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:
Oct. 01, 2019

Filed:

Dec. 21, 2016
Applicants:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Thomas Kruse, Hamburg, DE;

Thomas Körwien, Höhenkirchen, DE;

Alois Friedberger, Oberpframmern, DE;

Andreas Helwig, München, DE;

Assignees:

AIRBUS DEFENCE AND SPACE GMBH, Taufkirchen, DE;

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01M 3/26 (2006.01); G01M 3/04 (2006.01); G01N 19/08 (2006.01); B29C 65/48 (2006.01); B29C 65/82 (2006.01); B29C 65/00 (2006.01); G01M 3/32 (2006.01); G01N 3/12 (2006.01); G01N 19/04 (2006.01); B64C 1/12 (2006.01); B64C 3/26 (2006.01); B64D 45/00 (2006.01); B29C 65/52 (2006.01);
U.S. Cl.
CPC ...
G01M 3/26 (2013.01); B29C 65/48 (2013.01); B29C 65/8246 (2013.01); B29C 66/1122 (2013.01); B29C 66/131 (2013.01); B29C 66/474 (2013.01); B29C 66/721 (2013.01); B29C 66/7394 (2013.01); B64C 1/12 (2013.01); B64C 3/26 (2013.01); B64D 45/00 (2013.01); G01M 3/04 (2013.01); G01M 3/3272 (2013.01); G01N 3/12 (2013.01); G01N 19/04 (2013.01); G01N 19/08 (2013.01); B29C 65/52 (2013.01); B29C 65/522 (2013.01); B29C 65/526 (2013.01); B29C 66/026 (2013.01); B29C 66/71 (2013.01); B29C 66/73753 (2013.01); B29C 66/73754 (2013.01); B29C 66/73755 (2013.01); B29C 66/73756 (2013.01); B29C 66/742 (2013.01); B64D 2045/0085 (2013.01);
Abstract

The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, the component device having a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, and a detector device having at least one interior space sensor device configured to measure a change in a pressure and/or a concentration of a gas surrounding the interior space sensor device. The first component element, the second component element, and the bonding confine an interior space. The interior space sensor device is arranged in the interior space.


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