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公开(公告)号：US20130040255A1
公开(公告)日：2013-02-14
申请号：US13207352
申请日：2011-08-10
CPC分类号： F23D17/00 , C10J3/503 , C10J3/506 , C10J3/723 , C10J3/74 , C10J3/76 , C10J2200/152 , C10J2300/092 , C10J2300/093 , C10J2300/0943 , C10J2300/0946 , C10J2300/0956 , C10J2300/0959 , C10J2300/0969 , C10J2300/0973 , C10J2300/0976 , F23D2214/00 , F23N1/002 , F23N2037/08 , F23R3/28 , F23R3/36 , F23R2900/00004 , Y02E20/16 , Y02E20/18
摘要： A system includes a gasification fuel injector, which includes a first fuel conduit configured to inject a first fuel flow from a first fuel tip, a second fuel conduit configured to inject a second fuel flow from a second fuel tip, a first gas conduit configured to inject a first gas flow from a first gas tip, a second gas conduit configured to inject a second gas flow from a second gas tip, and a third gas conduit configured to inject a third gas flow from a third gas tip. At least one of the first fuel tip, the second fuel tip, the first gas tip, the second gas tip, or the third gas tip is recessed a distance away from an outlet of the gasification fuel injector. The first and second fuel conduits and the first, second, and third gas conduits are coaxial with one another.
摘要翻译： 一种系统包括气化燃料喷射器，其包括构造成从第一燃料尖端喷射第一燃料流的第一燃料管道，以及被配置为从第二燃料尖端喷射第二燃料流的第二燃料管道，配置成 从第一气体末端注入第一气体流，配置成从第二气体末端喷射第二气体流的第二气体导管和被配置为从第三气体末端喷射第三气体流的第三气体导管。 所述第一燃料尖端，所述第二燃料尖端，所述第一气体末端，所述第二气体末端或所述第三气体末端中的至少一个与所述气化燃料喷射器的出口相距一定距离。 第一和第二燃料管道以及第一，第二和第三气体管道彼此同轴。
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公开(公告)号：US09488371B2
公开(公告)日：2016-11-08
申请号：US13207352
申请日：2011-08-10
IPC分类号： F23D14/62 , F23N5/00 , B05B7/08 , F02C1/00 , F23D17/00 , F23N1/00 , F23R3/28 , F23R3/36 , C10J3/50 , C10J3/72 , C10J3/74 , C10J3/76
CPC分类号： F23D17/00 , C10J3/503 , C10J3/506 , C10J3/723 , C10J3/74 , C10J3/76 , C10J2200/152 , C10J2300/092 , C10J2300/093 , C10J2300/0943 , C10J2300/0946 , C10J2300/0956 , C10J2300/0959 , C10J2300/0969 , C10J2300/0973 , C10J2300/0976 , F23D2214/00 , F23N1/002 , F23N2037/08 , F23R3/28 , F23R3/36 , F23R2900/00004 , Y02E20/16 , Y02E20/18
摘要： A system includes a gasification fuel injector, which includes a first fuel conduit configured to inject a first fuel flow from a first fuel tip, a second fuel conduit configured to inject a second fuel flow from a second fuel tip, a first gas conduit configured to inject a first gas flow from a first gas tip, a second gas conduit configured to inject a second gas flow from a second gas tip, and a third gas conduit configured to inject a third gas flow from a third gas tip. At least one of the first fuel tip, the second fuel tip, the first gas tip, the second gas tip, or the third gas tip is recessed a distance away from an outlet of the gasification fuel injector. The first and second fuel conduits and the first, second, and third gas conduits are coaxial with one another.
摘要翻译： 一种系统包括气化燃料喷射器，其包括构造成从第一燃料尖端喷射第一燃料流的第一燃料管道，以及被配置为从第二燃料尖端喷射第二燃料流的第二燃料管道，配置成 从第一气体末端注入第一气体流，配置成从第二气体末端喷射第二气体流的第二气体导管和被配置为从第三气体末端喷射第三气体流的第三气体导管。 所述第一燃料尖端，所述第二燃料尖端，所述第一气体末端，所述第二气体末端或所述第三气体末端中的至少一个与所述气化燃料喷射器的出口相距一定距离。 第一和第二燃料管道以及第一，第二和第三气体管道彼此同轴。
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公开(公告)号：US08424877B2
公开(公告)日：2013-04-23
申请号：US12464579
申请日：2009-05-12
申请人： Constantin Dinu , James Michael Storey , Aaron John Avagliano , Douglas S. Byrd , Shaoping Shi , Judeth Brannon Corry , Allyson Joy Jimenez Huyke
发明人： Constantin Dinu , James Michael Storey , Aaron John Avagliano , Douglas S. Byrd , Shaoping Shi , Judeth Brannon Corry , Allyson Joy Jimenez Huyke
IPC分类号： F16J15/447
CPC分类号： F01K23/068 , Y02E20/16 , Y02E20/18
摘要： A method and systems for a purged seal for an annular space are provided. The purged seal includes a first baffle element that extends from an inner surface of the annular space into the annular space at an oblique angle and a second baffle element that extends from an outer surface of the annular space above the first baffle element in a direction opposite gravity flow into the annular space wherein the second baffle element extends at an oblique angle. The system also includes a third baffle element that extends from the inner surface above the first baffle element in a direction of gravity flow into the annular space wherein the third baffle element extends into the annular space at an oblique angle with respect to the inner surface and wherein a distal end of the third baffle element is positioned proximate a distal end of the second baffle element.
摘要翻译： 提供了一种用于环形空间的清洗密封件的方法和系统。 清除的密封件包括第一挡板元件，其从环形空间的内表面以倾斜角延伸到环形空间中，第二挡板元件从第一挡板元件上方的环形空间的外表面沿相反方向延伸 重力流入环形空间，其中第二挡板元件以倾斜角延伸。 该系统还包括第三挡板元件，其从第一挡板元件上方的内表面沿着重力流向环形空间的方向延伸，其中第三挡板元件以相对于内表面倾斜的角度延伸到环形空间中， 其中所述第三挡板元件的远端位于所述第二挡板元件的远端附近。
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公开(公告)号：US20100288474A1
公开(公告)日：2010-11-18
申请号：US12464579
申请日：2009-05-12
申请人： Constantin Dinu , James Michael Storey , Aaron John Avagliano , Douglas S. Byrd , Shaoping Shi , Judeth Brannon Corry , Allyson Joy Jimenez Huyke
发明人： Constantin Dinu , James Michael Storey , Aaron John Avagliano , Douglas S. Byrd , Shaoping Shi , Judeth Brannon Corry , Allyson Joy Jimenez Huyke
IPC分类号： F28C3/06 , F16J15/447 , C10K1/04 , F28D7/00
CPC分类号： F01K23/068 , Y02E20/16 , Y02E20/18
摘要： A method and systems for a purged seal for an annular space are provided. The purged seal includes a first baffle element that extends from an inner surface of the annular space into the annular space at an oblique angle and a second baffle element that extends from an outer surface of the annular space above the first baffle element in a direction opposite gravity flow into the annular space wherein the second baffle element extends at an oblique angle. The system also includes a third baffle element that extends from the inner surface above the first baffle element in a direction of gravity flow into the annular space wherein the third baffle element extends into the annular space at an oblique angle with respect to the inner surface and wherein a distal end of the third baffle element is positioned proximate a distal end of the second baffle element.
摘要翻译： 提供了一种用于环形空间的清洗密封件的方法和系统。 清除的密封件包括第一挡板元件，其从环形空间的内表面以倾斜角延伸到环形空间中，第二挡板元件从第一挡板元件上方的环形空间的外表面沿相反方向延伸 重力流入环形空间，其中第二挡板元件以倾斜角延伸。 该系统还包括第三挡板元件，其从第一挡板元件上方的内表面沿着重力流向环形空间的方向延伸，其中第三挡板元件以相对于内表面倾斜的角度延伸到环形空间中， 其中所述第三挡板元件的远端位于所述第二挡板元件的远端附近。
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