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111. 发明授权

US09376219B2 Actuating system of sectors of a device for producing an airplane fuselage 有权
标题翻译：用于生产飞机机身的装置的部件的致动系统
公开(公告)号：US09376219B2
公开(公告)日：2016-06-28
申请号：US13852021
申请日：2013-03-28
申请人： Alenia Aermacchi S.p.A.
发明人： Guido Sibona , Ettore Mostarda , Giuseppe Iovine
IPC分类号： B64F5/00 , B29C33/48 , B29C53/82 , F16H25/20 , F16H25/24
CPC分类号： B64F5/0009 , B29C33/485 , B29C53/824 , B64F5/10 , F16H25/2021 , F16H2025/249 , Y02T50/43 , Y10T29/53961
摘要： An actuating system of sectors of a device for producing an airplane fuselage in which a lamination mandrel includes a plurality of sectors that are angularly spaced about an axis and mobile between an expanded lamination position and a contracted dissembled position. Each sector has screw-nut screw type actuating system in which a threaded element is rotated about the axis by a motor. The threaded element includes an internal shaft made of a first material extending along the axis, an external tubular portion made of a second material that is mounted axially on the shaft and constraint element arranged between the internal shaft and the external tubular portion to prevent angular displacement of the external tubular portion with respect to the internal shaft and allow a linear sliding of the external tubular portion with respect to the internal shaft.
摘要翻译：一种用于生产飞机机身的装置的扇区的致动系统，其中层压心轴包括多个扇形，所述多个扇形体围绕轴线成角度地间隔开，并且在膨胀的层压位置和收缩的拆卸位置之间可移动。每个扇区具有螺母螺母型致动系统，其中螺纹元件通过电动机绕轴线旋转。螺纹元件包括由沿轴线延伸的第一材料制成的内轴，由轴向安装在轴上的第二材料制成的外部管状部分和布置在内部轴与外部管状部分之间的约束元件，以防止角位移的外部管状部分相对于内部轴线允许外部管状部分相对于内部轴线线性滑动。

112. 发明授权

US09296187B2 Bagging process and mandrel for fabrication of elongated composite structure 有权
标题翻译：用于制造细长复合结构的装袋工艺和芯棒
公开(公告)号：US09296187B2
公开(公告)日：2016-03-29
申请号：US12332190
申请日：2008-12-10
申请人： Doan D. Pham , Mark W. Tollan , John D. Morris
发明人： Doan D. Pham , Mark W. Tollan , John D. Morris
IPC分类号： B32B37/10 , B29C33/48 , B29C70/44
CPC分类号： B29C70/30 , B29C33/485 , B29C33/505 , B29C70/446 , B29K2105/253 , B29L2031/3076 , B32B37/10 , B32B37/1009
摘要： A mandrel for composite fabrication includes an open cell foam carrier and at least one vacuum bag enclosing the open cell foam carrier.
摘要翻译：用于复合制造的心轴包括开孔泡沫载体和包围开孔泡沫载体的至少一个真空袋。

113. 发明授权

US09261124B2 Corrugated angle bracket consisting of a composite material 有权
标题翻译：由复合材料组成的瓦楞角支架
公开(公告)号：US09261124B2
公开(公告)日：2016-02-16
申请号：US13877142
申请日：2011-09-30
申请人： Jean-Michel Buchin
发明人： Jean-Michel Buchin
IPC分类号： F16B12/46 , B29C33/48
CPC分类号： F16B12/46 , B29C33/485 , Y10T403/42
摘要： The invention relates to an angle bracket including a composite material for connecting parts. The angle bracket has two wings forming an angle along a longitudinal folding axis and coupling regions on the outside of the fold. The coupling regions attach to parts to be connected, and is associated with a securing means. At least in the longitudinal direction, the angle bracket has at least one succession of domed sections with a concave or convex profile on the inside and/or outside of the fold, providing the bracket with a corrugated form in the longitudinal direction.
摘要翻译：本发明涉及包括用于连接部件的复合材料的角架。角托架具有两个翼沿纵向折叠轴线形成一个角度并且在折叠部分的外侧上形成一个连接区域。联接区域连接到要连接的部件，并且与固定装置相关联。至少在纵向方向上，角托架具有至少一个连续的圆顶部分，其在折叠的内侧和/或外侧具有凹形或凸形轮廓，从而在纵向方向上提供波形形状的托架。

114. 发明申请

US20160023406A1 APPARATUS AND METHOD FOR A SHAPE MEMORY ALLOY MANDREL 有权
标题翻译：形状记忆合金手册的装置和方法
公开(公告)号：US20160023406A1
公开(公告)日：2016-01-28
申请号：US14340914
申请日：2014-07-25
申请人： THE BOEING COMPANY
发明人： Moushumi Shome , Sahrudine Apdalhaliem , Frederick T. Calkins , Waeil M. Ashmawi , Kimberly Meredith
IPC分类号： B29C70/34 , B32B37/10 , B32B37/18 , B29C70/54 , B32B37/00
CPC分类号： B32B37/1036 , B29C33/38 , B29C33/485 , B29C70/446 , B29C70/54 , B29K2905/00 , B29L2031/3076 , B32B37/0046 , B32B37/18 , B32B2605/18 , Y02T50/43
摘要： In one or more aspects of the present disclosure, a mandrel is disclosed. The mandrel having a shape memory alloy (SMA) shell having a longitudinal axis, an interior extending along the longitudinal axis and an exterior contour, the SMA shell being configured to interface with a structure to be cured, and at least one SMA actuation member disposed within the interior and connected to the SMA shell, where the at least one SMA actuation member is configured to exert pressure against the SMA shell effecting an interface pressure between the exterior contour of the SMA shell and the structure to be cured where the exterior contour has a predetermined actuated shape that corresponds to a predetermined cured shape of the structure to be cured.
摘要翻译：在本公开的一个或多个方面，公开了一种心轴。心轴具有具有纵向轴线的形状记忆合金（SMA）壳体，沿着纵向轴线延伸的内部和外部轮廓，SMA壳体被配置为与要固化的结构相接触，并且至少一个SMA致动构件设置在在内部并且连接到SMA壳体，其中至少一个SMA致动构件构造成对SMA壳施加压力，从而影响SMA外壳的外部轮廓与外部轮廓具有的待固化结构之间的界面压力对应于要固化的结构的预定固化形状的预定的致动形状。

115. 发明申请

US20150274326A1 ASSEMBLING METHOD OF MANDREL USED FOR MANUFACTURING COMPOSITE MATERIAL STRUCTURE AND ASSEMBLING APPARATUS OF MANDREL 审中-公开
标题翻译：用于制造复合材料结构和装配装置的人造装配方法
公开(公告)号：US20150274326A1
公开(公告)日：2015-10-01
申请号：US14704492
申请日：2015-05-05
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： Toshikazu SANA , Naoki TAMURA , Tomoya TAKAHASHI , Toshiaki TAKECHI
IPC分类号： B64F5/00
CPC分类号： B64F5/0009 , B29C33/38 , B29C33/485 , B29L2031/3082 , B64C1/069 , B64F5/10 , Y02T50/43 , Y10T29/4978 , Y10T29/49828 , Y10T29/53539
摘要： A technique which can assemble a mandrel having a substantially cylindrical shape and being dividable into plurality of segments, which is used for manufacturing, for example, a fuselage of an aircraft, with high position accuracy and an easy manner. In a segment fastening step, a segment which is a fastened target is fastened to a specified fastening portion which is one of a plurality of fastening portions set along a pair of support rings placed to face each other. In a rotation step, before the segment fastening step, the support rings are rotated so that the specified fastening portion is located at an uppermost portion of the support rings. In the segment fastening step, the segment which is the fastened target is placed between the support rings and lifted vertically up to a height corresponding to the specified fastening portion and then fastened to the support rings.
摘要翻译：一种可以组装具有大致圆柱形形状的心轴的技术，其可以高精度和容易的方式组装成用于制造例如飞机的机身的多个段。在段紧固步骤中，作为紧固目标的段被紧固到指定的紧固部，该固定部是沿着彼此相对配置的一对支撑环设置的多个紧固部中的一个。在旋转步骤中，在节段紧固步骤之前，支撑环旋转，使得指定的紧固部分位于支撑环的最上部。在节段紧固步骤中，作为紧固目标的段被放置在支撑环之间并垂直提升到与指定的紧固部分相对应的高度，然后紧固到支撑环。

116. 发明授权

US09138919B2 Method for producing composite laminates using a collapsible mandrel 有权
标题翻译：使用可折叠心轴制造复合层压板的方法
公开(公告)号：US09138919B2
公开(公告)日：2015-09-22
申请号：US14326440
申请日：2014-07-08
申请人： The Boeing Company
发明人： John D. Morris , Michael A. Lee , Kenneth L. Brook
IPC分类号： B29C33/48 , B29C70/44 , B29D99/00
CPC分类号： B29C33/485 , B29C33/505 , B29C70/446 , B29D99/001
摘要： A collapsible bladder has flexible outer walls and at least one strut inside the enclosure. The strut is connected to the outer walls and controls the shape into which the enclosure may be collapsed.
摘要翻译：可折叠的气囊具有柔性外壁和外壳内的至少一个支柱。支柱连接到外壁并控制外壳可能被折叠的形状。

117. 发明申请

US20150246491A1 RIGID CORE MOLD REMOVAL DEVICE AND TIRE MANUFACTURING METHOD 审中-公开
标题翻译：刚性芯片去除装置和轮胎制造方法
公开(公告)号：US20150246491A1
公开(公告)日：2015-09-03
申请号：US14427574
申请日：2013-09-17
申请人： SUMITOMO RUBBER INDUSTRIES, LTD.
发明人： Hiroyuki Onimatsu
IPC分类号： B29D30/06 , B29C33/76 , B29D30/10
CPC分类号： B29D30/0649 , B29C33/485 , B29C33/76 , B29D30/0645 , B29D30/0661 , B29D30/0662 , B29D30/10 , B29D30/12 , B29D2030/0646 , B29L2030/00
摘要： A method for manufacturing a tire T comprises a step for forming a green tire on the outside of a rigid core mold 2, a step for vulcanization-molding and obtaining a tire-accompanying rigid core mold G, a step for setting, at an assembly station P3, a core 5 taken out from the tire-accompanied rigid core mold G, and a removal and assembly step for removing one core segment 3 from the tire T by moving in inwardly in the tire radial direction from the tire-accompanying rigid core mold G and mounting it on the core 5 set at the assembly station. The removal and assembly step is performed for every core segment in the tire, whereby a rigid core mold 2 is assembled at the assembly station P3, while removing the rigid core mold 2 from the tire T.
摘要翻译：制造轮胎T的方法T包括在刚性芯模2的外侧形成生胎的步骤，硫化成型步骤和获得与轮胎相关的刚性芯模G，在组装时设定的步骤站P3，从轮胎伴随的刚性芯模G取出的芯5，以及通过从轮胎相邻的刚性芯向内径向轮胎径向移动而从轮胎T移除一个芯段3的拆卸和组装步骤模具G，并将其安装在设在组装站的芯5上。对轮胎中的每个芯段执行拆卸和组装步骤，由此在组装工位P3处组装刚性芯模2，同时从轮胎T移除刚性芯模2。

118. 发明授权

US09079654B2 Assembling method of mandrel used for manufacturing composite material structure and assembling apparatus of mandrel 有权
标题翻译：用于制造复合材料结构的心轴的组装方法和心轴的组装装置
公开(公告)号：US09079654B2
公开(公告)日：2015-07-14
申请号：US13518984
申请日：2010-12-21
申请人： Toshikazu Sana , Naoki Tamura , Tomoya Takahashi , Toshiaki Takechi
发明人： Toshikazu Sana , Naoki Tamura , Tomoya Takahashi , Toshiaki Takechi
IPC分类号： B29C70/44 , B29C33/00 , B64C1/06 , B29C33/38 , B64F5/00
CPC分类号： B64F5/0009 , B29C33/38 , B29C33/485 , B29L2031/3082 , B64C1/069 , B64F5/10 , Y02T50/43 , Y10T29/4978 , Y10T29/49828 , Y10T29/53539
摘要： A technique which can assemble a mandrel having a substantially cylindrical shape and being dividable into plurality of segments, which is used for manufacturing, for example, a fuselage of an aircraft, with high position accuracy and an easy manner. In a segment fastening step, a segment which is a fastened target is fastened to a specified fastening portion which is one of a plurality of fastening portions set along a pair of support rings placed to face each other. In a rotation step, before the segment fastening step, the support rings are rotated so that the specified fastening portion is located at an uppermost portion of the support rings. In the segment fastening step, the segment which is the fastened target is placed between the support rings and lifted vertically up to a height corresponding to the specified fastening portion and then fastened to the support rings.
摘要翻译：一种可以组装具有大致圆柱形形状的心轴的技术，其可以高精度和容易的方式组装成用于制造例如飞机的机身的多个段。在段紧固步骤中，作为紧固目标的段被紧固到指定的紧固部，该固定部是沿着彼此相对配置的一对支撑环设置的多个紧固部中的一个。在旋转步骤中，在节段紧固步骤之前，支撑环旋转，使得指定的紧固部分位于支撑环的最上部。在节段紧固步骤中，作为紧固目标的段被放置在支撑环之间并垂直提升到与指定的紧固部分相对应的高度，然后紧固到支撑环。

119. 发明申请

US20150145170A1 Method of Making A Bayonet Sealing Closure For Containers and Lids 有权
标题翻译：用于容器和盖子的卡口密封方法
公开(公告)号：US20150145170A1
公开(公告)日：2015-05-28
申请号：US14552722
申请日：2014-11-25
申请人： Eveready Battery Company Inc.
发明人： Vincent Valderrama , John Rousso , Dmitriy Faktorovich , Stephen Mowers
IPC分类号： B29C45/26
CPC分类号： B29C45/2618 , B29C33/485 , B29C45/4435 , B29K2905/12 , B29L2031/56 , B29L2031/7158 , B65D41/06
摘要： A method for forming a container assembly having a lid, a container and a cooperative closure mechanism, includes providing a lid form and flexible members biased toward the lid form, wherein the lid form and the flexible members are operable between a forming position defined by the lid form exerting a biasing force against the flexible members, and an extraction position defined by the biasing force being substantially removed from the flexible members, creating a lid form cavity defined by the lid form and the flexible members disposed in the forming position, injecting a lid material throughout the lid form cavity to form a lid, disposing the lid form and the flexible members in the extraction position, wherein the lid form is moved distal from the lid and the flexible members are biased away from the lid to separate the lid from the flexible members.
摘要翻译：一种用于形成具有盖，容器和协同闭合机构的容器组件的方法，包括提供盖形式和朝向盖形式偏置的柔性构件，其中，盖形式和柔性构件可在由盖形式对柔性构件施加偏置力，并且由偏置力限定的抽出位置基本上从柔性构件移除，形成由盖形式限定的盖形腔和设置在成形位置的柔性构件，盖子材料贯穿盖子形成腔体以形成盖子，将盖子形式和柔性构件设置在提取位置，其中盖子形式从盖子的远侧移动，并且柔性构件偏离盖子以将盖子从盖子灵活的会员。

120. 发明授权

US09011748B2 Plastic component with a complex and bifurcated structure 有权
标题翻译：具有复杂和分叉结构的塑料部件
公开(公告)号：US09011748B2
公开(公告)日：2015-04-21
申请号：US13477453
申请日：2012-05-22
申请人： Thomas Eifflaender , Daniel Wolf , Jens Heimann
发明人： Thomas Eifflaender , Daniel Wolf , Jens Heimann
IPC分类号： B29C70/44 , B29C70/34 , B29C33/48
CPC分类号： B32B5/12 , B29C33/485 , B29C45/0005 , B29C70/345 , B32B2605/08 , B60G11/02 , B60G2206/71 , Y10T428/24124
摘要： A die for producing pressed, fiber-reinforced plastic components, as well as a method for producing the plastic component, and the plastic component itself. The plastic components comprising at least two structural parts which overlap one another a pressing direction such that the die comprises at least one upper die portion formed with a pressing unit for applying a pressing force in the pressing direction, and at least one lower die portion which cooperates with the upper die portion to form a cavity in which the plastic component is formed. A die insert is fitted in the die and can move by and with the upper die portion and is designed to transmit the pressing force to the at least one structural part of the plastic component which is overlapped by the other structural part of the plastic component in the pressing direction.
摘要翻译：用于生产压制，纤维增强塑料部件的模具，以及用于生产塑料部件的方法和塑料部件本身。所述塑料部件包括至少两个彼此重叠的结构部件的挤压方向，使得所述模具包括形成有用于在按压方向上施加按压力的按压单元的至少一个上模具部分和至少一个下模具部分，与上模具部分配合形成塑料部件形成的空腔。模具插入件装配在模具中并且可以与上模具部分一起移动并且被设计成将挤压力传递到与塑料部件的另一结构部分重叠的塑料部件的至少一个结构部分，按压方向。

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