发明名称 METROLOGY-BASED SYSTEM FOR OPERATING A FLEXIBLE MANUFACTURING SYSTEM
摘要 <p>A method and apparatus for positioning an end effector relative to a fuselage assembly. A configuration of the fuselage assembly may be determined. The end effector may be positioned relative to the fuselage assembly based on the configuration determined. A set of actual reference locations may be identified for a set of reference points on the fuselage assembly. The end effector may be positioned at an operation location based on the set of actual reference locations identified.</p>
申请公布号 CA2894306(A1) 申请公布日期 2016.01.09
申请号 CA20152894306 申请日期 2015.06.15
申请人 THE BOEING COMPANY 发明人 OBEROI, HARINDER;REESE IV, RICHARD GRIFFITH;BARRICK, KEVIN MARION;DO, QUANG T.;DRAPER, ALAN S.;GEROSA, ALFREDO JOSE;SARH, BRANKO;GUDZINSKI, GREGORY;HU, YUANXIN CHARLES;MILLER, JEFFREY LAWRENCE;STOJANOSKI, VANCO;KOZAK, MICHAEL J.;FINDLAY, MELISSA ANN;ARRIAGA, JORGE ALBERTO
分类号 B64F5/00;B25H7/00;B25J9/00;B25J19/02 主分类号 B64F5/00
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