发明名称 SATELLITE SUPPORT STRUCTURE COMPRISING A DAMPING CONNECTING DEVICE
摘要 A satellite support structure to support at least one device of the satellite. The support structure includes structural elements with at least one of the structural elements being a damping connector linking at least two other structural elements of the support structure. The damping connector includes an elastomer element and at least one flat angle bracket having at least two wings to be linked by the respective connectors to the damped structural elements. The elastomer element is made from elastomer material with loss angle δ greater than ten degrees and is arranged such that the transmission of forces between one of the wings of the flat angle bracket and the connectors is achieved entirely via the elastomer element.
申请公布号 EP3071483(A1) 申请公布日期 2016.09.28
申请号 EP20140802060 申请日期 2014.11.21
申请人 AIRBUS DEFENCE AND SPACE SAS 发明人 ARIDON, GWENAËLLE;CAMARASA, PATRICK
分类号 B64G1/10;B64G1/22;B64G1/64;F16F1/38 主分类号 B64G1/10
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