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1. 发明授权

US08916252B2 Structural longitudinal composite joint for aircraft structure 有权
标题翻译：飞机结构结构纵向复合接头
公开(公告)号：US08916252B2
公开(公告)日：2014-12-23
申请号：US13377068
申请日：2009-06-11
申请人： Per Hallander , Mikael Petersson , Bjorn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin , Rustan Önnefors
发明人： Per Hallander , Mikael Petersson , Bjorn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin , Rustan Önnefors
IPC分类号： B32B3/14 , B32B7/14 , B29C70/58 , B29C65/50 , B29C65/00 , B29C70/30 , B32B3/02 , B32B5/26 , B32B5/28 , B64C3/20 , B64C3/26 , B29C65/48 , B29K31/00 , B29K63/00 , B29K67/00 , B29K71/00 , B29K79/00 , B29K81/00 , B29K101/10 , B29K101/12 , B29K105/06 , B29K105/16 , B29K307/00 , B29K309/02 , B29K309/08 , B29L31/30
CPC分类号： B29C70/58 , B29C65/4875 , B29C65/488 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/1142 , B29C66/43 , B29C66/435 , B29C66/721 , B29C70/30 , B29K2031/00 , B29K2063/00 , B29K2067/00 , B29K2071/00 , B29K2079/085 , B29K2081/04 , B29K2101/10 , B29K2101/12 , B29K2105/06 , B29K2105/167 , B29K2307/00 , B29K2309/02 , B29K2309/08 , B29L2031/3076 , B29L2031/3085 , B32B3/02 , B32B3/14 , B32B3/18 , B32B5/02 , B32B5/22 , B32B5/26 , B32B5/28 , B32B7/005 , B32B2250/20 , B32B2260/021 , B32B2260/046 , B32B2262/02 , B32B2262/101 , B32B2262/105 , B32B2262/106 , B32B2307/50 , B32B2307/558 , B32B2605/18 , B64C3/20 , B64C3/26 , Y02T50/43 , Y10T428/16 , Y10T428/17 , Y10T428/18 , B29C65/00
摘要： A structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure arranged within the composite joint. A method of producing a structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure and an aircraft structure comprising such structural composite parts.
摘要翻译：由预浸纤维层制成的结构复合部件。两个相邻的纤维层的边缘通过纵向复合接头连接，纵向复合接头通过布置在复合接头内的纳米结构构成。一种由预浸纤维层制成的结构复合部件的制造方法。两个相邻纤维层的边缘通过由纳米结构构成的纵向复合接头和包括这种结构复合部件的飞行器结构连接。

2. 发明授权

US08871126B2 Manufacturing method for trumpet spar and other curved objects 有权
标题翻译：小号翼梁和其他弯曲物体的制造方法
公开(公告)号：US08871126B2
公开(公告)日：2014-10-28
申请号：US11538442
申请日：2006-10-04
申请人： Max Krogager , Mikael Petersson , Björn Weidmann , Ingemar Turesson , Anders Westerdahl , Jan Vaara
发明人： Max Krogager , Mikael Petersson , Björn Weidmann , Ingemar Turesson , Anders Westerdahl , Jan Vaara
IPC分类号： B29C70/34 , B32B27/04 , B32B37/00 , B29C70/30 , B29C70/54 , B29L31/30 , B32B38/18
CPC分类号： B29C70/342 , B29C70/30 , B29C70/34 , B29C70/543 , B29D99/0003 , B29L2031/3085 , B32B27/04 , B32B37/0015 , B32B38/1808 , B32B38/1841 , B32B38/1866 , Y10T156/1051 , Y10T156/1092 , Y10T428/31504
摘要： A method for producing an object of composite material comprising the steps of: placing one or several prepregs on a plane surface, forming a fiber stack; lifting over the fiber stack to a molding tool; downforming the fiber stack; curing the downformed fiber stack; where the method also comprises the step of: orienting the fiber directions so that all fibers, when the fiber stack is lifted over to the molding tool, will cross an edge of the molding tool only once.
摘要翻译：一种用于生产复合材料的方法，包括以下步骤：将一个或多个预浸料放置在平面上，形成纤维堆叠; 将纤维堆叠提升到模具上; 降低纤维堆叠; 固化下降的纤维堆叠; 其中该方法还包括以下步骤：使光纤方向定向，使得当纤维堆叠被提升到模制工具时，所有纤维将仅跨过成型工具的边缘一次。

3. 发明申请

US20130240110A1 SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF 有权
标题翻译： SMOOTH表面成型工具及其制造
公开(公告)号：US20130240110A1
公开(公告)日：2013-09-19
申请号：US13642898
申请日：2010-02-04
申请人： Per Hallander , Mikael Petersson , Björn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
发明人： Per Hallander , Mikael Petersson , Björn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
IPC分类号： B64F5/00
CPC分类号： B64F5/0009 , B29C33/40 , B29C45/73 , B29C70/443 , B29C70/88 , B29K2105/165 , B64F5/10 , B82Y30/00 , H05B2214/04 , Y10T156/10
摘要： An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein.
摘要翻译：一种飞机制品复合成形工具及其制造方法。待成形的飞机制品包括包括外表面的复合材料。飞机制品复合成形工具包括由至少一个包括用于形成飞机制品的成形表面和外表面的上层制成的基体层压材料。上层包括嵌入其中的纳米丝结构。

4. 发明申请

US20120292439A1 ARTICLE WITH DE-ICING/ANTI-ICING FUNCTION 有权
标题翻译：具有去除/反制功能的文章
公开(公告)号：US20120292439A1
公开(公告)日：2012-11-22
申请号：US13522343
申请日：2010-01-14
申请人： Per Hallander , Mikael Petersson , Björn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
发明人： Per Hallander , Mikael Petersson , Björn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
IPC分类号： B64D15/12 , B64D45/02 , B82Y30/00
CPC分类号： H05B3/267 , B64D15/12 , B64D45/02 , H05B2214/02 , H05B2214/04
摘要： A structural article including an outer surface that serves as an aerodynamic surface when the structural article is subjected for an air stream. A resin matrix laminate includes an upper ply and a bottom ply. A heating element is arranged in contact with the bottom ply and coupled to a power supply unit in purpose to deice/anti-ice the outer surface. Each ply includes a thermally conductive filament structure having a filament orientation such that the prolongation of the filaments has an extension essentially perpendicular to the extension of the laminate. The thermally conductive filament structure of the upper ply is embedded in the upper ply in such way that at least a portion of the thermally conductive filament structure is exposed in the outer surface.
摘要翻译：包括当结构制品经受气流时用作空气动力学表面的外表面的结构制品。树脂基质层压体包括上层和底层。加热元件布置成与底层接触并且耦合到电源单元以用于对外表面进行去冰/防冰。每个层包括具有长丝取向的导热细丝结构，使得长丝的延伸具有基本上垂直于层压体的延伸部的延伸。上层的导热丝结构被嵌入上层，使得至少一部分导热丝结构在外表面露出。

5. 发明授权

US08282375B2 Method and device for shaping of composite material 失效
标题翻译：复合材料成型方法及装置
公开(公告)号：US08282375B2
公开(公告)日：2012-10-09
申请号：US13220514
申请日：2011-08-29
申请人： Mikael Petersson , Bjorn Weidmann
发明人： Mikael Petersson , Bjorn Weidmann
IPC分类号： B29C59/02
CPC分类号： B29C70/44 , B29C43/12 , B29C43/3642 , B29C53/025 , B29C53/04 , B29C2043/3644 , Y02T50/43
摘要： A device for shaping of an article of composite material. The device includes a tool including a top surface and side surface for shaping at least one blank of composite material into an article having a predetermined profile; and a air-tight foil. The device further includes at least one support arranged to be in supporting contact with the underside of the protruding part of the blank.
摘要翻译：用于成型复合材料制品的装置。该装置包括工具，其包括顶表面和侧表面，用于将复合材料的至少一个坯料成型为具有预定轮廓的制品; 和气密箔。该装置还包括布置成与坯件的突出部分的下侧支撑接触的至少一个支撑件。

6. 发明申请

US20110254207A1 HOT DRAPE FORMING BY MEANS OF A STIFFNESS CONTROLLED VACUUM BAG 有权
标题翻译：由硬度控制真空袋形成的热成型
公开(公告)号：US20110254207A1
公开(公告)日：2011-10-20
申请号：US13126990
申请日：2008-10-29
申请人： Per Hallander , Mikael Petersson
发明人： Per Hallander , Mikael Petersson
IPC分类号： B29C51/36
CPC分类号： B29C70/44
摘要： An apparatus and a method of conforming a blank onto forming surface sections of a forming tool by drawing a first vacuum against an elastic forming medium for transmitting forming forces from the elastic forming medium to the blank. The elastic forming medium is evacuated with the first vacuum for allowing the elastic forming medium to stretch and conform the blank to the forming surface sections. The elastic forming medium includes at least one void. A second vacuum is applied to the void for achieving a stiffened section of the elastic forming medium corresponding with the location of the void and corresponding with, when the elastic forming medium after the completion lies against the forming tool having the blank in between, a forming surface section of the forming tool where the blank requires a forming force being larger than that of surrounding sections of the elastic forming medium.
摘要翻译：通过对弹性成形介质抽取第一真空以将成形力从弹性成形介质传递到坯料，使毛坯与成形工具的成形表面部分相一致的装置和方法。弹性成形介质用第一真空抽真空，以使弹性成形介质拉伸并使毛坯与成形表面部分相一致。弹性成形介质包括至少一个空隙。第二真空被施加到空隙上，以实现对应于空隙的位置的弹性成形介质的加强部分，并且对应于当完成后的弹性成形介质抵靠在其间具有坯料的成形工具时，形成成形工具的表面部分，其中坯料需要大于弹性成形介质的周围部分的成形力。

7. 发明申请

US20100292049A1 METHOD AND A SYSTEM FOR BRAKING A VEHICLE 有权
标题翻译：用于制动车辆的方法和系统
公开(公告)号：US20100292049A1
公开(公告)日：2010-11-18
申请号：US12811626
申请日：2008-01-22
申请人： Mikael Petersson
发明人： Mikael Petersson
IPC分类号： B60T11/10 , G06F19/00 , B60T8/176 , B60T8/34 , B60W30/00 , F16D65/32 , F16D55/22 , B60T7/04 , B60W10/04 , B60W10/18 , B60W10/10
CPC分类号： B60T10/00 , B60T13/585 , B60T2220/04 , B60W30/18109 , B60W30/18136 , Y10T477/82
摘要： A method for braking a vehicle is provided, wherein the vehicle includes a circuit adapted for transmitting a brake signal from an operator controlled braking element to brake devices arranged at a plurality of the vehicle's ground engaging elements via a brake fluid. The method includes detecting a fluid pressure in the circuit, using the detected fluid pressure level as an input for determining a brake power for at least one auxiliary brake in the vehicle, and controlling the auxiliary brake responsively.
摘要翻译：提供了一种用于制动车辆的方法，其中车辆包括适于将来自操作者控制的制动元件的制动信号经由制动流体传送到布置在多个车辆地面接合元件的制动装置的电路。该方法包括使用检测到的流体压力水平作为用于确定车辆中的至少一个辅助制动器的制动功率的输入来检测回路中的流体压力，并响应地控制辅助制动器。

8. 发明授权

US07758715B2 Method of forming a composite structure 失效
标题翻译：形成复合结构的方法
公开(公告)号：US07758715B2
公开(公告)日：2010-07-20
申请号：US12258469
申请日：2008-10-27
申请人： Mikael Petersson , Per Hallander , Björn Weidmann
发明人： Mikael Petersson , Per Hallander , Björn Weidmann
IPC分类号： F02F1/06 , C09J5/10 , B29C65/00 , B29C45/14 , B32B37/00 , B32B3/00 , C08J5/00
CPC分类号： B29D99/0003 , B29C35/0266 , B29C2791/001 , Y10T428/197
摘要： A method of manufacturing a composite structure including a plurality of sheets and a radius filler. The radius filler is adapted to fill a gap at least partially formed by the sheets of the composite structure. The radius filler includes a plastic material with a first curing temperature. The sheets include a plastic material with a second curing temperature. The method includes arranging the sheets in a desired shape, applying the radius filler material into the gap, exposing the sheets and the radius filler material to the first temperature, whereby the material of the radius filler cures, and exposing the sheets and the radius filler to the second temperature, which exceeds the first temperature, whereby the material of the sheets cures. A radius filler for filling gaps between sheets of a composite structure. The material of the radius filler has a curing temperature which is below the curing temperature of the sheets of the composite structure.
摘要翻译：一种制造包括多个片材和半径填料的复合结构体的方法。半径填料适于填充由复合结构的片材至少部分地形成的间隙。半径填料包括具有第一固化温度的塑料材料。片材包括具有第二固化温度的塑料材料。该方法包括将片材布置成所需的形状，将半径填充材料施加到间隙中，将片材和半径填充材料暴露于第一温度，由此半径填充材料固化并暴露片材和半径填料达到超过第一温度的第二温度，由此片材的材料固化。用于填充复合结构的板之间的间隙的半径填料。半导体填料的材料的固化温度低于复合结构的片材的固化温度。

9. 发明申请

US20090152775A1 METHOD AND APPARATUS FOR MANUFACTURING OF AN ARTICLE INCLUDING AN EMPTY SPACE 失效
标题翻译：用于制造包括空白空间的文章的方法和装置
公开(公告)号：US20090152775A1
公开(公告)日：2009-06-18
申请号：US12330185
申请日：2008-12-08
申请人： Tommy GRANKALL , Mikael Petersson , Per Hallander , Jan-Erik Lindback , Bjorn Weidmann , Jan Andersson
发明人： Tommy GRANKALL , Mikael Petersson , Per Hallander , Jan-Erik Lindback , Bjorn Weidmann , Jan Andersson
IPC分类号： B29C49/70
CPC分类号： B29C33/3821 , B29C33/505 , Y10S264/44
摘要： A tool assembly including a male tool including an inner shape tool including a bag having a connection connectable to a depressurization source for providing a vacuum in the bag such that beads therein form a body of firm cohesion providing the inner shape tool rigid. The male tool further includes a flexible, hollow curing support arranged around the rigid inner shape tool, the inner shape tool is arranged to be removable from the flexible, hollow curing support by rupturing the vacuum.
摘要翻译：一种工具组件，包括一个包括内部形状工具的内部工具的内部工具，该内部工具包括具有可连接到减压源的连接的袋子，用于在袋子中提供真空，使得其中的珠子形成提供内部形状工具刚性的牢固内聚力的主体。阳型工具还包括围绕刚性内部形状工具布置的柔性中空固化支撑件，内部形状工具被布置成通过破坏真空而从柔性中空固化支撑件移除。

10. 发明申请

US20090025865A1 Method and apparatus for manufacturing of a wing spar profile element 审中-公开
标题翻译：用于制造翼梁型材的方法和装置
公开(公告)号：US20090025865A1
公开(公告)日：2009-01-29
申请号：US12010180
申请日：2008-01-22
申请人： Bjorn Weidmann , Jan Vaara , Mikael Petersson , Max Krogager
发明人： Bjorn Weidmann , Jan Vaara , Mikael Petersson , Max Krogager
IPC分类号： B29C63/22
CPC分类号： B29C70/342 , B29C70/38 , B29C70/386 , B29D99/0007 , B29L2031/3085 , Y10T156/1007
摘要： A method and an apparatus for manufacture of an elongated beam profile element including a recess configured to accommodate a support element. The method includes forming the blank into the web portion with at least one first protrusion formed to extend across the web portion and to protrude outward from the web portion's outer surface; and into the first flange portion with at least one second protrusion formed to extend across the first flange portion and to protrude inward from the first flange portion's inner surface, wherein this second protrusion merges into the first protrusion and constitutes the recess for accommodating the support element under a wing.
摘要翻译：一种用于制造细长梁剖面元件的方法和装置，其包括构造成容纳支撑元件的凹部。所述方法包括将所述坯件形成到所述幅材部分中，其中至少一个第一突起形成为跨越所述幅材部分延伸并从所述幅材部分的外表面向外突出; 并且进入第一凸缘部分，其中至少一个第二突起形成为跨过第一凸缘部分延伸并且从第一凸缘部分的内表面向内突出，其中该第二突起汇合到第一突起中并且构成用于容纳支撑元件的凹部在翅膀下。

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