MIXING NOZZLES
    1.
    发明申请
    MIXING NOZZLES 审中-公开

    公开(公告)号:US20200306703A1

    公开(公告)日:2020-10-01

    申请号:US16370731

    申请日:2019-03-29

    Applicant: Delavan Inc.

    Abstract: A nozzle includes an outer gas flow path, an inner gas flow path radially inward from the outer gas flow path, a liquid flow path defined radially between the inner gas flow path and the outer air flow path, and a core conduit defined radially inward from the inner gas flow path. An injector assembly includes an outer housing, a nozzle within the outer housing, and an outer housing gas flow path defined radially outward from the nozzle between an inner surface of the outer housing and an outer surface of the nozzle. The nozzle includes an outer gas flow path, an inner gas flow path radially inward from the outer gas flow path, a liquid flow path defined radially between the inner gas flow path and the outer gas flow path and a core conduit defined radially inward from the inner gas flow path.

    Air swirlers
    3.
    发明授权

    公开(公告)号:US10161633B2

    公开(公告)日:2018-12-25

    申请号:US13783832

    申请日:2013-03-04

    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.

    AIR SWIRLERS
    4.
    发明申请
    AIR SWIRLERS 审中-公开

    公开(公告)号:US20140245742A1

    公开(公告)日:2014-09-04

    申请号:US13783832

    申请日:2013-03-04

    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.

    Abstract translation: 旋流器,例如用于燃气涡轮发动机的燃料喷射器中的旋转空气,包括具有相对的入口端和出口端的旋流器主体,其中沿着纵向轴线在其间延伸有旋流器壁。 旋流器主体的入口端限定入口开口。 多个涡流槽通过旋流器壁的一部分限定,该部分沿着从旋流器主体的入口开口朝向出口端的方向朝着纵向轴线会聚。 漩涡槽相对于纵向轴线径向偏移,以在从入口开口,通过涡流槽并经过旋流器主体的出口端的流动上产生涡流。

    VARIABLE ANGLE MULTI-POINT INJECTION
    5.
    发明申请
    VARIABLE ANGLE MULTI-POINT INJECTION 有权
    可变角度多点注射

    公开(公告)号:US20130214063A1

    公开(公告)日:2013-08-22

    申请号:US13767402

    申请日:2013-02-14

    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.

    Abstract translation: 用于注射液体的喷嘴包括限定流动通道的喷嘴主体和与流动通道流体连通的旋流室。 注射点孔口限定在涡流前室中。 流动通道进入涡流前室,以在进入涡流前室的流体上产生切向流分量,以在从注射口孔喷出的喷雾产生涡流。 可以将第二流动通道包括在与涡流室内流体连通。 第二流动通道与第一流动通道协作或与第一流动通道相配合地进入涡流前室。 第一流动通道,第二流动通道和涡流前室被构造和适于通过改变第一和第二流动通道之间的流量分配来调整从喷射口孔喷出的喷雾角度。

    Fuel injectors for exhaust heaters

    公开(公告)号:US11454397B2

    公开(公告)日:2022-09-27

    申请号:US17405276

    申请日:2021-08-18

    Applicant: Delavan Inc.

    Abstract: A fuel injector for an exhaust heater includes a cover and an air blast nozzle. The cover has a nozzle seat, a fuel inlet, and an air inlet, the nozzle seat arranged along a flow axis. The air blast nozzle is seated in the nozzle seat and has a unibody. The air blast nozzle unibody is in fluid communication with the fuel inlet and the air inlet arranged along the flow axis to port fuel and air into a combustion volume, e.g., to heat a stream of exhaust gas flowing between an engine and a catalytic reactor by combustion with fuel introduced through the fuel inlet and air introduced through the air inlet.

    FUEL INJECTORS FOR EXHAUST HEATERS

    公开(公告)号:US20210372621A1

    公开(公告)日:2021-12-02

    申请号:US17405276

    申请日:2021-08-18

    Applicant: Delavan Inc.

    Abstract: A fuel injector for an exhaust heater includes a cover and an air blast nozzle. The cover has a nozzle seat, a fuel inlet, and an air inlet, the nozzle seat arranged along a flow axis. The air blast nozzle is seated in the nozzle seat and has a unibody. The air blast nozzle unibody is in fluid communication with the fuel inlet and the air inlet arranged along the flow axis to port fuel and air into a combustion volume, e.g., to heat a stream of exhaust gas flowing between an engine and a catalytic reactor by combustion with fuel introduced through the fuel inlet and air introduced through the air inlet.

    FLUID DISTRIBUTORS FOR FLUID NOZZLES

    公开(公告)号:US20210332981A1

    公开(公告)日:2021-10-28

    申请号:US17243246

    申请日:2021-04-28

    Applicant: Delavan Inc.

    Abstract: A fluid nozzle includes a first fluid circuit, a second fluid circuit spaced apart from the first fluid circuit and a fuel circuit. The fuel circuit is defined between the first and second fluid circuits and between a first fuel circuit wall and a second fuel circuit wall. A ring-shaped permeable barrier is positioned between the first and second fuel circuit walls configured and adapted to provide a controlled resistance to fuel flow. A fuel distributor includes a first fuel circuit wall and a second fuel circuit wall spaced apart from the first fuel circuit wall. A fuel circuit is defined between the first and second fuel circuit walls. A ring-shaped permeable barrier is positioned between first and second fuel circuit walls. A combustion assembly includes a combustor housing, a combustor dome positioned at an upstream end of the combustor housing, and a fluid nozzle positioned adjacent the combustor dome.

Patent Agency Ranking