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    • 2. 发明申请
    • MOLDING PROCESSES AND TOOLS THEREFOR
    • 成型工艺和工具
    • WO2008128167A2
    • 2008-10-23
    • PCT/US2008060211
    • 2008-04-14
    • PURDUE RESEARCH FOUNDATIONGALLAGHER JEFF MCIPRA RAYMOND JSIEGMUND THOMAS H
    • GALLAGHER JEFF MCIPRA RAYMOND JSIEGMUND THOMAS H
    • B29C45/26G06F17/50
    • B29C51/10B29C33/0011B29C33/18B29C33/302B29C70/382B29C70/48B29K2707/04B33Y80/00
    • A molding process and apparatus suitable for use in molding processes, including rapid prototyping processes and short run production processes. The molding process and apparatus entail the use of a reconfigurable screen tool (10) having a housing (12) defining a manifold cavity (22) and a plurality of substantially parallel pins (16), each having a head (20) protruding from the housing (12) and a shank (18) protruding into the housing (12). The heads (20) of the pins (16) define a screen surface (28) through which air is able to flow, for example, through gaps between adjacent heads (20) or through internal passages (21 ) within the pins (16). The process further includes axially moving the pins (16) to configure the screen surface (28), preventing further axial movement of the pins (16) relative to each other, and then drawing a vacuum within the manifold cavity (22) and creating a vacuum at the screen surface (28).
    • 适用于模塑工艺的模塑工艺和设备,包括快速成型工艺和短期生产工艺。 模制过程和设备需要使用具有限定歧管空腔(22)和多个基本上平行的销(16)的壳体(12)的可重新构造的筛工具(10),每个销具有从 壳体(12)和伸入壳体(12)中的柄部(18)。 销(16)的头部(20)限定了空气能够例如通过销(16)内的相邻头部(20)之间的间隙或通过内部通道(21)流动的筛面(28) 。 该过程还包括轴向移动销(16)以构造筛面(28),防止销(16)相对于彼此进一步轴向移动,然后在歧管腔(22)内抽吸真空并产生 真空在筛面(28)处。
    • 5. 发明申请
    • MANUFACTURE OF THICK PREFORM COMPOSITES VIA MULTIPLE PRE-SHAPED FABRIC MAT LAYERS
    • 通过多个预成型的织物层制造厚预制复合材料
    • WO2006127002A1
    • 2006-11-30
    • PCT/US2005/018353
    • 2005-05-25
    • HONEYWELL INTERNATIONAL INC.LA FOREST, Mark, L.GHARBIEH, Nabil, AbuFATZ, Alan, E.CIPRA, Raymond, J.SIEGMUND, Thomas, H.
    • LA FOREST, Mark, L.GHARBIEH, Nabil, AbuFATZ, Alan, E.CIPRA, Raymond, J.SIEGMUND, Thomas, H.
    • C04B35/83
    • C04B35/83B29B11/16B29C70/305B29K2033/20B29K2105/128B29K2633/20B29L2031/7482B32B2315/02C04B2237/385D04H1/4242D04H1/593F16D69/023F16D2069/008
    • A preform for a carbon-carbon composite part (55) comprising multiple layers of fibrous mats (51, 52, 53) wherein each of the fibrous mats (51, 52, 53) comprises a random carbon-containing fibrous matrix (11) within which is distributed a polymeric binder and wherein adjacent mat layers (51, 52, 53) are bound together by additional polymer binder, stitching and interlocking tabs. The preform of the present invention may be an aircraft landing system brake disc. Also, a method of manufacturing a thick multi-layer composite preform. The method includes the steps of: providing an optionally reconfigurable tool including a perforated screen through which a vacuum can be drawn; delivering chopped fibers (b), such as pitch fibers, polyacrylonitrile fibers, or mixtures thereof, to said tool while drawing vacuum therethrough, to form a fibrous object; delivering binder (c), for instance in the form of a spray, to said fibrous object; melting or curing said binder (d), for instance by the application of heat or ultraviolet light, to make a fibrous mat (51, 52, 53); assembling, preferably in the substantial absence of cutting or other mechanical modification, a plurality of said fibrous mats (51, 52, 53) and additional binder into the shape of a preform (e); and heat-pressing the resulting mat assembly (f) into a finished thick preform (55).
    • 一种用于碳 - 碳复合材料部件(55)的预成型件,其包括多层纤维垫(51,52,53),其中每个纤维垫(51,52,53)包括含有无规碳的纤维基质(11) 其分布有聚合物粘合剂,并且其中相邻的垫层(51,52,53)通过另外的聚合物粘合剂,缝合和互锁接头结合在一起。 本发明的预成型件可以是飞机着陆系统制动盘。 另外,制造厚的多层复合预型体的方法。 该方法包括以下步骤:提供可选地可重新配置的工具,其包括穿孔筛网,通过该筛孔可抽出真空; 将诸如沥青纤维,聚丙烯腈纤维或其混合物的短切纤维(b)输送到所述工具同时抽真空从而形成纤维物体; 将粘合剂(c),例如以喷雾的形式递送到所述纤维物体; 熔化或固化所述粘合剂(d),例如通过施加热或紫外线来制成纤维垫(51,52,53); 优选地在实质上不存在切割或其它机械改性的情况下将多个所述纤维垫(51,52,53)和另外的粘合剂组装成预成型件(e)的形状; 并将所得的垫组件(f)热压成成品厚的预成型件(55)。