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:
Apr. 24, 2018

Filed:

Dec. 09, 2013
Applicant:

European Aeronautic Defence and Space Company Eads France, Paris, FR;

Inventors:

Catherine Bosquet, Sucé sur Erdre, FR;

Bruno Thomas, Paris, FR;

Louis Le Pinru, Rezé, FR;

Assignee:

AIRBUS, Blagnac, FR;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01N 29/00 (2006.01); G01N 29/04 (2006.01); G01N 29/22 (2006.01); G01N 29/265 (2006.01);
U.S. Cl.
CPC ...
G01N 29/043 (2013.01); G01N 29/226 (2013.01); G01N 29/265 (2013.01); G01N 2291/0231 (2013.01); G01N 2291/02827 (2013.01); G01N 2291/2694 (2013.01);
Abstract

A device for testing a stiffener of an aircraft structure made from composite materials. At least one ultrasound sensor is configured to provide measurements relative to a material health state of the stiffener. The device includes a protective enclosure for housing the ultrasound sensor and a mobile gantry configured to move along the stiffener. The protective enclosure with the ultrasound sensor is mounted inside the mobile gantry. A driver is configured to drive the mobile gantry along the stiffener. A clamper is rigidly connected to the protective enclosure and configured to hold the ultrasound sensor pressed against the surface of the stiffener to be controlled. A locator to synchronize each area of the surface of the stiffener with the measurement of the ultrasound sensor.


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