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1. 发明申请

US20050156786A1 Outside structure conformal antenna in a supporting structure of a vehicle 有权
标题翻译：车辆支撑结构中的外部结构保形天线
公开(公告)号：US20050156786A1
公开(公告)日：2005-07-21
申请号：US11000916
申请日：2004-12-02
申请人： Detlev Blaschke , Clemens Brand , Kay Dittrich , Oliver Nagy , Jan Ritter , Robert Sekora , Herbert Zippold
发明人： Detlev Blaschke , Clemens Brand , Kay Dittrich , Oliver Nagy , Jan Ritter , Robert Sekora , Herbert Zippold
IPC分类号： H01Q1/28 , H01Q1/32 , H01Q1/38
CPC分类号： H01Q1/286 , H01Q1/32
摘要： An antenna mounted on a supporting system primary structure of a vehicle, in which the supporting system primary structure has an indentation. The antenna includes an EM functional core incorporated into the indentation of the supporting system primary structure, and a cover plate forming one of an upper and outer cover of the EM functional core that is structured and arranged as a conformal outside. Furthermore, boundary areas of the cover plate are connected with the supporting system primary structure. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：一种安装在车辆的支撑系统主结构上的天线，其中支撑系统主结构具有压痕。天线包括并入到支撑系统一次结构的压痕中的EM功能芯，以及形成EM功能芯的上盖和外盖之一的盖板，其被构造和布置为外形。此外，盖板的边界区域与支撑系统一次结构连接。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

2. 发明授权

US07253777B2 Outside structure conformal antenna in a supporting structure of a vehicle 有权
标题翻译：车辆支撑结构中的外部结构保形天线
公开(公告)号：US07253777B2
公开(公告)日：2007-08-07
申请号：US11000916
申请日：2004-12-02
申请人： Detlev Blaschke , Clemens Brand , Kay Dittrich , Oliver Nagy , Jan Ritter , Robert Sekora , Herbert Zippold
发明人： Detlev Blaschke , Clemens Brand , Kay Dittrich , Oliver Nagy , Jan Ritter , Robert Sekora , Herbert Zippold
IPC分类号： H01Q1/32
CPC分类号： H01Q1/286 , H01Q1/32
摘要： An antenna mounted on a supporting system primary structure of a vehicle, in which the supporting system primary structure has an indentation. The antenna includes an EM functional core incorporated into the indentation of the supporting system primary structure, and a cover plate forming one of an upper and outer cover of the EM functional core that is structured and arranged as a conformal outside. Furthermore, boundary areas of the cover plate are connected with the supporting system primary structure. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：一种安装在车辆的支撑系统主结构上的天线，其中支撑系统主结构具有压痕。天线包括并入到支撑系统一次结构的压痕中的EM功能芯，以及形成EM功能芯的上盖和外盖之一的盖板，其被构造和布置为外形。此外，盖板的边界区域与支撑系统一次结构连接。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

3. 发明授权

US08159407B2 Radome with integrated plasma shutter 有权
标题翻译：集成等离子快门雷达
公开(公告)号：US08159407B2
公开(公告)日：2012-04-17
申请号：US12257555
申请日：2008-10-24
申请人： Kay Dittrich , Joachim Kaiser , Robert Sekora , Herbert Zippold
发明人： Kay Dittrich , Joachim Kaiser , Robert Sekora , Herbert Zippold
IPC分类号： H01Q1/52
CPC分类号： H01Q1/422 , H01Q1/425
摘要： Radome with an integrated plasma shutter covering an antenna and method for selectively shielding an antenna. The radome includes a honeycomb core formed to contain a plasma-guiding layer, and coverplates arranged to sandwich the honeycomb core. Electrodes are structured and arranged for plasma excitation, the electrodes being high frequency (HF)—transparent at least in an operating frequency range of the antenna. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：具有覆盖天线的集成等离子体快门的天线罩和用于选择性地屏蔽天线的方法。雷达罩包括形成为容纳等离子体引导层的蜂窝状芯和布置成夹住蜂窝芯的盖板。电极被构造和布置用于等离子体激发，电极至少在天线的工作频率范围内是高频（HF） - 透明的。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

4. 发明申请

US20090109115A1 RADOME WITH INTEGRATED PLASMA SHUTTER 有权
标题翻译： RADOME与集成等离子切换器
公开(公告)号：US20090109115A1
公开(公告)日：2009-04-30
申请号：US12257555
申请日：2008-10-24
申请人： Kay Dittrich , Joachim Kaiser , Robert Sekora , Herbert Zippold
发明人： Kay Dittrich , Joachim Kaiser , Robert Sekora , Herbert Zippold
IPC分类号： H01Q1/42 , H01Q1/52
CPC分类号： H01Q1/422 , H01Q1/425
摘要： Radome with an integrated plasma shutter covering an antenna and method for selectively shielding an antenna. The radome includes a honeycomb core formed to contain a plasma-guiding layer, and coverplates arranged to sandwich the honeycomb core. Electrodes are structured and arranged for plasma excitation, the electrodes being high frequency (HF)-transparent at least in an operating frequency range of the antenna. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：具有覆盖天线的集成等离子体快门的天线罩和用于选择性地屏蔽天线的方法。雷达罩包括形成为容纳等离子体引导层的蜂窝状芯和布置成夹住蜂窝芯的盖板。电极被构造和布置用于等离子体激发，电极至少在天线的工作频率范围内是高频（HF） - 透明的。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

5. 发明授权

US06877377B2 Non-destructive ultrasound test method for detection of damage and device for carrying out same 失效
标题翻译：用于检测损伤的非破坏性超声波检测方法及其执行装置
公开(公告)号：US06877377B2
公开(公告)日：2005-04-12
申请号：US10477454
申请日：2002-05-04
申请人： Kay Dittrich , Klaus-Peter Kress
发明人： Kay Dittrich , Klaus-Peter Kress
IPC分类号： G01N29/11 , G01N29/30 , G01N29/48 , G01N29/04
CPC分类号： G01N29/30 , G01N29/11 , G01N29/48 , G01N2291/044 , G01N2291/103 , G01N2291/2694
摘要： In a nondestructive ultrasonic testing method for an implementation in a testing device, defects are installed in a testing area of a structural part by determining reflections on inhomogeneities in a testing area of the structural part. At least one ultrasonic transmitter is provided for coupling ultrasonic excitations into the structural part, and at least two ultrasonic receivers are installed for receiving structure responses to the excitations coupled into the structure. A number of testing points are determined and for each testing point and each location of the ultrasonic receivers, expectancy range data are determined and stored for signal forms being implemented in the testing device. When, an inhomogeneity is present in the respective testing point, excitations are reflected thereon and are measured by the respective ultrasonic receiver. The received reflection data are compared with the stored expectancy ranges to determine the location of a defect.
摘要翻译：在用于在测试装置中实现的非破坏性超声波测试方法中，通过确定结构部件的测试区域中的不均匀性的反射来将缺陷安装在结构部件的测试区域中。提供至少一个超声波发射器用于将超声波激发耦合到结构部分中，并且安装至少两个超声波接收器以接收对耦合到该结构中的激励的结构响应。确定多个测试点，并且对于每个测试点和超声波接收器的每个位置，确定并存储期望范围数据以用于在测试装置中实现的信号形式。当在各测试点中存在不均匀性时，激发被反射在其上，并由相应的超声波接收器测量。将接收的反射数据与存储的预期范围进行比较以确定缺陷的位置。

6. 发明申请

US20060163431A1 Cover skin for a variable-shape aerodynamic area 有权
标题翻译：覆盖皮肤为可变形气动区域
公开(公告)号：US20060163431A1
公开(公告)日：2006-07-27
申请号：US11286834
申请日：2005-11-23
申请人： Kay Dittrich
发明人： Kay Dittrich
IPC分类号： B64B1/14
CPC分类号： B64C3/48 , B64C3/26
摘要： A cover skin for a variable-shape aerodynamic area, such as a wing structure, tail unit structure, control surface structure or flap structure is described. A cover skin is deformable in one direction without exhibiting substantial deformation in a transverse direction. A deformable framework structure is embedded in a layer of an elastic material, such as rubber or polymer. The framework structure may be comprised of non-deformable elements joined pivotably in auxetic and non-auxetic assemblies of elements that are capable of substantially eliminating transversal contraction, when the cover skin is longitudinal stretched, and substantially eliminating transversal expansion, when the cover skin is longitudinally contracted.
摘要翻译：描述了用于可变形空气动力学区域的覆盖皮肤，例如机翼结构，尾部单元结构，控制表面结构或翼片结构。覆盖皮肤在一个方向上是可变形的，而不会在横向方向上发生显着的变形。可变形骨架结构嵌入弹性材料层，如橡胶或聚合物。框架结构可以包括不可变形的元件，其可枢转地接合在元件的辅助和非使用组件中，当覆盖皮肤被纵向拉伸时，能够基本上消除横向收缩，并且基本上消除横向膨胀，纵向收缩。

7. 发明申请

US20050029406A1 Cellular actuator device and methods of making and using same 失效
标题翻译：蜂窝致动器装置及其制造和使用方法
公开(公告)号：US20050029406A1
公开(公告)日：2005-02-10
申请号：US10866103
申请日：2004-06-14
申请人： Kay Dittrich
发明人： Kay Dittrich
IPC分类号： B64C3/46 , B64C13/40 , B64C13/04
CPC分类号： B64C3/46 , B64C13/40
摘要： A cellular actuator device suitable for a control surface of an aircraft or space craft has a number of elementary cells which are combined to a common arrangement and are formed by pressure-tight chambers. The elementary cells can be acted upon by a pressure medium and, when acted upon by the pressure medium, can be deformed in at least one work direction while changing their length. The elementary cells are coupled for combining their length changes in the at least one working direction to an overall movement of the elementary cell arrangement. The actuator device is particularly suitable for actuating a control surface of an aircraft or spacecraft.
摘要翻译：适用于飞机或航天飞机的控制表面的蜂窝致动器装置具有多个基本单元，它们组合成共同的布置，并由压力密封室形成。基本细胞可以被压力介质作用，并且当被压力介质作用时，可以在改变其长度的同时在至少一个工作方向上变形。耦合基本单元以将它们在至少一个工作方向上的长度变化与基本单元布置的整体运动相结合。致动器装置特别适于致动飞行器或航天器的控制表面。

8. 发明授权

US4987425A Antenna support structure 失效
标题翻译：天线支撑结构
公开(公告)号：US4987425A
公开(公告)日：1991-01-22
申请号：US271037
申请日：1988-11-14
申请人： Rudolf Zahn , Hans W. Schroeder , Christian Borgwardt , Albert Braig , Gunter Helwig , Kay Dittrich
发明人： Rudolf Zahn , Hans W. Schroeder , Christian Borgwardt , Albert Braig , Gunter Helwig , Kay Dittrich
IPC分类号： B64C1/36 , H01Q1/18 , H01Q1/28 , H01Q21/00 , H01Q21/06
CPC分类号： H01Q1/28 , H01Q21/0087 , H01Q21/065
摘要： Carrying structure of an active antenna in the aerospace industry uses basically fiber reinforced synthetic material in which heat conductive elements and/or elements conducting electromagnetic waves (electro, optic) are integrated into that support structure for the antenna.
摘要翻译：航空航天工业中的有源天线的承载结构主要使用纤维增强的合成材料，其中传导电磁波（电，光学）的导热元件和/或元件被集成到天线的支撑结构中。

9. 发明授权

US07055782B2 Cellular actuator device and methods of making and using same 失效
标题翻译：蜂窝致动器装置及其制造和使用方法
公开(公告)号：US07055782B2
公开(公告)日：2006-06-06
申请号：US10866103
申请日：2004-06-14
申请人： Kay Dittrich
发明人： Kay Dittrich
IPC分类号： B64C13/36
CPC分类号： B64C3/46 , B64C13/40
摘要： A cellular actuator device suitable for a control surface of an aircraft or space craft has a number of elementary cells which are combined to a common arrangement and are formed by pressure-tight chambers. The elementary cells can be acted upon by a pressure medium and, when acted upon by the pressure medium, can be deformed in at least one work direction while changing their length. The elementary cells are coupled for combining their length changes in the at least one working direction to an overall movement of the elementary cell arrangement. The actuator device is particularly suitable for actuating a control surface of an aircraft or spacecraft.
摘要翻译：适用于飞机或航天飞机的控制表面的蜂窝致动器装置具有多个基本单元，它们组合成共同的布置，并由压力密封室形成。基本细胞可以被压力介质作用，并且当被压力介质作用时，可以在改变其长度的同时在至少一个工作方向上变形。耦合基本单元以将它们在至少一个工作方向上的长度变化与基本单元布置的整体运动相结合。致动器装置特别适于致动飞行器或航天器的控制表面。

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