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    • 2. 发明公开
    • Method for manufacturing a fibre composite component, fibre composite component, and structural component for an aircraft or spacecraft
    • 用于制造飞机或航天器的纤维复合部件,纤维复合部件和结构部件的方法
    • EP2857186A3
    • 2015-07-29
    • EP14184219.5
    • 2014-09-10
    • Airbus Operations GmbH
    • Joern, Paul
    • B29D99/00B29C70/08B29C33/76
    • B29C70/68B29C33/76B29C70/086B29C70/30B29C70/84B29D99/0014B29K2063/00B29K2105/0872B29K2307/04B29K2715/003B29L2031/3076B32B5/18B32B2262/106B32B2266/0271B32B2605/18B64C1/12Y02T50/43
    • The invention relates to a method for manufacturing a fibre composite component comprising a skin portion and a backing structure. Initially, a single-piece foam body or the parts of a multi-part foam body, which comprises at least one recess which is open towards a first side of the foam body, are prepared and positioned. Prior to, during or after the positioning of the foam body or the parts thereof, a rigidifying element for the backing structure or a preform or first semi-finished product for forming the rigidifying element is arranged in the recess at least in portions. A skin portion or a second semi-finished product for forming the skin portion is provided, and brought into contact, in regions, with the foam body on the first side thereof and with the rigidifying element or preform or first semi-finished product, causing the skin portion or second semi-finished product to be placed against the foam body at least in portions and the rigidifying element or preform or first semi-finished product to be positioned relative to the skin portion or second semi-finished product. The skin portion or second semi-finished product and the rigidifying element or preform or first semi-finished product in contact therewith are processed further in such a way that a fibre composite component is obtained in which the skin portion and the rigidifying element are interconnected. The invention additionally relates to a fibre composite component and to a structural component for an aircraft or spacecraft.
    • 本发明涉及一种用于制造包括表皮部分和背衬结构的纤维复合部件的方法。 首先,准备并定位单件式泡沫体或包括至少一个朝向泡沫体的第一侧开放的凹部的多部分泡沫体的部分。 在定位泡沫体或其部件之前,期间或之后,用于背衬结构的硬化元件或用于形成硬化元件的预成型件或第一半成品至少部分地布置在凹部中。 提供用于形成蒙皮部分的蒙皮部分或第二半成品,并使其与第一侧上的泡沫体以及刚性化元件或预型体或第一半成品在区域中接触,从而引起 所述表皮部分或第二半成品至少部分地靠着所述泡沫主体放置,并且所述硬化元件或预成型件或第一半成品相对于所述表皮部分或第二半成品进行定位。 表皮部分或第二半成品以及与其接触的刚性化元件或预成型体或第一半成品进一步处理,使得获得表层部分和刚性化元件相互连接的纤维复合材料部件。 本发明另外涉及纤维复合材料部件以及用于飞机或航天器的结构部件。
    • 4. 发明公开
    • PHENOLIC RESIN FOAMED PLATE AND METHOD FOR PRODUCING SAME
    • GERCHÄUMTEPHENOLHARZPLATTE UND VERFAHREN ZU IHRER HERSTELLUNG
    • EP2514786A1
    • 2012-10-24
    • EP10837637.7
    • 2010-12-15
    • Asahi Kasei Construction Materials Corporation
    • MIHORI HisashiWATANABE HirofumiSAITO Yuki
    • C08J9/12
    • C08J9/141B29C44/24B29C44/321B29C44/326B29C44/468B32B5/32B32B2266/0271C08G14/08C08J2361/24C08L61/34
    • The present invention provides a phenolic resin foamed plate having a thickness of 50 mm or more, in which when the phenolic resin foamed plate is sliced from one main surface of the phenolic resin foamed plate along the main surface in a thickness direction at 5 mm intervals to produce n pieces, which are designated as Q1 to Qn in order from the main surface side, where average densities of Q1 to Qn are d q1 to d qn , respectively, the ratio (d qmin /d qave ) of a minimum value d qmin of d q2 to d q(n-1) to an average value d qave of d q2 to d q(n-1) is 0.91 ≤ d qmin /d qave ≤ 0.98, and when a density distribution line is obtained by calculating D i = (d q(i-1) + d qi + d q(i+1) )/3 [where i is an integer of 2 to (n-1), and if i is 2 or (n-1), D 2 = d q2 or D (n-1) = d q(n-1) , respectively], plotting Di in order of numerical values of i (i on the axis of abscissas, Di on the axis of ordinates), and connecting the values of Di, there exists a straight line parallel with the axis of abscissas that intersects the density distribution line at four points.
      The present invention provides a phenolic resin foamed plate exhibiting practically sufficient compressive strength and thermal conductivity even when the product thickness is increased.
    • 本发明提供一种厚度为50mm以上的酚醛树脂发泡板,其中当酚醛树脂发泡板沿酚醛树脂发泡板的主表面沿厚度方向以5mm间隔从主表面切片时, 从主表面侧分别按照Q1〜Qn的平均密度d q1〜d qn分别指定为Q1〜Qn的n个,最小值d的比(d qmin / d qave) d q2至dq(n-1)的qmin与d q2至dq(n-1)的平均值d qave为0.91‰¤d qmin / d qave‰¤0.98,并且当通过计算得到密度分布线 D i =(dq(i-1)+ d qi + dq(i + 1))/ 3 [其中i是2至(n-1)的整数,如果i是2或(n-1) D 2 = d q2或D(n-1)= dq(n-1)],按照i(i在横轴上的i,纵轴上的Di)的数值的顺序绘制Di, Di的值存在与斧平行的直线 是在四点处与密度分布线相交的横坐标。 本发明提供即使在产品厚度增加时也具有足够的抗压强度和导热性的酚醛树脂发泡板。