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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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3.发明授权Method for infiltrating silicone into a fiber composite structure and device for executing a method for producing a fiber composite workpiece 有权将硅氧烷渗透到纤维复合结构体中的方法和用于执行纤维复合工件的制造方法的装置公开(公告)号：US08961726B2
公开(公告)日：2015-02-24
申请号：US13737643
申请日：2013-01-09
Applicant: Airbus Operations GmbH
Inventor： Tamas Havar , Oliver Meyer , York Caesar Roth , Oliver Seack
IPC: B29C70/48 , B64C3/46 , B29C70/68 , B29C70/44 , B29B11/16 , B29C70/20 , B29C70/36 , B29C70/46 , B29C70/86 , B60R21/00 , B64C9/38 , B29K703/00 , B29B11/12 , B29K83/00 , B29K105/24 , B29L31/30
CPC classification number: B29C70/682 , B29B11/12 , B29B11/16 , B29C70/20 , B29C70/36 , B29C70/443 , B29C70/46 , B29C70/48 , B29C70/865 , B29K2083/005 , B29K2105/24 , B29K2703/00 , B29L2031/3055 , B29L2031/3085 , B60R21/00 , B64C9/38 , Y02T50/43 , Y10T156/15
Abstract: The invention relates to a method for producing a fiber composite workpiece. In the method according to the invention, cross-linking silicone is used with the aid of a volatile diluent for infiltrating individual mats of a mat composite. A further object of the present invention is a device for performing the method according to the invention.
Abstract translation: 本发明涉及一种纤维复合工件的制造方法。 在根据本发明的方法中，借助于挥发性稀释剂使用交联硅氧烷，以渗透垫复合材料的各个垫。 本发明的另一个目的是用于执行根据本发明的方法的装置。
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4.发明申请METHOD FOR INFILTRATING SILICONE INTO A FIBER COMPOSITE STRUCTURE AND DEVICE FOR EXECUTING A METHOD FOR PRODUCING A FIBER COMPOSITE WORKPIECE 有权用于将硅胶浸入纤维复合结构中的方法和用于执行生产纤维复合材料工艺的方法的装置公开(公告)号：US20130200652A1
公开(公告)日：2013-08-08
申请号：US13737643
申请日：2013-01-09
Applicant: Airbus Operations GmbH
Inventor： Tamas Havar , Oliver Meyer , York Caesar Roth , Oliver Seack
CPC classification number: B29C70/682 , B29B11/12 , B29B11/16 , B29C70/20 , B29C70/36 , B29C70/443 , B29C70/46 , B29C70/48 , B29C70/865 , B29K2083/005 , B29K2105/24 , B29K2703/00 , B29L2031/3055 , B29L2031/3085 , B60R21/00 , B64C9/38 , Y02T50/43 , Y10T156/15
Abstract: The invention relates to a method for producing a fiber composite workpiece. In the method according to the invention, cross-linking silicone is used with the aid of a volatile diluent for infiltrating individual mats of a mat composite. A further object of the present invention is a device for performing the method according to the invention.
Abstract translation: 本发明涉及一种纤维复合工件的制造方法。 在根据本发明的方法中，借助于挥发性稀释剂使用交联硅氧烷，以渗透垫复合材料的各个垫。 本发明的另一个目的是用于执行根据本发明的方法的装置。
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