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1. 发明授权

EP2264830B1 Antenne à reflecteur avec couverture et fréquences d'opération variable et satellite comportant une telle antenne 有权转让
公开(公告)号：EP2264830B1
公开(公告)日：2018-08-29
申请号：EP10164352.6
申请日：2010-05-28
申请人： THALES
发明人： Schreider, Ludovic , Bosshard, Pierre , Depeyre, Serge
IPC分类号： H01Q1/28 , H01Q5/00 , H01Q15/16 , H01Q19/18 , H01Q25/00 , H01Q3/20
CPC分类号： H01Q1/288 , H01Q3/20 , H01Q5/45 , H01Q15/161 , H01Q19/18 , H01Q25/002

2. 发明授权

EP2904662B1 DEPLOYABLE ANTENNA FRAME 有权转让
标题翻译：可部署的线框架
公开(公告)号：EP2904662B1
公开(公告)日：2016-12-14
申请号：EP12775199.8
申请日：2012-10-01
申请人： European Space Agency
发明人： MEDZMARIASHVILI, Elguja , TSIGNADZE, Nodar , MEDZMARIASHVILI, Nikoloz , DATASHVILI, Leri , IHLE, Alexander , SANTIAGO PROWALD, Julian B. , VAN'T KLOOSTER, Cornelis
IPC分类号： H01Q15/16
CPC分类号： H01Q15/161 , H01Q1/1235
摘要： A multi-faceted deployable antenna frame including a six-bar linkage structure in a lateral facet of the antenna frame, the six-bar linkage structure being convertible from a folded state into a deployed state and having two first bars and four second bars, each bar being coupled to two others by a hinge to form a closed loop, where in the deployed state, the six-bar linkage structure has a quadrilateral shape. The antenna frame also includes a deployment means for deploying the antenna frame by moving the six-bar linkage structures from the folded state into the deployed state, the deployment means including: a flexible, elongated member of a substantially inextensible material; a first guiding means provided at an end portion of one of the first bars and coupled to the elongated member; a storage means provided at the first bar that includes the first guiding means for storing a part of the elongated member; a driving means that is coupled to the elongated member to pull the elongated member to the storing means when deploying the antenna frame; and a second guiding means between two adjacent second bars, the elongated member being coupled to the second guiding means. A first end of the elongated member is attached to the storing means and a second end of the elongated member is coupled to another first bar, and wherein the elongated member is extending between said first end and said second end along a plurality of second bars.

3. 发明公开

EP3092684A1 MESH REFLECTOR WITH TRUSS STRUCTURE 审中-公开
标题翻译：有支撑结构振动功率反射器
公开(公告)号：EP3092684A1
公开(公告)日：2016-11-16
申请号：EP14803324.4
申请日：2014-11-14
申请人： Northrop Grumman Systems Corporation
发明人： MOBREM, Mehran , MARKS, Geoffrey W.
IPC分类号： H01Q15/16 , H01Q1/28
CPC分类号： H01Q15/168 , G02B5/10 , G02B7/182 , H01Q1/288 , H01Q15/161
摘要： A reflector assembly includes a frame centered about a longitudinal axis and having a first height along the axis. A curved body extends from the frame and has a second height along the longitudinal axis could be greater than the first height. A stretchable membrane has an electromagnetically reflective surface and is secured to the curved body.

4. 发明公开

EP2915213A1 LARGE DEPLOYABLE REFLECTOR FOR A SATELLITE ANTENNA 有权
标题翻译：用于卫星天线的可能大型反射
公开(公告)号：EP2915213A1
公开(公告)日：2015-09-09
申请号：EP13818412.2
申请日：2013-11-04
申请人： Thales Alenia Space Italia S.p.A. Con Unico Socio
发明人： MESCHINI, Alberto , RIGATO, Riccardo , SCAROZZA, Davide
IPC分类号： H01Q1/28 , H01Q15/16 , B64G1/22
CPC分类号： H01Q15/161 , B64G1/222 , B64G1/66 , H01Q1/288
摘要： A large deployable reflector (1) for an antenna suitable for being installed on board a satellite (2) and provided with a support structure (6), a parabolic mirror (5a) carried by the support structure (6) and a connection arm (7) for mounting the support structure (6) on the satellite; the support structure (6) being a jointed reticulate structure- that is able to assume a compact inoperative stowed configuration and an operative deployed configuration and is composed of 'xn' elements (13) articulated to form tetrahedrons (8) having respective triangular bases (9), which are connected to each other at the axial ends of respective first sides (9a) and have respective external vertices (11), which are opposite to said respective first sides (9a) and, when the reflector (1) is arranged in the deployed configuration, ideally lie on a cone tangent to the parabolic mirror (5a).

5. 发明公开

EP2904662A1 DEPLOYABLE ANTENNA FRAME 有权转让
标题翻译：可部署的线框架
公开(公告)号：EP2904662A1
公开(公告)日：2015-08-12
申请号：EP12775199.8
申请日：2012-10-01
申请人： European Space Agency
发明人： MEDZMARIASHVILI, Elguja , TSIGNADZE, Nodar , MEDZMARIASHVILI, Nikoloz , DATASHVILI, Leri , IHLE, Alexander , SANTIAGO PROWALD, Julian B. , VAN'T KLOOSTER, Cornelis
IPC分类号： H01Q15/16
CPC分类号： H01Q15/161 , H01Q1/1235
摘要： A multi-faceted deployable antenna frame including a six-bar linkage structure in a lateral facet of the antenna frame, the six-bar linkage structure being convertible from a folded state into a deployed state and having two first bars and four second bars, each bar being coupled to two others by a hinge to form a closed loop, where in the deployed state, the six-bar linkage structure has a quadrilateral shape. The antenna frame also includes a deployment means for deploying the antenna frame by moving the six-bar linkage structures from the folded state into the deployed state, the deployment means including: a flexible, elongated member of a substantially inextensible material; a first guiding means provided at an end portion of one of the first bars and coupled to the elongated member; a storage means provided at the first bar that includes the first guiding means for storing a part of the elongated member; a driving means that is coupled to the elongated member to pull the elongated member to the storing means when deploying the antenna frame; and a second guiding means between two adjacent second bars, the elongated member being coupled to the second guiding means. A first end of the elongated member is attached to the storing means and a second end of the elongated member is coupled to another first bar, and wherein the elongated member is extending between said first end and said second end along a plurality of second bars.

6. 发明公开

EP2640643A1 LOW WEIGHT, COMPACTLY DEPLOYABLE SUPPORT STRUCTURE 有权
标题翻译： KOMPAKTE AUSKLAPPBARESTÜTZSTRUKTURMIT GERINGEM GEWICHT
公开(公告)号：EP2640643A1
公开(公告)日：2013-09-25
申请号：EP10781844.5
申请日：2010-11-19
申请人： European Space Agency
发明人： SANTIAGO PROWALD, Julian B. , SUCH TABOADA, Miguel
IPC分类号： B64G1/22 , B64G1/66
CPC分类号： B64G1/66 , B64G1/222 , E04B1/3441 , H01Q1/288 , H01Q15/161 , H01Q15/20
摘要： The present invention relates to deployable support structures, such as but not limited to large deployable apertures for space applications. A six-bar linkage structure is proposed as the lateral facet of a truncated pyramid. This six-bar linkage comprises six articulated struts 1, 2, 3, 4, 5, 6, each coupled to two others by a revolute joint 7 to form a closed loop. The six-bar linkage structure 10 being convertible from a deployed state 10A into a folded state 10D and vice versa. In the deployed state 10A, the six-bar linkage structure 10 forming a trapezoid with two opposing first and second parallel sides, each of the first and second opposing parallel sides being formed by two struts 3,4; 5,6 arranged in series and coupled by a revolute joint 7a; 7b at the center of the first and second parallel sides. In the folded state 10D, the two struts 3, 4 of the first side being pivoted around the first revolute joint 7a so that the opposing end portions 3c, 4e of the two struts 3, 4 are located side by side and the two struts 5, 6 of the second side being pivoted around the second revolute joint 7b so that the opposing end portions 5f, 6g of the two struts 5, 6 are located side by side. The six-bar linkage structure constitutes the key element that allows constructing unit cells of scalable and modular deployable structures with double curvature. This deployable structure concept can be used for civil constructions, including but not limited to domes, roofs, housing, tents and bridges.
摘要翻译：可部署的支撑结构包括六柱连杆结构作为截顶棱锥的侧面。六杆连杆结构包括六个铰接支柱，每个支柱通过旋转接头连接到另外两个支柱，以形成闭环。六杆联动结构可以从部署状态转换成折叠状态，反之亦然。在一个实施例的展开状态下，六杆连杆结构形成梯形，其中两个相对的第一和第二平行侧由两个串联布置的支柱形成，并且通过在平行侧的中心处的旋转接头联接。在折叠状态下，每个平行侧的两个支柱围绕接头枢转，使得支柱的相对端部并排定位。可扩展和模块化的可部署结构可用于空间应用以及民用结构，如圆顶，屋顶，住房，帐篷和桥梁。

7. 发明公开

EP2005521A2 ARBITRARILY SHAPED DEPLOYABLE MESH REFLECTORS 有权
标题翻译： ARBITRÄRGEFORMTE EINSETZBARE MESH-REFLEKTOREN
公开(公告)号：EP2005521A2
公开(公告)日：2008-12-24
申请号：EP07751916.3
申请日：2007-02-28
申请人： The Boeing Company
发明人： BASSILY, Samir, F.
IPC分类号： H01Q15/16
CPC分类号： H01Q15/168 , H01Q15/161 , Y10T29/49904
摘要： A method and apparatus for making a mesh reflector that may be used to produce a shaped reflector is provided. The mesh reflector may be an umbrella-style deployable mesh reflector capable of approximating both parabolic and arbitrarily shaped reflecting surfaces, including those with regions of reversed curvature. The reflecting surface may be provided by a soft mesh attached to a highly pre-tensioned net composed of two sets of substantially parallel chords forming a plurality of parallelogram-shaped facets. The net/mesh may be made to conform to the desired shape by pulling and/or pushing on it at each of its facet corners via a set of finely adjustable tension ties and/or compression rods, the distal ends of which react against a set of pre-tensioned catenary-shaped chords disposed on the aft side of the mesh. The net/mesh and the aft catenaries may be supported and pre-tensioned by a set of substantially stiff radial ribs connected to a central hub by a means capable of providing high deployment torque and a means for controlling and coordinating the deployment of the ribs so that they reach their fully deployed positions nearly simultaneously. Methods for fabricating the mesh and attaching it to the net are also provided.
摘要翻译：提供了一种用于制造可用于生产成形反射器的网状反射器的方法和装置。网格反射器可以是能够近似抛物面和任意形状的反射表面的伞形可部署网状反射器，包括具有反曲率区域的反射表面。反射表面可以由连接到形成多个平行四边形形小面的由两组基本上平行的和弦组成的高度预张紧网的软网提供。网/网可以通过在其每个小角上通过一组精细调节的张紧系带和/或压缩杆拉动和/或推动它来使其符合期望的形状，其远端对抗一组布置在网格的后侧的预张紧的悬链状和弦。网/网和后悬链可以由一组通过能够提供高展开扭矩的装置连接到中心毂的基本上刚性的径向肋来支撑和预张紧，以及用于控制和协调肋的展开的装置，使得它们几乎同时到达其完全部署的位置。还提供了用于制造网并将其附接到网的方法。

8. 发明公开

EP1727239A1 Reflective surface for deployabe reflector 审中-公开
标题翻译： ReflektierendeFlächefüreinen entfaltbaren Reflektor
公开(公告)号：EP1727239A1
公开(公告)日：2006-11-29
申请号：EP06252660.3
申请日：2006-05-22
申请人： Northrop Grumman Corporation
发明人： Marks, Geoffrey Willilam
IPC分类号： H01Q15/14 , H01Q15/16
CPC分类号： H01Q1/288 , H01Q15/141 , H01Q15/142 , H01Q15/161 , H05K9/0088 , Y10T442/164 , Y10T442/40 , Y10T442/475
摘要： A radio frequency reflective film includes a radio frequency reflective mesh, a plurality of carbon nano-structure materials, and an elastomer. The elastomer encapsulates the radio frequency reflective mesh and the carbon nano-structure materials.
摘要翻译：射频反射膜包括射频反射网，多个碳纳米结构材料和弹性体。弹性体封装射频反射网和碳纳米结构材料。

9. 发明公开

EP1331095A3 Deployable structure 审中-公开
标题翻译：展开结构
公开(公告)号：EP1331095A3
公开(公告)日：2004-04-07
申请号：EP03250433.4
申请日：2003-01-23
申请人： National Space Development Agency of Japan
发明人： Yamawaki, Koji, Nat. Space Dev. Agency of Japan
IPC分类号： B41G1/00 , B64G1/22 , H01Q1/08 , H01L31/045 , E04B7/10 , E04B1/344
CPC分类号： H01Q1/08 , B64G1/222 , B64G1/44 , B64G9/00 , H01Q1/288 , H01Q15/161
摘要： An unfoldable connected structure (1) has a structural unit movable from a folded to an unfolded state. The structural unit includes five arm units (2), and each of the arm units (2) includes an inner arm member (3) having first and second ends, an outer arm member (4) having first and second ends, an elbow joint mechanism (5) movably connecting the first end of the inner arm member (3) to the first end of the outer arm member (4), a shoulder joint mechanism (6) movably connected to the second end of the inner arm member (3), and a wrist joint mechanism (7) movably connected to the second end of the outer arm member (4); and means (19) for connecting the arm units radially through their respective shoulder joint mechanism (6) to form a frame of a pentagonal pyramid configuration when the structural unit is in an unfolded state (Fig. 8). The unfoldable connected structure (1) forms no void at its outer surface when it is in an unfolded state, has improved structural strength, and allows for a smooth folding and unfolding action.

10. 发明公开

EP1387438A1 Remotely adjustable mesh deployable reflector 有权
标题翻译： Ferneinstellbarer，entfaltbarer Netzreflektor
公开(公告)号：EP1387438A1
公开(公告)日：2004-02-04
申请号：EP03017697.8
申请日：2000-01-31
申请人： Northrop Grumman Corporation
发明人： Gilger, Dwight L.
IPC分类号： H01Q15/16 , H01Q1/28 , H01Q15/14
CPC分类号： H01Q15/147 , H01Q1/288 , H01Q15/14 , H01Q15/161 , H01Q15/168
摘要： The reflective mesh material that forms the reflector in a foldable perimeter truss antenna is remotely adjusted to shape using remotely controlled stepper motors carried on the truss. Connected to the end of the catenaries, which shape and support the pliant reflective mesh material on the truss, the stepper motors adjust the tension on the catenaries and thereby change its shape. An RF receiver and electronic controller associated with each stepper motor receives the tension command information from a remote source and controls the stepper motor in accordance with that information.
摘要翻译：在可折叠的周边桁架天线中形成反射器的反射网状材料通过在桁架上承载的远程控制的步进电机进行远程调节以成形。连接到悬链线的末端，其形状和支撑桁架上的柔性反光网格材料，步进电机调节悬链上的张力，从而改变其形状。与每个步进电机相关联的RF接收器和电子控制器从远程源接收张力指令信息，并根据该信息控制步进电机。

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