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41. 发明授权

US08992709B2 Sandwich structure having arrestment feature and method of making the same 有权
标题翻译：具有逮捕特征的三明治结构及其制作方法
公开(公告)号：US08992709B2
公开(公告)日：2015-03-31
申请号：US12631029
申请日：2009-12-04
申请人： Charles R. Saff , John H. Fogarty , Haozhong Gu , Terry D. Richardson , Kevin M Retz
发明人： Charles R. Saff , John H. Fogarty , Haozhong Gu , Terry D. Richardson , Kevin M Retz
IPC分类号： B32B3/04 , B29C65/00 , B31B1/60 , B32B37/00 , B31F5/00 , B65H19/00 , B65H69/02 , G03D15/04 , C09J5/02 , B32B3/18 , B32B3/06 , B32B3/12
CPC分类号： 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
摘要： 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.
摘要翻译：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。

42. 发明授权

US08413762B1 Thermal-acoustic sections for an aircraft 有权
公开(公告)号：US08413762B1
公开(公告)日：2013-04-09
申请号：US13314954
申请日：2011-12-08
申请人： Tongan Wang , John Willett Maxon, Jr. , Andrew Foose , David Charles Hornick , Josef Fila
发明人： Tongan Wang , John Willett Maxon, Jr. , Andrew Foose , David Charles Hornick , Josef Fila
IPC分类号： E04B1/82 , E04B1/84 , H02N2/00 , B32B3/12
CPC分类号： B64C1/40 , B29C65/00 , B29C66/11 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29K2105/04 , B32B3/12 , B32B5/26 , B32B5/32 , B32B7/02 , B32B2250/02 , B32B2250/03 , B32B2250/04 , B32B2250/05 , B32B2250/20 , B32B2250/22 , B32B2266/0257 , B32B2266/0285 , B32B2266/06 , B32B2307/102 , B32B2307/718 , B32B2605/18 , B64C1/00 , E04B1/82 , E04B1/84 , G10K11/00 , G10K11/02 , Y02T50/46 , Y10T428/24149
摘要： Embodiments of thermal-acoustic sections for an aircraft for reducing noise along an acoustic path produced from an acoustic source are provided herein. The thermal-acoustic section comprises a first porous layer having a first characteristic acoustic impedance. A second porous layer is disposed adjacent to the first porous layer and has a second characteristic acoustic impedance that is greater than the first characteristic acoustic impedance. The thermal-acoustic section is configured to be positioned along the acoustic path such that at least a portion of the noise from the acoustic source is directed through the first porous layer to the second porous layer to promote absorption of the noise.

43. 发明申请

US20120193016A1 Sandwich Structure Having Arrestment Feature and Method of Making the Same 审中-公开
标题翻译：具有逮捕特征的三明治结构及其制作方法
公开(公告)号：US20120193016A1
公开(公告)日：2012-08-02
申请号：US13431706
申请日：2012-03-27
申请人： Charles R. Saff , John H. Fogarty , Haozhong Gu , Terry D. Richardson , Kevin M. Retz
发明人： Charles R. Saff , John H. Fogarty , Haozhong Gu , Terry D. Richardson , Kevin M. Retz
IPC分类号： B32B37/02 , B32B37/12
CPC分类号： 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
摘要： 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.
摘要翻译：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。

44. 发明公开

EP3307518A1 THERMOPLASTISCHER REIBVERBINDER 审中-公开
标题翻译：热塑性磨削连接器
公开(公告)号：EP3307518A1
公开(公告)日：2018-04-18
申请号：EP16738366.0
申请日：2016-06-15
申请人： EJOT GmbH & Co. KG
发明人： BECKER, Mirko , LORENZ, Steffen , KRAUSSER, Ingo
IPC分类号： B29C65/06 , B29C65/60 , F16B37/06 , B29K101/12
CPC分类号： B29C65/06 , B29C65/0672 , B29C65/069 , B29C65/56 , B29C65/602 , B29C65/607 , B29C66/11 , B29C66/1122 , B29C66/21 , B29C66/41 , B29C66/474 , B29C66/49 , B29C66/53 , B29C66/7392 , B29C66/81429 , B29C66/81431 , B29C66/83221 , B29L2031/7288 , F16B5/04 , F16B37/065
摘要： The invention relates to a method for producing a component bond (70, 140) comprising: a fastening structure (60, 160) that has at least one component layer (60A, 60a;160a, 160b); and a thermoplastic connecting element (10, 110) having a head (12, 112) and a shank (14, 114), in which method the connecting element (10, 110) is driven into the fastening structure (60, 160) under pressure whilst rotating, such that the shank (14, 114) penetrates the fastening structure (60, 160). The connecting element (10, 110), after penetrating the fastening structure (60, 160), is converted by friction into a softened, free-flowing state in a die (44, 144) which is placed against the fastening structure (60, 160) in the opposite direction to the driving direction, resulting in a thicker section (22, 22) that extends beyond the radial extent of some sections of the shank (14, 114). The fastening structure (60, 160) is thus interlockingly held between the head (12, 112) and the thicker section (22, 122).

45. 发明公开

EP3159256A1 IMPROVED THERMAL-ACOUSTIC SECTIONS FOR AN AIRCRAFT 有权
标题翻译：改进了飞机的热声部分
公开(公告)号：EP3159256A1
公开(公告)日：2017-04-26
申请号：EP16189056.1
申请日：2012-12-06
申请人： Gulfstream Aerospace Corporation
发明人： Wang, Tongan , Maxon, John Willet , Foose, Andrew , Hornick, David C. , Fila, Josef
IPC分类号： B64C1/40 , G10K11/02
CPC分类号： B64C1/40 , B29C65/00 , B29C66/11 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29K2105/04 , B32B3/12 , B32B5/26 , B32B5/32 , B32B7/02 , B32B2250/02 , B32B2250/03 , B32B2250/04 , B32B2250/05 , B32B2250/20 , B32B2250/22 , B32B2266/0257 , B32B2266/0285 , B32B2266/06 , B32B2307/102 , B32B2307/718 , B32B2605/18 , B64C1/00 , E04B1/82 , E04B1/84 , G10K11/00 , G10K11/02 , Y02T50/46 , Y10T428/24149
摘要： Thermal-acoustic section (436) for an aircraft (10) for reducing noise along an acoustic path (22) produced from an acoustic source (16) is provided herein. The thermal-acoustic section (436) comprises a plurality of juxtaposed porous layers (400) forming a thermal-acoustic stack (447) that has a first outermost portion (474), a second outermost portion (476) and a central portion (478). The thermal-acoustic stack has a gradually deecreasing characteristic acoustic impedance from the first outermost portion to the central portion and a gradually increasing characteristic acoustic impedance from the central portion to the second outermost portion, to promote transmission loss of the transmitted portion of the noise through the thermal-acoustic stack.
摘要翻译：本文提供了用于飞机（10）的热声部分（436），用于降低从声源（16）产生的沿着声学路径（22）的噪声。热声部分436包括形成热声叠层447的多个并置的多孔层400，所述热声叠层447具有第一最外部分474，第二最外部分476和中央部分478 ）。热声叠层具有从第一最外部分到中心部分的逐渐减小的特性声阻抗和从中心部分到第二最外部分逐渐增加的特性声阻抗，以促进透过的噪声部分热声叠层。

46. 发明授权

EP2788557B1 IMPROVED THERMAL-ACOUSTIC SECTIONS FOR AN AIRCRAFT 有权
标题翻译：改善的热声段，成为平面
公开(公告)号：EP2788557B1
公开(公告)日：2016-09-21
申请号：EP12855026.6
申请日：2012-12-06
申请人： Gulfstream Aerospace Corporation
发明人： WANG, Tongan , MAXON, John, Willett , FOOSE, Andrew , HORNICK, David, Charles , FILA, Josef
IPC分类号： B64C1/40 , G10K11/02
CPC分类号： B64C1/40 , B29C65/00 , B29C66/11 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29K2105/04 , B32B3/12 , B32B5/26 , B32B5/32 , B32B7/02 , B32B2250/02 , B32B2250/03 , B32B2250/04 , B32B2250/05 , B32B2250/20 , B32B2250/22 , B32B2266/0257 , B32B2266/0285 , B32B2266/06 , B32B2307/102 , B32B2307/718 , B32B2605/18 , B64C1/00 , E04B1/82 , E04B1/84 , G10K11/00 , G10K11/02 , Y02T50/46 , Y10T428/24149

47. 发明公开

EP2788557A4 IMPROVED THERMAL-ACOUSTIC SECTIONS FOR AN AIRCRAFT 有权
标题翻译：改善的热声段，成为平面
公开(公告)号：EP2788557A4
公开(公告)日：2015-08-12
申请号：EP12855026
申请日：2012-12-06
申请人： GULFSTREAM AEROSPACE CORP
发明人： WANG TONGAN , MAXON JOHN WILLETT , FOOSE ANDREW , HORNICK DAVID CHARLES , FILA JOSEF
IPC分类号： B64C1/40 , G10K11/02
CPC分类号： B64C1/40 , B29C65/00 , B29C66/11 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29K2105/04 , B32B3/12 , B32B5/26 , B32B5/32 , B32B7/02 , B32B2250/02 , B32B2250/03 , B32B2250/04 , B32B2250/05 , B32B2250/20 , B32B2250/22 , B32B2266/0257 , B32B2266/0285 , B32B2266/06 , B32B2307/102 , B32B2307/718 , B32B2605/18 , B64C1/00 , E04B1/82 , E04B1/84 , G10K11/00 , G10K11/02 , Y02T50/46 , Y10T428/24149

48. 发明公开

KR1020140101132A 벨트 단부의 부분 박피장치 有权
标题翻译：皮带端部分条
公开(公告)号：KR1020140101132A
公开(公告)日：2014-08-19
申请号：KR1020130014410
申请日：2013-02-08
申请人： 장병천
发明人： 장병천
IPC分类号： B29C65/78 , B29C65/48
CPC分类号： B29C66/02241 , B26D1/125 , B29C66/11 , B29D29/00
摘要： The present invention relates to a portion stripper of belt ends and, more specifically, to a portion stripper of belts ends for automatically peeling one-half of the thickness of a belt for a predetermined length of the end portions using a rotating stripper, and for manufacturing a belt having one closed curve by adhering the peeled ends. The portion stripper of belt ends of the present invention comprises: a stripper (12) which rotates by a motor (11) and peels one half of the thickness of a belt (B) for a predetermined length of the end portions; a main body (13) for providing a space for installing the motor (11) and the stripper (12); and a belt guide path (14) for introducing the belt from the front-outside of the main body (13) to the inner stripper (12) direction.
摘要翻译：本发明涉及带端部的剥离部分，更具体地说，涉及带端部的剥离部分，用于使用旋转剥离器自动剥离预定长度的端部的带的厚度的一半，并且通过粘合剥离端来制造具有一个闭合曲线的带。本发明的带端部的剥离器包括：剥离器（12），其通过马达（11）旋转并且将端部的预定长度的一半皮带（B）的一半剥离; 主体（13），用于提供用于安装电动机（11）和汽提器（12）的空间; 以及用于将带从主体（13）的前侧引导到内剥离器（12）方向的带引导路径（14）。

49. 发明授权

KR101829075B1 억제 형상을 갖춘 샌드위치 구조 및 그 제작 방법 有权
公开(公告)号：KR101829075B1
公开(公告)日：2018-02-13
申请号：KR1020127011336
申请日：2010-10-12
申请人： 더 보잉 컴파니
发明人： 새프,찰스알. , 포가티,존에이치. , 구,하오중 , 리차드손,테리디. , 리츠,케빈엠.
IPC分类号： B32B3/06 , B32B3/12 , B23B3/04 , B29C65/00 , B32B3/04 , B32B3/14 , B32B3/18
CPC分类号： 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
摘要： 복합재샌드위치구조는복합재박형표면시트(composite laminate facesheets) 사이에샌드위치된코어를구비하여구성된다. 코어는표면시트에서불규칙의전파를억제하기위한필수형상을통합하는조인트에서함께접합된다수의코어를포함한다.

50. 发明公开

KR1020170071539A 워크의 붙임 방법 审中-实审
标题翻译：如何附加工作
公开(公告)号：KR1020170071539A
公开(公告)日：2017-06-23
申请号：KR1020177012951
申请日：2015-10-09
申请人： 우시오덴키 가부시키가이샤
发明人： 와사모토마코토 , 다케모토후미토시 , 스즈키신지
IPC分类号： B29C65/00 , B29C65/14 , C03C27/06 , C30B25/18 , H01L21/18
CPC分类号： B29C65/1406 , B29C65/02 , B29C65/7847 , B29C65/8215 , B29C65/8223 , B29C66/0222 , B29C66/0242 , B29C66/026 , B29C66/028 , B29C66/11 , B29C66/1122 , B29C66/45 , B29C66/54 , B29C66/712 , B29C66/7465 , B29L2031/756 , B32B38/0008 , B32B38/164 , B32B2037/0092 , B32B2038/166 , B32B2309/68 , B32B2310/0472 , B32B2310/0831 , B32B2310/14 , B81C3/001 , B81C2201/019 , C08J5/121 , C08J7/00 , G01N2035/00455 , H01L21/48 , B29C65/14 , C03C27/06 , C30B25/186 , H01L21/187
摘要： 높은강도의접합상태를달성할수 있고, 또한, 접합상태에대해양호한재현성이얻어지는워크의붙임방법을제공한다. 본발명의워크의붙임방법은, 각각합성수지, 유리, 실리콘웨이퍼, 수정및 사파이어로이루어지는군으로부터선택되는재료로이루어지는 2개의워크들을붙이는방법으로서, 적어도한쪽의워크의붙임면을활성화하는표면활성화공정과, 2개의워크를각각의붙임면이서로접촉하도록적층하는적층공정을가지며, 상기표면활성화공정을행하기전에, 상기표면활성화공정에제공되는워크의붙임면으로부터수분을이탈시키는전처리공정을행하는것을특징으로한다.
摘要翻译：可以实现的高强度的结合状态，并且还提供安装方法的一个工作是在接合状态下获得良好的再现性。根据本发明的工作的附接方法，该表面活化步骤，每个合成树脂制成，作为一种方法来连接所述两个工件由选自玻璃，硅晶片，修改和蓝宝石组成的组中选择的材料，使至少一个的工件的安装面并且，具有层叠两个工作的每个安装面是在相互接触，用于执行释放前的表面活化处理中的水分，从工作的安装表面的预处理步骤的层叠步骤被提供给表面活化处理和被表征。

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