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    COMPOSITE STRUCTURES
    23.
    发明申请
    COMPOSITE STRUCTURES 有权

    公开(公告)号：US20230111679A1

    公开(公告)日：2023-04-13

    申请号：US17484985

    申请日：2021-09-24

    Applicant: Goodrich Corporation

    Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Joyel M. Schaefer

    IPC: B29C70/30 ,  B29C70/38 ,  B29C70/54

    Abstract: In accordance with at least one aspect of this disclosure, a composite structure can be formed of or including a plurality of composite strips. The plurality of composite strips include one or more filler strips which can have at least one filler edge having a filler edge geometry between a first surface and second surface, the second surface being opposite the first surface. The filler edge geometry can be configured to prevent formation of one or more gaps between one or more adjacent composite strips.

    HYBRID COMPOSITE DRIVE SHAFT AND A METHOD OF MAKING
    26.
    发明申请
    HYBRID COMPOSITE DRIVE SHAFT AND A METHOD OF MAKING 审中-公开

    公开(公告)号：US20200309186A1

    公开(公告)日：2020-10-01

    申请号：US16370489

    申请日：2019-03-29

    Applicant: Goodrich Corporation

    Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Brayton Reed ,  Joyel M. Schaefer ,  Michael King

    IPC: F16C3/02 ,  B29C43/20 ,  B32B1/08 ,  B32B27/08

    Abstract: A drive shaft for transferring torque including a tubular insert extending along an axis and defining a first layer of the drive shaft including at least one straight portion and at least one undulation, wherein the tubular insert includes a first material having a first deformation temperature, and a polymeric tubular covering defining a second layer of the drive shaft surrounding the tubular insert including a second material having a deformation temperature lower than the deformation temperature of the first material, wherein the covering includes at least one straight portion adjacent to the straight portion of the tubular insert and at least one undulation adjacent to the at least one undulation of the tubular insert.

    Manufacturing method of polymer composite/metal load transfer joint for landing gear
    27.
    发明授权
    Manufacturing method of polymer composite/metal load transfer joint for landing gear 有权

    公开(公告)号：US10556673B2

    公开(公告)日：2020-02-11

    申请号：US15193968

    申请日：2016-06-27

    Applicant: Goodrich Corporation

    Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Rony Giovanni Ganis

    IPC: B64C25/34 ,  B64C25/02 ,  F16C7/02

    Abstract: A landing gear arrangement may comprise a first composite layer, the first composite layer having a cylindrical geometry, a metallic ring comprising an inner surface and an outer surface, the metallic ring perimetrically surrounding at least a portion of the first composite layer, the inner surface being in contact with the first composite layer, a metallic connecting tab extending away from the outer surface, and a second composite layer at least partially perimetrically surrounding the metallic ring and at least partially perimetrically surrounding the first composite layer, the outer surface being in contact with the second composite layer.

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