专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20180316169A1 LEADTHROUGH DEVICE AND BUILDING WITH A LEADTHROUGH DEVICE 审中-公开
公开(公告)号：US20180316169A1
公开(公告)日：2018-11-01
申请号：US15964504
申请日：2018-04-27
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： DIETER HEIDRICH , ACHIM VON SECK , FAIDON SACHSAMANOGLOU , ANTONIOS KOPANOUDIS
IPC分类号： H02G3/22 , H02G3/00
CPC分类号： H02G3/22 , F16F15/06 , F16L5/025 , H02B1/54 , H02G3/263
摘要： A leadthrough device holds a conduit in a wall opening of a wall, in particular building wall; and guides the conduit through the wall. The leadthrough device has a holding element with a passage hole, through which the conduit can be led, and has an outer frame. The holding element is resiliently held in the frame interior by at least one spring device.

2. 发明申请

US20180259095A1 LINE FEEDTHROUGH FOR FEEDING LINES THROUGH A COMPONENT 审中-公开
公开(公告)号：US20180259095A1
公开(公告)日：2018-09-13
申请号：US15761937
申请日：2016-09-27
申请人： HILTI AKTIENGESELLSCHAFT
发明人： Wolfgang SCHULZ-HANKE
IPC分类号： F16L5/02 , F16L5/04 , H02G3/22 , H02G3/08
CPC分类号： F16L5/025 , F16L5/04 , H02G3/083 , H02G3/22
摘要： A line penetration for routing a line through a building part, which has a closure plate for covering a passage opening in the building part and a fastening arrangement. The closure plate has at least one line opening for receiving the line. The fastening arrangement can be fastened to the building part, for holding the closure plate, so that a relative displacement of the closure plate along a surface direction of the closure plate is permitted and the closure plate is fixed perpendicular to the surface direction of the closure plate.

3. 发明申请

US20180251973A1 LINE LEADTHROUGH FOR THE LEADTHROUGH OF LINES THROUGH A COMPONENT 审中-公开
公开(公告)号：US20180251973A1
公开(公告)日：2018-09-06
申请号：US15760238
申请日：2016-09-27
申请人： HILTI AKTIENGESELLSCHAFT
发明人： SCHULZ-HANKE Wolfgang , Herbert MUENZENBERGER
IPC分类号： E04B1/94 , F16L5/04 , H02G3/04 , H02G3/22
CPC分类号： E04B1/947 , F16L5/025 , F16L5/04 , H02G3/0412 , H02G3/0481 , H02G3/22
摘要： A line penetration for routing a line through a passage opening of a building part that includes a first and a second building-part wall, between which an intermediate space is provided. The line penetration has a closure element that includes: an inner part for filling the intermediate space in the region of the passage opening; holding parts, with cross section smaller than that of the inner part, disposed on both sides of the inner part; a straight-through line opening, which penetrates the inner part and the holding parts in the direction in which they are disposed; and a sliding device, which is formed in order to guide the line slidingly and gas-tightly through the line opening.

4. 发明申请

US20180142810A1 AIR, ACOUSTIC AND/OR FIRE SEALING DEVICE 审中-公开
公开(公告)号：US20180142810A1
公开(公告)日：2018-05-24
申请号：US15355148
申请日：2016-11-18
申请人： Hilti Aktiengesellschaft
发明人： Joshua Vandertook , Tamara Sarg , Lukas Schwaiger , Chad Stroike
IPC分类号： F16L5/02 , F16L5/10
CPC分类号： F16L5/025 , F16L5/04 , F16L5/10 , F16L27/11 , F16L55/0336 , H02G3/0412 , H02G3/085 , H02G3/22
摘要： An air, acoustic and/or fire sealing device comprising an air, acoustic and/or fire sealing insert body comprising molded foam material, the body having a first end and a second end and a bulk continuous with the first end and the second end; wherein the body has an outer diameter, and the body is adapted to allow one or more pipes, fibers and/or cables to pass through the first and second ends and the bulk; and, a flexible hollow sleeve having an inner diameter, a first open end and a second open end, the ends being axially arranged; wherein the outer diameter of the air, acoustic and/or fire sealing insert body is greater than, equal to, or less than, the inner diameter of the flexible hollow sleeve; and, the air, acoustic and/or fire sealing insert body is arranged in the sleeve, is disclosed.

5. 发明授权

US09506403B2 Fastener 有权
标题翻译：紧固件
公开(公告)号：US09506403B2
公开(公告)日：2016-11-29
申请号：US14593483
申请日：2015-01-09
申请人： ROLLS-ROYCE PLC
发明人： Samuel John MacLaren Clarke
IPC分类号： F16L27/11 , F02C7/06 , F16L27/111 , F01D9/06 , F01D25/04 , F01D25/18 , F01D25/24 , F16B5/02 , F16L5/02 , F16L5/12
CPC分类号： F02C7/06 , F01D9/06 , F01D25/04 , F01D25/18 , F01D25/24 , F05D2250/184 , F16B5/0241 , F16B5/0258 , F16L5/025 , F16L5/12 , F16L27/11 , F16L27/111
摘要： The present invention provides a fastener for securing two pipe adapters within a casing such as a gas turbine casing. The fastener comprises a fastener body having a central bore for receiving the pipe adapters and having a first engagement portion, e.g. a radial projection extending into said central bore, for engagement with a first pipe adapter. The central bore has a second engagement portion, e.g. a threaded portion, for engagement with a second pipe adapter. The fastener further comprises an outer wall at least partly surrounding and spaced from the fastener body in a concentric arrangement. The outer wall comprises a fastener flange extending radially in a direction away from the fastener body for overlaying the casing. At least a portion of the outer wall is deformable (e.g. formed as bellows) so that, in use, axial and/or radial movement of the pipe adapters is dampened.
摘要翻译：本发明提供了一种紧固件，用于将诸如燃气轮机壳体的壳体内的两个管接头固定。紧固件包括具有用于接收管接头并具有第一接合部分的中心孔的紧固件本体，径向突起延伸到所述中心孔中，用于与第一管适配器接合。中心孔具有第二接合部分，例如，螺纹部分，用于与第二管适配器接合。紧固件还包括外壁，该外壁至少部分地以同心的方式围绕并与紧固件本体隔开。外壁包括沿远离紧固件主体的方向径向延伸的紧固件凸缘，用于覆盖外壳。外壁的至少一部分是可变形的（例如形成为波纹管），使得在使用中管道适配器的轴向和/或径向运动受到抑制。

6. 发明授权

US09447899B2 Tube support structure for aircraft 有权
标题翻译：飞机支架结构
公开(公告)号：US09447899B2
公开(公告)日：2016-09-20
申请号：US13877952
申请日：2011-10-21
申请人： Keisuke Minami
发明人： Keisuke Minami
IPC分类号： F16L3/08 , F16L3/12 , B64D37/00 , F16L3/16 , F16L5/10 , F16L3/22 , F16L3/00 , A47F5/12 , A47G29/00 , F16L3/10 , F16M11/10
CPC分类号： F16L3/1222 , B64D37/005 , F16L3/10 , F16L3/1008 , F16L3/1016 , F16L3/1091 , F16L3/16 , F16L5/025 , F16L5/10 , F16M11/10 , Y02T50/44
摘要： A tube support structure for an aircraft includes: a parallel movement mechanism configured to support the tube movably in parallel; and an angle adjustment mechanism configured to support the tube angle-adjustably. The parallel movement mechanism includes: an eccentric sleeve, through which the tube passes, configured to adjust a position of the tube in a Z direction perpendicular to the X direction, and a Y direction adjustment mechanism configured to adjust a position of the eccentric sleeve in a Y direction perpendicular to the X direction and the Z direction. The angle adjustment mechanism includes: a first member configured to have a first curved surface and support the tube, and a second member configured to have a second curved surface with a shape corresponding to the first curved surface, have contact slidably with the first curved surface at the second curved surface, and support the first member by the second curved surface. Each of the first curved surface and the second curved surface is formed such that a cross-sectional shape in an XZ plane is a circular arc shape, and an angle of the tube is adjusted by sliding the first curved surface with respect to the second curved surface. Thus, a tube support structure for aircraft, which can suppress a preload, is provided.
摘要翻译：一种用于飞行器的管支撑结构，包括：平行运动机构，被配置为平行地可移动地支撑所述管; 以及角度调节机构，其被配置为可调节地支撑所述管。所述平行运动机构包括：所述管通过的偏心套筒，被配置为调节所述管子沿垂直于所述X方向的Z方向的位置;以及Y方向调节机构，被配置为调节所述偏心套筒的位置垂直于X方向和Z方向的Y方向。所述角度调整机构包括：第一构件，其具有第一曲面并支撑所述管，以及构造成具有与所述第一曲面对应的形状的第二曲面的第二构件，其具有与所述第一曲面在第二弯曲表面处，并且通过第二弯曲表面支撑第一构件。第一弯曲表面和第二弯曲表面中的每一个形成为使得XZ平面中的横截面形状为圆弧形状，并且通过相对于第二弯曲部分滑动第一弯曲表面来调节管的角度表面。因此，提供了能够抑制预载的用于飞行器的管支撑结构。

7. 发明授权

US09423057B2 Acoustical seal system 有权
标题翻译：声封系统
公开(公告)号：US09423057B2
公开(公告)日：2016-08-23
申请号：US13938483
申请日：2013-07-10
申请人： General Electric Company
发明人： Christophe Vasinis
IPC分类号： H02G3/22 , F16L5/02 , F01D25/04 , F16L5/00 , F16L51/00 , F16L55/035
CPC分类号： F16L5/025 , F01D25/04 , F16L5/00 , F16L51/00 , F16L55/035
摘要： Various embodiments include systems and apparatuses adapted for acoustical insulation. In some embodiments apparatuses include a seal assembly for a conduit, the assembly includes a substantially inflexible collar member sized to form an axial seal around the conduit, the substantially inflexible collar member having a flange extending substantially radially and a substantially flexible axial seal member in sealing contact with the substantially inflexible collar member, the substantially flexible axial seal member including a first portion in sealing contact with a first face of the flange and a second portion in sealing contact with a second face of the flange, wherein the substantially flexible axial seal member and the substantially inflexible collar member maintain the axial seal around the conduit and permit axial movement, translational movement and rotational movement of the conduit relative to a conduit passage panel.
摘要翻译：各种实施例包括适用于隔音的系统和装置。在一些实施例中，设备包括用于导管的密封组件，该组件包括尺寸适于形成围绕导管的轴向密封件的基本上不弯曲的套管构件，该基本上不弯曲的套管构件具有基本径向延伸的凸缘和基本上柔性的轴向密封构件，与基本上不弯曲的套环构件接触，基本上柔性的轴向密封构件包括与凸缘的第一面密封接触的第一部分和与凸缘的第二面密封接触的第二部分，其中基本上柔性的轴向密封构件并且基本上不弯曲的套环构件保持围绕导管的轴向密封，并允许管道相对于导管通道面板的轴向运动，平移运动和旋转运动。

8. 发明申请

US20150204242A1 FASTENER 有权
标题翻译：紧固件
公开(公告)号：US20150204242A1
公开(公告)日：2015-07-23
申请号：US14593483
申请日：2015-01-09
申请人： ROLLS-ROYCE PLC
发明人： Samuel John MacLaren CLARKE
IPC分类号： F02C7/06
CPC分类号： F02C7/06 , F01D9/06 , F01D25/04 , F01D25/18 , F01D25/24 , F05D2250/184 , F16B5/0241 , F16B5/0258 , F16L5/025 , F16L5/12 , F16L27/11 , F16L27/111
摘要： The present invention provides a fastener for securing two pipe adapters within a casing such as a gas turbine casing. The fastener comprises a fastener body having a central bore for receiving the pipe adapters and having a first engagement portion, e.g. a radial projection extending into said central bore, for engagement with a first pipe adapter. The central bore has a second engagement portion, e.g. a threaded portion, for engagement with a second pipe adapter. The fastener further comprises an outer wall at least partly surrounding and spaced from the fastener body in a concentric arrangement. The outer wall comprises a fastener flange extending radially in a direction away from the fastener body for overlaying the casing. At least a portion of the outer wall is deformable (e.g. formed as bellows) so that, in use, axial and/or radial movement of the pipe adapters is dampened.
摘要翻译：本发明提供了一种紧固件，用于将诸如燃气轮机壳体的壳体内的两个管接头固定。紧固件包括具有用于接收管接头并具有第一接合部分的中心孔的紧固件本体，径向突起延伸到所述中心孔中，用于与第一管适配器接合。中心孔具有第二接合部分，例如，螺纹部分，用于与第二管适配器接合。紧固件还包括外壁，该外壁至少部分地以同心的方式围绕并与紧固件本体隔开。外壁包括沿远离紧固件主体的方向径向延伸的紧固件凸缘，用于覆盖外壳。外壁的至少一部分是可变形的（例如形成为波纹管），使得在使用中管道适配器的轴向和/或径向运动受到抑制。

9. 发明申请

US20130212833A1 DUCTWORK 有权
公开(公告)号：US20130212833A1
公开(公告)日：2013-08-22
申请号：US13883112
申请日：2011-11-02
申请人： Hans Lohmann
发明人： Hans Lohmann
IPC分类号： F16L5/08
CPC分类号： F16L5/08 , B63B13/00 , F16B13/0833 , F16B13/0891 , F16B37/067 , F16L5/025 , Y10T16/05
摘要： Ductwork (1) for arranging at least one pipe through an opening (2) in a partitioning (3), including a flange (4) having an outer periphery area (5) and a central area (7) which is formed with a guide opening (8) for every pipe, the flange (4) being provided with a number of mounting apertures (11), the flange (4) having an inner side (9) and an outer side (10) opposite the inner side (9), where the inner side (9) is adapted for bearing against one side (6) of the partitioning, wherein the ductwork (1) further includes a connecting arrangement mounted in each mounting aperture (13), the connecting arrangement including force transmission means (15) with an operating member (22) disposed over the outer side (10) of the flange, and with a shank (17) extending through the mounting aperture (11), a clamping means (23) disposed on the shank (17) of the force transmission means and which is displaceable around and/or along the shank (17) by actuating the operating member (22), and an engagement arrangement (19) disposed between the inner side (9) of the flange and the clamping means (23), and which is adapted with contact surfaces (23) interacting with contact surfaces (18) on the clamping means (23), and engaging faces (20) that may be displaced radially relative to the orientation of the shank by actuating the operating member (22).
摘要翻译：一种用于在隔板（3）内通过开口（2）布置至少一根管子的管道（1），包括具有外围区域（5）的凸缘（4）和形成有导向件每个管的开口（8），凸缘（4）设有多个安装孔（11），凸缘（4）具有内侧（9）和与内侧（9）相对的外侧（10）），其中所述内侧（9）适于支撑所述分隔件的一侧（6），其中所述管道系统（1）还包括安装在每个安装孔（13）中的连接装置，所述连接装置包括力传递装置（15），其具有设置在所述凸缘的外侧（10）上方的操作构件（22）以及延伸穿过所述安装孔（11）的柄部（17），设置在所述柄部（17）上的夹紧装置（23）），并且其可通过致动操作构件（22）而沿柄（17）和/或沿柄（17）移动，并且接合设置在凸缘的内侧（9）和夹紧装置（23）之间并且适于与夹紧装置（23）上的接触表面（18）相互作用的接触表面（23）的入口装置（19）以及接合面（20）可以通过致动操作构件（22）而相对于柄的取向径向地位移。

10. 发明申请

US20130187013A1 TUBE SUPPORT STRUCTURE FOR AIRCRAFT 有权
标题翻译：用于飞机的管支撑结构
公开(公告)号：US20130187013A1
公开(公告)日：2013-07-25
申请号：US13877952
申请日：2011-10-21
申请人： Keisuke Minami
发明人： Keisuke Minami
IPC分类号： F16L3/12
CPC分类号： F16L3/1222 , B64D37/005 , F16L3/10 , F16L3/1008 , F16L3/1016 , F16L3/1091 , F16L3/16 , F16L5/025 , F16L5/10 , F16M11/10 , Y02T50/44
摘要： A tube support structure for an aircraft includes: a parallel movement mechanism configured to support the tube movably in parallel; and an angle adjustment mechanism configured to support the tube angle-adjustably. The parallel movement mechanism includes: an eccentric sleeve, through which the tube passes, configured to adjust a position of the tube in a Z direction perpendicular to the X direction, and a Y direction adjustment mechanism configured to adjust a position of the eccentric sleeve in a Y direction perpendicular to the X direction and the Z direction. The angle adjustment mechanism includes: a first member configured to have a first curved surface and support the tube, and a second member configured to have a second curved surface with a shape corresponding to the first curved surface, have contact slidably with the first curved surface at the second curved surface, and support the first member by the second curved surface. Each of the first curved surface and the second curved surface is formed such that a cross-sectional shape in an XZ plane is a circular arc shape, and an angle of the tube is adjusted by sliding the first curved surface with respect to the second curved surface. Thus, a tube support structure for aircraft, which can suppress a preload, is provided.
摘要翻译：一种用于飞行器的管支撑结构，包括：平行运动机构，被配置为平行地可移动地支撑所述管; 以及角度调节机构，其被配置为可调节地支撑所述管。所述平行运动机构包括：所述管通过的偏心套筒，被配置为调节所述管子沿垂直于所述X方向的Z方向的位置;以及Y方向调节机构，被配置为调节所述偏心套筒的位置垂直于X方向和Z方向的Y方向。所述角度调整机构包括：第一构件，其具有第一曲面并支撑所述管，以及构造成具有与所述第一曲面对应的形状的第二曲面的第二构件，其具有与所述第一曲面在第二弯曲表面处，并且通过第二弯曲表面支撑第一构件。第一弯曲表面和第二弯曲表面中的每一个形成为使得XZ平面中的横截面形状为圆弧形状，并且通过相对于第二弯曲部分滑动第一弯曲表面来调节管的角度表面。因此，提供了能够抑制预载的用于飞行器的管支撑结构。

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