ATOMIZERS
    61.
    发明申请
    ATOMIZERS 有权
    原型

    公开(公告)号:US20160236215A1

    公开(公告)日:2016-08-18

    申请号:US15044814

    申请日:2016-02-16

    Applicant: Delavan Inc

    Abstract: An atomizer includes an atomizer body with a plurality of air passages defined therethrough from an upstream end of the atomizer body to a downstream end thereof. The air passages together define an air circuit through the atomizer body. A fuel circuit is defined in the atomizer body extending from a fuel inlet to a respective fuel outlet opening into each air passage. The air passages can be arranged circumferentially about a central axis defined by the atomizer body. The fuel circuit can include a manifold extending circumferentially about the atomizer body in fluid communication with a fuel opening in each respective air passage.

    Abstract translation: 雾化器包括雾化器主体,其具有从雾化器主体的上游端到其下游端限定的多个空气通道。 空气通道一起限定通过雾化器主体的空气回路。 燃料电路限定在雾化器主体中,从燃料入口延伸到相应的燃料出口到每个空气通道。 空气通道可以围绕由雾化器主体限定的中心轴线周向布置。 燃料回路可以包括围绕雾化器主体周向延伸的歧管,其与每个相应空气通道中的燃料开口流体连通。

    HEAT SHIELDING FOR INTERNAL FUEL MANIFOLDS

    公开(公告)号:US20220136443A1

    公开(公告)日:2022-05-05

    申请号:US17578926

    申请日:2022-01-19

    Applicant: Delavan Inc.

    Abstract: A fuel injector system includes an outer support and an inner support, with a feed arm extending radially between the inner support and the outer support. A plurality of outlet openings extend in an axial direction from the feed arm for feeding respective injection nozzles. The outer support and feed arm define a plurality of fuel passages therethrough to convey fluid from an external source through the outer support and feed arm to the outlet openings. A heat shield extends around the feed arm from the outer support to the inner support. The heat shield is spaced apart from the feed arm with an insulative gap therebetween.

    Fuel injectors for exhaust heaters
    63.
    发明授权

    公开(公告)号:US11118785B2

    公开(公告)日:2021-09-14

    申请号:US16171859

    申请日:2018-10-26

    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.

    Gas turbine combustion liner comprising heat transfer cell heat pipes

    公开(公告)号:US11073282B2

    公开(公告)日:2021-07-27

    申请号:US15686944

    申请日:2017-08-25

    Applicant: Delavan Inc.

    Abstract: A heat transfer arrangement includes two or more heat transfer cells. The heat transfer cells together define a boundary between a higher temperature region and a lower temperature region. Each of the two or more heat transfer cells includes two or more walls defining a fluid tight cavity. One or more wick is fused to an inner surface of one or more of the walls to wick liquid from a lower temperature portion of the cavity to a higher temperature portion of the cavity. Combustors having heat transfer arrangements with heat transfer cells and methods of making heat transfer arrangements are also described.

    Internal manifold for multipoint injection

    公开(公告)号:US11060459B2

    公开(公告)日:2021-07-13

    申请号:US16031696

    申请日:2018-07-10

    Applicant: Delavan Inc.

    Abstract: A multipoint injection system includes a manifold with a plurality of flow passages defined through the manifold in the circumferential direction. The flow passages are spaced apart from one another in an axial direction. A plurality of feed arms extends radially inward from the manifold. Feed arm portions of the flow passages extend through each of the feed arms to respective outlets. The feed arm portions of the flow passages are within the axial width of the manifold. A plurality of injection nozzles are included, each in fluid communication with a respective one of the outlets. Each injection nozzle includes an air passage therethrough with an air inlet. The feed arms each follow a path that is circumferentially offset from the air inlets so each of the feed arms is clear from a flow path directly upstream in the axial direction of each of the air inlets.

    Internal fuel manifolds
    68.
    发明授权

    公开(公告)号:US10774748B2

    公开(公告)日:2020-09-15

    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.

    Fuel nozzle manifold systems for turbomachines

    公开(公告)号:US10605171B2

    公开(公告)日:2020-03-31

    申请号:US15949776

    申请日:2018-04-10

    Applicant: Delavan Inc.

    Abstract: An internal fuel manifold for a turbomachine can include an outer ring defining one or more fuel supply channels configured to allow fuel flow around at least a portion of a circumference of the outer ring, and a plurality of branches extending radially inward from the outer ring. The branches include a high aspect ratio shape. The plurality of branches can include one or more branch fuel channels in fluid communication with at least one of the one or more fuel supply channels. The manifold includes one or more injector connectors extending axially aft from each branch, each injector connector in fluid communication with a branch fuel channel and configured to connect to a fuel injector. The manifold can include an inner ring extending from the plurality of branches. The inner ring and the outer ring are configured to receive a fuel injector and combustor assembly therebetween and to allow retaining of the fuel injector assembly and combustor assembly to the internal fuel manifold.

    DISCRETE JET ORIFICES
    70.
    发明申请

    公开(公告)号:US20200072129A1

    公开(公告)日:2020-03-05

    申请号:US16676855

    申请日:2019-11-07

    Applicant: Delavan Inc.

    Abstract: A nozzle tip includes a nozzle tip body defining an upstream surface and an opposed downstream surface. An outlet orifice is defined through the nozzle tip body for fluid communication from a space upstream of the upstream surface to a space downstream of the downstream surface. The outlet orifice includes a cylindrical outlet portion defining an outlet axis, and a tapered inlet portion upstream of the outlet portion. The tapered inlet portion converges down towards the outlet axis in a direction from the upstream surface toward the downstream surface.

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