中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

22 records (took 0.017 seconds)

    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS
    1.
    发明申请
    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS 有权

    公开(公告)号：US20230033578A1

    公开(公告)日：2023-02-02

    申请号：US17664528

    申请日：2022-05-23

    Applicant: Rolls-Royce Corporation

    Inventor： Charles Alan Bulgrin ,  Carl R. Russo ,  Joseph Peter Henderkott ,  Matthew T. Kush ,  Greg Lopshire

    IPC: B23K35/22 ,  B23K1/008 ,  B23K1/20 ,  B23K1/00 ,  B23K1/19

    Abstract: The disclosure describes example techniques and assemblies for joining a first component and a second component. The techniques may include positioning the first and second component adjacent to each other to define a joint region between adjacent portions of the first component and the second component, the joint region being coated with an adhesion resistant coating. The techniques may also include positioning a braze material in the joint region, heating the braze material to form an at least softened material, and cooling the at least softened material to form a mechanical interlock including the braze material in the joint region joining the first and second components. The braze material does not metallurgically bond to the joint surface.

    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS USING SOLID RETAINER MATERIALS
    2.
    发明申请
    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS USING SOLID RETAINER MATERIALS 有权

    公开(公告)号：US20210146485A1

    公开(公告)日：2021-05-20

    申请号：US16685265

    申请日：2019-11-15

    Applicant: Rolls-Royce Corporation

    Inventor： Charles Alan Bulgrin ,  Matthew T. Kush ,  Rusty M. Garner ,  Carl R. Russo

    IPC: B23K35/02 ,  B23K1/00

    Abstract: The disclosure describes example techniques and assemblies for joining a first component and a second component. The techniques may include positioning the first and second component adjacent to each other to define a joint region between adjacent portions of the first component and the second component. The techniques may also include inserting a solid retainer material into the joint region through an aperture in one of the first component or the second component to form a mechanical interlock between the first component and the second component and sealing the aperture to retain the solid retainer material within the joint region. The solid retainer material includes at least one of a metal, a metal alloy, or a ceramic.

    FORMING FEATURES IN ADDITIVELY MANUFACTURED COMPOSITE MATERIALS USING SACRIFICIAL SUPPORT MATERIALS
    5.
    发明申请
    FORMING FEATURES IN ADDITIVELY MANUFACTURED COMPOSITE MATERIALS USING SACRIFICIAL SUPPORT MATERIALS 有权

    公开(公告)号：US20210060866A1

    公开(公告)日：2021-03-04

    申请号：US16555820

    申请日：2019-08-29

    Applicant: Rolls-Royce Corporation

    Inventor： Cory Nation ,  Matthew T. Kush

    IPC: B29C64/40 ,  B29C64/118 ,  B29C64/245

    Abstract: A method may include depositing a sacrificial support material on or adjacent to a build surface. The sacrificial support material may be configured to support a continuous reinforcement material during an additive manufacturing technique. The method also may include extruding the continuous reinforcement material from an additive manufacturing device such that at least a portion of the continuous reinforcement material contacts and is supported by the sacrificial support material; and removing the sacrificial support material to result in a feature defined at least in part by the continuous reinforcement material at the absence of sacrificial support material.

    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS
    6.
    发明申请
    TECHNIQUES AND ASSEMBLIES FOR JOINING COMPONENTS 审中-公开

    公开(公告)号：US20190275617A1

    公开(公告)日：2019-09-12

    申请号：US16294415

    申请日：2019-03-06

    Applicant: Rolls-Royce Corporation

    Inventor： Charles Alan Bulgrin ,  Carl R. Russo ,  Joseph Peter Henderkott ,  Matthew T. Kush ,  Greg Lopshire

    IPC: B23K35/22 ,  B23K1/008 ,  B23K1/20

    Abstract: The disclosure describes example techniques and assemblies for joining a first component and a second component. The techniques may include positioning the first and second component adjacent to each other to define a joint region between adjacent portions of the first component and the second component, the joint region being coated with an adhesion resistant coating. The techniques may also include positioning a braze material in the joint region, heating the braze material to form an at least softened material, and cooling the at least softened material to form a mechanical interlock including the braze material in the joint region joining the first and second components. The braze material does not metallurgically bond to the joint surface.

    Cooled single walled blisk for gas turbine engine
    10.
    发明授权
    Cooled single walled blisk for gas turbine engine 有权

    公开(公告)号：US10934865B2

    公开(公告)日：2021-03-02

    申请号：US15405508

    申请日：2017-01-13

    Applicant: Rolls-Royce Corporation

    Inventor： Matthew T. Kush

    IPC: F01D5/34 ,  F01D5/18

    Abstract: A gas turbine engine and a blisk are disclosed, including methods of making the same. The blisk may include a disk, spars of airfoils, platforms, and shanks of the airfoils integrally formed as a unit. Such blisk features may be integrally formed by a casting process or additive manufacturing. The blisk includes cooled airfoils, such that the spar includes standoffs, and a cover panel is bonded to an outer surface of the standoffs to define passages between the cover panel and the spar. Cooling air is fed through an inlet port formed in a base standoff to the passages of the spar through a cooling feed channel defined in the disk or shank portion.

Patent Agency Ranking