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1. 发明授权

US07431978B2 Reinforced matrix composite containment duct 有权
标题翻译：钢筋基复合材料防渗管
公开(公告)号：US07431978B2
公开(公告)日：2008-10-07
申请号：US11021805
申请日：2004-12-22
申请人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Warren Rosal Ronk
发明人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Warren Rosal Ronk
IPC分类号： D04H13/00 , D04H5/00
CPC分类号： F01D21/045 , B29C70/465 , B29L2031/7504 , F05D2300/614 , F05D2300/702 , Y02T50/672 , Y10T428/249924
摘要： A reinforced matrix composite containment duct for gas turbine engines comprising a reinforced matrix composite containment duct having high strength integral flanges and pre-stressed reinforcing fibers, the reinforced matrix composite having uniform distribution of matrix material; and the reinforced matrix composite having less than or equal to 2.5% void space.
摘要翻译：一种用于燃气涡轮发动机的增强基体复合容纳管，其包括具有高强度整体凸缘和预应力增强纤维的增强基体复合容纳管，所述增强基体复合材料具有均匀的基体材料分布; 和具有小于或等于2.5％空隙空间的增强基质复合材料。

2. 发明授权

US07335012B2 Apparatus for fabricating reinforced composite materials 有权
标题翻译：用于制造增强复合材料的装置
公开(公告)号：US07335012B2
公开(公告)日：2008-02-26
申请号：US11021893
申请日：2004-12-22
申请人： Lee Alan Blanton , Gregory Joseph Meibers , Stephen Mark Whiteker , Matthew Bernard Buczek , Robert Paul Fairbanks , Richard Thomas Price
发明人： Lee Alan Blanton , Gregory Joseph Meibers , Stephen Mark Whiteker , Matthew Bernard Buczek , Robert Paul Fairbanks , Richard Thomas Price
IPC分类号： B28B21/36
CPC分类号： B29C70/446 , B29C33/48 , B29C70/548 , B29L2031/7504
摘要： A mold tool for forming a reinforced matrix composite part for a gas turbine engine, comprising a body. The body comprises a body surface capable of receiving a first portion of a composite preform. A first endplate and second endplate are attached to the body and include a substantially planar surface disposed perpendicular to the body surface. A first and second set of plates are attached to the first and second endplate adjacent to the body surface and have a geometries that includes a first and second cavity bounded by the first and second plate and first and second endplate. The first and second cavities have a volume sufficient to receive a second portion of a composite preform. The second cavity is in fluid communication with the first cavity, which is in fluid communication with a vacuum source.
摘要翻译：一种用于形成用于燃气涡轮发动机的增强基体复合部件的模具，包括主体。主体包括能够接收复合预型件的第一部分的主体表面。第一端板和第二端板附接到主体并且包括垂直于主体表面设置的基本平坦的表面。第一组和第二组板邻近身体表面附接到第一和第二终板，并具有包括由第一和第二板以及第一和第二终板限定的第一和第二腔的几何形状。第一和第二空腔具有足以容纳复合预制件的第二部分的体积。第二腔与第一空腔流体连通，第一空腔与真空源流体连通。

3. 发明申请

US20080160122A1 Continuous debulking systems 审中-公开
标题翻译：连续减压系统
公开(公告)号：US20080160122A1
公开(公告)日：2008-07-03
申请号：US11646767
申请日：2006-12-28
申请人： Lee Alan Blanton , Curt Brian Curtis , David Scott Miller , Robert Paul Fairbanks
发明人： Lee Alan Blanton , Curt Brian Curtis , David Scott Miller , Robert Paul Fairbanks
IPC分类号： C03C25/10
CPC分类号： B29C70/32 , B29C35/02 , B29C35/16 , B29C53/562 , B29C53/566 , B29C53/585 , B29C53/8075 , B29K2063/00 , B29K2079/08
摘要： Continuous debulking systems including in combination a spool for providing a fabric, a heating apparatus for heating the fabric as the fabric is unrolled from the spool to produce a heated fabric, a composite structure forming tool for wrapping the heated fabric thereabout, a resin applicator for applying resin to the heated fabric as the heated fabric is wrapped about the composite structure forming tool to produce a resin rich fabric surface to which a subsequent ply of heated fabric is applied to produce an impregnated composite material, and a pressure roller for concurrently debulking and cooling the impregnated composite material to produce a composite structure preform.
摘要翻译：连续减粘系统包括组合用于提供织物的卷轴，用于当织物从卷轴展开以加热织物以加热织物以产生加热织物的加热装置，用于在其周围包裹加热的织物的复合结构形成工具，用于当加热的织物围绕复合结构形成工具缠绕以产生富含树脂的织物表面时，将树脂施加到加热的织物上，随后加热的织物的层被施加到其上以产生浸渍的复合材料，以及压力辊，用于同时减压和冷却浸渍的复合材料以产生复合结构预制件。

4. 发明授权

US07867566B2 Method for fabricating reinforced composite materials 失效
标题翻译：制造增强复合材料的方法
公开(公告)号：US07867566B2
公开(公告)日：2011-01-11
申请号：US11925331
申请日：2007-10-26
申请人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
发明人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
IPC分类号： B05D3/00 , B05D3/12
CPC分类号： B29C70/546 , B29C70/44 , B29C70/465 , B29L2031/7504 , F01D21/045 , F05D2300/614 , F05D2300/702 , Y02T50/672 , Y10T428/249928 , Y10T428/249933 , Y10T428/24994 , Y10T428/249944
摘要： A method for fabricating a reinforced matrix composite comprising the step of providing a composite preform having a fibrous structure and applying matrix material onto the preform in locations along the preform. A barrier material is applied to at least a portion of the coated preform to direct the flow of matrix material into the preform. The composite preform is heated to a temperature sufficient to render the matrix material viscous and insufficient to cure the matrix material. The pressure to the interior of the composite preform is reduced, while the pressure to the barrier material is increased. The temperature is maintained to flow the matrix material into the composite preform and to force gases from the fibrous structure. The composite preform is then cured and cooled to form a reinforced matrix composite having a low void content and a substantially uniform matrix distribution.
摘要翻译：一种用于制造增强基质复合材料的方法，包括提供具有纤维结构的复合预型件并将基体材料施加到预制件上的预型件沿着预制件的位置的步骤。将阻挡材料施加到涂覆预型件的至少一部分以将基体材料流引导到预成型件中。将复合预制件加热到足以使基质材料粘稠并且不足以固化基质材料的温度。对复合预制件内部的压力降低，同时对阻挡材料的压力增加。保持温度以使基质材料流入复合预制件并迫使来自纤维结构的气体。然后将复合预成型件固化并冷却以形成具有低空隙含量和基本均匀的基体分布的增强基质复合材料。

5. 发明申请

US20090142496A1 METHOD FOR FABRICATING REINFORCED COMPOSITE MATERIALS 失效
标题翻译：用于制备增强复合材料的方法
公开(公告)号：US20090142496A1
公开(公告)日：2009-06-04
申请号：US11925331
申请日：2007-10-26
申请人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
发明人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
IPC分类号： B05D3/00
CPC分类号： B29C70/546 , B29C70/44 , B29C70/465 , B29L2031/7504 , F01D21/045 , F05D2300/614 , F05D2300/702 , Y02T50/672 , Y10T428/249928 , Y10T428/249933 , Y10T428/24994 , Y10T428/249944
摘要： A method for fabricating a reinforced matrix composite comprising the step of providing a composite preform having a fibrous structure and applying matrix material onto the preform in locations along the preform. A barrier material is applied to at least a portion of the coated preform to direct the flow of matrix material into the preform. The composite preform is heated to a temperature sufficient to render the matrix material viscous and insufficient to cure the matrix material. The pressure to the interior of the composite preform is reduced, while the pressure to the barrier material is increased. The temperature is maintained to flow the matrix material into the composite preform and to force gases from the fibrous structure. The composite preform is then cured and cooled to form a reinforced matrix composite having a low void content and a substantially uniform matrix distribution.
摘要翻译：一种用于制造增强基质复合材料的方法，包括提供具有纤维结构的复合预型件并将基体材料施加到预制件上的预型件沿着预制件的位置的步骤。将阻挡材料施加到涂覆预型件的至少一部分以将基体材料流引导到预成型件中。将复合预制件加热到足以使基质材料粘稠并且不足以固化基质材料的温度。对复合预制件内部的压力降低，同时对阻挡材料的压力增加。保持温度以使基质材料流入复合预制件并迫使来自纤维结构的气体。然后将复合预成型件固化并冷却以形成具有低空隙含量和基本均匀的基体分布的增强基质复合材料。

6. 发明授权

US07332049B2 Method for fabricating reinforced composite materials 失效
标题翻译：制造增强复合材料的方法
公开(公告)号：US07332049B2
公开(公告)日：2008-02-19
申请号：US11021804
申请日：2004-12-22
申请人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
发明人： Lee Alan Blanton , Gregory Joseph Meibers , Robert Paul Fairbanks , Stephen Mark Whiteker , Richard Thomas Price , Matthew Bernard Buczek , Warren Rosal Ronk
IPC分类号： B32B37/00 , B22D19/00
CPC分类号： B29C70/546 , B29C70/44 , B29C70/465 , B29L2031/7504 , F01D21/045 , F05D2300/614 , F05D2300/702 , Y02T50/672 , Y10T428/249928 , Y10T428/249933 , Y10T428/24994 , Y10T428/249944
摘要： A method for fabricating a reinforced matrix composite comprising the step of providing a composite preform having a fibrous structure and applying matrix material onto the preform in locations along the preform. A barrier material is applied to at least a portion of the coated preform to direct the flow of matrix material into the preform. The composite preform is heated to a temperature sufficient to render the matrix material viscous and insufficient to cure the matrix material. The pressure to the interior of the composite preform is reduced, while the pressure to the barrier material is increased. The temperature is maintained to flow the matrix material into the composite preform and to force gases from the fibrous structure. The composite preform is then cured and cooled to form a reinforced matrix composite having a low void content and a substantially uniform matrix distribution.
摘要翻译：一种用于制造增强基质复合材料的方法，包括提供具有纤维结构的复合预型件并将基体材料施加到预制件上的预型件沿着预制件的位置的步骤。将阻挡材料施加到涂覆预型件的至少一部分以将基体材料流引导到预成型件中。将复合预制件加热到足以使基质材料粘稠并且不足以固化基质材料的温度。对复合预制件内部的压力降低，同时对阻挡材料的压力增加。保持温度以使基质材料流入复合预制件并迫使来自纤维结构的气体。然后将复合预成型件固化并冷却以形成具有低空隙含量和基本均匀的基体分布的增强基质复合材料。

7. 发明申请

US20080156419A1 Continuous debulking methods 审中-公开
标题翻译：连续减压方法
公开(公告)号：US20080156419A1
公开(公告)日：2008-07-03
申请号：US11646796
申请日：2006-12-28
申请人： Lee Alan Blanton , Curt Brian Curtis , David Scott Miller , Robert Paul Fairbanks
发明人： Lee Alan Blanton , Curt Brian Curtis , David Scott Miller , Robert Paul Fairbanks
IPC分类号： C03C25/10
CPC分类号： B29C70/32 , B29C35/02 , B29C35/16 , B29C53/562 , B29C53/566 , B29C53/585 , B29C53/8075 , B29K2063/00 , B29K2079/08
摘要： Continuous debulking methods involving providing a spool of fabric, heating the fabric to produce a heated fabric while concurrently transferring the heated fabric to a composite structure forming tool, wrapping the heated fabric about the composite structure forming tool, applying resin to the heated fabric to obtain a resin rich fabric surface, applying a subsequent ply of heated fabric to the resin rich fabric surface to obtain an impregnated composite material, and debulking and cooling the impregnated composite to obtain a composite structure preform.
摘要翻译：连续减粘方法包括提供织物卷轴，加热织物以产生加热的织物，同时将加热的织物转移到复合结构形成工具，将加热的织物缠绕在复合结构形成工具上，将树脂施加到加热的织物上以获得树脂丰富的织物表面，将随后的加热织物层施加到富含树脂的织物表面上，以获得浸渍的复合材料，并对浸渍的复合材料进行减压和冷却以获得复合结构预制件。

8. 发明授权

US06551678B1 Deep embossed tile design postformable high pressure decorative laminate and method for producing same 有权
标题翻译：深压花瓦设计可成形高压装饰层压板及其制造方法
公开(公告)号：US06551678B1
公开(公告)日：2003-04-22
申请号：US09414937
申请日：1999-10-09
申请人： Kevin Francis O'Brien , Robert Paul Fairbanks , Kenneth Allan Nilsson
发明人： Kevin Francis O'Brien , Robert Paul Fairbanks , Kenneth Allan Nilsson
IPC分类号： B32B330
CPC分类号： B44C1/24 , B44C5/0469 , Y10T156/1039 , Y10T156/1044 , Y10T428/16 , Y10T428/161 , Y10T428/24479 , Y10T428/24521 , Y10T428/24537 , Y10T428/2457
摘要： A deep embossed high pressure decorative laminate having a plurality of integral tiles with various surface textures bordered by deep embossed portions. Each tile of the laminate has a peripheral thickness greater than the thickness of the non-peripheral portions of the tile. Preferably, each tile has a concave profile along its upper surface when viewed in cross section. A method of producing artwork necessary for the deep embossed high pressure decorative laminate of the present invention comprises assembling a first layer of fibrous sheets impregnated with a thermosetting resin, a second layer comprising a plurality of adjacent tiles comprising a plurality of fibrous sheets impregnated with a thermosetting resin, wherein the tiles were previously pressed and heated, and a third layer comprising a plurality of shims. The assembly is then pressed and heated against a rigid substrate whereby the second layer forms a substantially convex shape on the upper surface of each tile, thus imparting substantially concave impressions on the first layer. The first layer is subsequently removed from the second and third layers, and grooves are formed in the first layer, preferably by machining.
摘要翻译：深压花高压装饰层压板，其具有多个具有与深压花部分相邻的各种表面纹理的整体瓦片。层压体的每个瓷砖的周边厚度大于瓷砖的非周边部分的厚度。优选地，当在横截面中观察时，每个瓦片沿其上表面具有凹形轮廓。本发明的深压花高压装饰层压板所需的生产艺术品的方法包括组装浸渍有热固性树脂的第一层纤维片，第二层包括多个相邻的瓷砖，所述第二层包括多个浸渍有热固性树脂，其中预先压制和加热瓦片，以及包括多个垫片的第三层。然后将组件按压并加热抵靠刚性基板，由此第二层在每个瓦片的上表面上形成基本上凸起的形状，从而在第一层上施加基本上凹的印模。随后从第二层和第三层移除第一层，优选通过机械加工在第一层中形成槽。

9. 发明授权

US06106646A Method for joining composite materials 失效
标题翻译：复合材料接合方法
公开(公告)号：US06106646A
公开(公告)日：2000-08-22
申请号：US265971
申请日：1994-06-27
申请人： Robert Paul Fairbanks
发明人： Robert Paul Fairbanks
IPC分类号： B29C65/62 , B29C70/24 , B29C70/54 , B32B31/18 , B32B31/26
CPC分类号： B29C65/7443 , B26F1/24 , B29C65/08 , B29C65/7437 , B29C66/721 , B29C66/8322 , B29C70/24 , B29C70/543 , B29C70/545 , B26D7/086 , B29C2793/0045 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29L2009/00 , Y10T156/1057
摘要： A plurality of layers of nonfully cured composite material are joined by a unique combination of steps including debulking and precuring the layers using vacuum followed by pressure and heating. Then spaced apart holes through the layers are generated with a pointed tool using ultrasonic energy which at least softens and smooths the hole wall. The layers are stitched through the holes prior to final curing.
摘要翻译：多层非固化复合材料通过独特的步骤组合连接在一起，包括减压，并使用真空随后进行加压和加热来预固化层。然后通过使用超声能量的尖锐工具产生穿过层的间隔开的孔，其至少使孔壁软化和平滑。在最终固化之前，这些层被缝合穿过孔。

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