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公开(公告)号：EP2133263B2
公开(公告)日：2016-06-29
申请号：EP09251515.4
申请日：2009-06-09
申请人： The Boeing Company
CPC分类号： B29C70/446 , B29C70/46 , B29D99/0003 , B29D99/0014 , B29L2031/3082 , B64F5/10 , Y02T50/43 , Y10T29/49622 , Y10T29/53978
摘要： A hands-free method and related apparatus are used to shape, place and compact a composite stringer (34) on a composite skin (24) of an aircraft. A composite charge is placed on a tool assembly (20) that used to shape the charge into a preformed stringer. With the stringer held on the tool assembly, the tool assembly is used to move the preformed stringer into proximity with the skin and both place and compact the stringer against the skin. Following compaction of the stringer, the tool assembly is removed and the skin and the stringer are co-cured.
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公开(公告)号：EP4140683A1
公开(公告)日：2023-03-01
申请号：EP22178132.1
申请日：2022-06-09
申请人： The Boeing Company
IPC分类号： B29C31/08 , B29C51/08 , B29C70/34 , B29C70/38 , B29C70/42 , B29C70/44 , B29C70/54 , B29C70/56 , B29D99/00 , B29C43/36 , B29C70/30
摘要： A method for forming a composite part includes positioning a composite ply over a forming surface of a forming tool, moving a forming feature into engagement with the composite ply to yield a formed ply, and, after the moving, securing the formed ply relative to the forming tool.
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4.发明公开Method and apparatus for forming and installing stringers 有权Verfahren und Vorrichtung zur Herstellung und Montage von Stringern
公开(公告)号：EP2133263A2
公开(公告)日：2009-12-16
申请号：EP09251515.4
申请日：2009-06-09
申请人： THE BOEING COMPANY
CPC分类号： B29C70/446 , B29C70/46 , B29D99/0003 , B29D99/0014 , B29L2031/3082 , B64F5/10 , Y02T50/43 , Y10T29/49622 , Y10T29/53978
摘要： A hands-free method and related apparatus are used to shape, place and compact a composite stringer (34) on a composite skin (24) of an aircraft. A composite charge is placed on a tool assembly (20) that used to shape the charge into a preformed stringer. With the stringer held on the tool assembly, the tool assembly is used to move the preformed stringer into proximity with the skin and both place and compact the stringer against the skin. Following compaction of the stringer, the tool assembly is removed and the skin and the stringer are co-cured.
摘要翻译： 使用免提方法和相关装置来在飞机的复合皮肤（24）上成形，放置和压制复合纵梁（34）。 将复合电荷放置在用于将电荷成形为预成形的纵梁的工具组件（20）上。 将工具组件固定在工具组件上时，工具组件用于将预成形的桁条移动到皮肤附近，并将绷带放置并紧固在皮肤上。 在桁条的压实之后，移除工具组件并且皮肤和桁条共同固化。
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公开(公告)号：EP4140712A1
公开(公告)日：2023-03-01
申请号：EP22178130.5
申请日：2022-06-09
申请人： The Boeing Company
IPC分类号： B29C70/38 , B29C70/54 , B29D99/00 , B29C31/08 , B29C51/08 , B29C70/30 , B29C70/44 , B29C70/56 , B29C70/34 , B29C70/42 , B29L31/30 , B29C43/36
摘要： A composite forming apparatus includes an end effector and a forming feature that is coupled to the end effector. The end effector moves the forming feature relative to a forming tool to form a composite ply over a forming surface of the forming tool or over previously formed composite material on the forming surface of the forming tool. The composite forming apparatus further includes a positioning member engaged with the forming feature. The engagement between the positioning member and the forming feature facilitates a position between the forming feature and the composite ply to promote uniform application of compaction force over the forming surface of the forming tool.
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公开(公告)号：EP4140711A1
公开(公告)日：2023-03-01
申请号：EP22178136.2
申请日：2022-06-09
申请人： The Boeing Company
IPC分类号： B29C70/34 , B29C70/38 , B29C70/42 , B29C70/44 , B29C70/54 , B29C70/56 , B29D99/00 , B29C31/08 , B29C51/08 , B29C35/08 , B29C70/30 , B29C43/36
摘要： A composite forming apparatus includes an end effector, a forming feature, and a non-contact heater. The forming feature is coupled to the end effector. The end effector moves the forming feature relative to a composite ply to form the composite ply over a forming tool or a prior formed composite ply. The non-contact heater heats to a portion of the composite ply before the portion of the composite ply is formed over the forming tool or the prior formed composite ply.
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7.发明公开
公开(公告)号：EP2977189A1
公开(公告)日：2016-01-27
申请号：EP15170418.6
申请日：2015-06-03
申请人： The Boeing Company
CPC分类号： B29C70/46 , B21D11/18 , B29C33/308 , B29C43/203 , B29C43/36 , B29C70/462 , B29C70/543 , B29C2043/3605
摘要： Apparatuses and methods for forming a joggle (24) and a longitudinal ridge (18) in a multi-ply composite charge (34) are disclosed. Charges may be formed in a forming press (40) that comprises a joggled die (80), with a longitudinal ridge (84) and a joggle (88) that crosses the longitudinal ridge, and a conforming die (50), with a series of longitudinally-spaced die fingers (52). The die fingers include pairs of die members (54) configured to move laterally between a closed position and an open position, with each die member configured to tilt longitudinally.
摘要翻译： 装置和用于在多层复合装料（34）形成一榫（24）和一纵向凸脊（18）的方法是游离缺失盘。 电荷可以在成形压力机（40）形成确实包括一具有纵向凸脊（84）和一个啮合（88）的Joggled（80）做有一系列横穿纵向脊，和一个一致的（50） 的纵向间隔开的指状物（52）。 手指包括对被配置为移动一个关闭位置和打开位置之间尾盘反弹，与每个构件已配置的纵向倾斜件（54）的。
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8.发明授权Method and apparatus for forming and applying composite layups having complex geometries 有权用于复合片材材料的具有复杂几何形状的形成和存储的方法和装置
公开(公告)号：EP2383106B1
公开(公告)日：2013-07-10
申请号：EP11160866.7
申请日：2011-04-01
申请人： The Boeing Company
CPC分类号： B29C70/384 , B29C70/382 , B29C70/44 , B29C70/541 , B29C73/12 , B29C73/32 , B29C2037/903 , B29L2031/3076 , B29L2031/3082 , B32B37/10 , Y10T156/10 , Y10T156/17
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公开(公告)号：EP2133263B1
公开(公告)日：2013-03-27
申请号：EP09251515.4
申请日：2009-06-09
申请人： THE BOEING COMPANY
CPC分类号： B29C70/446 , B29C70/46 , B29D99/0003 , B29D99/0014 , B29L2031/3082 , B64F5/10 , Y02T50/43 , Y10T29/49622 , Y10T29/53978
摘要： A hands-free method and related apparatus are used to shape, place and compact a composite stringer (34) on a composite skin (24) of an aircraft. A composite charge is placed on a tool assembly (20) that used to shape the charge into a preformed stringer. With the stringer held on the tool assembly, the tool assembly is used to move the preformed stringer into proximity with the skin and both place and compact the stringer against the skin. Following compaction of the stringer, the tool assembly is removed and the skin and the stringer are co-cured.
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公开(公告)号：EP2133263A3
公开(公告)日：2011-11-16
申请号：EP09251515.4
申请日：2009-06-09
申请人： THE BOEING COMPANY
CPC分类号： B29C70/446 , B29C70/46 , B29D99/0003 , B29D99/0014 , B29L2031/3082 , B64F5/10 , Y02T50/43 , Y10T29/49622 , Y10T29/53978
摘要： A hands-free method and related apparatus are used to shape, place and compact a composite stringer (34) on a composite skin (24) of an aircraft. A composite charge is placed on a tool assembly (20) that used to shape the charge into a preformed stringer. With the stringer held on the tool assembly, the tool assembly is used to move the preformed stringer into proximity with the skin and both place and compact the stringer against the skin. Following compaction of the stringer, the tool assembly is removed and the skin and the stringer are co-cured.
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