The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 11, 2020

Filed:

Jun. 16, 2015
Applicant:

Airbus Defence and Space, S.a., Madrid, ES;

Inventor:

Miguel Lancho Doncel, Madrid, ES;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16F 1/373 (2006.01); F16F 1/34 (2006.01); B64G 1/64 (2006.01); F16F 3/087 (2006.01); F16F 3/12 (2006.01); B64G 1/22 (2006.01);
U.S. Cl.
CPC ...
B64G 1/641 (2013.01); F16F 1/3732 (2013.01); F16F 3/0876 (2013.01); F16F 3/12 (2013.01); B64G 2001/228 (2013.01); F16F 1/34 (2013.01); F16F 2224/0208 (2013.01); F16F 2226/04 (2013.01);
Abstract

A lightweight passive attenuator () for spacecraft includes two omega cross-section rings (), placed symmetrically and defining a gap therebetween, and being the main load path of the light passive attenuator (). A plurality of damper elements () are placed in the gap defined between the two omega cross-section rings (), and not in the main load path of the light passive attenuator (), such that the omega cross-section rings () and the damper elements () are assembled at their ends by attachment elements. The omega cross-section rings () have a protruding central part () with a plurality of holes () for connection with adjacent structures () of the spacecraft.


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