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    Hybrid pole structure and method of assembly
    11.
    发明授权
    Hybrid pole structure and method of assembly 有权
    混合杆结构及组装方法

    公开(公告)号：US09062662B1

    公开(公告)日：2015-06-23

    申请号：US14226471

    申请日：2014-03-26

    Applicant: Ebert Composites Corporation

    Inventor： David W. Johnson ,  H. Peter Fay

    IPC: E04H12/34 ,  F03D11/04 ,  B65D90/12

    CPC classification number: E04H12/342 ,  E04H12/02 ,  E04H12/12 ,  F03D13/10 ,  F03D13/20 ,  F03D13/22 ,  F03D13/25 ,  F05B2230/60 ,  F05B2240/912 ,  Y02E10/728 ,  Y02P70/523

    Abstract: A hybrid wind turbine tower support structure that combines pultruded fiber glass composites lineals with reinforced concrete, effectively creating a low cost structure for holding large, laterally-forced-thrusts from wind turbine rotor blades. The structure is designed to be lower in installed costs then its counterpart steel support structure, yet be capable of withstanding very large thrust loads, deflecting-under-load less than or equal to, but no more, under extreme wind loading, than its counterpart, steel support structure.

    Abstract translation: 将拉挤玻璃纤维复合材料线与钢筋混凝土结合在一起的混合式风力涡轮机塔架支撑结构，有效地创造了一种低成本的结构，用于保持来自风力涡轮机转子叶片的大的横向强制推力。 该结构被设计为较低的安装成本，然后是其对应的钢支撑结构，但是能够承受非常大的推力载荷，在极端风荷载下小于或等于但不超过其的负载，而不是在其对应物 钢支架结构。

    ADVANCED COMPOSITE NACELLE
    12.
    发明申请
    ADVANCED COMPOSITE NACELLE 审中-公开

    公开(公告)号：US20190293052A1

    公开(公告)日：2019-09-26

    申请号：US15676255

    申请日：2017-08-14

    Applicant: Ebert Composites Corporation

    Inventor： David W. Johnson ,  Scott A. Garrett ,  Stephen G. Moyers

    IPC: F03D13/20 ,  F03D80/80 ,  B29C65/00

    Abstract: A nacelle for a wind turbine system includes a plurality of interconnected curved nacelle thermoplastic composite material panels, each curved nacelle thermoplastic composite material panel having a plurality of interconnecting edges, a foam core, an inner skin, an outer skin, and a plurality of three-dimensional fiber bundles tying the inner skin and the outer skin to each other through the foam core, inhibiting delamination, wherein the plurality of three-dimensional Z-axis fiber bundles include Z-axis fibers, which extend through the foam core from the inner skin to the outer skin, include opposite ends that are thermocured into and with the inner skin and outer skin.

    3D THERMOPLASTIC COMPOSITE PULTRUSION SYSTEM AND METHOD
    15.
    发明申请
    3D THERMOPLASTIC COMPOSITE PULTRUSION SYSTEM AND METHOD 有权
    3D热塑复合材料挤压系统及方法

    公开(公告)号：US20160361879A1

    公开(公告)日：2016-12-15

    申请号：US14967784

    申请日：2015-12-14

    Applicant: Ebert Composites Corporation

    Inventor： David W. Johnson ,  Scott A. Garrett ,  Stephen G. Moyers

    IPC: B29C70/54 ,  F01D5/28 ,  B29C70/52

    CPC classification number: F01D5/28 ,  B29C33/02 ,  B29C33/308 ,  B29C43/22 ,  B29C43/48 ,  B29C47/88 ,  B29C51/14 ,  B29C51/20 ,  B29C51/26 ,  B29C51/261 ,  B29C51/42 ,  B29C51/46 ,  B29C70/525 ,  B29C70/526 ,  B29K2105/06 ,  B29K2105/256 ,  B29K2715/00 ,  E04B1/32 ,  F05D2300/43 ,  F05D2300/6012 ,  F05D2300/603 ,  G05B19/4099

    Abstract: A 3D thermoplastic pultrusion system, comprises one or more sets of 3D thermoplastic forming machines; a CNC control system controlling the one or more sets of 3D thermoplastic forming machines to form a heated prepreg thermoplastic composite material into a 3D thermoplastic composite pultrusion, the one or more sets of 3D thermoplastic forming machines include a plurality of motion control CNC rotational motors and CNC actuators operatively coupled to the motion control CNC rotational motors, a flexible chilled band shapeable by the CNC actuators to form the heated prepreg thermoplastic composite material into the thermoplastic composite pultrusion, and bearings that the motion control CNC rotational motors pivot the actuators about and hold the actuators in position during a consolidation process.

    Abstract translation: 3D热塑性拉挤成型系统，包括一组或多组3D热塑性成型机; 控制所述一组或多组3D热塑性成型机的CNC控制系统以将加热的预浸料热塑性复合材料形成为3D热塑复合拉挤成型机，所述一组或多组3D热塑性成型机包括多个运动控制CNC旋转马达和 可操作地连接到运动控制CNC旋转马达的CNC致动器，由CNC执行器可形成的柔性冷却带，以将加热的预浸料热塑性复合材料形成到热塑性复合拉挤成型机中，以及运动控制CNC旋转马达围绕并保持 执行器在合并过程中就位。

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