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    COMPOSITE STRUCTURES
    1.
    发明申请
    COMPOSITE STRUCTURES 有权

    公开(公告)号：US20230099452A1

    公开(公告)日：2023-03-30

    申请号：US17485013

    申请日：2021-09-24

    申请人： Goodrich Corporation

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

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

    摘要： 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.

    ANTIVIRAL AIRCRAFT INTERIOR COMPONENTS AND METHOD OF ANTIVIRAL PROTECTION
    2.
    发明申请
    ANTIVIRAL AIRCRAFT INTERIOR COMPONENTS AND METHOD OF ANTIVIRAL PROTECTION 有权

    公开(公告)号：US20210361800A1

    公开(公告)日：2021-11-25

    申请号：US17327057

    申请日：2021-05-21

    申请人： Goodrich Corporation

    发明人： Mark R. Gurvich

    IPC分类号： A61L2/10 ,  B64F5/30

    摘要： An antiviral system comprises, an interior space, and an ultra-violet (UV) illuminator system fixedly mounted within the interior space for illumination of surfaces within the interior space for destruction of pathogens on the surfaces. A plurality of seats can be arranged within the interior space such that the UV illuminator system is configured to illuminate full or partial surfaces of individual seats of the plurality of seats.

    METALLIC COMPOSITE JOINT
    3.
    发明申请
    METALLIC COMPOSITE JOINT 审中-公开

    公开(公告)号：US20170369157A1

    公开(公告)日：2017-12-28

    申请号：US15190978

    申请日：2016-06-23

    申请人： Goodrich Corporation

    发明人： Mark R. Gurvich ,  Rony Giovanni Ganis

    IPC分类号： B64C25/00

    CPC分类号： B64C25/00 ,  B29C70/72 ,  B32B3/06 ,  B64C25/60 ,  F16C7/026 ,  F16C2326/05 ,  F16C2326/43

    摘要： A composite metallic joint assembly may include a composite metal rod having a metal liner and a composite material disposed around the metal liner. A first portion of the composite metal rod may comprise the composite material and the metal liner and a second portion of the composite metal rod may comprise the metal liner exposed at a radially outer surface of the composite metal rod. The metal liner may have a first radial thickness at a first axial position corresponding to the first portion of the composite metal rod and a second radial thickness at a second axial position corresponding to the second portion of the composite metal rod. The second thickness may be greater than the first thickness.

    INTEGRATED COMPOSITE DRIVE SHAFTS
    5.
    发明公开
    INTEGRATED COMPOSITE DRIVE SHAFTS 审中-公开

    公开(公告)号：US20240328453A1

    公开(公告)日：2024-10-03

    申请号：US18127584

    申请日：2023-03-28

    申请人： Goodrich Corporation

    发明人： Mark R. Gurvich ,  Michael J. King ,  Brayton Reed ,  Joyel M. Schaefer

    IPC分类号： F16C3/02

    CPC分类号： F16C3/026 ,  F16C2220/42 ,  F16C2326/06

    摘要： In accordance with at least one aspect of this disclosure, a composite shaft includes a plurality of composite elements arranged about an axis to form a hollow shaft with at least one undulation. The plurality of composite elements incudes a first group of the composite elements arranged about the axis offset by an angle +α and a second group of the composite elements arranged about the axis offset by an angle −α to form a web with the first group of composite elements. The first and second groups of the plurality of composite elements are configured to cooperate with one another to allow the hollow shaft to be flexible under axial load and stiff under rotational load.

    Composite/metal joints for composite rods
    6.
    发明授权
    Composite/metal joints for composite rods 有权

    公开(公告)号：US12090586B2

    公开(公告)日：2024-09-17

    申请号：US17654389

    申请日：2022-03-10

    申请人： Goodrich Corporation

    发明人： Mark R. Gurvich

    IPC分类号： B23P11/00 ,  B29C65/00 ,  B29C70/76

    CPC分类号： B23P11/00 ,  B29C66/126 ,  B29C66/3032 ,  B29C66/5221 ,  B29C66/721 ,  B29C66/742 ,  B29C70/766 ,  B29C66/534 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/7392 ,  B29C66/7394

    摘要： A method of forming a joint between a composite component and a metallic component is disclosed. The method includes forming a first groove in an outer surface of the metallic component on a first end of the metallic component. The first groove extends circumferentially on the outer surface relative to a center axis of the metallic component, and the first groove extends radially inward from the outer surface relative the center axis. The method further includes inserting the first end of the metallic component into a first end of the composite component. A second groove on the composite component over the first groove of the metallic component such that the composite component extends radially inward into the first groove of the metallic component. A composite hoop reinforcement is then applied in the second groove in a circumferential direction and the composite component, and the composite hoop reinforcement are solidified.

    COMPOSITE/METAL JOINTS FOR COMPOSITE RODS
    7.
    发明公开
    COMPOSITE/METAL JOINTS FOR COMPOSITE RODS 审中-公开

    公开(公告)号：US20230287914A1

    公开(公告)日：2023-09-14

    申请号：US17654389

    申请日：2022-03-10

    申请人： Goodrich Corporation

    发明人： Mark R. Gurvich

    IPC分类号： F16B5/06

    CPC分类号： F16B5/0621

    摘要： A method of forming a joint between a composite component and a metallic component is disclosed. The method includes forming a first groove in an outer surface of the metallic component on a first end of the metallic component. The first groove extends circumferentially on the outer surface relative to a center axis of the metallic component, and the first groove extends radially inward from the outer surface relative the center axis. The method further includes inserting the first end of the metallic component into a first end of the composite component. A second groove on the composite component over the first groove of the metallic component such that the composite component extends radially inward into the first groove of the metallic component. A composite hoop reinforcement is then applied in the second groove in a circumferential direction and the composite component, and the composite hoop reinforcement are solidified.

    MANUFACTURING METHODS FOR COMPOSITE DRIVESHAFTS
    9.
    发明申请
    MANUFACTURING METHODS FOR COMPOSITE DRIVESHAFTS 审中-公开

    公开(公告)号：US20200298505A1

    公开(公告)日：2020-09-24

    申请号：US16360975

    申请日：2019-03-21

    申请人： Goodrich Corporation

    发明人： Brayton Reed ,  Joyel M. Schaefer ,  Mark R. Gurvich ,  Gianfranco Barbato

    IPC分类号： B29C69/02 ,  B29C70/32 ,  B29C70/38

    摘要： A flexible composite driveshaft is formed by modifying the shape of a preliminary composite driveshaft. A fiber tape is applied to a temporary mandrel using automated fiber placement to form a preliminary composite driveshaft having a flexible shaft element with an initial geometry. The temporary mandrel from the preliminary composite driveshaft is removed and the initial geometry of the flexible shaft element is modified to form the flexible composite driveshaft having a flexible shaft element with a final geometry.