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. 28, 2020

Filed:

Oct. 03, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jake A. Wilson, Charleston, SC (US);

Craig A. Charlton, Charleston, SC (US);

Andrew M. Huckey, Charleston, SC (US);

Mark E. Nestleroad, Charleston, SC (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64F 1/36 (2017.01); B64F 5/10 (2017.01); B64C 1/06 (2006.01); B23P 19/10 (2006.01); B25J 13/08 (2006.01); B23P 21/00 (2006.01); B25J 9/08 (2006.01); G01C 25/00 (2006.01);
U.S. Cl.
CPC ...
B64F 5/10 (2017.01); B23P 19/102 (2013.01); B25J 13/081 (2013.01); B64C 1/068 (2013.01); B23P 21/00 (2013.01); B25J 9/08 (2013.01); G01C 25/005 (2013.01); G05B 2219/31068 (2013.01);
Abstract

A system for moving first and second fuselage structures into assembly alignment, the system including a first transmitter indexed to a first seat track of the first fuselage structure, a first reflector target indexed to a first seat track of the second fuselage structure, a second transmitter indexed to a second seat track of the first fuselage structure, a second reflector target indexed to a second seat track of the second fuselage structure, wherein the first and second transmitters and the first and second reflector targets cooperate to provide first and second measurements indicative of position of the first fuselage structure relative to the second fuselage structure, and a manipulator system including at least one assembly actuator coupled to the first fuselage structure to move the first fuselage structure into assembly alignment with the second fuselage structure based upon the first and second measurements.


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