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    Tangential on-board injectors for gas turbine engines
    1.
    发明授权
    Tangential on-board injectors for gas turbine engines 有权

    公开(公告)号：US10450960B2

    公开(公告)日：2019-10-22

    申请号：US14860167

    申请日：2015-09-21

    Applicant: United Technologies Corporation

    Inventor： Mark F. Zelesky ,  Joel H. Wagner ,  Shayan Ahmadian

    IPC: F02C7/18 ,  F01D5/08

    Abstract: A tangential on-board injector (TOBI) for a gas turbine engine is provided. The TOBI includes a body having an entrance and an exit, the body having an outer curved wall and defining an air passageway between the entrance and the exit and a purge cavity configured on an exterior surface of the body with a purge cavity entry fluidly connecting the air passageway to the purge cavity. The purge cavity is configured such that particles in an airflow through the passageway will enter the purge cavity.

    PARTICLE CAPTURE FOR COMBUSTOR
    3.
    发明申请
    PARTICLE CAPTURE FOR COMBUSTOR 审中-公开

    公开(公告)号：US20190086084A1

    公开(公告)日：2019-03-21

    申请号：US15709333

    申请日：2017-09-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Carey Clum ,  Shayan Ahmadian ,  Christopher W. Robak

    IPC: F23R3/04 ,  F23R3/00

    CPC classification number: F23R3/04 ,  F23M20/00 ,  F23R3/002 ,  F23R2900/03041 ,  F23R2900/03044

    Abstract: A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.

    TANGENTIAL ON-BOARD INJECTORS FOR GAS TURBINE ENGINES
    6.
    发明申请
    TANGENTIAL ON-BOARD INJECTORS FOR GAS TURBINE ENGINES 审中-公开

    公开(公告)号：US20170082027A1

    公开(公告)日：2017-03-23

    申请号：US14860167

    申请日：2015-09-21

    Applicant: United Technologies Corporation

    Inventor： Mark F. Zelesky ,  Joel H. Wagner ,  Shayan Ahmadian

    IPC: F02C7/18 ,  F01D5/08

    Abstract: A tangential on-board injector (TOBI) for a gas turbine engine is provided. The TOBI includes a body having an entrance and an exit, the body having an outer curved wall and defining an air passageway between the entrance and the exit and a purge cavity configured on an exterior surface of the body with a purge cavity entry fluidly connecting the air passageway to the purge cavity. The purge cavity is configured such that particles in an airflow through the passageway will enter the purge cavity.

    Combustor with particle collection panel having a plurality of particle collection chambers
    7.
    发明授权
    Combustor with particle collection panel having a plurality of particle collection chambers 有权

    公开(公告)号：US10823417B2

    公开(公告)日：2020-11-03

    申请号：US15709333

    申请日：2017-09-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Carey Clum ,  Shayan Ahmadian ,  Christopher W. Robak

    IPC: F23R3/04 ,  F23R3/00 ,  B01D45/08 ,  F23R3/06

    Abstract: A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.

    PROCESSES AND TOOLING FOR TEMPERATURE CONTROLLED PLASMA SPRAY COATING
    8.
    发明申请
    PROCESSES AND TOOLING FOR TEMPERATURE CONTROLLED PLASMA SPRAY COATING 审中-公开

    公开(公告)号：US20190033138A1

    公开(公告)日：2019-01-31

    申请号：US15662871

    申请日：2017-07-28

    Applicant: United Technologies Corporation

    Inventor： Shayan Ahmadian ,  Kevin W. Schlichting

    IPC: G01J5/10 ,  C23C4/134 ,  H04N5/33

    Abstract: A plasma spray system including a temperature sensor operable to determine a temperature of the workpiece at a measurement zone; a heater operable to selectively heat the workpiece at a heating zone downstream of the measurement zone; a plasma spray subsystem operable to plasma spray a workpiece, the plasma spray defines an application zone on the workpiece downstream of the heating zone and a control in communication with the plasma spray subsystem, the temperature sensor, and the heater, the control operable to control the heater to heat the workpiece in the heating zone to a desired temperature in response to a temperature determined by the temperature sensor.

    HEAT FLUX MEASUREMENT SYSTEM
    9.
    发明申请
    HEAT FLUX MEASUREMENT SYSTEM 审中-公开

    公开(公告)号：US20170211408A1

    公开(公告)日：2017-07-27

    申请号：US15002724

    申请日：2016-01-21

    Applicant: United Technologies Corporation

    Inventor： Shayan Ahmadian ,  Charles W. Haldeman ,  Mark F. Zelesky ,  Christopher T. Bergman ,  Sebastian Martinez

    IPC: F01D17/08 ,  G01J5/00 ,  G01J5/10 ,  F02C7/18

    Abstract: A turbine section according to an example of the present disclosure includes, among other things, a component including a coating on a substrate, and at least one sensor positioned a distance from the component, the at least one sensor configured to detect radiation emitted from at least one localized region of the coating at a first wavelength and configured to detect radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength. The first wavelength and the second wavelength are utilized to determine a heat flux relating to the at least one localized region. A method of measuring a gas turbine engine component is also disclosed.

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