中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

25 records (took 0.013 seconds)

    Drive shafts
    11.
    发明授权
    Drive shafts 有权

    公开(公告)号：US12123458B2

    公开(公告)日：2024-10-22

    申请号：US17484793

    申请日：2021-09-24

    Applicant: Goodrich Corporation

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

    IPC: F16C1/02 ,  F16D3/00

    CPC classification number: F16C1/02 ,  F16D3/005

    Abstract: A drive shaft which includes a first tube body having one or more first body channels defined through a wall thickness thereof. The one or more channels are configured to increase bending and/or axial flexibility of the first tube body while only allowing for a less than proportional reduction in torsional stiffness of the first tube body. A second tube body can be concentrically disposed relative to the first tube body and connected to the first tube body at a first end portion and a second end portion. The second tube body can include one or more second body channels defined through a wall thickness thereof. The one or more channels are configured to increase bending and/or axial flexibility of the second tube body while only allowing for a less than proportional reduction in torsional stiffness of the second tube body.

    DRIVE SHAFT WITH INCREASED BALLISTIC TOLERANCE
    13.
    发明申请
    DRIVE SHAFT WITH INCREASED BALLISTIC TOLERANCE 有权

    公开(公告)号：US20230002039A1

    公开(公告)日：2023-01-05

    申请号：US17367085

    申请日：2021-07-02

    Applicant: Goodrich Corporation

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

    IPC: B64C27/12 ,  B64D7/00 ,  F16C3/02

    Abstract: An aircraft drive shaft including an outer shaft having a first diameter configured to couple a first gearbox and a second gearbox to provide power transfer between the two gearboxes, an inner shaft concentric with the outer shaft and having a second diameter configured to provide structural support to the outer shaft, a gap defined between an outer peripheral surface of the inner shaft and an inner peripheral surface of the outer shaft, wherein the gap is sized according to a ballistic projectile cross-section size that the aircraft is considered to encounter on an upcoming mission, and a sleeve located at least at first end of the outer shaft connecting the outer shaft to the inner shaft.

    FLEXIBLE THERMOPLASTIC COMPOSITE COUPLING AND METHOD OF MANUFACTURE
    15.
    发明申请
    FLEXIBLE THERMOPLASTIC COMPOSITE COUPLING AND METHOD OF MANUFACTURE 有权

    公开(公告)号：US20210221072A1

    公开(公告)日：2021-07-22

    申请号：US16748308

    申请日：2020-01-21

    Applicant: Goodrich Corporation

    Inventor： Raghu Iyer ,  Joyel M. Schaefer ,  Brayton Reed

    IPC: B29C70/38 ,  F16C3/02

    Abstract: A process for forming a flexible composite driveshaft includes providing a mandrel having a rigid region and a compressible region, applying fiber tape to the mandrel using automated fiber placement with in-situ laser curing in the rigid region and without in-situ laser curing the compressible region, and compressing the fiber tape and compressible material in the compressible region to form diaphragms that extend radially outward to a diameter that is at least twice the size of a diameter of the composite driveshaft in the rigid region.

    Drive shaft with ballistic tolerance
    16.
    发明授权
    Drive shaft with ballistic tolerance 有权

    公开(公告)号：US12258122B2

    公开(公告)日：2025-03-25

    申请号：US17367085

    申请日：2021-07-02

    Applicant: Goodrich Corporation

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

    IPC: B64C27/12 ,  F16C3/02 ,  B64C27/82

    Abstract: An aircraft drive shaft that includes an outer shaft with a first diameter that is configured to couple a first gearbox and a second gearbox to provide power transfer between the two gearboxes. An inner shaft that is concentric with the outer shaft and has a second diameter that is configured to provide structural support to the outer shaft. A gap is located between an outer peripheral surface of the inner shaft and an inner peripheral surface of the outer shaft. The gap has a size from the outer peripheral surface to the inner peripheral surface that is at least as large as a largest ballistic projectile cross-section size that the aircraft is expected to encounter on an upcoming mission. A sleeve is located at least at a first end of the outer shaft and connects the outer shaft to the inner shaft.

    COMPOSITE DRIVE SHAFTS
    18.
    发明申请
    COMPOSITE DRIVE SHAFTS 有权

    公开(公告)号：US20250067301A1

    公开(公告)日：2025-02-27

    申请号：US18238451

    申请日：2023-08-25

    Applicant: Goodrich Corporation

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

    IPC: F16C3/02

    Abstract: In accordance with at least one aspect of this disclosure, a composite shaft comprises a plurality of composite elements arranged about an axis to form a hollow cylindrical shaft extending along the axis between a first end of the shaft and a second end of the shaft. The plurality of composite elements incudes: a first group of the composite elements aligned parallel to the axis, a second group of the composite elements arranged about the axis offset by an angle α relative to the first group in a first direction, a third group of the composite elements arranged about the axis offset by an angle γ relative to the first group in a second direction opposite the first direction, wherein the third group is offset from the second group by an angle 2α, and a fourth group of the composite elements arranged about the axis offset by an angle θ.

    FLEXIBLE METALLIC COUPLINGS FOR DRIVE SHAFTS
    19.
    发明公开
    FLEXIBLE METALLIC COUPLINGS FOR DRIVE SHAFTS 审中-公开

    公开(公告)号：US20240240675A1

    公开(公告)日：2024-07-18

    申请号：US18096900

    申请日：2023-01-13

    Applicant: Goodrich Corporation

    Inventor： Mark R. Gurvich ,  Jeffrey L. Mathis ,  Joyel M. Schaefer ,  Michael J. King ,  Brayton Reed

    IPC: F16D3/10 ,  F16D3/06

    CPC classification number: F16D3/10 ,  F16D3/06 ,  F16D2250/00

    Abstract: A flexible coupling includes a first flange and a second flange, wherein in a relaxed state the first flange and the second flange are each aligned along a longitudinal axis. A plurality of first coupling members extends from the first flange. Each first coupling member includes a first and second driving beam meeting at a first node to form a topologically triangular truss. A plurality of second coupling members extend from the second flange. Each second coupling member includes a first and second driven beam extending from the second flange and meeting at a second node to form a topologically triangular truss. The first node of each of the first coupling members is connected to the second node of a respective one of the second coupling members.

Patent Agency Ranking