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1. 发明授权

US08860627B2 Reconfigurable reflector for electromagnetic waves 有权
标题翻译：用于电磁波的可重构反射器
公开(公告)号：US08860627B2
公开(公告)日：2014-10-14
申请号：US11902586
申请日：2007-09-24
申请人： Lucio Gerardo Scolamiero , Marco Sabbadini
发明人： Lucio Gerardo Scolamiero , Marco Sabbadini
IPC分类号： H01Q15/16 , H01Q19/10 , H01Q1/08 , H01Q15/14 , H01Q19/19
CPC分类号： H01Q15/147 , H01Q1/08 , H01Q15/161 , H01Q15/168 , H01Q19/192
摘要： A reconfigurable reflector for electromagnetic waves, comprising: a rigid support element (10) having a front surface (13); an elastically deformable reflective membrane (30) lying over the front surface of said rigid support element; and a plurality of linear actuators (20) for deforming said reflective membrane by operating on predetermined points thereof; wherein said linear actuators are embedded within said rigid support element, and have shafts (22) protruding by the front surface thereof for operating on predetermined points of said elastically deformable reflective membrane.Preferably, the rigid support element comprises a reflector dish having a sandwich structure having a honeycomb core (11) made of CFRP or aluminum, in which the linear actuators are embedded by conventional potting techniques.Antenna system comprising such a reconfigurable reflector, possibly operating as a subreflector (SR), and spacecraft telecommunication.
摘要翻译：一种用于电磁波的可重构反射器，包括：具有前表面（13）的刚性支撑元件（10）; 位于所述刚性支撑元件的前表面上的可弹性变形的反射膜（30）; 以及多个线性致动器（20），用于通过在其预定点上操作来使所述反射膜变形; 其中所述线性致动器嵌入在所述刚性支撑元件内，并且具有由其前表面突出的轴（22），用于在所述可弹性变形的反射膜的预定点上操作。优选地，刚性支撑元件包括具有具有由CFRP或铝制成的蜂窝芯（11）的夹层结构的反射器盘，其中通过常规灌封技术嵌入线性致动器。包括可能作为子反射器（SR）操作的这种可重构反射器的天线系统以及航天器通信。

2. 发明申请

US20120229355A1 Reconfigurable reflector for electromagnetic waves 有权
标题翻译：用于电磁波的可重构反射器
公开(公告)号：US20120229355A1
公开(公告)日：2012-09-13
申请号：US11902586
申请日：2007-09-24
申请人： Lucio Gerardo Scolamiero , Marco Sabbadini
发明人： Lucio Gerardo Scolamiero , Marco Sabbadini
IPC分类号： H01Q15/16 , H01Q19/10
CPC分类号： H01Q15/147 , H01Q1/08 , H01Q15/161 , H01Q15/168 , H01Q19/192
摘要： A reconfigurable reflector for electromagnetic waves, comprising: a rigid support element (10) having a front surface (13); an elastically deformable reflective membrane (30) lying over the front surface of said rigid support element; and a plurality of linear actuators (20) for deforming said reflective membrane by operating on predetermined points thereof; wherein said linear actuators are embedded within said rigid support element, and have shafts (22) protruding by the front surface thereof for operating on predetermined points of said elastically deformable reflective membrane.Preferably, the rigid support element comprises a reflector dish having a sandwich structure having a honeycomb core (11) made of CFRP or aluminum, in which the linear actuators are embedded by conventional potting techniques.Antenna system comprising such a reconfigurable reflector, possibly operating as a subreflector (SR), and spacecraft telecommunication.
摘要翻译：一种用于电磁波的可重构反射器，包括：具有前表面（13）的刚性支撑元件（10）; 位于所述刚性支撑元件的前表面上的可弹性变形的反射膜（30）; 以及多个线性致动器（20），用于通过在其预定点上操作来使所述反射膜变形; 其中所述线性致动器嵌入在所述刚性支撑元件内，并且具有由其前表面突出的轴（22），用于在所述可弹性变形的反射膜的预定点上操作。优选地，刚性支撑元件包括具有具有由CFRP或铝制成的蜂窝芯（11）的夹层结构的反射器盘，其中通过常规灌封技术嵌入线性致动器。包括可能作为子反射器（SR）操作的这种可重构反射器的天线系统以及航天器通信。

3. 发明授权

US09815574B2 Deployable tensegrity structure, especially for space applications 有权
公开(公告)号：US09815574B2
公开(公告)日：2017-11-14
申请号：US14386095
申请日：2012-03-19
申请人： Lucio Gerardo Scolamiero , Valfredo Zolesi , Pier Luigi Ganga , Paolo Podio-Guidugli , Gunnar Tibert , Andrea Micheletti
发明人： Lucio Gerardo Scolamiero , Valfredo Zolesi , Pier Luigi Ganga , Paolo Podio-Guidugli , Gunnar Tibert , Andrea Micheletti
IPC分类号： B64G1/22 , H01Q1/28 , H01Q15/16
CPC分类号： B64G1/222 , H01Q1/288 , H01Q15/161
摘要： A deployable structure comprises a first and second flexible tension members respectively defining a first and second contours of a ring. A first plurality of rigid compression members extends between the first and second contours. Only one end of each first plurality compression member is mounted on the first contour. A second plurality of rigid compression members extends between the first and second contours. Only one end of each second plurality compression member is mounted on the second contour. The first and second plurality of compression members are arranged with a repetitive crossing pattern around the ring. A first plurality of flexible tension members link each end of a compression member mounted on one of said contours to an end of another non-mounted compression member and a second plurality of flexible tension members link each end of a non-mounted compression member to an end of another non-mounted compression member.

4. 发明申请

US20150151854A1 DEPLOYABLE TENSEGRITY STRUCTURE, ESPECIALLY FOR SPACE APPLICATIONS 有权
标题翻译：可应用的灵敏度结构，特别适用于空间应用
公开(公告)号：US20150151854A1
公开(公告)日：2015-06-04
申请号：US14386095
申请日：2012-03-19
申请人： Lucio Gerardo Scolamiero , Valfredo Zolesi , Plei Luigi Ganga , Paolo Podio-Guidugli , Gunnar Tibert , Andren Micheletti
发明人： Lucio Gerardo Scolamiero , Valfredo Zolesi , Plei Luigi Ganga , Paolo Podio-Guidugli , Gunnar Tibert , Andren Micheletti
IPC分类号： B64G1/22
CPC分类号： B64G1/222 , H01Q1/288 , H01Q15/161
摘要： A deployable structure comprises a first and second flexible tension members respectively defining a first and second contours of a ring. A first plurality of rigid compression members extends between the first and second contours. Only one end of each first plurality compression member is mounted on the first contour. A second plurality of rigid compression members extends between the first and second contours. Only one end of each second plurality compression member is mounted on the second contour. The first and second plurality of compression members are arranged with a repetitive crossing pattern around the ring. A first plurality of flexible tension members link each end of a compression member mounted on one of said contours to an end of another non-mounted compression member and a second plurality of flexible tension members link each end of a non-mounted compression member to an end of another non-mounted compression member.
摘要翻译：可部署结构包括分别限定环的第一和第二轮廓的第一和第二柔性张紧构件。第一多个刚性压缩构件在第一和第二轮廓之间延伸。每个第一多个压缩构件的仅一端安装在第一轮廓上。第二多个刚性压缩构件在第一和第二轮廓之间延伸。每个第二多个压缩构件的仅一端安装在第二轮廓上。第一和第二多个压缩构件以围绕环的重复交叉图案布置。第一多个柔性张紧构件将安装在一个所述轮廓上的压缩构件的每个端部连接到另一个未安装的压缩构件的端部，并且第二多个柔性张紧构件将非安装的压缩构件的每个端部连接到另一个未安装的压缩构件的端部。

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