TENSILE TEST GEOMETRY
    3.
    发明专利

    公开(公告)号:CA2917872A1

    公开(公告)日:2015-01-15

    申请号:CA2917872

    申请日:2014-07-09

    Abstract: A plated polymer test specimen for measuring strain imparted to the plated polymer test specimen includes a polymeric substrate including a top, a bottom, a pair of opposing edges and a pair of opposing end edges, the top and bottom being plated with top and bottom metal layers respectively, the side edges and the end edges being at least substantially free of plating. The substrate includes two spaced-apart holes that extend through the top metal layer, substrate and the bottom metal layer. Alternatively, the substrate may comprise a composite layup structure. A method for testing the strain imparted to a plated polymer test specimen is also disclosed.

    THERMOPLASTIC NOSECONE FOR A TURBINE ENGINE
    6.
    发明申请
    THERMOPLASTIC NOSECONE FOR A TURBINE ENGINE 审中-公开
    用于涡轮发动机的热塑性NOSECONE

    公开(公告)号:WO2014120123A2

    公开(公告)日:2014-08-07

    申请号:PCT/US2013023635

    申请日:2013-01-29

    Inventor: ROACH JAMES T

    Abstract: A nosecone for a turbine engine includes a nosecone body and a nosecone mount. The nosecone body extends along an axis between a tip end and a base end. The nosecone body is configured from or otherwise includes thermoplastic material. The nosecone body includes a shell and an arrangement of ribs, which structurally support at least a portion of the shell. A thickness of the arrangement of ribs is greater than or substantially equal to approximately one half of a thickness of the shell. The nosecone mount is adapted to connect the nosecone body to a component of the turbine engine.

    Abstract translation: 用于涡轮发动机的鼻锥包括鼻锥体和鼻锥座。 鼻锥体沿着尖端和基端之间的轴线延伸。 鼻锥体由热塑性材料构成或以其他方式包括热塑性材料。 鼻锥体包括壳体和肋的布置,其在结构上支撑壳体的至少一部分。 肋的布置的厚度大于或基本上等于壳的厚度的大约一半。 鼻锥安装座适于将鼻锥体与涡轮发动机的部件连接。

    PLATED POLYMER AVIATION COMPONENTS

    公开(公告)号:CA2917880A1

    公开(公告)日:2015-01-15

    申请号:CA2917880

    申请日:2014-07-09

    Abstract: Aviation components comprising a polymeric substrate having an outer surface wherein a metal is plated onto the outer surface to form a plated layer are disclosed. A method to make aviation components comprising a polymeric substrate having an outer surface and where a metal is plated onto the outer surface is disclosed. An over-plated heating element for shedding ice from an aircraft component having a polymeric substrate with a pocket to receive a heating element, a metal deposited onto the substrate, a heating element positioned within the pocket and a covering layer deposited onto the heating element and the plated layer is disclosed.

    PLATED POLYMER COMPOSITE MOLDING
    9.
    发明专利

    公开(公告)号:CA2917888A1

    公开(公告)日:2015-01-15

    申请号:CA2917888

    申请日:2014-07-09

    Abstract: Plated polymeric articles having a composite layup structure and method of making the same are disclosed. A plated polymeric article comprises a composite layup having first and second polymer layers. The plated polymeric article further comprises a first metal plated onto the polymer. Additionally, methods for fabricating a plated polymeric article are disclosed. A composite layup is provided and compression molded into a desired shape having an outer surface. The outer surface of the article is prepared to receive a catalyst and then is activated with the catalyst. A first metallic layer is then plated onto the outer surface.

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