发明名称 Large Deployable Reflector For A Satellite Antenna
摘要 A large deployable reflector for an antenna suitable for being installed on board a satellite and provided with a support structure, a parabolic mirror carried by the support structure and a connection arm for mounting the support structure on the satellite; the support structure being a jointed reticulate structure that is able to assume a compact inoperative stowed configuration and an operative deployed configuration and is composed of ‘n’ elements articulated to form tetrahedrons having respective triangular bases, which are connected to each other at the axial ends of respective first sides and have respective external vertices, which are opposite to said respective first sides and, when the reflector is arranged in the deployed configuration, ideally lie on a cone tangent to the parabolic mirror.
申请公布号 US2015303582(A1) 申请公布日期 2015.10.22
申请号 US201314440515 申请日期 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
分类号 H01Q15/16 主分类号 H01Q15/16
代理机构 代理人
主权项 1. A large deployable reflector for a satellite antenna; the reflector (1) comprising a support structure (6) provided with connection means (7) for mounting the support structure (6) on a satellite (2) and a reflector assembly (5) carried by the support structure (6) and comprising a reflective parabolic mirror (5a); the support structure (6) being a jointed reticulate structure comprising building blocks (8) and being able to assume a compact inoperative stowed configuration and an operative deployed configuration; the reflector (1) being characterized in that said building blocks (8) are tetrahedron-shaped elements (8), connected to each other to form a ring-like structure; the tetrahedrons (8) have 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 an elliptical cone tangent to the parabolic mirror (5a).
地址 Roma IT