公开(公告)号：US20160046183A1

公开(公告)日：2016-02-18

申请号：US14782120

申请日：2014-04-03

Applicant: PLASTIC OMNIUM ADVANCED INNOVATION AND RESEARCH

Inventor： David HILL ,  Philippe BOURNONVILLE ,  Bjorn CRIEL

IPC: B60K15/035 ,  B60K15/03 ,  B29C65/00 ,  B29C49/48 ,  B29C49/42

CPC classification number: B60K15/035 ,  B29C49/04 ,  B29C49/20 ,  B29C49/4273 ,  B29C49/4802 ,  B29C66/05 ,  B29C66/342 ,  B29C66/532 ,  B29C2049/2008 ,  B29C2049/2047 ,  B29K2105/253 ,  B29L2031/30 ,  B29L2031/7172 ,  B60K15/03177 ,  B60K15/04 ,  B60K2015/03032 ,  B60K2015/0346 ,  B60K2015/047 ,  B60K2015/0477

Abstract: A component is made for a vehicle plastic hollow article, such as a fuel tank, wherein the article includes a wall obtained from a plastic parison. The component is configured to be welded to the wall and includes a main hollow body including an external face, a shoulder protruding from the external face, and at least one recess configured to receive air when the shoulder contacts the wall during welding of the component.

Abstract translation: 制造用于车辆塑料中空制品（例如燃料箱）的部件，其中制品包括从塑料型坯获得的壁。 该部件被构造成焊接到壁上并且包括主空心体，其包括外表面，从外表面突出的肩部，以及至少一个凹部，其构造成在焊接部件期间肩部与壁接触时接纳空气。

公开(公告)号：US20150183181A1

公开(公告)日：2015-07-02

申请号：US14644348

申请日：2015-03-11

Applicant: The Boeing Company

Inventor： Charles R. Saff ,  John H. Fogarty ,  Haozhang Gu ,  Terry D. Richardson ,  Kevin M. Retz

IPC: B32B3/18 ,  B32B3/04 ,  B32B3/14 ,  B32B3/06 ,  B32B3/12

CPC classification number: B32B3/18 ,  B23B3/04 ,  B29C65/00 ,  B29C66/01 ,  B29C66/05 ,  B29C66/10 ,  B29C66/11 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/114 ,  B29C66/1142 ,  B29C66/118 ,  B29C66/1182 ,  B29C66/122 ,  B29C66/128 ,  B32B3/04 ,  B32B3/06 ,  B32B3/12 ,  B32B3/14 ,  B32B2250/03 ,  B32B2307/718 ,  B32B2605/18 ,  Y10T29/49622 ,  Y10T29/49982 ,  Y10T156/10 ,  Y10T156/1002 ,  Y10T156/1034 ,  Y10T156/1093 ,  Y10T428/239 ,  Y10T428/24174 ,  Y10T428/24752 ,  Y10T428/24777 ,  Y10T428/249923

Abstract: A composite sandwich structure comprises a core sandwiched between composite laminate facesheets. The core includes a plurality of core sections spliced together at joints that incorporate integral features for arresting the propagation of irregularities in the facesheets.

Abstract translation: 复合夹层结构包括夹在复合层压板之间的芯。 芯包括在接头处拼接在一起的多个芯部分，其包含用于阻止面板中的凹凸的传播的整体特征。

公开(公告)号：US08955290B2

公开(公告)日：2015-02-17

申请号：US13716593

申请日：2012-12-17

Applicant: The Boeing Company

Inventor： Charles R. Saff ,  John H. Fogarty ,  Haozhong Gu ,  Terry D. Richardson ,  Kevin M. Retz

IPC: E04C2/54 ,  E04C2/34 ,  E04C2/36 ,  E04B1/74 ,  E04C3/00 ,  B32B3/18 ,  B32B3/06 ,  B32B3/12

CPC classification number: B32B3/18 ,  B23B3/04 ,  B29C65/00 ,  B29C66/01 ,  B29C66/05 ,  B29C66/10 ,  B29C66/11 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/114 ,  B29C66/1142 ,  B29C66/118 ,  B29C66/1182 ,  B29C66/122 ,  B29C66/128 ,  B32B3/04 ,  B32B3/06 ,  B32B3/12 ,  B32B3/14 ,  B32B2250/03 ,  B32B2307/718 ,  B32B2605/18 ,  Y10T29/49622 ,  Y10T29/49982 ,  Y10T156/10 ,  Y10T156/1002 ,  Y10T156/1034 ,  Y10T156/1093 ,  Y10T428/239 ,  Y10T428/24174 ,  Y10T428/24752 ,  Y10T428/24777 ,  Y10T428/249923

Abstract: A composite sandwich structure comprises a core sandwiched between composite laminate facesheets. The core includes a plurality of core sections spliced together at joints that incorporate integral features for arresting the propagation of irregularities in the facesheets.

公开(公告)号：US20130295369A1

公开(公告)日：2013-11-07

申请号：US13916036

申请日：2013-06-12

Applicant: Max-Planck-Gesellschaft zur Forderung der Wissenschaften e.V. ,  Fraunhofer-Gesellschaft zur Forderung der angewandten Forschung e.V.

Inventor： Ralf WEHRSPOHN ,  Martin STEINHART

IPC: C03C23/00

CPC classification number: C03C23/0095 ,  B29C65/64 ,  B29C66/05 ,  B29C66/30326 ,  B29C66/341 ,  B29C66/71 ,  B29C66/712 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/742 ,  B29C66/7461 ,  B29C66/7465 ,  B29C66/91411 ,  B29C66/919 ,  B29C66/91921 ,  B29C66/91933 ,  B29K2023/06 ,  B29K2025/00 ,  B29K2027/18 ,  B29K2033/08 ,  B29K2067/00 ,  B29K2069/00 ,  B29K2071/00 ,  B29K2083/00 ,  B29K2105/045 ,  B29K2305/10 ,  B29K2305/12 ,  B29K2305/14 ,  B29K2309/04 ,  B29K2309/08 ,  B29L2031/3406 ,  B29L2031/756 ,  Y10T428/249921 ,  Y10T428/249978 ,  B29K2081/06 ,  B29K2081/00 ,  B29K2079/08 ,  B29K2077/00 ,  B29K2075/00 ,  B29K2067/006 ,  B29K2067/003 ,  B29K2065/00 ,  B29K2033/26 ,  B29K2025/06 ,  B29K2023/38 ,  B29K2023/083 ,  B29K2023/00 ,  B29K2011/00 ,  B29K2009/00

Abstract: A three-dimensional molded body, a method for producing a three-dimensional molded body and a method for producing an adhesive bond between a polymer-containing material and a molded body having an inorganic porous framework structure in at least partial areas are described. In all cases the porous structure of the molded body comprising inorganic material is brought in contact with a polymer-containing material which is heated until the heated material enters into a joint connection with the molded body based on adhesive interactions, interfacial interactions, electrostatic interactions or any combination thereof, in which the pore-like voids of the porous structure are filled completely with the polymer-containing material, which stabilizes the molded body so that it has dimensional stability after cooling.

Abstract translation: 描述了三维成型体，三维成型体的制造方法以及含有聚合物的材料与至少部分区域中具有无机多孔骨架结构的成型体之间的粘结剂的制造方法。 在所有情况下，包含无机材料的成型体的多孔结构与含聚合物的材料接触，所述材料被加热直到加热的材料基于粘合剂相互作用，界面相互作用，静电相互作用或与其成为接合连接 其中多孔结构的孔状空隙完全被含聚合物的材料填充的任何组合，这使得成型体稳定，使得其在冷却后具有尺寸稳定性。

公开(公告)号：US20080210824A1

公开(公告)日：2008-09-04

申请号：US11974246

申请日：2007-10-12

Applicant: Ulrich Eberth

Inventor： Ulrich Eberth

IPC: B64C1/06

CPC classification number: B64C1/12 ,  B29C65/02 ,  B29C65/4815 ,  B29C65/486 ,  B29C66/05 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/532 ,  B29C66/61 ,  B29C66/7212 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/81422 ,  B29C70/24 ,  B29C70/543 ,  B29K2995/0089 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/3085 ,  B64F5/10 ,  Y02T50/43 ,  B29K2307/04

Abstract: The present invention relates to a connecting structure for an aircraft or spacecraft, with a structural component and a stringer. The stringer is connected to the structural component by means of connecting regions. In order to reduce stress peaks that result for example from impact in the structural component, a high impact material is introduced into at least one of the connecting regions to provide a local increase in the energy absorbing capacity of the at least one connecting region.

Abstract translation: 本发明涉及一种具有结构部件和纵梁的飞机或航天器的连接结构。 桁条通过连接区连接到结构部件。 为了减少例如由于结构部件的冲击引起的应力峰值，将高冲击材料引入至少一个连接区域中，以提供至少一个连接区域的能量吸收能力的局部增加。

公开(公告)号：US06802919B2

公开(公告)日：2004-10-12

申请号：US10135494

申请日：2002-04-30

Applicant: Samuel M. Massey ,  Richard Phillips ,  Victor J. Jodts, Jr. ,  Thomas A. Lord

Inventor： Samuel M. Massey ,  Richard Phillips ,  Victor J. Jodts, Jr. ,  Thomas A. Lord

IPC: B65B728

CPC classification number: B65D77/2032 ,  B29C65/18 ,  B29C66/05 ,  B29C66/112 ,  B29C66/131 ,  B29C66/24221 ,  B29C66/30223 ,  B29C66/53461 ,  B29C66/71 ,  B29C66/723 ,  B29C66/72321 ,  B29C66/72328 ,  B29C66/72343 ,  B29C66/7373 ,  B29C66/8322 ,  B29L2009/00 ,  B65D2577/2041 ,  B29K2023/06 ,  B29K2023/065 ,  B29K2023/12

Abstract: A method for sealing a container comprising a cup and lid is disclosed. The cup has a lip with a raised sealing bead along its length. During sealing, the raised sealing bead compresses, thereby stretching the adhesive layer on the lower portion of the lid out of the way and forming a direct welded seal with the heat-resistant layer of the lid. The adhesive to either side of the sealing bead forms an adhesive seal between the lid and the remaining portion of the lip. This type of double seal is particularly effective in forming a durable, consistent seal when product is present on the lip of the container. The welded seal is also well suited to situations when the cup may be warped or the sealing bead is otherwise caused to be higher along some portion of its length than along other portions.

Abstract translation: 公开了一种用于密封包括杯和盖的容器的方法。 杯子具有沿其长度具有凸起的密封珠的唇缘。 在密封期间，凸起的密封珠被压缩，从而拉伸盖的下部的粘合剂层，并与盖的耐热层形成直接的焊接密封。 密封珠的任一侧的粘合剂形成在盖和唇部的剩余部分之间的粘合密封。 当产品存在于容器的唇缘上时，这种双重密封件特别有效地形成耐用且一致的密封。 焊接的密封件也非常适合于杯子翘曲的情况，或者密封珠沿着其长度的某些部分比沿着其它部分更高。

公开(公告)号：US6068718A

公开(公告)日：2000-05-30

申请号：US95168

申请日：1998-06-10

Applicant: James Medal

Inventor： James Medal

IPC: B29C65/00 ,  B29C65/08 ,  B29C65/56 ,  B29C65/64 ,  B65D23/10 ,  F16B4/00 ,  F16B37/04 ,  F16B37/12 ,  H05K7/14 ,  B32B31/16

CPC classification number: H05K7/142 ,  B29C65/08 ,  B29C65/56 ,  B29C65/562 ,  B29C65/565 ,  B29C66/05 ,  B29C66/30221 ,  B29C66/30223 ,  B29C66/474 ,  B29C66/532 ,  B29C66/53245 ,  B29C66/73921 ,  B65D23/104 ,  B65D23/106 ,  F16B37/048 ,  F16B37/122 ,  F16B4/004 ,  B29C66/534 ,  B29C66/5344 ,  B29C66/71 ,  B29C66/8322 ,  B29L2031/463 ,  B29L2031/7158 ,  B29L2031/737

Abstract: A hollow container is formed with a thin-walled, plastic body; and a discrete plastic handle is attached by ultrasonic energy to the plastic body. The handle has a pair of spaced bosses at each end of the handle with a central opening therein to receive an ultrasonic horn. A plurality of integral, energy-directing protrusions are spaced from one another on the bosses to be melted and mixed with the plastic of the container. The energy directors melt first and mix with the plastic of thin-walled bottle to provide a secure attachment. The preferred container and preferred handle are each made of PET plastic.

Abstract translation: 中空容器形成有薄壁的塑料体; 并且通过超声能量将分立的塑料手柄附接到塑料体。 手柄在手柄的每个端部处具有一对间隔开的凸起，其中的中心开口用于接收超声波喇叭。 多个整体的能量引导突起在凸台上彼此间隔开以熔化并与容器的塑料混合。 能量指挥首先熔化，并与薄壁瓶的塑料混合，以提供牢固的附件。 优选的容器和优选的手柄均由PET塑料制成。

公开(公告)号：US20170015053A1

公开(公告)日：2017-01-19

申请号：US15121198

申请日：2015-07-08

Applicant: GUNYANG ITT CO., LTD.

Inventor： Teak-Hyun KIM

IPC: B29C65/60 ,  B29C65/00 ,  B29C65/04

CPC classification number: B29C65/607 ,  B29C65/04 ,  B29C65/1412 ,  B29C65/72 ,  B29C66/0342 ,  B29C66/05 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/135 ,  B29C66/21 ,  B29C66/3494 ,  B29C66/41 ,  B29C66/5326 ,  B29C66/73115 ,  B29C66/73921 ,  B29C66/80 ,  B29C66/81423 ,  B29C66/81429 ,  B29C66/8181 ,  B29C66/8322 ,  B29C66/8324 ,  B29C66/91421 ,  B29C66/919 ,  B29K2701/12 ,  B29L2031/3014

Abstract: The objective of the present invention is to provide a vehicle door trim bonding device capable of quickly bonding sub-trims. In order to achieve the objective, the present invention provides a vehicle door trim bonding device for coupling a first sub-trim in which a projection is formed and which is made of a thermoplastic resin material, and a second sub-trim in which a receiving hole for receiving the projection of the first sub-trim is formed and which is made of a thermoplastic resin material, the device comprising: a heat supply unit for melting a part of the protrusion with radiation heat; and a molding part for compression-molding the molten protrusion.

Abstract translation: 本发明的目的是提供一种能够快速粘合子修剪的车门装饰接合装置。 为了达到上述目的，本发明提供一种车辆用门装饰接合装置，其用于联接形成突起的第一副装饰件，其由热塑性树脂材料制成，其中第二副装饰件 形成用于接收第一副装饰件的突起的孔，其由热塑性树脂材料制成，该装置包括：用辐射热熔化突起的一部分的供热单元; 以及用于压缩熔融突起的模制部件。

公开(公告)号：US07997534B2

公开(公告)日：2011-08-16

申请号：US11974246

申请日：2007-10-12

Applicant: Ulrich Eberth

Inventor： Ulrich Eberth

IPC: B64C1/06

CPC classification number: B64C1/12 ,  B29C65/02 ,  B29C65/4815 ,  B29C65/486 ,  B29C66/05 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/532 ,  B29C66/61 ,  B29C66/7212 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/81422 ,  B29C70/24 ,  B29C70/543 ,  B29K2995/0089 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/3085 ,  B64F5/10 ,  Y02T50/43 ,  B29K2307/04

Abstract: The present invention relates to a connecting structure for an aircraft or spacecraft, with a structural component and a stringer. The stringer is connected to the structural component by means of connecting regions. In order to reduce stress peaks that result for example from impact in the structural component, a high impact material is introduced into at least one of the connecting regions to provide a local increase in the energy absorbing capacity of the at least one connecting region.

Abstract translation: 本发明涉及一种具有结构部件和纵梁的飞机或航天器的连接结构。 桁条通过连接区连接到结构部件。 为了减少例如由于结构部件的冲击引起的应力峰值，将高冲击材料引入至少一个连接区域中，以提供至少一个连接区域的能量吸收能力的局部增加。

公开(公告)号：US20070041205A1

公开(公告)日：2007-02-22

申请号：US11505723

申请日：2006-08-17

Applicant: Volker Teichmann

Inventor： Volker Teichmann

IPC: F21V5/00

CPC classification number: F21S41/29 ,  B29C65/02 ,  B29C65/06 ,  B29C65/08 ,  B29C65/16 ,  B29C65/18 ,  B29C65/20 ,  B29C66/05 ,  B29C66/54 ,  B29L2031/747 ,  F21S41/28 ,  F21V3/04 ,  F21V15/015 ,  F21V17/101

Abstract: A component assembly includes a first part having a transparent section. The first part defines an outer surface. A second part is fixedly secured to the first part at a portion of the transparent section. The first and second parts create a connecting seam through the portion of the transparent section. An optically covering surface extends between the connecting seam and the outer surface of the first part to cover the connecting seam from view from the outer surface.

Abstract translation: 部件组件包括具有透明部分的第一部分。 第一部分定义了外表面。 第二部分在透明部分的一部分处牢固地固定到第一部分。 第一和第二部分通过透明部分的部分形成连接缝。 光学覆盖表面在连接接缝和第一部分的外表面之间延伸，以从外表面的角度覆盖连接接缝。