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    HOLLOW LIGHTWEIGHT FIBRE REINFORCED PLASTIC HANDLES
    4.
    发明申请
    HOLLOW LIGHTWEIGHT FIBRE REINFORCED PLASTIC HANDLES 有权
    中空轻质纤维增强塑料手柄

    公开(公告)号：US20160263812A1

    公开(公告)日：2016-09-15

    申请号：US14641810

    申请日：2015-03-09

    Applicant: BFG International

    Inventor： Anjal Motwani ,  Vivek Govindaraj

    IPC: B29C53/56

    CPC classification number: B29C53/824 ,  B29C53/582 ,  B29C70/446 ,  B29L2023/22 ,  B29L2031/463

    Abstract: A method of producing, for example, handles for using in rolling stock or other transport situations, employs a flexible core mould that is coated with an impregnated glass fibre. The coated core mould is placed into a tool for curing, whereupon the rubber core is pulled out of the center of the resulting handle member after curing. The method helps create 3D shapes of any form and cross section in a cost effective manner and using a standardized methodology and process. Further, the method enables creation of a hollow and lightweight part. The method allows use of standard glass fiber instead of more specialized braided fibre of the prior art.

    Abstract translation: 制造例如在车辆或其他运输情况下使用的手柄的方法采用涂覆有浸渍玻璃纤维的柔性芯模。 将涂覆的芯模放置在用于固化的工具中，由此在固化之后将橡胶芯从所得手柄构件的中心拉出。 该方法有助于以成本有效的方式创建任何形式和横截面的3D形状，并使用标准化的方法和过程。 此外，该方法能够创建中空轻质部件。 该方法允许使用标准玻璃纤维代替现有技术的更专门的编织纤维。

    Constraint system of sectors of a device for producing an airplane fuselage
    5.
    发明授权
    Constraint system of sectors of a device for producing an airplane fuselage 有权
    用于生产飞机机身的装置的部分的约束系统

    公开(公告)号：US09038687B2

    公开(公告)日：2015-05-26

    申请号：US13852031

    申请日：2013-03-28

    Applicant: ALENIA AERMACCHI S.p.A.

    Inventor： Guido Sibona ,  Ettore Mostarda ,  Giuseppe Iovine

    IPC: B64C1/00 ,  B32B37/00 ,  B29C53/82 ,  B29C33/48

    CPC classification number: B32B37/0046 ,  B29C33/485 ,  B29C53/824 ,  B64C2001/0054 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T156/14

    Abstract: A constraint system of sectors of a device for producing an airplane fuselage in which a lamination mandrel is adapted to receive and support a band of impregnated synthetic material. The lamination mandrel comprises a plurality of sectors angularly spaced about the axis and mobile between: an expanded lamination position and a contracted disassembling position. A constraint system is provided between each sector and the sectors adjacent thereto which guarantees a predetermined arrangement of the first sector with respect to the second sector adjacent thereto, preventing any translation along two directions which lie in an adjustment plane perpendicular to an axis RD which extends radially from the symmetry axis to the external surface.

    Abstract translation: 用于生产飞机机身的装置的扇区的约束系统，其中层压心轴适于接收和支撑浸渍的合成材料带。 层压心轴包括围绕轴线成角度地间隔开的多个扇区，并且可以在膨胀层压位置和收缩的拆卸位置之间移动。 在每个扇区和与其相邻的扇区之间提供约束系统，其确保第一扇区相对于与其相邻的第二扇区的预定布置，防止位于垂直于延伸的轴RD的调整平面中的两个方向的任何平移 径向从对称轴到外表面。

    WINDING METHOD FOR THE PRODUCTION OF A ROTATIONALLY SYMMETRIC, TUBE-LIKE HOLLOW BODY PREFORM, DEVICE AND METHOD FOR THE PRODUCTION OF A DEVICE FOR PRODUCING THE SAME
    7.
    发明申请
    WINDING METHOD FOR THE PRODUCTION OF A ROTATIONALLY SYMMETRIC, TUBE-LIKE HOLLOW BODY PREFORM, DEVICE AND METHOD FOR THE PRODUCTION OF A DEVICE FOR PRODUCING THE SAME 审中-公开
    用于制造旋转对称性，管状中空体系预制件的卷绕方法，用于生产其制造装置的装置和方法

    公开(公告)号：US20140352873A1

    公开(公告)日：2014-12-04

    申请号：US14365911

    申请日：2012-12-13

    Applicant: Robert Bosch GmbH

    Inventor： Ingo Bork ,  Thomas Seufert

    IPC: B29D23/00

    CPC classification number: B29D23/00 ,  B29C33/505 ,  B29C53/60 ,  B29C53/824 ,  B29L2023/00

    Abstract: Winding method for the production of a rotationally symmetric, tube-like hollow body preform, device (10) for the production of a rotationally symmetric, tube-like hollow body preform and a method for the production of a device for producing a rotationally symmetric, tube-like hollow body preform, wherein reinforcing fibres soaked with a resin are wound in a winding process on a rotatably driven winding core (1) having an outside diameter corresponding to the inside diameter of the hollow body preform and wherein the hollow body preform is removed from the winding core after a subsequent hardening of the hollow body preform by means of supplied heat. For the winding process and/or hardening of the hollow body preform, the outside diameter of the winding core corresponds to the inside diameter of the hollow body preform to be produced, wherein the outside diameter of the winding core is reduced to a smaller outside diameter for the removal of the hollow body preform from the winding core.

    Abstract translation: 用于制造旋转对称的管状中空体预制件的卷绕方法，用于制造旋转对称的管状中空体预制件的装置（10），以及用于制造旋转对称的管状空心体预制件的装置的方法， 管状中空体预制件，其中用树脂浸泡的增强纤维在卷绕过程中缠绕在具有对应于中空本体预制件的内径的外径的可旋转驱动的卷芯（1）上，并且其中中空体预制件是 在通过提供的热量随后硬化中空本体预成型件之后，从卷芯上除去。 对于中空体预制件的卷绕过程和/或硬化，卷芯的外径对应于待生产的中空体预制件的内径，其中卷芯的外径减小到更小的外径 用于从卷绕芯去除中空体预制件。

    METHOD OF AND APPARATUS FOR FORMING ONE OR MORE FLANGES ON OR IN A HOLLOW CONTINUOUSLY WOUND STRUCTURAL MEMBER
    8.
    发明申请
    METHOD OF AND APPARATUS FOR FORMING ONE OR MORE FLANGES ON OR IN A HOLLOW CONTINUOUSLY WOUND STRUCTURAL MEMBER 有权
    在中空连续结构构件上形成一个或多个法兰的方法和装置

    公开(公告)号：US20140287171A1

    公开(公告)日：2014-09-25

    申请号：US14355746

    申请日：2012-10-31

    Applicant: Camplas Technology Limited

    Inventor： Anthony Carey Williams

    IPC: B29C41/02 ,  B29C41/42

    CPC classification number: B29C41/02 ,  B29C41/42 ,  B29C53/585 ,  B29C53/62 ,  B29C53/824 ,  B29C57/00 ,  B29L2031/766 ,  Y10T428/1314

    Abstract: A method of and apparatus for forming one or more flanges or formations, which may conveniently be inwardly facing, on or in a hollow continuously wound structural member, such as a hollow pole, the method including the steps of providing a tapered mandrel on which to continuously wind a loop of filament or filaments to form a hollow structural member, providing an end-forming plate at at least one end of the mandrel, placing one or more formers on the outside of the mandrel adjacent to and spaced from the or each end plate by a required amount to form one or more flanges when the member has been fully wound and set within a resin, and subsequently removing the continuously wound structural member from the mandrel.

    Abstract translation: 用于在中空连续卷绕的结构构件（例如中空杆）上形成一个或多个凸缘或结构的方法和装置，其可以方便地向内面对，所述方法包括以下步骤：提供锥形心轴， 连续地缠绕细丝或细丝的环以形成中空的结构构件，在心轴的至少一端提供终端形成板，将一个或多个成形器放置在心轴的外侧，邻近于或与每个端部间隔开 当所述构件被完全卷绕并固定在树脂中时，形成一个或多个凸缘，然后从心轴移除连续卷绕的结构构件。

    CONSTRAINT SYSTEM OF SECTORS OF A DEVICE FOR PRODUCING AN AIRPLANE FUSELAGE
    10.
    发明申请
    CONSTRAINT SYSTEM OF SECTORS OF A DEVICE FOR PRODUCING AN AIRPLANE FUSELAGE 有权
    用于生产机场配件的装置的部件的约束系统

    公开(公告)号：US20130299095A1

    公开(公告)日：2013-11-14

    申请号：US13852031

    申请日：2013-03-28

    Applicant: ALENIA AERMACCHI S.p.A.

    Inventor： Guido SIBONA ,  Ettore Mostarda ,  Giuseppe Iovine

    IPC: B32B37/00

    CPC classification number: B32B37/0046 ,  B29C33/485 ,  B29C53/824 ,  B64C2001/0054 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T156/14

    Abstract: A constraint system of sectors of a device for producing an airplane fuselage in which a lamination mandrel is adapted to receive and support a band of impregnated synthetic material. The lamination mandrel comprises a plurality of sectors angularly spaced about the axis and mobile between: an expanded lamination position and a contracted disassembling position. A constraint system is provided between each sector and the sectors adjacent thereto which guarantees a predetermined arrangement of the first sector with respect to the second sector adjacent thereto, preventing any translation along two directions which lie in an adjustment plane perpendicular to an axis RD which extends radially from the symmetry axis to the external surface.

    Abstract translation: 用于生产飞机机身的装置的扇区的约束系统，其中层压心轴适于接收和支撑浸渍的合成材料带。 层压心轴包括围绕轴线成角度地间隔开的多个扇区，并且可以在膨胀层压位置和收缩的拆卸位置之间移动。 在每个扇区和与其相邻的扇区之间提供约束系统，其确保第一扇区相对于与其相邻的第二扇区的预定布置，防止位于垂直于延伸的轴RD的调整平面中的两个方向的任何平移 径向从对称轴到外表面。

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