专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

91. 发明授权

US09145998B2 System for sealing a pipeline system 有权
标题翻译：管道系统密封系统
公开(公告)号：US09145998B2
公开(公告)日：2015-09-29
申请号：US13208005
申请日：2011-08-11
申请人： Hans Bohnet , Jens Eitel
发明人： Hans Bohnet , Jens Eitel
IPC分类号： F16L23/00 , F16J15/46 , F16L55/163 , F16L37/62 , F16L55/134 , F16L17/10 , B29C73/32
CPC分类号： F16L55/163 , B29C73/32 , F16L17/10 , F16L37/62 , F16L55/134
摘要： A system is provided that includes a fluid-tight tube, which for insertion can be introduced into the area of a gap to be sealed between two pipes of the pipeline system to be sealed. The tube is provided with a feed element for introducing a fluid, with whose aid the tube is filled and thereby increased in its volume. The feed element contains a valve, which facilitates the introduction of the fluid and at the same time prevents the outward flow via the feed element.
摘要翻译：提供了一种包括流体密封管的系统，其可插入待密封的管道系统的两个管之间的间隙的区域中。该管设置有用于引入流体的进料元件，其中有助于管子的填充，从而增加其体积。进料元件包含一个阀，这便于引入流体，同时防止通过进料元件的向外流动。

92. 发明申请

US20150158258A1 Systems and Methods for On-Aircraft Composite Repair Using Double Vacuum Debulking 审中-公开
标题翻译：使用双重真空去雾的飞机复合材料修复的系统和方法
公开(公告)号：US20150158258A1
公开(公告)日：2015-06-11
申请号：US14621634
申请日：2015-02-13
申请人： The Boeing Company
发明人： Karl Edward Nelson , Michael W. Evens , John F. Spalding, JR. , James D. Chanes , Joel P. Baldwin , Paul S. Rutherford
IPC分类号： B29C73/32 , B32B37/10 , B32B37/00
CPC分类号： B29C73/32 , B29C65/18 , B29C66/81455 , B29C66/82661 , B29C73/10 , B29C73/12 , B29C73/30 , B29C2043/3644 , B29L2031/3076 , B30B5/02 , B30B9/22 , B32B37/0046 , B32B37/10 , B32B37/1009 , B32B37/1018 , B32B2605/18
摘要： An in-situ double vacuum debulk (DVD) composite repair system designed to produce partially or fully cured autoclave-quality hot-bond composite repairs on contoured structures. The system provides vacuum pressure for hot bond repairs to be performed on flat and contoured structures using one set-up capable of debulking (partially curing) and then fully curing composite repairs on composite and metallic aircraft structures. The use of in-situ DVD also eliminates handling of the patch/adhesive when transferring from an off-aircraft DVD chamber to the repair site on the aircraft. This can increase the probability of successful repairs because the possibility of contaminating and misaligning the adhesive and repair patch are eliminated.
摘要翻译：原位双真空去磁（DVD）复合修复系统设计用于在轮廓结构上生产部分或完全固化的高压釜质量热粘合复合材料修复。该系统提供真空压力，用于使用能够减压（部分固化）的一个装置，然后在复合材料和金属飞机结构上完全固化复合材料修复的平面和轮廓结构上进行热粘合修复。使用原位DVD还可以消除从飞机上的DVD室转移到飞机上的维修部位时的贴片/粘合剂的处理。这可以增加成功维修的可能性，因为消除了粘合剂和修补补片污染和不对准的可能性。

93. 发明授权

US08936695B2 Method for forming and applying composite layups having complex geometries 有权
标题翻译：用于形成和应用具有复杂几何形状的复合叠层的方法
公开(公告)号：US08936695B2
公开(公告)日：2015-01-20
申请号：US12768007
申请日：2010-04-27
申请人： Daniel M. Rotter , Kurtis S. Willden , William S. Hollensteiner , Brian G. Robins
发明人： Daniel M. Rotter , Kurtis S. Willden , William S. Hollensteiner , Brian G. Robins
IPC分类号： B32B37/10 , B29C70/38 , B29C70/44 , B29C70/54 , B29C73/12 , B29C73/32 , B29C37/00 , B29L31/30
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
摘要： A composite layup is formed on a tool and placed on a contoured part. The tool is contoured to substantially match the contour of the part. A set of location data is generated which represents the location of the part in space relative to the tool. An automated manipulator uses the location data to move the tool into proximity to the part and place the contoured layup on the part.
摘要翻译：复合叠层形成在工具上并放置在轮廓部分上。该工具的轮廓是基本匹配零件的轮廓。生成一组位置数据，表示零件相对于工具的空间位置。自动操纵器使用位置数据将工具移动到零件的附近，并将轮廓叠加放置在零件上。

94. 发明申请

US20110232829A1 METHOD AND A DEVICE FOR REPAIRING PARTS OF COMPOSITE MATERIAL OF AN AIRCRAFT 有权
标题翻译：用于修理飞机复合材料部件的方法和装置
公开(公告)号：US20110232829A1
公开(公告)日：2011-09-29
申请号：US13073719
申请日：2011-03-28
申请人： Pierluigi CACACE , Nicola GALLO
发明人： Pierluigi CACACE , Nicola GALLO
IPC分类号： B29C73/00
CPC分类号： B29C73/12 , B29C73/10 , B29C73/32 , B29L2031/3076
摘要： In order to repair a composite-material panel forming part of the external surface of an aircraft, a portable device is applied onto that surface, the portable device including an inflatable chamber consisting of a flexible and airtight membrane and a concave body of rubber-like material sealed with the membrane. The concave body incorporates an inextensible inner reinforcement. Pressurized air is introduced into the chamber via a valve. A further valve, which passes through the membrane in a zone of the membrane external to the chamber, is used to suck air from one side of the membrane to the other.
摘要翻译：为了修复形成飞行器外表面的一部分的复合材料面板，便携式装置被施加到该表面上，便携式装置包括由柔性和气密膜组成的可充气室和橡胶状凹入体材料用膜密封。凹形体包含不可伸展的内部加强件。加压空气通过阀被引入腔室。用于在膜的外部区域中通过膜的另一个阀将空气从膜的一侧吸入另一侧。

95. 发明申请

US20080226818A1 Method for Through Repair of a Composite Structure Comprising Three Skins and Two Core Layers 审中-公开
标题翻译：包括三个皮肤和两个核心层的复合结构的修复方法
公开(公告)号：US20080226818A1
公开(公告)日：2008-09-18
申请号：US12066668
申请日：2006-09-27
申请人： Christophe Bernus , Jean-Claude Marty , Jacques Fournie
发明人： Christophe Bernus , Jean-Claude Marty , Jacques Fournie
IPC分类号： B32B43/00
CPC分类号： B32B43/00 , B29C73/04 , B29C73/32 , B29C2073/268 , B29L2031/3076 , B29L2031/3456 , B29L2031/608 , B32B2305/024
摘要： A method for through-repair of a composite material structure. Repair portions, established through two core layers, for example as a honeycomb and three polymer skins, including two external skins and a middle skin inserted between the core layers to obtain a composite structure, are set up and the polymer is hardened in vacuum. A counter-form is pressed onto one of the skins to guarantee a good aspect and surface quality. Vents are provided through the middle skin and possibly through the skin receiving the counter-form for proper degassing of the underlying cellular core.
摘要翻译：一种复合材料结构的通过修复的方法。通过两个核心层建立的例如蜂巢和三个聚合物表皮的修复部分，其中包括两个外表皮和插入在芯层之间的中间皮肤以获得复合结构，聚合物在真空中硬化。将一种反面形式压在其中一个表皮上，以保证良好的表面和表面质量。排气口通过中间皮肤提供，并且可能通过接收对抗形式的皮肤，以便底层细胞芯的正确脱气。

96. 发明申请

US20070196635A1 Method for the fabrication of a former for manufacture of composite articles and manufacture and repair of composite articles using said former 审中-公开
标题翻译：用于制造复合制品的前者的制造方法，以及使用所述前者制造和修复复合制品的方法
公开(公告)号：US20070196635A1
公开(公告)日：2007-08-23
申请号：US11790001
申请日：2007-04-23
申请人： Max Krogager , Bjorn Weidmann , Mikael Petersson
发明人： Max Krogager , Bjorn Weidmann , Mikael Petersson
IPC分类号： D04H3/00
CPC分类号： B29C73/04 , B29C33/448 , B29C70/44 , B29C73/26 , B29C73/32 , Y10T428/249924 , Y10T442/20
摘要： The present invention relates to a method for the fabrication of a former for manufacture of composite articles. The method is characterized by the following steps: forming a wetted water-soluble fiber composite on a master tool such that the fiber composite material lies against a surface area of the master tool, allowing the water-soluble fiber composite to dry on the master tool and removing the dry water-soluble fiber composite from the master tool, wherein the dry fiber composite forms the walls of the thus fabricated former. The invention also relates to the manufacture and repair of articles using said former
摘要翻译：本发明涉及制造复合制品用前体的方法。该方法的特征在于以下步骤：在主工具上形成润湿的水溶性纤维复合材料，使得纤维复合材料位于主工具的表面区域上，使水溶性纤维复合材料在主工具上干燥并从主工具中除去干水溶性纤维复合材料，其中干纤维复合材料形成如此制造的前者的壁。本发明还涉及使用所述前者制造和修理制品

97. 发明申请

US20060137823A1 Portable curing system for use with vacuum bag repairs and the like 审中-公开
标题翻译：便携式固化系统，用于真空袋修理等
公开(公告)号：US20060137823A1
公开(公告)日：2006-06-29
申请号：US11249818
申请日：2005-10-13
申请人： Brad Bivens
发明人： Brad Bivens
IPC分类号： G05G15/00
CPC分类号： B29C73/32 , B29C73/10 , B29C73/12 , B29C73/34
摘要： A portable curing system includes a carrying case, a controller located within the carrying case and having a microprocessor, a vacuum pump located within the case and having at least two vacuum ports for connection of vacuum lines, at least two vacuum sensor connectors for receiving leads of vacuum sensors, at least two heater connectors for receiving leads of electrical heaters, and at least two temperature sensor connectors for receiving leads of thermocouples. A display is provided to display information from the controller. A PC port is provided to download data to the controller and to upload data from the controller. A voltage input is operably connected the heater connectors and a voltage detection circuit is operably connected to the voltage input and the heater connectors to prevent providing voltage to the heater connectors when voltage supplied to the voltage input is above a predetermined voltage level.
摘要翻译：便携式固化系统包括便携箱，位于携带箱内并具有微处理器的控制器，位于壳体内的真空泵，具有用于连接真空管线的至少两个真空端口，用于接收引线的至少两个真空传感器连接器的真空传感器，用于接收电加热器引线的至少两个加热器连接器和用于接收热电偶引线的至少两个温度传感器连接器。提供显示器来显示来自控制器的信息。提供PC端口将数据下载到控制器并从控制器上传数据。电压输入可操作地连接加热器连接器，并且电压检测电路可操作地连接到电压输入和加热器连接器，以防止在提供给电压输入的电压高于预定电压电平时向加热器连接器提供电压。

98. 发明申请

US20050191919A1 Method for the fabrication of a former for manufacture of composite articles and manufacture and repair of composite articles using said former 审中-公开
标题翻译：用于制造复合制品的前者的制造方法，以及使用所述前者制造和修复复合制品的方法
公开(公告)号：US20050191919A1
公开(公告)日：2005-09-01
申请号：US11053911
申请日：2005-02-10
申请人： Max Krogager , Bjorn Weidmann , Mikael Petersson
发明人： Max Krogager , Bjorn Weidmann , Mikael Petersson
IPC分类号： B29C33/44 , B29C70/44 , B29C70/30
CPC分类号： B29C73/04 , B29C33/448 , B29C70/44 , B29C73/26 , B29C73/32 , Y10T428/249924 , Y10T442/20
摘要： The present invention relates to a method for the fabrication of a former for manufacture of composite articles. The method is characterized by the following steps: forming a wetted water-soluble fiber composite on a master tool such that the fiber composite material lies against a surface area of the master tool, allowing the water-soluble fiber composite to dry on the master tool and removing the dry water-soluble fiber composite from the master tool, wherein the dry fiber composite forms the walls of the thus fabricated former. The invention also relates to the manufacture and repair of articles using said former
摘要翻译：本发明涉及制造复合制品用前体的方法。该方法的特征在于以下步骤：在主工具上形成润湿的水溶性纤维复合材料，使得纤维复合材料位于主工具的表面区域上，使水溶性纤维复合材料在主工具上干燥并从主工具中除去干水溶性纤维复合材料，其中干纤维复合材料形成如此制造的前者的壁。本发明还涉及使用所述前者制造和修理制品

99. 发明授权

US06468372B2 On-site tooling and method for repairing a damaged zone in a composite structure 有权
标题翻译：现场加工和修复复合结构受损区域的方法
公开(公告)号：US06468372B2
公开(公告)日：2002-10-22
申请号：US09780403
申请日：2001-02-12
申请人： Fabienne Kociemba , Daniel Soro
发明人： Fabienne Kociemba , Daniel Soro
IPC分类号： B32B3100
CPC分类号： B29C43/3642 , B29C73/10 , B29C73/32 , B29L2031/3082 , B64F5/40
摘要： The present invention relates to on-site repairs of a composite structure (10) such as an aircraft structure in which a concave recess (14) is machined in the damaged zone, a non-polymerized composite part (16) is set into said recess and part (16) is polymerized under pressure using tooling (18) comprising a stack of plates (32) that increase the pressure applied to the composite part. The present invention thus obtains invisible repairs with mechanical characteristics that are similar to those of the initial structure.
摘要翻译：本发明涉及复合结构（10）的现场修理，例如飞机结构，其中在损坏区域中加工凹形凹部（14），未聚合的复合部件（16）被设置在所述凹部并且部分（16）在加压下使用包括增加施加到复合部件的压力的板（32）的堆叠（18）进行聚合。因此，本发明获得与初始结构类似的机械特性的不可见修复。

100. 发明申请

US20010008161A1 On-site tooling and method for repairing a damaged zone in a composite structure 有权
标题翻译：现场加工和修复复合结构受损区域的方法
公开(公告)号：US20010008161A1
公开(公告)日：2001-07-19
申请号：US09780403
申请日：2001-02-12
发明人： Fabienne Kociemba , Daniel Soro
IPC分类号： B32B035/00 , B32B001/00
CPC分类号： B29C43/3642 , B29C73/10 , B29C73/32 , B29L2031/3082 , B64F5/40
摘要： The present invention relates to on-site repairs of a composite structure (10) such as an aircraft structure in which a concave recess (14) is machined in the damaged zone, a non-polymerized composite part (16) is set into said recess and part (16) is polymerized under pressure using tooling (18) comprising a stack of plates (32) that increase the pressure applied to the composite part. The present invention thus obtains invisible repairs with mechanical characteristics that are similar to those of the initial structure.
摘要翻译：本发明涉及复合结构（10）的现场修理，例如飞机结构，其中在损坏区域中加工凹形凹部（14），未聚合的复合部件（16）被设置在所述凹部并且部分（16）在加压下使用包括增加施加到复合部件的压力的板（32）的堆叠（18）进行聚合。因此，本发明获得与初始结构类似的机械特性的不可见修复。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式