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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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