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    • 7. 发明申请
    • TRUSS STRUCTURE
    • TRUSS结构
    • WO2016138426A1
    • 2016-09-01
    • PCT/US2016/019855
    • 2016-02-26
    • SPACE SYSTEMS/LORAL, LLC
    • HIJMANS, Carey, GrahamFREESTONE, Michael, Paul
    • B64G99/00E04B1/19E04H12/02
    • E04H12/02B64G1/10B64G9/00
    • A spacecraft includes a 3-D closed truss structure including at least four coupling nodes (220.1-4) and at least six strut elements (210.1-6), attached together by a plurality of joints (221), each coupling node (220) including at least two legs, each strut element (210) disposed between and attached with a respective pair of the plurality of coupling nodes (220). Each coupling node (220) is attached, at respective ones of the plurality of joints (221), with at least two strut elements (210). Each strut element (210) is attached at a first end with a first leg of a first coupling node (220) and is attached at a second end with a second leg of a second coupling node (220), the first leg being substantially longer than the second leg.
    • 航天器包括三维闭合桁架结构,其包括至少四个耦合节点(220.1-4)和至少六个支撑元件(210.1-6),其由多个接头(221)连接在一起,每个耦合节点(220) 包括至少两个腿,每个支撑元件(210)设置在相应的一对所述多个耦合节点(220)之间并且附接到所述多个耦合节点(220)中。 每个耦合节点(220)在多个关节(221)中的相应的一个处连接有至少两个支柱元件(210)。 每个支柱元件(210)在第一端处与第一联接节点(220)的第一腿连接,并且在第二端处与第二联接节点(220)的第二腿连接,第一腿部基本上更长 比第二条腿。