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1.发明授权Support strut for supporting primary components as well as guiding systems with such a support strut and method for manufacturing such a support strut 有权用于支撑主要部件的支撑支柱以及具有这种支撑支柱的引导系统以及用于制造这种支撑支柱的方法公开(公告)号：US09494185B2
公开(公告)日：2016-11-15
申请号：US13923572
申请日：2013-06-21
Applicant: Airbus Operations GmbH
Inventor： M. Ichwan Zuardy , Claus Fastert , Holger Purol , Pierre Zahlen , York Caesar Roth
CPC classification number: F16C11/04 , B29C43/18 , B29C70/462 , B29C70/86 , B29L2031/75 , B64C1/06 , B64C13/28 , F16C7/02 , F16C2326/43 , Y02T50/43 , Y10T16/558
Abstract: A support strut for use as a primary load-bearing structural component for the hinged coupling of at least one additional primary load-bearing structural component. The support strut includes: a rod-shaped base body extending in a longitudinal direction, a fiber composite with an annular cross section, central hole originating from the first end of the base body, and with annular holes spaced apart relative to each other in the circumferential direction of the annular cross section and originating from the first end of the base body as well as running along the longitudinal direction in the base body; roving bundles imbedded in a matrix material that fills up the respective annular hole; and a hinged connecting body with a bearing receptacle for holding a swivel joint; as well as a guiding system with such a support strut and a method for manufacturing such a support strut.
Abstract translation: 支撑支柱，用作至少一个额外的主要承重结构部件的铰接联接的主要承载结构部件。 支撑支柱包括：沿纵向方向延伸的杆状基体，具有环形横截面的纤维复合材料，源自基体的第一端的中心孔和在该基体的第一端部间隔开的环形孔 环形横截面的圆周方向并且源自基体的第一端，并且沿着基体的纵向方向延伸; 镶嵌在填充相应环形孔的基质材料中的粗纱束; 以及具有用于保持旋转接头的轴承座的铰接连接体; 以及具有这种支撑支柱的引导系统和用于制造这种支撑支柱的方法。
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2.发明申请PRESSURIZED FUSELAGE OF AN AIRCRAFT, WITH A FUSELAGE STRUCTURE AND A PRESSURE BULKHEAD SPECIALLY MOUNTED THEREIN 审中-公开具有FUSELAGE结构和特殊安装的压力容器的飞机的加压熔断器公开(公告)号：US20150083862A1
公开(公告)日：2015-03-26
申请号：US14558800
申请日：2014-12-03
Applicant: Airbus Operations GmbH
Inventor： Karim Grase , M. Ichwan Zuardy , Dieter Hachenberg , Henning Scheel , B. Claudio Vultaggio
IPC: B64C1/10
CPC classification number: B64C1/10
Abstract: A pressurized fuselage of an aircraft includes a fuselage structure and a pressure bulkhead mounted therein for forming a fuselage-internal pressure region. The pressure bulkhead is attached on the edge region, by way of mounting means, to the inside of the fuselage structure. The mounting means comprise at least one pivoting socket arrangement, arranged on the edge side of the pressure bulkhead, which edge side faces away from the pressure region, and interacts with the fuselage structure, as well as a supporting frame element, arranged on the opposite edge side and supporting itself on the fuselage structure.
Abstract translation: 飞机的加压机身包括机身结构和安装在其中的用于形成机身内部压力区域的压力隔板。 压力舱壁通过安装方式附接在边缘区域到机身结构的内部。 安装装置包括布置在压力隔板的边缘侧上的至少一个枢转插座装置，该边缘侧背离压力区域，并且与机身结构相互作用以及布置在相对的机架结构上的支撑框架元件 边缘并支撑在机身结构上。
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公开(公告)号：US09902483B2
公开(公告)日：2018-02-27
申请号：US14469146
申请日：2014-08-26
Applicant: Airbus Operations GmbH
Inventor： Pierre C. Zahlen , Johannes Born , Lars Meyer , Gregor Baumbach , Claus Hanske , Jens Prowe , Johan Oentoro , M. Ichwan Zuardy , Wouter Brok , Martin Metten
IPC: B32B3/24 , B32B3/26 , B32B5/18 , B32B5/24 , B32B5/26 , B32B5/28 , B32B7/04 , B60J1/00 , B64C1/14 , B29C70/02 , B32B3/08 , B32B37/16 , B32B37/30 , B32B37/12 , B32B38/04 , B29C70/30 , B29L7/00 , B32B3/02 , B29C70/54 , B29L9/00 , B29L31/30 , B29L31/00 , B64C1/12 , B64C1/00
CPC classification number: B64C1/1484 , B29C70/023 , B29C70/026 , B29C70/30 , B29C70/545 , B29C2793/0018 , B29C2793/0081 , B29L2007/002 , B29L2009/00 , B29L2031/005 , B29L2031/30 , B29L2031/3082 , B32B3/02 , B32B3/08 , B32B3/263 , B32B3/266 , B32B5/18 , B32B5/245 , B32B5/26 , B32B5/28 , B32B7/04 , B32B37/16 , B32B37/30 , B32B38/04 , B32B2250/03 , B32B2250/24 , B32B2250/40 , B32B2250/44 , B32B2260/00 , B32B2266/08 , B32B2305/022 , B32B2305/07 , B32B2605/00 , B32B2605/006 , B32B2605/18 , B60J1/00 , B60J1/004 , B60J1/006 , B64C1/12 , B64C1/14 , B64C1/1492 , B64C2001/0072 , Y02T50/43 , Y10T29/49163 , Y10T29/49165 , Y10T428/12667 , Y10T428/239 , Y10T428/24322 , Y10T428/24521 , Y10T428/25 , Y10T428/256 , Y10T428/257 , Y10T428/26 , Y10T428/2982
Abstract: The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.
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4.发明申请PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN 有权具有熔断壳的飞机的压力熔断器和其中的压力容器公开(公告)号：US20150008285A1
公开(公告)日：2015-01-08
申请号：US14491251
申请日：2014-09-19
Applicant: AIRBUS OPERATIONS GMBH
Inventor： M. Ichwan Zuardy , Karim Grase , Carsten Rowedder , Claas DeJong , Markus Mueller , Mathias Jessrang
IPC: B64C1/10
CPC classification number: B64C1/10
Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.
Abstract translation: 具有机身壳体和压力舱壁的飞机的压力舱壁优选地设置在后部区域中，用于形成机身内部压力区域，该压力舱壁附接在机身壳体内部的边缘上，其中压力舱壁 具有透镜状横截面和夹层结构，其包括夹在两个相对的外壳之间的泡沫芯。
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Patent Agency Ranking
公开(公告)号：US09592640B2
公开(公告)日：2017-03-14
申请号：US14522786
申请日：2014-10-24
Applicant: Airbus Operations GmbH
Inventor： Thomas Hoffmeister , Markus Mueller , M. Ichwan Zuardy
CPC classification number: B29C70/34 , B29C33/02 , B29C33/48 , B29C70/345 , B29C70/462 , B29C70/54 , B29D99/0003 , B29L2031/3076 , B29L2031/3082
Abstract: A curing tool for a shell component, includes a first tool component, which is a polyhedron and has a wedge-shaped bevel forming a first sheared edge on a first side edge, and a second tool component, which is a polyhedron, has a wedge-shaped bevel forming a second sheared edge on a first side edge and has a first corner bevel on a second side edge diagonally opposite the first side edge. The wedge angles of the first and the second sheared edge are equal.
Abstract translation: 一种用于外壳部件的固化工具，包括第一工具部件，其是多面体并且具有在第一侧边缘上形成第一剪切边缘的楔形斜面，并且作为多面体的第二工具部件具有楔形 在第一侧边缘上形成第二剪切边缘并且在与第一侧边缘对角地相对的第二侧边缘上具有第一角部斜面。 第一和第二剪切边缘的楔角相等。
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公开(公告)号：US20150064389A1
公开(公告)日：2015-03-05
申请号：US14469146
申请日：2014-08-26
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Pierre C. Zahlen , Johannes Born , Lars Meyer , Gregor Baumbach , Claus Hanske , Jens Prowe , Johan Oentoro , M. Ichwan Zuardy , Wouter Brok , Martin Metten
CPC classification number: B64C1/1484 , B29C70/023 , B29C70/026 , B29C70/30 , B29C70/545 , B29C2793/0018 , B29C2793/0081 , B29L2007/002 , B29L2009/00 , B29L2031/005 , B29L2031/30 , B29L2031/3082 , B32B3/02 , B32B3/08 , B32B3/263 , B32B3/266 , B32B5/18 , B32B5/245 , B32B5/26 , B32B5/28 , B32B7/04 , B32B37/16 , B32B37/30 , B32B38/04 , B32B2250/03 , B32B2250/24 , B32B2250/40 , B32B2250/44 , B32B2260/00 , B32B2266/08 , B32B2305/022 , B32B2305/07 , B32B2605/00 , B32B2605/006 , B32B2605/18 , B60J1/00 , B60J1/004 , B60J1/006 , B64C1/12 , B64C1/14 , B64C1/1492 , B64C2001/0072 , Y02T50/43 , Y10T29/49163 , Y10T29/49165 , Y10T428/12667 , Y10T428/239 , Y10T428/24322 , Y10T428/24521 , Y10T428/25 , Y10T428/256 , Y10T428/257 , Y10T428/26 , Y10T428/2982
Abstract: The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.
Abstract translation: 本公开涉及一种用于车辆的车体结构的窗板，特别是飞机或航天器的机身，包括在面板的第一侧上延伸以形成车身结构的外皮的第一皮肤; 第二皮肤，其在所述面板的第二侧上延伸以形成所述车身结构的内表皮; 以及位于三明治结构中的第一和第二表层之间并覆盖的核心，特别是泡沫芯。 窗口面板包括通过第一层，芯部和第二层形成的至少一个窗孔。 芯可以限制在或限制在面板的有限程度，区域或部分上。 因此，第一皮肤和/或第二皮肤可以延伸超过或覆盖面板的比芯的更大的面积。
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7.发明授权公开(公告)号：US09834298B2
公开(公告)日：2017-12-05
申请号：US14491251
申请日：2014-09-19
Applicant: Airbus Operations GmbH
Inventor： M. Ichwan Zuardy , Karim Grase , Carsten Rowedder , Claas De Jong , Markus Mueller , Mathias Jessrang
IPC: B64C1/10
CPC classification number: B64C1/10
Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.
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8.发明申请公开(公告)号：US20150298401A1
公开(公告)日：2015-10-22
申请号：US14522786
申请日：2014-10-24
Applicant: Airbus Operations GmbH
Inventor： Thomas Hoffmeister , Markus Mueller , M. Ichwan Zuardy
CPC classification number: B29C70/34 , B29C33/02 , B29C33/48 , B29C70/345 , B29C70/462 , B29C70/54 , B29D99/0003 , B29L2031/3076 , B29L2031/3082
Abstract: A curing tool for a shell component, includes a first tool component, which is cuboid and has a wedge-shaped bevel forming a first sheared edge on a first side edge, and a second tool component, which is cuboid, has a wedge-shaped bevel forming a second sheared edge on a first side edge and has a first corner bevel on a second side edge diagonally opposite the first side edge. The wedge angles of the first and the second sheared edge are equal.
Abstract translation: 一种用于外壳部件的固化工具，包括第一工具部件，该第一工具部件是长方体形的并且具有在第一侧边缘上形成第一剪切边缘的楔形斜面，以及长方体形状的第二工具部件，具有楔形 斜面在第一侧边缘上形成第二剪切边缘，并且在与第一侧边缘对角地相对的第二侧边缘上具有第一角部斜面。 第一和第二剪切边缘的楔角相等。
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9.发明申请SUPPORT STRUT FOR SUPPORTING PRIMARY COMPONENTS AS WELL AS GUIDING SYSTEMS WITH SUCH A SUPPORT STRUT AND METHOD FOR MANUFACTURING SUCH A SUPPORT STRUT 有权用于支持主要组件的支持条件以及具有这样的支持条件的指导系统以及用于制造支持条件的方法公开(公告)号：US20140014771A1
公开(公告)日：2014-01-16
申请号：US13923572
申请日：2013-06-21
Applicant: Airbus Operations GmbH
Inventor： M. Ichwan Zuardy , Claus Fastert , Holger Purol , Pierre Zahlen , York Caesar Roth
CPC classification number: F16C11/04 , B29C43/18 , B29C70/462 , B29C70/86 , B29L2031/75 , B64C1/06 , B64C13/28 , F16C7/02 , F16C2326/43 , Y02T50/43 , Y10T16/558
Abstract: A support strut for use as a primary load-bearing structural component for the hinged coupling of at least one additional primary load-bearing structural component. The support strut includes: a rod-shaped base body extending in a longitudinal direction, a fiber composite with an annular cross section, central hole originating from the first end of the base body, and with annular holes spaced apart relative to each other in the circumferential direction of the annular cross section and originating from the first end of the base body as well as running along the longitudinal direction in the base body; roving bundles imbedded in a matrix material that fills up the respective annular hole; and a hinged connecting body with a bearing receptacle for holding a swivel joint; as well as a guiding system with such a support strut and a method for manufacturing such a support strut.
Abstract translation: 支撑支柱，用作至少一个额外的主要承重结构部件的铰接联接的主要承载结构部件。 支撑支柱包括：沿纵向方向延伸的杆状基体，具有环形横截面的纤维复合材料，源自基体的第一端的中心孔和在该基体的第一端部间隔开的环形孔 环形横截面的圆周方向并且源自基体的第一端，并且沿着基体的纵向方向延伸; 镶嵌在填充相应环形孔的基质材料中的粗纱束; 以及具有用于保持旋转接头的轴承座的铰接连接体; 以及具有这种支撑支柱的引导系统和用于制造这种支撑支柱的方法。
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