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公开(公告)号:US20140319401A1
公开(公告)日:2014-10-30
申请号:US13872970
申请日:2013-04-29
Applicant: DELAVAN INC
Inventor: Jason Allen Ryon , Chien-Jung Yu , Philip E. O. Buelow , Neal Thomson
IPC: F16K1/32
CPC classification number: F23R3/28 , F23K2301/206 , F23K2401/201 , F23K2900/05001
Abstract: A valve for regulating fluid flowing bidirectionally therethrough includes a first flow body defining a passage configured to direct fluid flow in a downstream direction defined from the inlet to the outlet. The inlet includes an enlargement configured to provide decreased resistance to fluid flow in the downstream direction relative to flow in an upstream direction opposite the downstream direction.
Abstract translation: 用于调节流体双向流动的阀通过其中包括限定通道的第一流动体,所述通道被构造成沿着从入口到出口限定的下游方向引导流体流动。 入口包括放大部件,其被构造成相对于沿着与下游方向相反的上游方向的流动而向下游方向提供降低的流体流动阻力。
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公开(公告)号:US09745936B2
公开(公告)日:2017-08-29
申请号:US13767402
申请日:2013-02-14
Applicant: Delavan Inc
Inventor: Jason Allen Ryon , Philip E. O. Buelow , John Earl Short
CPC classification number: F02M61/162 , F23D11/383 , F23D2213/00 , F23D2900/11101 , F23R3/28
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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公开(公告)号:US09080772B2
公开(公告)日:2015-07-14
申请号:US13917053
申请日:2013-06-13
Applicant: Delavan Inc
Inventor: Lev Alexander Prociw , Jason Allen Ryon , Steven Jay Myers , Nicole L. Nelson , Roger A. Seei
CPC classification number: F23R3/20 , F23C2900/03005 , F23D2207/00 , F23D2900/11401 , F23N2027/02 , F23R3/14 , F23R3/28
Abstract: An ignition system includes a housing defining an interior and an exhaust outlet. The housing is configured and adapted to be mounted to a combustor to issue flame from the exhaust outlet into the combustor for ignition and flame stabilization within the combustor. A fuel injector is mounted to the housing with an outlet of the fuel injector directed to issue a spray of fuel into the interior of the housing. An igniter is mounted to the housing with an ignition point of the igniter proximate the outlet of the fuel injector for ignition within the interior of the housing.
Abstract translation: 点火系统包括限定内部和排气出口的壳体。 壳体被构造和适于安装到燃烧室,以将火焰从排气出口发射到燃烧器中,用于燃烧器内的点燃和火焰稳定。 燃料喷射器安装到壳体上,燃料喷射器的出口被引导以将燃料喷射发射到壳体的内部。 点火器被安装到壳体上,点火器的点火点靠近燃料喷射器的出口,用于在壳体的内部点燃。
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公开(公告)号:US20140366551A1
公开(公告)日:2014-12-18
申请号:US13917053
申请日:2013-06-13
Applicant: Delavan Inc.
Inventor: Lev Alexander Prociw , Jason Allen Ryon , Steven Jay Myers , Nicole L. Nelson , Roger A. Seei
CPC classification number: F23R3/20 , F23C2900/03005 , F23D2207/00 , F23D2900/11401 , F23N2027/02 , F23R3/14 , F23R3/28
Abstract: An ignition system includes a housing defining an interior and an exhaust outlet. The housing is configured and adapted to be mounted to a combustor to issue flame from the exhaust outlet into the combustor for ignition and flame stabilization within the combustor. A fuel injector is mounted to the housing with an outlet of the fuel injector directed to issue a spray of fuel into the interior of the housing. An igniter is mounted to the housing with an ignition point of the igniter proximate the outlet of the fuel injector for ignition within the interior of the housing.
Abstract translation: 点火系统包括限定内部和排气出口的壳体。 壳体被构造和适于安装到燃烧室,以将火焰从排气出口发射到燃烧器中,用于燃烧器内的点火和火焰稳定。 燃料喷射器安装到壳体上,燃料喷射器的出口被引导以将燃料喷射发射到壳体的内部。 点火器被安装到壳体上,点火器的点火点靠近燃料喷射器的出口,用于在壳体的内部点燃。
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公开(公告)号:US10161633B2
公开(公告)日:2018-12-25
申请号:US13783832
申请日:2013-03-04
Applicant: Delavan Inc , Phyllis Hetheriton
Inventor: Gary Chew , Viraphand Cholvibul , Philip E. O. Buelow , Jason Allen Ryon
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.
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公开(公告)号:US20140245742A1
公开(公告)日:2014-09-04
申请号:US13783832
申请日:2013-03-04
Applicant: Phyllis Hetheriton , DELAVAN INC
Inventor: Gary Chew , Viraphand Cholvibul , Philip E. O. Buelow , Jason Allen Ryon
IPC: F23R3/14
CPC classification number: F23R3/14 , F05D2240/127 , F23C7/002 , F23D11/103 , F23D11/105 , F23D11/107 , F23D11/383 , F23D14/24 , F23D2900/11101 , F23D2900/14021 , F23D2900/14701 , F23R3/12 , F23R3/28 , F23R3/286 , F23R3/343
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。
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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
Inventor: Jason Allen Ryon , Philip E. O. Buelow , John Earl Short
IPC: F02M61/16
CPC classification number: F02M61/162 , F23D11/383 , F23D2213/00 , F23D2900/11101 , F23R3/28
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。
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