发明名称 ADJUSTABLE RETAINING STRUCTURE FOR CRADLE FIXTURE
摘要 PROBLEM TO BE SOLVED: To provide a method and apparatus for adjusting an adjustable retaining structure that may be applied to manufacturing of different types of aircraft fuselages.SOLUTION: A method comprises: placing an aircraft fuselage panel onto a cradle fixture 600 having an adjustable retaining structure 655; and engaging the adjustable retaining structure 655 with the aircraft fuselage panel. The adjustable retaining structure 655 is passively rotated about the spherical interface 654 as a panel applies a load to the adjustable retaining structure 655.SELECTED DRAWING: Figure 6
申请公布号 JP2016016862(A) 申请公布日期 2016.02.01
申请号 JP20150119173 申请日期 2015.06.12
申请人 BOEING CO 发明人 OBEROI HARINDER S;RICHARD GRIFFITH REESE IV;KEVIN MARION BARRICK;QUANG T DO;ALAN S DRAPER;ALFREDO JOSE GEROSA;SARH BRANKO;GREGORY GUDZINSKI;YUANXIN CHARLES HU;JEFFREY LAWRENCE MILLER;VANCO STOJANOSKI;MICHAEL J KOZAK;MELISSA ANN FINDLAY;JORGE ALBERTO ARRIAGA
分类号 B64F5/00;B64C1/00 主分类号 B64F5/00
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