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1. 发明授权

US09180979B2 Smooth surface forming tool and manufacture thereof 有权
标题翻译：平滑的表面成型工具及其制造
公开(公告)号：US09180979B2
公开(公告)日：2015-11-10
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： B29C33/02 , B64F5/00 , B29C45/73 , B29C33/40 , B29C70/44 , B29C70/88 , B82Y30/00 , B29K105/16
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。

2. 发明授权

US08662452B2 Article with de-icing/anti-icing function 有权
标题翻译：文章具有除冰/防冰功能
公开(公告)号：US08662452B2
公开(公告)日：2014-03-04
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
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。

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. 发明申请

US20120074265A1 NANO-REINFORCED RADIUS FILLER FOR AN AIRCRAFT STRUCTURE AND A METHOD OF PRODUCING AN AIRCRAFT STRUCTURE COMPRISING SUCH FILLER 审中-公开
标题翻译：用于飞机结构的纳米增强半径填料和一种生产包含这种填料的飞机结构的方法
公开(公告)号：US20120074265A1
公开(公告)日：2012-03-29
申请号：US13377054
申请日：2009-06-11
申请人： Per Hallander , Mikael Petersson , Bjorn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
发明人： Per Hallander , Mikael Petersson , Bjorn Weidmann , Tommy Grankäll , Göte Strindberg , Pontus Nordin
IPC分类号： B64C9/00 , C08L63/00 , C08L35/00 , C08L31/02 , C08L79/04 , C08L61/16 , C08L61/06 , C08L79/08 , C08L81/04 , C08L79/00 , C08L67/00 , B32B37/12 , B32B37/14 , B32B3/26 , C08K3/04 , B82Y30/00
CPC分类号： B64C1/06 , B29C35/02 , B29C65/02 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/43441 , B29C66/49 , B29C66/496 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73754 , B29C66/73941 , B29C70/14 , B29C70/46 , B29K2105/06 , B29K2105/167 , B29K2105/243 , B29K2307/00 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , Y02T50/43 , Y10T428/24479 , B29K2307/04 , B29K2071/00 , B29K2067/00 , B29K2063/00 , B29K2031/00 , B29K2049/00 , B29K2061/04 , B29K2079/08 , B29K2081/04
摘要： A composite radius filler for use in an aircraft structure. The aircraft structure includes structural composite parts assembled together to form the aircraft structure. The composite radius filler is arranged between rounded sections of the structural composite parts for filling a gap formed between the structural composite parts. The composite radius filler is made structural by a nanostructure arranged within the composite radius filler for the reinforcement of the interface between the radius filler and the structural composite part. A method for producing an aircraft structure including a nano-reinforced radius filler.
摘要翻译：用于飞机结构的复合半径填料。飞机结构包括组装在一起以形成飞行器结构的结构复合部件。复合半径填料布置在结构复合部件的圆形部分之间，用于填充形成在结构复合部件之间的间隙。复合半径填料通过布置在复合半径填料内的纳米结构构成，用于加强半径填料和结构复合材料部分之间的界面。一种用于生产包括纳米增强半径填料的飞行器结构的方法。

6. 发明申请

US20120088056A1 STRUCTURAL LONGITUDINAL COMPOSITE JOINT FOR AIRCRAFT STRUCTURE 有权
标题翻译：用于飞机结构的结构纵向复合材料接头
公开(公告)号：US20120088056A1
公开(公告)日：2012-04-12
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 , B82Y30/00
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。

7. 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。

8. 发明申请

US20130291979A1 PLASMA-ENHANCED ACTIVE LAMINAR FLOW ACTUATOR SYSTEM 有权
标题翻译：等离子体增强活性层流法致动器系统
公开(公告)号：US20130291979A1
公开(公告)日：2013-11-07
申请号：US13821196
申请日：2010-09-15
申请人： Pontus Nordin , Göte Strindberg
发明人： Pontus Nordin , Göte Strindberg
IPC分类号： B64C23/00
CPC分类号： B64C23/00 , B64C23/005 , B64C2230/12 , B82Y30/00 , F15D1/0075 , H05H1/2406 , H05H2001/2418 , Y02T50/166 , Y10T137/206
摘要： The invention regards a plasma-enhanced active laminar flow actuator system (1) adapted to an aerodynamic surface (3) which has a nano-engineered composite material layer(5) comprising a set of electrodes arranged (7′, 7″) in at least an upper (P1) and a lower (P2) plane extending parallel with the aerodynamic surface (3); the electrodes (7′, 7″) comprising nano filaments (9); the electrodes (7′) of the upper plane (P1) are arranged in the aerodynamic surface (3) such that they define a smooth and hard aerodynamic surface (3);conductors (11, 11′) of nano filaments (9″) arranged for electrical communication between a control unit (13) and each of the electrodes (7′, 7″), wherein the control unit (13) is adapted to address current between cooperating electrodes (7′, 7″) of the upper and lower plane (P1, P2) from a current supply depending upon air flow characteristic signals fed from air flow sensor means (19).
摘要翻译：本发明涉及一种适用于空气动力学表面（3）的等离子体增强型有源层流致动器系统（1），其具有纳米工程复合材料层（5），其包括一组电极（7'，7“）至少与空气动力学表面（3）平行延伸的上部（P1）和下部（P2）平面; 包括纳米细丝（9）的电极（7'，7“）; 上平面（P1）的电极（7'）布置在空气动力学表面（3）中，使得它们限定平滑且硬的空气动力学表面（3）;纳米细丝（9“）的导体（11,11'）），其布置成用于控制单元（13）和每个电极（7'，7“）之间的电气通信，其中所述控制单元（13）适于解决所述电极（7'，7”）的协作电极根据从气流传感器装置（19）馈送的气流特性信号，来自电流源的上平面（P1，P2）。

9. 发明申请

US20130028738A1 MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM OF A WIND TURBINE 审中-公开
标题翻译：风力涡轮机的多功能防雷系统
公开(公告)号：US20130028738A1
公开(公告)日：2013-01-31
申请号：US13522393
申请日：2010-01-14
申请人： Pontus Nordin , Göte Strindberg
发明人： Pontus Nordin , Göte Strindberg
IPC分类号： F03D11/00
CPC分类号： H05B3/145 , F03D80/30 , F03D80/40 , H05B2214/04 , Y02E10/721
摘要： A de-icing/anti-icing system including at least two conductive structures embedded in a wind turbine blade. An outer surface is designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. One conductive structure includes a first conductive nano structure. A conductive property of the conductive structure differs from a conductive property of the other conductive structure including a second conductive nano structure, for achieving different degrees of heat depending on the needed mode of the system.
摘要翻译：一种除冰/防冰系统，其包括嵌入在风力涡轮机叶片中的至少两个导电结构。外表面设计为空气动力学表面。导电结构中的至少一个布置成与外表面相邻。控制单元，其适于控制向导电结构的能量供应，以向外表面产生热量。一个导电结构包括第一导电纳米结构。导电结构的导电特性与包括第二导电纳米结构的另一导电结构的导电性不同，用于根据系统的所需模式实现不同程度的热。

10. 发明申请

US20130028744A1 AERODYNAMIC SURFACE WITH IMPROVED PROPERTIES 审中-公开
标题翻译：具有改进性质的空气动力学表面
公开(公告)号：US20130028744A1
公开(公告)日：2013-01-31
申请号：US13522364
申请日：2010-01-14
申请人： Pontus Nordin , Göte Strindberg
发明人： Pontus Nordin , Göte Strindberg
IPC分类号： B64C11/18 , B32B5/12
CPC分类号： B64C21/10 , B29C70/081 , B29C70/882 , B29K2105/124 , B29K2105/167 , B29L2031/3076 , B64C2230/26 , F15D1/12 , Y02T50/166 , Y10T428/24124 , Y10T428/24132
摘要： An article including an outer surface that serves as an aerodynamic surface when the article is subjected for an air stream. A resin matrix made of a polymeric composite laminate of at least one ply includes the outer surface. The at least one ply includes a nano structure embedded therein such that nano filaments of the nano structure in the ply essentially have the same angular orientation relative the plane of the outer surface. The outer ply is a ply of a laminate including at least two plies. Each ply includes large fibers having an orientation different from or identical to the orientation of large fibers of an adjacent ply.
摘要翻译：一种制品，其包括当制品经受空气流时用作空气动力学表面的外表面。由至少一层的聚合物复合层压材料制成的树脂基体包括外表面。所述至少一个层包括嵌入其中的纳米结构，使得所述层中的所述纳米结构的纳米长丝相对于所述外表面的平面基本上具有相同的角度取向。外层是包括至少两层的叠层层。每个帘布层包括具有与相邻帘布层的大纤维的取向不同或相同的取向的大纤维。

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