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:
Dec. 02, 2025

Filed:

Nov. 25, 2019
Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Thomas Körwien, Taufkirchen, DE;

Anton Maier, Taufkirchen, DE;

Thomas Kruse, Hamburg, DE;

Jens Holtmannspötter, Erding, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 5/40 (2017.01); B29C 65/82 (2006.01); B29C 73/10 (2006.01); B29C 73/24 (2006.01); B64F 5/00 (2017.01); B64F 5/60 (2017.01); G01N 19/04 (2006.01);
U.S. Cl.
CPC ...
B64F 5/40 (2017.01); B29C 73/10 (2013.01); B29C 73/24 (2013.01); B64F 5/00 (2013.01); B64F 5/60 (2017.01); G01N 19/04 (2013.01); B29C 65/8207 (2013.01);
Abstract

An indication device for monitoring the structural integrity of a repair location on a laminate structure, produced from a composite material, of a part of an aircraft outer skin is specified. The indication device has at least one elongate, thin indicator strip. The indicator strip is detachably applied to the outer layer of the laminate structure in the immediate vicinity of the repair location. The indicator strip is designed to indicate a predefined residual strength of an adhesive joint of a repair patch to the surrounding composite material.


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