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. 21, 2015

Filed:

Jun. 27, 2012
Applicants:

William P. Motzer, Seattle, WA (US);

James C. Kennedy, Renton, WA (US);

Michael C. Hutchinson, Kent, WA (US);

Martin L. Freet, Federal Way, WA (US);

Ronald E. Vonwahlde, Puyallup, WA (US);

Steven Ray Walton, Wilkeson, WA (US);

Jeffry J. Garvey, Burien, WA (US);

Scott W. Lea, Renton, WA (US);

James J. Troy, Issaquah, WA (US);

Daniel James Wright, Mercer Island, WA (US);

Hien T. Bui, Kent, WA (US);

Michael Joseph Duncan, Lake Tapps, WA (US);

Mark L. Little, Auburn, WA (US);

William Joseph Tapia, Kapowsin, WA (US);

Barry A. Fetzer, Renton, WA (US);

Richard C. Krotzer, Enumclaw, WA (US);

Inventors:

William P. Motzer, Seattle, WA (US);

James C. Kennedy, Renton, WA (US);

Michael C. Hutchinson, Kent, WA (US);

Martin L. Freet, Federal Way, WA (US);

Ronald E. VonWahlde, Puyallup, WA (US);

Steven Ray Walton, Wilkeson, WA (US);

Jeffry J. Garvey, Burien, WA (US);

Scott W. Lea, Renton, WA (US);

James J. Troy, Issaquah, WA (US);

Daniel James Wright, Mercer Island, WA (US);

Hien T. Bui, Kent, WA (US);

Michael Joseph Duncan, Lake Tapps, WA (US);

Mark L. Little, Auburn, WA (US);

William Joseph Tapia, Kapowsin, WA (US);

Barry A. Fetzer, Renton, WA (US);

Richard C. Krotzer, Enumclaw, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B64C 30/00 (2006.01); G01N 29/22 (2006.01); G01N 29/265 (2006.01); G01N 29/04 (2006.01);
U.S. Cl.
CPC ...
G01N 29/043 (2013.01); G01N 29/225 (2013.01); G01N 29/265 (2013.01); G01N 2291/0231 (2013.01); G01N 2291/2694 (2013.01);
Abstract

A system and method that allow inspection of hollow structures made of composite material, such as an integrally stiffened wing box of an aircraft. A wing box comprises top and bottom skins connected by a plurality of spaced spars. The system employs a plurality of scanners for inspecting different portions of each spar. The system uses dynamically controlled magnetic coupling to connect an external drive tractor to computer-controlled scanners that carry respective sensors, e.g., linear ultrasonic transducer arrays. A system operator can control the various components by means of a graphical user interface comprising multiple interaction regions that represent the individual scanner motion paths and are associated with respective motion script files.


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