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    Internally heated engine inlet screen for aircraft engines
    4.
    发明授权
    Internally heated engine inlet screen for aircraft engines 有权

    公开(公告)号：US10450954B2

    公开(公告)日：2019-10-22

    申请号：US15072662

    申请日：2016-03-17

    Applicant: General Electric Company

    Inventor： Alan Scott Grissino ,  John Alan Manteiga ,  Jonathan Harry Kerner

    IPC: F02C7/047 ,  B64D15/04 ,  B64D33/02 ,  F02C7/05 ,  F04D29/52 ,  F02C6/08 ,  F02C7/055

    Abstract: An apparatus for providing foreign object debris protection and anti-icing capabilities to an air intake of an aircraft engine. The apparatus includes a frame having at least a portion configured to conduct fluids. A tube is positioned such that different portions of the frame are fluidly connected. There is a discharge outlet defined within the frame that is configured to discharge fluids from the frame into the air intake. An inlet is defined within the frame and is fluidly connected to a compressor section of the aircraft engine. In this manner, air from the compressor section of the aircraft engine can flow through the inlet, through the tube, and through the discharge outlet, to return to the compressor section of the aircraft engine.

    Frame for a heat engine
    9.
    发明授权
    Frame for a heat engine 有权

    公开(公告)号：US11560843B2

    公开(公告)日：2023-01-24

    申请号：US16800410

    申请日：2020-02-25

    Applicant: General Electric Company

    Inventor： Matti Veikko Kalevi Makela ,  Emilio Eramo ,  Christopher Lloyd McKenzie ,  Apostolos Pavlos Karafillis ,  John Alan Manteiga

    IPC: F02C7/047 ,  F01D25/02

    Abstract: A turbo machine including a plenum is formed within a double wall structure including an opening configured to provide fluid communication of a first flow of fluid between the plenum through the double wall structure, and an outer wall forming a passage configured to receive a second flow of fluid separate from the first flow of fluid, wherein a flowpath structure is formed at least in part within an inner wall, the flowpath structure configured to receive a third flow of fluid therethrough, the third flow of fluid separate from the first flow of fluid, the flowpath structure comprising an exit opening configured to provide fluid communication from the flowpath structure to the flowpath.

    MONOLITHIC SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION
    10.
    发明申请
    MONOLITHIC SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION 有权

    公开(公告)号：US20220074346A1

    公开(公告)日：2022-03-10

    申请号：US17526340

    申请日：2021-11-15

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Joshua Tyler Mook ,  John Alan Manteiga ,  Christopher Williams

    IPC: F02C7/06 ,  F01D25/16 ,  F01D25/24 ,  F02C7/20 ,  F02C3/14 ,  F02C7/18 ,  F04D29/053 ,  F04D29/056 ,  F04D29/32 ,  F04D29/54

    Abstract: The present disclosure generally relates to monolithic superstructures for supporting a rotating shaft coupled to a rotor relative to a stator. An integral superstructure supports the rotating component. The superstructure includes a bearing portion that contacts the shaft. A stator portion, is spaced a critical dimension radially outward, from the rotor. A first annular transfer portion extends axially forward from the bearing to the stator portion. A second annular transfer portion extends axially aft from the stator portion to a mounting flange. The mounting flange connects the superstructure to a frame. The superstructure maintains a critical dimension between the rotor and the stator as the temperature of the superstructure increases. The rotor may be a compressor impeller in a gas turbine engine and the stator may be an aero component that transfers air into a combustor.

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