请人： Johannes Hendricus Alphonsus Peeters
发明人： Johannes Hendricus Alphonsus Peeters
IPC分类号： B29C45/14 , B32B3/00
CPC分类号： B29C45/14065 , B29C45/77 , B29C70/086 , B29C70/443 , B29C70/48 , B29C70/547 , B29C70/865 , B29K2105/08 , B29K2105/20 , Y10T428/24479
摘要： A method of producing a panel includes: placing an assembly including core elements and impregnatable material webs extending along and between the core elements on a mould, which assembly includes a first side and a second side which is situated opposite the first side, enclosing the assembly under a cover layer in a sealing manner with respect to the mould, introducing at least one inlet for injection material, which inlet ends at a first side of the assembly, connecting the space which is enclosed by the cover layer and the mould to a discharge, injecting injection material via the inlet on the first side of the assembly and causing the injection material to move along via paths formed by the material webs between the core elements, discharging air and/or gas from the enclosed space via the discharge via underpressure at a position which is at a different level to the position where the inlet ends.
摘要翻译：制造面板的方法包括：将包括芯元件和可浸渍材料网的组件放置在模具上并且在芯元件之间并且在模具之间，该组件包括与第一侧相对的第一侧和第二侧，包围组件在相对于模具的密封方式的覆盖层下方，引入至少一个用于注射材料的入口，该入口入口在组件的第一侧，将由覆盖层和模具包围的空间连接到排出口通过所述组件的第一侧上的入口注入注射材料，并且使得所述注射材料沿着由所述芯元件之间的所述材料网形成的通路径移动，通过所述排出通过负压从所述封闭空间排出空气和/或气体，位于与入口终止的位置不同的位置。

58. 发明授权

US08038408B2 Composite aerofoil 有权
标题翻译：复合机翼
公开(公告)号：US08038408B2
公开(公告)日：2011-10-18
申请号：US11262781
申请日：2005-11-01
申请人： Alison J. McMillan
发明人： Alison J. McMillan
IPC分类号： B32B5/02 , B64C27/46 , D03D11/00
CPC分类号： B29C70/222 , B29C70/865 , B29D99/0028 , B29L2031/08 , D03D25/005 , F01D5/147 , F01D5/282 , F05C2201/025 , F05D2230/60 , F05D2240/301 , F05D2250/20 , F05D2250/293 , F05D2300/2261 , F05D2300/2283 , F05D2300/44 , F05D2300/603 , F05D2300/612 , F05D2300/614 , Y02E10/721 , Y02T50/43 , Y02T50/672 , Y02T50/673 , Y10T442/20 , Y10T442/2975 , Y10T442/3195
摘要： A composite blade (26) comprises a three-dimensional arrangement of reinforcing fibres (58) and a matrix material (60) infiltrated around the three-dimensional arrangement of woven reinforcing fibres (60). The three-dimensional arrangement of woven reinforcing fibres (58) defines a plurality of cavities (56) within the aerofoil (28). The composite blade (26) comprises an aerofoil portion (38) and a root portion (36). The aerofoil portion (38) comprises a leading edge (44), a trailing edge (46), a concave pressure surface wall (50), a convex suction surface wall (52) and a tip (48). The aerofoil portion (36) comprises a plurality of webs (54) extending between, and being secured to, the concave pressure surface wall (50) and the convex suction surface wall (52) to produce a Warren girder structure. The three-dimensional arrangement of woven reinforcing fibres (58) are arranged to produce the concave pressure surface wall (50), the convex suction surface wall (52) and the plurality of webs (54). The matrix material (60) is an organic resin and the reinforcing fibres (58) comprise carbon fibres.
摘要翻译：复合叶片（26）包括加强纤维（58）和渗透在编织增强纤维（30）的三维布置周围的基质材料（60）的三维排列。编织增强纤维（58）的三维布置在机翼（28）内限定多个空腔（56）。复合叶片（26）包括机翼部分（38）和根部（36）。机翼部分（38）包括前缘（44），后缘（46），凹压表面壁（50），凸起的吸力表面壁（52）和尖端（48）。机翼部分（36）包括在凹压表面壁（50）和凸起的吸入表面壁（52）之间延伸并固定到凸起的吸入表面壁（52）上并且固定到凸起的吸力表面壁（52）上的多个腹板（54），以产生沃伦梁结构。编织增强纤维（58）的三维布置被布置成产生凹压表面壁（50），凸形吸力表面壁（52）和多个腹板（54）。基质材料（60）是有机树脂，增强纤维（58）包含碳纤维。

59. 发明申请

US20110217160A1 COMPONENT COMPRISING A RESIN MATRIX 有权
标题翻译：包含树脂基质的组分
公开(公告)号：US20110217160A1
公开(公告)日：2011-09-08
申请号：US13025650
申请日：2011-02-11
申请人： Alison J. MCMILLAN
发明人： Alison J. MCMILLAN
IPC分类号： F01D25/24 , F01D5/14 , B32B5/16 , B32B17/06 , B32B27/06 , B32B27/04
CPC分类号： B29C66/721 , B29C65/564 , B29C65/62 , B29C66/004 , B29C66/1122 , B29C66/45 , B29C66/7212 , B29C66/72141 , B29C66/73752 , B29C66/8122 , B29C70/086 , B29C70/865 , B29C70/88 , B29K2027/18 , B29K2105/246 , B29L2009/00 , B32B37/0076 , B32B2305/076 , Y10T428/25 , Y10T428/30 , Y10T428/31504 , Y10T428/31544 , B29K2827/18 , B29K2307/04 , B29K2309/08
摘要： A composite material comprises plies 2, 4, 6, 8, which may be prepregs. Film elements 10 are provided between at least two adjacent ones of the plies 2, 4, 6, 8. The film elements are made from a release material which inhibits adhesion between regions of the resin on opposite sides of the respective film elements, and are randomly distributed. The film elements 10 provide delamination sites within the component. The component may be a test piece for assessing the delamination behaviour of the material. Alternatively, the delamination behaviour caused by the film elements 10 may have a useful purpose, for example to control regions of a component in which delamination occurs following events such as a bird strike on a fan blade of a gas turbine engine.
摘要翻译：复合材料包括层2,4,6,8，它们可以是预浸料。薄膜元件10设置在层叠件2,4,6,8中的至少两个相邻层之间。薄膜元件由剥离材料制成，该剥离材料抑制树脂在各个薄膜元件的相对侧上的区域之间的粘附，并且是随机分布。薄膜元件10提供部件内的分层位置。该组件可以是用于评估材料的分层行为的测试件。或者，由薄膜元件10引起的分层行为可以具有有用的目的，例如用于控制在诸如燃气涡轮发动机的风扇叶片上的鸟撞击之类的事件之后发生分层的部件的区域。

60. 发明授权

US07926233B2 Buildings, building walls and other structures 有权
标题翻译：建筑物，建筑物墙壁和其他结构
公开(公告)号：US07926233B2
公开(公告)日：2011-04-19
申请号：US11900987
申请日：2007-09-13
申请人： Glenn P. Schiffmann , Gerhard P. Schiffmann
发明人： Glenn P. Schiffmann , Gerhard P. Schiffmann
IPC分类号： E04C2/34
CPC分类号： E04C2/243 , B29C70/086 , B29C70/30 , B29C70/443 , B29C70/86 , B29C70/865 , B29D99/0014 , B29D99/0021 , B29L2007/002 , B29L2031/08 , B32B3/22 , B32B5/28 , B32B38/08 , B32B2038/0076 , B32B2305/022 , B32B2315/085 , B32B2607/00 , E02D27/02 , E04B1/0007 , E04B1/14 , E04B1/2612 , E04B2001/405 , E04C2/246 , E04C2/3405 , E04C2/38 , E04C2002/3455 , E04C2002/3461 , Y10T156/1016 , Y10T428/24994
摘要： A tough, water-proof building system, and methods of making the system elements and constructing buildings, which provides wall, ceiling, and floor structural panels and corresponding walls, ceilings, and floors. The walls can be designed to have vertical and horizontal strengths sufficient to be used in place of concrete, as an engineered solution, both above grade and below-grade, including in severe weather conditions, such that no concrete need be used except for floor slabs. Panels have inner and outer layers, and structurally reinforcing members. Structurally-reinforcing members extend, typically as a layer and/or stud, the full height of a wall, at spaced locations along the length of the wall. Spaces between the structurally reinforcing members are optionally filled with rigid foam. An optional reinforcing stud is attached to, or overlaid by, the inner layer, and extends inwardly into the building from what is otherwise the inner surface of the building panel.
摘要翻译：一个坚固耐用的防水建筑系统，以及制作系统元素和建筑物的方法，提供墙壁，天花板和地板结构板及相应的墙壁，天花板和地板。墙壁可以设计成具有足够的垂直和水平强度来代替混凝土，作为工程解决方案，高于等级和低于等级，包括在恶劣的天气条件下，除了地板以外，不需要使用混凝土。面板具有内层和外层，以及结构上加强构件。结构上加强构件通常沿着壁的长度在间隔开的位置处延伸通常为壁和/或螺柱，壁的整个高度。在结构上加强构件之间的空间任选地填充有刚性泡沫。一个可选的加强螺柱连接在内层上或由内层覆盖，并从建筑面板的内表面向内延伸到建筑物内。

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