FUEL INJECTORS FOR TURBOMACHINES HAVING INNER AIR SWIRLING

    公开(公告)号:US20190309949A1

    公开(公告)日:2019-10-10

    申请号:US15949783

    申请日:2018-04-10

    Applicant: Delavan Inc.

    Abstract: A fuel injector for a turbomachine includes an inner heat shield having an air cavity wall defining an air cavity for allowing air to flow therethrough. The inner heat shield includes an integral air swirler forming a downstream end thereof. The integral air swirler extends in an axially downstream direction at least as far as a fuel distribution channel defined on or in a fuel distributor of the injector to direct airflow at an outlet of the fuel distributor.

    TAPERED HELICAL FUEL DISTRIBUTOR
    22.
    发明申请

    公开(公告)号:US20190186742A1

    公开(公告)日:2019-06-20

    申请号:US15844307

    申请日:2017-12-15

    Applicant: Delavan, Inc.

    CPC classification number: F23R3/28 F23R3/283 F23R3/36

    Abstract: A fuel distributor system for a turbomachine fuel injector can include a plurality of helical fuel flow channels defined between a fuel distributor and a shroud that surrounds the fuel distributor. A wind axis of the helical flow channels is an axial axis of the fuel injector and each of the helical fuel flow channels include an upstream opening configured to be in fluid communication with a liquid fuel source and a downstream opening configured to effuse fuel therefrom. Each of the plurality of helical fuel flow channels can reduce in flow area from the upstream opening to the downstream opening.

    FUEL INJECTORS AND METHODS OF MAKING FUEL INJECTORS

    公开(公告)号:US20190120141A1

    公开(公告)日:2019-04-25

    申请号:US15789735

    申请日:2017-10-20

    Applicant: Delavan Inc.

    Abstract: A fuel conduit for a fuel injector includes a coiled tube with a longitudinal segment arranged along a flow axis and a radial segment. The radial segment extends about the flow axis and is in fluid communication with the longitudinal segment. The wall one or more of the longitudinal and radial segments increases at a thickness transition location offset from a minimum radius of curvature location along the fuel conduit to limit stress within the fuel conduit. Fuel injectors and methods of making fuel injectors are also described.

    AIR SWIRLERS
    24.
    发明申请
    AIR SWIRLERS 审中-公开

    公开(公告)号:US20190101291A1

    公开(公告)日:2019-04-04

    申请号:US16206302

    申请日:2018-11-30

    Applicant: Delavan, Inc.

    Abstract: A swirler, such as for swirling air in a fuel injector of a gas turbine engine, includes a swirler body with opposed inlet and outlet ends with a swirler wall extending therebetween along a longitudinal axis. The inlet end of the swirler body defines an inlet opening. A plurality of swirl slots is defined through a portion of the swirler wall that converges toward the longitudinal axis in a direction from the inlet opening toward the outlet end of the swirler body. The swirl slots are radially off-set with respect to the longitudinal axis for imparting swirl on a flow passing from the inlet opening, through the swirl slots, and past the outlet end of the swirler body.

    Resonant modes in sprays
    25.
    发明授权

    公开(公告)号:US10227890B2

    公开(公告)日:2019-03-12

    申请号:US15240484

    申请日:2016-08-18

    Applicant: Delavan Inc

    Abstract: A system for inspecting spray nozzles includes a nozzle operatively connected to a source of pressurized liquid for issuing a spray from the nozzle. The system also includes a sensor positioned to detect frequencies of resonant modes in the spray. The nozzle and sensor can each be mounted to a spray test booth. A method of inspecting a spray nozzle includes issuing a liquid from a spray nozzle as a spray and using a sensor to detect frequencies of resonant modes in the spray. The sensor can include a diaphragm and detecting frequencies can include impinging at least some of the spray on the diaphragm, and monitoring vibrations of the diaphragm.

    INTERNAL FUEL MANIFOLDS
    27.
    发明申请

    公开(公告)号:US20180202364A1

    公开(公告)日:2018-07-19

    申请号:US15407972

    申请日:2017-01-17

    Applicant: Delavan Inc

    Abstract: A fluid manifold including a manifold body having a first annular passage defined between a first wall of the manifold body and a second wall of the manifold body, wherein the second wall is radially inward from the first wall. A second annular passage is nested radially inward of the firsts annular passage, wherein the second annular passage is defined between the second wall of the manifold body and a third wall of the manifold body radially inward from the second wall of the manifold body.

    VARIABLE ANGLE MULTI-POINT INJECTION
    29.
    发明申请

    公开(公告)号:US20180010563A1

    公开(公告)日:2018-01-11

    申请号:US15677617

    申请日:2017-08-15

    Applicant: Delavan Inc.

    Abstract: A nozzle for injecting liquid includes a nozzle body defining a flow channel and a swirl ante-chamber in fluid communication with the flow channel. An injection point orifice is defined in the swirl ante-chamber. The flow channel feeds into the swirl ante-chamber to impart a tangential flow component on fluids entering the swirl ante-chamber to generate swirl on a spray issuing from the injection point orifice. A second flow channel can be included in fluid communication with the swirl ante-chamber. The second flow channel feeds into the swirl ante-chamber in cooperation with or in opposition to the first flow channel. The first flow channel, second flow channel, and swirl ante-chamber are configured and adapted to adjust spray angle of a spray issuing from the injection point orifice by varying flow apportionment among the first and second flow channels.

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