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21. 发明申请

WO1990002621A1 COMPOSITIONS AND PROCESS FOR PRODUCING FOAM PLASTICS 审中-公开
标题翻译：用于生产泡沫塑料的组合物和方法
公开(公告)号：WO1990002621A1
公开(公告)日：1990-03-22
申请号：PCT/US1989003889
申请日：1989-09-08
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , KUO, Ching-Chi , ROBERTSON, Mark , LEE, Kyu, Wang
IPC分类号： B23B03/26
CPC分类号： C08J9/02 , C08J9/06 , C08J2333/02
摘要： Plastic foam materials having a high degree of structural integrity, cell network uniformity and small cell size are obtained from (meth)acrylic acid and (meth)acrylonitrile by incorporating acrylamide as a comonomer additive within certain ranges of concentration. Incorporation of the latter together with conventional additives normally used in preparing foams from the principal monomers helps to avoid preliminary precipitation during the polymerization process, and the gradients in the polymer microstructure which frequently result and cause internal stresses and weaknesses in the ultimate product.

22. 发明申请

WO1988006969A1 METHOD FOR MULTIPLE-END-CLOSE-SET UNIFORM DENSITY PARALLEL WEFT INSERTION AND PRODUCTS THEREOF 审中-公开
标题翻译：多端封闭均匀密度平行插入方法及其产品
公开(公告)号：WO1988006969A1
公开(公告)日：1988-09-22
申请号：PCT/US1988000674
申请日：1988-03-09
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , VEES, Frederick , FIEDLER, Michael, T.
IPC分类号： B32B03/06
CPC分类号： D04H3/04 , Y10T428/24033 , Y10T428/24132 , Y10T428/249924
摘要： A multiple-end weft-insertion process which is capable of achieving extremely high yarn density which is uniform in plys of structural fabrics is disclosed, making use of conventional machinery and systems. Yarn (104) is transferred from a shuttle (100) to yarn transfer elements (108) spaced a sufficient distance apart to avoid damage to the yarn, and then transferred to yarn holding elements (110). Each successive pass of the shuttle is adjusted by moving the yarn transfer element parallel to the holding elements, so as to overlap each band deposited by the shuttle. The amount of movement necessary to achieve any desired density is calculated according to established parameters.

23. 发明申请

WO1983003796A1 HEAT INSULATING BLANKET 审中-公开
标题翻译：保温隔热垫
公开(公告)号：WO1983003796A1
公开(公告)日：1983-11-10
申请号：PCT/US1983000646
申请日：1983-05-02
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , FELL, Barry, M. , CIRISCIOLI, Peter, R.
IPC分类号： B32B01/00
CPC分类号： B32B5/26 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/105 , B32B2262/106 , B32B2307/304 , B32B2363/00 , B32B2379/08 , E04B1/941 , F02C7/25 , F02K1/822 , Y02T50/672 , Y02T50/675 , Y10S428/92 , Y10T428/1314 , Y10T428/24785 , Y10T442/3488 , Y10T442/3724
摘要： A blanket (10) formed of heat and flame resistant materials and adapted to be placed adjacent to a structural part (24) to isolate it thermally from other, adjacent structural parts (22). The blanket (10) is comprised of a layer (12) of insulation material coupled to a layer (18) of fibrous material impregnated with a thermosetting resin. When the blanket (10) is in a desired shape, the resin is cured to render the layer (18) of fibrous material substantially rigid so it can support itself as well as the layer (12) of insulating material coupled to it. Layers (14) and (16) of glass fabric are placed on opposed sides of the layer (12) of insulating material to keep the insulating material intact. In one application, the blanket (10) is molded in the form of a box-like structure which can at least partially surround a structural part, such as an aircraft engine (24), to form a fireshield to isolate the engine (24) from adjacent structural partsof an aircraft. In another application, the resin-impregnated layer (18) of fibrous material of the blanket (10) is placed adjacent to one surface of a structural part and bonded thereto during the curing of the resin to thereby form a fireshield attached to the structural part. In a third application, the resin-impregnated layer (18) of fibrous material is used without the layer (12) of insulating material and, when the resin is cured, the layer (18) is rigid and forms a box-like structure for at least a partially enclosing a structural part.

24. 发明申请

WO1983002898A1 COMPOSITION OF MATERIALS FOR RETENTION ELEMENTS AND PLATES BASED ON SAID COMPOSITION 审中-公开
标题翻译：基于组合物的保留元素和板材的组成
公开(公告)号：WO1983002898A1
公开(公告)日：1983-09-01
申请号：PCT/BE1983000005
申请日：1983-02-23
申请人： HEXCEL CORPORATION , LIEGEOIS, Jean-Marie
发明人： HEXCEL CORPORATION
IPC分类号： A61L15/07
CPC分类号： A61L15/07 , C08L67/04 , C08L2666/04
摘要： A composition particularly appropriate for retention materials, prints for external prostheses or other fixing elements, is comprised of 90 to 60 parts by weight of a cyclic ester polymer having a molecular weight comprised between 20000 and 300000 and 10 to 40 parts by weight of ethylene copolymer-vinyl acetate having a viscosity index comprised between 0.5 and 12 and having a vinyl acetate content from 10 to 60 % by weight.
摘要翻译：特别适用于保留材料的组合物，用于外部假体或其他固定元件的印刷品由90至60重量份的分子量为20000至300000的环酯聚合物和10至40重量份的乙烯共聚物乙酸乙烯酯，其粘度指数为0.5-12，乙酸乙烯酯含量为10至60重量％。

25. 发明申请

WO1998038089A1 QUICK FIT OVERHEAD STOWAGE COMPARTMENT 审中-公开
标题翻译：快速搭便车
公开(公告)号：WO1998038089A1
公开(公告)日：1998-09-03
申请号：PCT/US1997003058
申请日：1997-02-28
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , SPENCER, Martin, C.
IPC分类号： B64D47/00
CPC分类号： B64D11/003
摘要： A removable stowage bin assembly (10) for quick conversion of an aircraft between a passenger-carrying mode and a cargo-carrying mode includes a stowage bin (14) and a first assembly comprised of a clevis fitting (32) attached to the framework of the aircraft (48) and a hook (34) attached to the stowage bin (14), the hook (34) being removably and pivotally attachable to the clevis fitting (32). A second assembly is comprised of a tie rod (54) having a first end pivotally attached to the framework of the aircraft (48) and a bracket (62) attached to the stowage bin (14). The tie rod (54) has a second end attachable to the framework of the aircraft (48) in a cargo-carrying mode. A third assembly is comprised of a female fitting (79) having an opening and attached to one of the framework of the aircraft (48) and the stowage bin (14), and a male fitting (84) having a protrusion and attached to the other end of the framework of the aircraft (48) and the stowage bin (14). The protrusion of the male fitting (84) is mateable in the opening of the female fitting (79) in the passenger-carrying mode.
摘要翻译：一种用于在乘客运载模式和货物运载模式之间快速转换飞机的可移动的存放箱组件（10）包括一个装载箱（14）和一个第一组件，该组合件包括一个U形夹配件（32）所述飞机（48）和附接到所述装载箱（14）的钩（34），所述钩（34）可拆卸地且可枢转地附接到所述U形夹配件（32）。第二组件包括具有枢转地附接到飞行器（48）的框架的第一端和连接到装载箱（14）的支架（62）的拉杆（54）。连杆（54）具有可以货物运送模式附接到飞行器（48）的框架的第二端。第三组件包括具有开口并连接到飞行器（48）的框架和收纳箱（14）中的一个的阴配件（79），以及具有突出部并附接到所述插座的阳配件（84）飞机（48）和储物箱（14）的框架的另一端。阳型配件（84）的突出部可以在乘客携带模式下在阴配件（79）的开口中配合。

26. 发明申请

WO1995011128A1 HIGH THERMAL CONDUCTIVITY TRIAXIAL NON-METALLIC HONEYCOMB 审中-公开
标题翻译：高热导率三元非金属蜂窝
公开(公告)号：WO1995011128A1
公开(公告)日：1995-04-27
申请号：PCT/US1994011329
申请日：1994-10-05
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , DARFLER, Stephen, C. , AHLSTROM, Carla , CALDWELL, Mark
IPC分类号： B32B03/12
CPC分类号： B32B3/12 , B29C70/083 , B29C70/88 , B29K2105/0845 , B29K2707/04 , B29K2995/0013 , B29L2031/608 , B32B2260/023 , B32B2260/046 , B32B2305/024 , B32B2307/302 , E04C2/365 , Y10S428/902 , Y10T428/24149 , Y10T428/24165
摘要： A non-metallic honeycomb structure (10) wherein the thermal conductivity of the structure is increased by incorporating high thermal conductivity pitch-based carbon fibers (20) into the non-metallic resin matrix. In addition to increasing thermal conductivity, the pitch-based carbon fibers (20) are utilized to provide controlled directional heat conductance through the honeycomb structure (10).
摘要翻译：一种非金属蜂窝结构（10），其中通过将高导热率沥青基碳纤维（20）并入非金属树脂基体中而增加了该结构的导热性。除了增加导热性之外，沥青基碳纤维（20）用于通过蜂窝结构（10）提供受控的定向热传导。

27. 发明申请

WO1995010412A1 HIGH THERMAL CONDUCTIVITY NON-METALLIC HONEYCOMB WITH OPTIMUM PITCH FIBER ANGLE 审中-公开
标题翻译：高导热性非金属蜂窝状电极
公开(公告)号：WO1995010412A1
公开(公告)日：1995-04-20
申请号：PCT/US1994011373
申请日：1994-10-05
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , DARFLER, Stephen, C.
IPC分类号： B32B03/12
CPC分类号： B32B3/12 , B29C70/08 , B29K2105/101 , B29K2307/00 , B29K2995/0013 , B29K2995/0015 , B29L2031/608 , B32B2260/023 , B32B2260/046 , B32B2305/024 , B32B2307/302 , Y10S428/902 , Y10T428/24149 , Y10T428/24165 , Y10T428/2918
摘要： A non-metallic honeycomb structure (10) wherein the thermal conductivity of the structure is increased by incorporating high thermal conductivity pitch-based carbon fibers (82) into the non-metallic resin matrix. In addition to increasing thermal conductivity, the pitch-based carbon fibers (82) are utilized to provide controlled directional heat conductance through the honeycomb structure (10). In one preferred embodiment, the pitch-based fibers (82) are oriented to extend at an angle of plus or minus 55 to 60 degrees relative to the lengthwise direction of the honeycomb structure to provide optimum performance characteristics at a reduced cost.
摘要翻译：一种非金属蜂窝结构体（10），其中通过在所述非金属树脂基体中引入高导热率沥青基碳纤维（82）来增加所述结构的导热性。除了增加导热性之外，沥青基碳纤维（82）用于通过蜂窝结构（10）提供受控的定向热传导。在一个优选实施例中，基于沥青的纤维（82）被定向成相对于蜂窝结构体的长度方向以正负55至60度的角度延伸，以降低成本提供最佳的性能特征。

28. 发明申请

WO1995010411A1 HIGH THERMAL CONDUCTIVITY NON-METALLIC HONEYCOMB WITH LAMINATED CELL WALLS 审中-公开
标题翻译：高导热性非金属蜂窝状电解槽与层状电解槽
公开(公告)号：WO1995010411A1
公开(公告)日：1995-04-20
申请号：PCT/US1994011372
申请日：1994-10-05
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , DARFLER, Stephen, C.
IPC分类号： B32B03/12
CPC分类号： B32B3/12 , A61K9/2018 , A61K9/2886 , A61K9/5073 , B29C70/08 , B29K2105/101 , B29K2307/00 , B29K2995/0013 , B29L2031/608 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2305/024 , B32B2307/302 , Y10T428/24149 , Y10T428/24165 , Y10T428/2918
摘要： A non-metallic honeycomb structure (10) wherein the thermal conductivity of the structure is increased by incorporating high thermal conductivity pitch-based carbon fibers (20) into the non-metallic resin matrix. In addition to increasing thermal conductivity, the pitch-based carbon fibers (20) are utilized to provide controlled directional heat conductance through the honeycomb structure. In a preferred exemplary embodiment, the cell walls (80) are formed from a plurality of non-metallic unidirectional fabric layers (82, 84, 86), at least one of which consists essentially of unidirectionally oriented high thermal conductivity fibers.
摘要翻译：一种非金属蜂窝结构（10），其中通过将高导热率沥青基碳纤维（20）并入非金属树脂基体中而增加了该结构的导热性。除了增加导热性之外，沥青基碳纤维（20）用于通过蜂窝结构提供受控的定向热传导。在优选的示例性实施例中，细胞壁（80）由多个非金属单向织物层（82,84,86）形成，其中至少一个基本上由单向取向的高导热性纤维构成。

29. 发明申请

WO1994016656A1 HIGH MODULUS FIBER PROTECTIVE CARRIER SYSTEMS AND METHODS FOR THEIR USE 审中-公开
标题翻译：高模块光纤保护载波系统及其使用方法
公开(公告)号：WO1994016656A1
公开(公告)日：1994-08-04
申请号：PCT/US1994000856
申请日：1994-01-21
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , CHRISTENSEN, Don, Coy , CUSTER, Milton, F.
IPC分类号： A61F13/02
CPC分类号： D04H3/04 , B32B3/266 , B32B5/00 , B32B5/02 , B32B5/024 , B32B7/06 , B32B7/12 , B32B15/14 , B32B19/04 , B32B27/12 , B32B27/36 , B32B37/203 , B32B38/1875 , B32B2037/268 , B32B2250/05 , B32B2255/02 , B32B2255/28 , B32B2260/021 , B32B2260/04 , B32B2262/0276 , B32B2262/10 , B32B2307/306 , B32B2307/412 , B32B2307/546 , B32B2307/558 , B32B2307/72 , B32B2307/732 , B32B2405/00 , B32B2571/00 , Y10S428/903 , Y10T428/24091 , Y10T428/24124 , Y10T428/2848 , Y10T428/31786
摘要： A composite pre-slit tape useful as a protective carrier system for storing and handling high modulus fibers and processes for protecting such fibers are disclosed. An exemplary composite pre-slit tape (12) includes a plurality of generally elongated and collimated pre-slit laminates (28, 30, 32) oriented in a single plane and releasably bonded to a removable continuous backing layer (33) which is in the form of a long thin tape. Each pre-slit laminate includes an adhesive layer (34) located adjacent the continuous backing layer and a fiber supporting layer (36) located adjacent the adhesive layer (34). In use as a fiber protective carrier (10), each pre-slit laminate (28, 30) is bonded to a fiber bundle (22, 24) of a plurality of collimated fibers (14, 16, 18, 20) arranged in a single layer. Each fiber (14, 16, 18, 20) is bonded along its length to the supporting layer (36) of the pre-slit laminate (28, 30). The combination of secured fibers and pre-slit laminate can be fed directly to a loom for forming woven fabric.
摘要翻译：公开了一种用作保存和处理高模量纤维的保护载体系统和用于保护这种纤维的方法的复合预切割带。示例性的复合预切割带（12）包括多个大致细长且准直的预切割层压板（28,30,32），其定向在单个平面中并且可释放地结合到可移除的连续背衬层（33）形式长薄薄带。每个预切割层压体包括位于连续背衬层附近的粘合剂层（34）和邻近粘合剂层（34）定位的纤维支撑层（36）。在作为纤维保护载体（10）使用时，每个预切割层压体（28,30）被结合到多个平行光纤（14,16,18,20）的纤维束（22,24）单层。每个纤维（14,16,18,20）沿着其长度被结合到预切层压板（28,30）的支撑层（36）上。固定纤维和预切层压板的组合可以直接进料到用于形成织物的织机上。

30. 发明申请

WO1992022509A1 POLYMERIC CERAMIC BINDER COMPOSITIONS 审中-公开
标题翻译：聚合物陶瓷组合物
公开(公告)号：WO1992022509A1
公开(公告)日：1992-12-23
申请号：PCT/US1992005044
申请日：1992-06-10
申请人： HEXCEL CORPORATION
发明人： HEXCEL CORPORATION , HAN, Jong, Hoon
IPC分类号： C08L33/04
CPC分类号： C04B35/63404 , C04B35/634 , C04B35/63424 , C04B35/63448 , C08K5/0025 , C08K5/103 , C08L33/12
摘要： Ceramic binder compositions used in ceramic formulations for molding ceramic parts are disclosed. The ceramic binder compositions are solutions of at least one polymer, at least one reactive monomer, solvent, and initiator. When the ceramic binder solutions are combined with ceramic raw materials, the resulting ceramic formulations have exceptional tack and drape properties which make them useful for molding large and intricately shaped three dimensional ceramic green parts. The green parts can be set using conventional polymeric processing techniques and have improved strengths.
摘要翻译：公开了用于模制陶瓷部件的陶瓷配方中使用的陶瓷粘合剂组合物。陶瓷粘合剂组合物是至少一种聚合物，至少一种反应性单体，溶剂和引发剂的溶液。当陶瓷粘合剂溶液与陶瓷原料结合时，所得到的陶瓷配方具有卓越的粘性和悬垂性能，使其可用于模制大而复杂的三维陶瓷绿色部件。绿色部件可以使用常规聚合物加工技术设置并具有改进的强度。

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