知搜-全球专利检索

  1. Login
  2. Sign Up

Search Results

58 records (took 0.024 seconds)

    SYSTEM AND METHODS FOR SELECTIVE CLEANING OF TURBINE ENGINE COMPONENTS
    38.
    发明申请
    SYSTEM AND METHODS FOR SELECTIVE CLEANING OF TURBINE ENGINE COMPONENTS 有权

    公开(公告)号：US20220243614A1

    公开(公告)日：2022-08-04

    申请号：US17682693

    申请日：2022-02-28

    Applicant: General Electric Company

    Inventor： Nicole Jessica Tibbetts ,  Andrew James Jenkins ,  Bernard Patrick Bewlay ,  Evan Jarrett Dolley ,  John Watt ,  Christopher Perrett ,  Vincent Gerard Lauria

    IPC: F01D25/00 ,  F04D29/70 ,  B08B3/08 ,  B08B3/14 ,  B08B3/04

    Abstract: System for selectively contacting a cleaning composition with a surface of a turbine engine component is presented. The system includes a cleaning apparatus and a manifold assembly. The cleaning apparatus includes an upper portion and a lower portion defining a cleaning chamber configured to allow selective contact between the cleaning composition and a surface of the first portion of the turbine engine component. The upper portion includes a plurality of fill holes in fluid communication with the cleaning chamber, and the lower portion includes a plurality of drain holes in fluid communication with the cleaning chamber. The manifold assembly is configured to selectively circulate the cleaning composition from a reservoir to the cleaning chamber via the plurality of fill holes, and recirculate the cleaning composition from the cleaning chamber to the reservoir via the plurality of drain holes. Methods for selectively cleaning a turbine engine component is also presented.

    Foaming nozzle of a cleaning system for turbine engines
    40.
    发明授权
    Foaming nozzle of a cleaning system for turbine engines 有权

    公开(公告)号：US11028727B2

    公开(公告)日：2021-06-08

    申请号：US15727269

    申请日：2017-10-06

    Applicant: General Electric Company

    Inventor： Ambarish Jayant Kulkarni ,  Keith Anthony Lauria ,  Michael Edward Eriksen ,  Nicole Jessica Tibbetts ,  Bernard Patrick Bewlay ,  Byron Andrew Pritchard, Jr. ,  Shantanu M. Sane

    IPC: F01D25/00 ,  B01F5/04 ,  B01F3/04 ,  B29C64/10 ,  B05B7/00 ,  B08B3/00 ,  F02C7/30 ,  B33Y10/00 ,  B33Y80/00

    Abstract: A turbine engine cleaning system includes a foaming nozzle. The foaming nozzle includes a wall having a thickness between an outer surface of the wall and an inner surface of the wall. The outer surface of the wall is configured to contact a detergent in which the foaming nozzle is configured to be disposed. The inner surface of the wall surrounds an inner plenum of the foaming nozzle, and the inner plenum is configured to receive an aerating gas. The foaming nozzle also includes a first row of first through holes fluidly coupled to, and extending between, a first row of first through hole inlets at the inner surface of the wall and a first row of first through hole outlets at the outer surface of the wall. The foaming nozzle also includes a second row of second through holes disposed axially adjacent to the first row of second through holes with respect to a longitudinal axis of the inner plenum, where the second row of second through holes is fluidly coupled to, and extending between, a second row of second through hole inlets at the inner surface of the wall and a second row of second through hole outlets at the outer surface of the wall. The foaming nozzle also includes cross-sections of the first through holes and the second through holes having regular shapes.

Patent Agency Ranking