PLANKING PANEL FOR A STRUCTURAL COMPONENT, FLOW BODY COMPRISING SUCH A PLANKING PANEL AND DEVICE FOR MONITORING MATERIAL DAMAGE ON SUCH A PLANKING PANEL
    8.
    发明申请
    PLANKING PANEL FOR A STRUCTURAL COMPONENT, FLOW BODY COMPRISING SUCH A PLANKING PANEL AND DEVICE FOR MONITORING MATERIAL DAMAGE ON SUCH A PLANKING PANEL 审中-公开
    用于结构构件的平面板,包含这样的平面板的流动体和用于监测这样的平面板上的材料损坏的装置

    公开(公告)号:US20140000381A1

    公开(公告)日:2014-01-02

    申请号:US13743767

    申请日:2013-01-17

    Abstract: The invention pertains to a planking panel (B) for a structural component (1) that is realized in the form of a sandwich component in its inner region (BI) that extends in a planar fashion and features a first skin section (11), a second skin section (12) and a core section (13) that is situated between these two skin sections, wherein the core section (13) connects the first and the second skin sections (11, 12) to one another in a planar fashion, with the invention being characterized in that a plurality of monitoring lines (14) is provided that extend over a planar section of the core section (13) to be monitored in order to detect damage in the core section (13) and respectively feature a first connection point (15) on a first end (14a) and a second connection point (16) on a second end (16a) in order to apply a monitoring signal (UK), wherein the monitoring lines (14) have a tear strength that lies in the range between 50% and 100% of the tear strength of the core section (13).

    Abstract translation: 本发明涉及一种用于结构部件(1)的板条板(B),其在其内部区域(BI)中以三明治部件的形式实现,其以平面方式延伸并且具有第一皮肤部分(11), 第二皮肤部分(12)和位于这两个皮肤部分之间的芯部分(13),其中,芯部分(13)以平面方式彼此连接第一和第二皮肤部分(11,12) 本发明的特征在于,提供了多个监测线(14),其在待监测的芯部分(13)的平面部分上延伸,以便检测芯部分(13)中的损伤,并且分别具有 为了施加监测信号(UK),第一端(14a)上的第一连接点(15)和第二端(16a)上的第二连接点(16),其中监测线(14)具有撕裂强度 其位于芯部(13)的撕裂强度的50%至100%的范围内。

    Pressure bulkhead for an aircraft fuselage

    公开(公告)号:US10384759B2

    公开(公告)日:2019-08-20

    申请号:US15361292

    申请日:2016-11-25

    Abstract: A pressure bulkhead for an aircraft fuselage having a skin element, with a first surface and a second surface, a circumferential edge and a center axis, and a reinforcement assembly, which has radially disposed reinforcement elements extending along the first surface radially between an outer end at the edge of the skin element and an inner end, which faces the center axis, wherein, in a cross section, which extends radially along the center axis, each of the radially disposed reinforcement elements defines first and second contour lines, each extending from the outer end of the radially disposed reinforcement elements to the inner end thereof, and the reinforcement assembly resting with the first contour lines thereof on the first surface of the skin element. A pressure bulkhead for an aircraft fuselage can efficiently absorb occurring pressure loads.

    Application Device And Method For Dispensing A Formed Fibre Composite Strand

    公开(公告)号:US20190061288A1

    公开(公告)日:2019-02-28

    申请号:US16113369

    申请日:2018-08-27

    Abstract: A mobile application device for dispensing a formed fibre composite strand has: a coupling unit for detachably fastening the application device to the handling device for moving the application device; a preforming unit for continuously forming an unprocessed fibre strand into a formed fibre strand with a formed fibre cross section settable by the preforming unit; an impregnating unit for continuously developing the formed fibre strand into a fibre composite strand by impregnation with a matrix material; and a postforming unit for continuously pressing the fibre composite strand to and through the dispensing unit and having a drive unit and an adjustable dispensing unit for continuously forming a fibre composite strand into a formed fibre composite strand with a dispensing cross section settable by the dispensing unit and for dispensing the same such that the formed fibre cross section is at least 70% congruent with the dispensing cross section.

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