会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 5. 发明公开
    • Method for manufacturing a foil laminate with a defined curvature and foil laminate obtained therewith
    • 一种用于具有一定曲率生产层压处理过程,因此产生的层压板
    • EP0822061A1
    • 1998-02-04
    • EP97202309.7
    • 1997-07-24
    • SALLMETALL B.V.
    • Reinders, Johannes Antonius Maria
    • B32B1/10B32B31/08B32B15/08
    • B32B15/09B32B7/12B32B15/20B32B27/36B32B37/00B32B37/144B32B37/206B32B38/1866B32B2309/105B32B2311/24B32B2367/00
    • A method for manufacturing a foil laminate with a defined curvature comprises the following steps of:

      providing an encapsulating device comprising:

      transporting means for carrying a carrier foil through the device;
      first supply means for supplying to the carrier foil a first skin laminate such that the glue layer forming part thereof is brought into contact with the first surface of the carrier foil;
      second supply means for supplying to the other side of the carrier foil a second skin laminate such that the glue layer forming part thereof is brought into contact with the second surface of the carrier foil; and
      pressing means comprising a pinch for exerting a pressure force on the stack passing through and consisting of the first skin laminate, the carrier foil and the second skin laminate; and

      controlling the first and the second supply means such that the first and the second skin laminates are each introduced into said pinch at a chosen tensile stress such that the skin laminates of the resulting laminate leaving the pinch which are mutually adhered via the carrier foil have respective tensions and in the free state the laminate has a curvature corresponding therewith.
    • 一种制造箔层压片具有限定的曲率方法包括以下步骤:在封装装置,其包括提供:输送装置,用于承载通过该器件的载体箔; 第一供料装置供给到所述载体箔检查的第一层压体的皮肤没有胶水层形成其一部分被带入与所述载体箔的第一表面接触; 第二供给装置,用于提供到所述载体的另一侧箔检查第二表层层叠体没有胶水层形成其一部分被带入与载体箔的第二表面接触; 和加压装置包括一个夹送堆栈上施加压力,通过与所述第一皮肤层叠体中,载体箔和第二皮肤层压由......组成; 和控制所述第一和第二供给装置检查做的第一和第二皮肤层压材料各自引入所述夹紧在检查所选择的拉伸应力所做的所得层压板的皮肤层压材料离开它们通过载体箔具有相互粘附的夹 respectivement张力和在自由状态下的层叠体具有曲率与对应那里。
    • 8. 发明公开
    • Moulding thermal insulation
    • 正式einerWärmeisolierung。
    • EP0297739A1
    • 1989-01-04
    • EP88305210.2
    • 1988-06-08
    • MICROPORE INTERNATIONAL LIMITED
    • Hughes, John Thomas
    • B32B1/10B29C43/00B32B31/20
    • B30B15/065B29C33/10B30B15/0017
    • Shaped pieces (14) of thermal insulation material are moulded in a mould assembly which incorporates a press tool (1) comprising a plurality of elements (2) secured together. Each element (2) defines a portion of the shaped piece of thermal insulation material to be produced and at least one element includes means permitting the escape of air through the press tool, for example the provision of grooves (3) or by making the element of a porous material. A predetermined amount of loose particulate thermal insulation material (13) is charged into the mould and is compressed with excess air escaping through the press tool (1). A compacted shaped piece of thermal insulation material (14) is formed which is removed from the mould.
    • 隔热材料的成型件(14)被模制在一个模具组件中,该模具组件包括一个包括固定在一起的多个元件(2)的冲压工具(1)。 每个元件(2)限定待制造的成型件的绝热材料的一部分,并且至少一个元件包括允许空气通过冲压工具逃逸的装置,例如提供槽(3)或通过使元件 的多孔材料。 将预定量的松散颗粒保温材料(13)装入模具中,并通过压制工具(1)逸出的多余空气被压缩。 形成压实成形的绝热材料片(14),其从模具中移除。
    • 10. 发明授权
    • Method of fabricating hybrid composite structures
    • 生产杂交复合结构的方法
    • EP0783959B1
    • 2004-01-02
    • EP97200021.0
    • 1997-01-06
    • THE BOEING COMPANY
    • Turner, C. WarrenLum, Matthew K.S.Evans, Richard B.
    • B32B1/10B32B3/12B29C70/30B29D9/00
    • B29C70/088B29C70/32B29K2705/00Y02T50/43
    • A hybrid composite structure is formed from layers of gore strips (12), polymeric matrix composite (71) comprising a resin impregnated slit tape or tow, and a central honeycomb layer formed from a plurality of rectangular sections (72). The first two steps include forming a plurality of the gore strips and providing a mold, or lay-up mandrel (10). Thereafter, a first set of gore strips is applied to the lay-up mandrel to form a first gore strip layer. Subsequently, the composite material in form of resin impregnated slit tape or tow is applied to the first gore strip layer to form a first composite material layer. Next, a second set of gore strips is applied to the first layer of polymeric matrix composite, opposite the first gore strip layer, to form at least one other gore strip layer. This creates a first sandwich structure having gore strips as the first and last layers of the structure. Thereafter, the layer of honeycomb material is applied to the last layer of the first sandwich structure. Finally, a second sandwich structure, substantially identical to the first sandwich structure, is formed on the side of the honeycomb layer opposite the first sandwich structure. Thus, a hybrid composite structure is formed having first and second sandwich structures separated by a central honeycomb layer.