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:
Jun. 28, 2022

Filed:

Oct. 25, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Fei Cai, Edmonds, WA (US);

Tanni Sisco, Mukilteo, WA (US);

Matthew Ryan Dunaj, Saint Clair, MI (US);

Brian Joseph Cobb, Columbiaville, MI (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23B 39/24 (2006.01); B64F 5/10 (2017.01); B23B 35/00 (2006.01); F16B 5/06 (2006.01); B25J 9/16 (2006.01); B25J 11/00 (2006.01); B64C 1/12 (2006.01); B23P 19/00 (2006.01);
U.S. Cl.
CPC ...
B23B 39/24 (2013.01); B23B 35/00 (2013.01); B25J 9/1687 (2013.01); B25J 11/0055 (2013.01); B64C 1/12 (2013.01); B64F 5/10 (2017.01); F16B 5/0642 (2013.01); B23B 2215/04 (2013.01); B23B 2270/08 (2013.01); B23P 19/001 (2013.01); G05B 2219/45059 (2013.01); G05B 2219/45064 (2013.01);
Abstract

An end effector provides one up assembly drilling through mated components, including a panel, by preloading the components. The end effector includes a drill and clamp dispenser for temporarily inserting and removing expansible single-sided clamps at various pre-drilled locations in the panel. In one method, pilot holes are first pre-drilled into mated components, for example an aircraft wing panel and a wing rib or spar; an initial pilot hole location is identified, and an expansible clamp is inserted into a pilot hole adjacent a desired initial fastener hole location. The clamp is torqued, causing its expansion for preloading the wing panel and rib and/or spar components under a predetermined load. The fastener hole is then drilled, the end effector untorques and removes the clamp and identifies a second (and/or next) pilot hole location, and the process is replicated.


Find Patent Forward Citations

Loading…