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:
Aug. 08, 2017

Filed:

Feb. 13, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Edward Batt, Bothell, WA (US);

Tanni Sisco, Mukilteo, WA (US);

Daniel Smith, Scottsdale, AZ (US);

Randy Woolridge, Saint Clair Shores, MI (US);

Samuel Edward Antonucci, Saint Clair Shores, MI (US);

Craig Roedel, Fenton, MI (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64F 5/00 (2017.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B64F 5/0009 (2013.01); B64F 5/10 (2017.01);
Abstract

A method for assembling an aircraft engine nacelle inlet lip includes automatically positioning, with a controller an automated workstation in two degrees of freedom to position an articulated assembly fixture docking station in at least two predetermined joining positions, and effecting, with the controller, an ordered assembly of at least a forward bulkhead joint, a forward bulkhead to lipskin joint, a chord member to lipskin joint, an inner barrel to lipskin joint, an aft bulkhead to lipskin joint and an outer barrel to lipskin joint through an interface between an automated assembly tool and at least one of a plurality of assembly fixtures interchangeably mounted on the docking station, where each assembly fixture corresponds to an assembly step of the aircraft engine nacelle inlet lip and at least one of the assembly fixtures is common to more than one assembly step of the aircraft engine nacelle inlet lip.


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