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公开(公告)号：US20070120013A1
公开(公告)日：2007-05-31
申请号：US10539016
申请日：2003-12-15
申请人： Andrew Levers
发明人： Andrew Levers
CPC分类号： B21D26/021 , B21D37/02 , Y10T29/49622
摘要： A creep forming tool modifies the shape of an aircraft component in the form of a wing skin portion. The tool includes a shaped surface defined by removable rib boards. The component is forced against the shaped surface, via a reusable intermediate plate. The shape of the shaped surface may be adjusted, if necessary, by replacing the rib boards with boards of a different shape.
摘要翻译： 蠕变成形工具以翼形部分的形式改变飞机部件的形状。 该工具包括由可移除的肋板限定的成形表面。 通过可重复使用的中间板将部件压在成形表面上。 如果需要，可以通过用不同形状的板代替肋板来调节成形表面的形状。
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公开(公告)号：US08715561B2
公开(公告)日：2014-05-06
申请号：US13059304
申请日：2009-08-28
申请人： Andrew Levers , Gary Wiles
发明人： Andrew Levers , Gary Wiles
CPC分类号： B29C70/44 , B29C31/08 , B29C70/342 , B29C70/386 , B29L2031/3076 , Y10T156/1044 , Y10T428/24628
摘要： A method of assembling and shaping a laminate panel. An intermediate member is mounted on a lay-up table and a lay-up is assembling by laying a series of plies onto the intermediate member on the lay-up table. The intermediate member and the lay-up are then removed from the lay-up table and placed them on a shaped surface. The lay-up is then forced against the shaped surface, via the intermediate member, in a manner that modifies the shape of the lay-up to form a shaped laminate panel. Finally the shaped laminate panel is removed from the intermediate member. The lay-up table can thus support the flexible intermediate member during assembly, and can be relatively flat to enable the lay-up to assembled by an automated process.
摘要翻译： 一种组装和成型层压板的方法。 中间构件安装在铺层台上，并且通过将一系列层叠放置在铺层台上的中间构件上组装。 然后将中间构件和叠层从铺设台上取下并将其放置在成形表面上。 然后通过中间构件将叠层件以成形的叠层板的形状进行修改，从而将叠层物压在成形表面上。 最后，从中间构件移除成形的层压板。 因此，组装台可以在组装期间支撑柔性中间构件，并且可以相对平坦，以使得能够通过自动化过程进行组装。
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公开(公告)号：US08303729B2
公开(公告)日：2012-11-06
申请号：US10539016
申请日：2003-12-15
申请人： Andrew Levers
发明人： Andrew Levers
IPC分类号： C22C1/00
CPC分类号： B21D26/021 , B21D37/02 , Y10T29/49622
摘要： A creep forming tool modifies the shape of an aircraft component in the form of a wing skin portion. The tool includes a shaped surface defined by removable rib boards. The component is forced against the shaped surface, via a reusable intermediate plate. The shape of the shaped surface may be adjusted, if necessary, by replacing the rib boards with boards of a different shape.
摘要翻译： 蠕变成形工具以翼形部分的形式改变飞机部件的形状。 该工具包括由可移除的肋板限定的成形表面。 通过可重复使用的中间板将部件压在成形表面上。 如果需要，可以通过用不同形状的板代替肋板来调节成形表面的形状。
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公开(公告)号：US07322223B2
公开(公告)日：2008-01-29
申请号：US10477228
申请日：2002-07-04
申请人： Andrew Levers
发明人： Andrew Levers
IPC分类号： C22F1/00
CPC分类号： B21D26/055 , B21D11/20 , B21D35/008
摘要： A method of creep forming a metallic component is provided. The method includes the steps of applying static loading and cyclic loading and/or vibration to the component during the creep forming thereof to act as a source of additional energy.
摘要翻译： 提供了形成金属部件的蠕变方法。 该方法包括以下步骤：在构件的蠕变过程中将元件施加静态载荷和循环加载和/或振动作为额外能量的来源。
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公开(公告)号：US20110143100A1
公开(公告)日：2011-06-16
申请号：US13059304
申请日：2009-08-28
申请人： Andrew Levers , Gary Wiles
发明人： Andrew Levers , Gary Wiles
CPC分类号： B29C70/44 , B29C31/08 , B29C70/342 , B29C70/386 , B29L2031/3076 , Y10T156/1044 , Y10T428/24628
摘要： A method of assembling and shaping a laminate panel. An intermediate member is mounted on a lay-up table and a lay-up is assembling by laying a series of plies onto the intermediate member on the lay-up table. The intermediate member and the lay-up are then removed from the lay-up table and placed them on a shaped surface. The lay-up is then forced against the shaped surface, via the intermediate member, in a manner that modifies the shape of the lay-up to form a shaped laminate panel. Finally the shaped laminate panel is removed from the intermediate member. The lay-up table can thus support the flexible intermediate member during assembly, and can be relatively flat to enable the lay-up to assembled by an automated process.
摘要翻译： 一种组装和成型层压板的方法。 中间构件安装在铺层台上，并且通过将一系列层叠放置在铺层台上的中间构件上组装。 然后将中间构件和叠层从铺设台上取下并将其放置在成形表面上。 然后通过中间构件将叠层件以成形的叠层板的形状进行修改，从而将叠层物压在成形表面上。 最后，从中间构件移除成形的层压板。 因此，组装台可以在组装期间支撑柔性中间构件，并且可以相对平坦，以使得能够通过自动化过程进行组装。
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公开(公告)号：US20060042347A1
公开(公告)日：2006-03-02
申请号：US10539017
申请日：2003-12-15
申请人： Andrew Levers
发明人： Andrew Levers
IPC分类号： B21D37/02
CPC分类号： B21D26/021 , B21D37/02
摘要： A creep forming tool modifies the shape of an aircraft component in the form of a wing skin portion. The tool includes a shaped surface defined by removable rib boards. The component is forced against the shaped surface, via a reusable intermediate plate. The shape of the shaped surface may be adjusted, if necessary, by replacing the rib boards with boards of a different shape.
摘要翻译： 蠕变成形工具以翼形部分的形式改变飞机部件的形状。 该工具包括由可移除的肋板限定的成形表面。 通过可重复使用的中间板将部件压在成形表面上。 如果需要，可以通过用不同形状的板代替肋板来调节成形表面的形状。
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