PERFORATED IMPELLER BLADES
    31.
    发明申请

    公开(公告)号:US20230099661A1

    公开(公告)日:2023-03-30

    申请号:US17484857

    申请日:2021-09-24

    Applicant: Delavan Inc.

    Abstract: A method of making an impeller includes building the impeller in a layer by layer process in a build direction along the rotational axis starting from a base of the hub. The plurality of blades includes a plurality of perforated blades that support the shroud during additively manufacturing the impeller. The method can include installing the impeller in a fuel pump, air compressor, or the like, without removing the perforated blades from the impeller.

    TEMPERATURE CONTROL FOR ADDITIVE MANUFACTURING

    公开(公告)号:US20210060922A1

    公开(公告)日:2021-03-04

    申请号:US16551903

    申请日:2019-08-27

    Applicant: Delavan Inc.

    Abstract: A method includes beginning an additively manufactured build by depositing initial layers of the build on a build plate, and additively manufacturing a temperature control channel as part of the build in progress. The method also includes controlling temperature in the temperature control channel while continuing to additively manufacture the build to provide temperature control for the build in progress. The method also includes completing additive manufacture of the build. The method can include removing the temperature control channel from the build after completion of the build.

    LATTICE SUPPORTED DUAL COILED FUEL TUBES
    35.
    发明申请

    公开(公告)号:US20200224876A1

    公开(公告)日:2020-07-16

    申请号:US16248235

    申请日:2019-01-15

    Applicant: Delavan Inc.

    Abstract: A fuel injector for a gas turbine engine includes a fuel inlet fitting for receiving fuel, with a feed arm mounted to the inlet. The feed arm has a lattice support structure. The lattice support structure may include a plurality of three-dimensional elements, a first conduit, and a second conduit in fluid communication with the inlet for conveying fuel from the inlet fitting through the feed arm, wherein the conduits are intertwined with each other, and a nozzle body operatively connected to the feed arm for injecting fuel from the conduits into a combustor of the gas turbine engine.

    TORSION TESTING MACHINE AND METHODS FOR ADDITIVE BUILDS

    公开(公告)号:US20200018675A1

    公开(公告)日:2020-01-16

    申请号:US16031224

    申请日:2018-07-10

    Applicant: Delavan Inc.

    Abstract: A system can include a torsion applicator (e.g., a torsion motor and shaft) configured to apply a torque to a test article that is additively built on and attached to a build plate. The system can include at least one twist sensor and at least one torque sensor. A method for determining quality of an additively manufactured article or batch thereof can include torsion testing at least one additively manufactured test article that is built on and attached to a build plate while the at least one test article is still attached to the build plate.

    DUAL FUEL GAS TURBINE ENGINE PILOT NOZZLES
    38.
    发明申请

    公开(公告)号:US20190195498A1

    公开(公告)日:2019-06-27

    申请号:US15850175

    申请日:2017-12-21

    Applicant: Delavan Inc.

    CPC classification number: F23R3/343 F23R3/10 F23R3/14 F23R3/16 F23R3/36

    Abstract: A pilot nozzle for a dual fuel turbine engine includes an inner air circuit, a gaseous fuel circuit radially outward from the inner air circuit, a liquid fuel circuit radially outward from the inner air circuit, an outer air circuit radially outward from the liquid fuel circuit and the gaseous fuel circuit, and a shroud radially outward from the outer air circuit. The shroud is configured to stabilize a pilot re-circulation zone downstream from outlets of the inner and outer air circuits and the liquid and gaseous fuel circuits.

    FUEL INJECTOR ASSEMBLIES
    39.
    发明申请

    公开(公告)号:US20190186750A1

    公开(公告)日:2019-06-20

    申请号:US15844216

    申请日:2017-12-15

    Applicant: Delavan, Inc.

    Abstract: A method for assembling a fuel distribution system for a turbomachine fuel injector includes inserting a liquid fuel distributor into an interior cavity of a shroud to create a liquid fuel distribution circuit between the liquid fuel distributor and the shroud and inserting a gas fuel distributor into the interior cavity of the shroud and into an interior cavity of the liquid fuel distributor to create a gas fuel distribution circuit between the gas fuel distributor and the liquid fuel distributor. The method includes inserting a fuel transfer tube into an outer diameter of the shroud. The method includes brazing or shrink fitting at least one of the fuel transfer tube, the gas fuel distributor, or the liquid fuel distributor to the shroud.

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