发明名称 Solid state heat pipe heat rejection system for space power systems
摘要 A heat rejection system includes a plurality of panel subassemblies and a solid state heat pipe flex joint. Each panel subassembly includes a fin, a solid state heat pipe manifold, a first solid state heat pipe tube operatively connected to the solid state heat pipe manifold and secured to the fin, a second solid state heat pipe tube operatively connected to the solid state heat pipe manifold adjacent to the first solid state heat pipe and secured to the fin. The solid state heat pipe flex joint operably connects the solid state heat pipe manifolds of two of the plurality of panel subassemblies in a hermetically sealed configuration, and is configured to permit repositioning of the two panel subassemblies relative to each other.
申请公布号 US8859882(B2) 申请公布日期 2014.10.14
申请号 US200812286480 申请日期 2008.09.30
申请人 Aerojet Rocketdyne of DE, Inc. 发明人 Lu Cheng-Yi;McClanahan James A.;Carroll Joseph P.;Determan William;Frye Patrick E.;Kudija Charles Thomas;Howerton Rick L.;Metcalf Kenneth John;Zillmer Andrew J.
分类号 H01L31/052;F28D15/00 主分类号 H01L31/052
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A heat rejection system comprising: a plurality of panel subassemblies, each panel subassembly comprising: a planar fin;a solid state heat pipe manifold;a first solid state heat pipe tube operatively connected to the solid state heat pipe manifold and secured to the fin; anda second solid state heat pipe tube operatively connected to the solid state heat pipe manifold adjacent to the first solid state heat pipe and secured to the fin; and a solid state heat pipe flex joint operably connecting the solid state heat pipe manifolds of two of the plurality of panel subassemblies in a hermetically sealed configuration, wherein the solid state heat pipe flex joint is configured to permit repositioning of the two panel subassemblies relative to each other.
地址 Sacramento CA US