Patent · US Active

Satellite support structure comprising a damping connecting device

US9592922B2 · kind B2 · utility

2Cited by
5References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2014
Grant dateMar 14, 2017
Priority date
Expiry dateNov 21, 2034

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64G1/64
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.