中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

40 records (took 0.023 seconds)

    HEAT INSULATING BLANKET
    21.
    发明申请
    HEAT INSULATING BLANKET 审中-公开
    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

    Applicant: HEXCEL CORPORATION

    Inventor： HEXCEL CORPORATION ,  FELL, Barry, M. ,  CIRISCIOLI, Peter, R.

    IPC: B32B01/00

    CPC classification number: 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

    Abstract: 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.

    COMPOSITION OF MATERIALS FOR RETENTION ELEMENTS AND PLATES BASED ON SAID COMPOSITION
    22.
    发明申请
    COMPOSITION OF MATERIALS FOR RETENTION ELEMENTS AND PLATES BASED ON SAID COMPOSITION 审中-公开
    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

    Applicant: HEXCEL CORPORATION ,  LIEGEOIS, Jean-Marie

    Inventor： HEXCEL CORPORATION

    IPC: A61L15/07

    CPC classification number: A61L15/07 ,  C08L67/04 ,  C08L2666/04

    Abstract: 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.

    Abstract translation: 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％。

    QUICK FIT OVERHEAD STOWAGE COMPARTMENT
    23.
    发明申请
    QUICK FIT OVERHEAD STOWAGE COMPARTMENT 审中-公开
    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

    Applicant: HEXCEL CORPORATION

    Inventor： HEXCEL CORPORATION ,  SPENCER, Martin, C.

    IPC: B64D47/00

    CPC classification number: B64D11/003

    Abstract: 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.

    Abstract translation: 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。

    HIGH THERMAL CONDUCTIVITY NON-METALLIC HONEYCOMB WITH OPTIMUM PITCH FIBER ANGLE
    26.
    发明申请
    HIGH THERMAL CONDUCTIVITY NON-METALLIC HONEYCOMB WITH OPTIMUM PITCH FIBER ANGLE 审中-公开
    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

    Applicant: HEXCEL CORPORATION

    Inventor： HEXCEL CORPORATION ,  DARFLER, Stephen, C.

    IPC: B32B03/12

    CPC classification number: 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

    Abstract: 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.

    Abstract translation: 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。

    POLYMERIC CERAMIC BINDER COMPOSITIONS
    29.
    发明申请
    POLYMERIC CERAMIC BINDER COMPOSITIONS 审中-公开
    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

    Applicant: HEXCEL CORPORATION

    Inventor： HEXCEL CORPORATION ,  HAN, Jong, Hoon

    IPC: C08L33/04

    CPC classification number: C04B35/63404 ,  C04B35/634 ,  C04B35/63424 ,  C04B35/63448 ,  C08K5/0025 ,  C08K5/103 ,  C08L33/12

    Abstract: 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.

    Abstract translation: 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。

Patent Agency Ranking