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公开(公告)号：US08869536B2
公开(公告)日：2014-10-28
申请号：US13558470
申请日：2012-07-26
Applicant: Robert Wade Clifford , Jonathan Hale Kegley
Inventor： Robert Wade Clifford , Jonathan Hale Kegley
CPC classification number: F23J13/00 , F23R3/002 , F23R3/46 , F23R3/60 , F23R2900/00017
Abstract: A liner stop for retaining a flow sleeve relative to a combustion liner in a combustor is disclosed. The liner stop includes a female component defining a recess and a male component comprising a protrusion, the protrusion insertable in the female component. The liner stop further includes an insert disposable between the female component and the male component, the insert comprising a surface protrusion configured to interfere with one of the female component or the male component.
Abstract translation: 公开了一种用于在燃烧器中相对于燃烧衬套保持流动套管的衬套止动件。 衬垫止动件包括限定凹部的阴部件和包括凸起的阳部件，突出部可插入阴部件中。 衬垫止挡件还包括在阴部件和阳部件之间一次性使用的插入件，插入件包括被配置为干涉阴部件或阳部件之一的表面突起。
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Patent Agency Ranking
公开(公告)号：US20140026581A1
公开(公告)日：2014-01-30
申请号：US13558470
申请日：2012-07-26
Applicant: Robert Wade Clifford , Jonathan Hale Kegley
Inventor： Robert Wade Clifford , Jonathan Hale Kegley
CPC classification number: F23J13/00 , F23R3/002 , F23R3/46 , F23R3/60 , F23R2900/00017
Abstract: A liner stop for retaining a flow sleeve relative to a combustion liner in a combustor is disclosed. The liner stop includes a female component defining a recess and a male component comprising a protrusion, the protrusion insertable in the female component. The liner stop further includes an insert disposable between the female component and the male component, the insert comprising a surface protrusion configured to interfere with one of the female component or the male component.
Abstract translation: 公开了一种用于在燃烧器中相对于燃烧衬套保持流动套管的衬套止动件。 衬垫止动件包括限定凹部的阴部件和包括凸起的阳部件，突出部可插入阴部件中。 衬垫止挡件还包括在阴部件和阳部件之间一次性使用的插入件，插入件包括被配置为干涉阴部件或阳部件之一的表面突起。
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公开(公告)号：US20120247108A1
公开(公告)日：2012-10-04
申请号：US13075055
申请日：2011-03-29
Applicant: Bryan Wesley Romig , Jonathan Hale Kegley , Robert Wade Clifford , Derrick Walter Simons
CPC classification number: G01N1/2252 , F01D21/003 , F05D2270/80 , F23N5/003 , F23N5/18 , F23N2031/18 , F23N2041/20 , F23N2900/05005 , F23R3/00
Abstract: Embodiments of the present disclosure are directed towards a turbine combustor probe having a combustion dynamics monitoring probe configured to monitor combustion dynamics within a turbine combustor. The turbine combustor probe also has a gas sampling sleeve configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor.
Abstract translation: 本公开的实施例涉及具有燃烧动力学监测探针的涡轮机燃烧器探头，其被配置为监测涡轮机燃烧器内的燃烧动力学。 涡轮机燃烧器探头还具有气体采样套筒，该气体采样套筒构造成从涡轮机燃烧器的衬套和流动套筒之间的气流通道收集气体样品。
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公开(公告)号：US08997558B2
公开(公告)日：2015-04-07
申请号：US13075055
申请日：2011-03-29
Applicant: Bryan Wesley Romig , Jonathan Hale Kegley , Robert Wade Clifford , Derrick Walter Simons
CPC classification number: G01N1/2252 , F01D21/003 , F05D2270/80 , F23N5/003 , F23N5/18 , F23N2031/18 , F23N2041/20 , F23N2900/05005 , F23R3/00
Abstract: Embodiments of the present disclosure are directed towards a turbine combustor probe having a combustion dynamics monitoring probe configured to monitor combustion dynamics within a turbine combustor. The turbine combustor probe also has a gas sampling sleeve configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor.
Abstract translation: 本公开的实施例涉及具有燃烧动力学监测探针的涡轮机燃烧器探头，其被配置为监测涡轮机燃烧器内的燃烧动力学。 涡轮机燃烧器探头还具有气体采样套筒，该气体采样套筒构造成从涡轮机燃烧器的衬套和流动套筒之间的气流通道收集气体样品。
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公开(公告)号：US08745987B2
公开(公告)日：2014-06-10
申请号：US12914537
申请日：2010-10-28
Applicant: Lucas John Stoia , Jonathan Hale Kegley , Crystal McGee McConnaughhay , Bryan Wesley Romig
Inventor： Lucas John Stoia , Jonathan Hale Kegley , Crystal McGee McConnaughhay , Bryan Wesley Romig
IPC: F02C7/228
CPC classification number: F02C7/22 , F05D2270/07 , F05D2270/31
Abstract: A late lean injection (LLI) manifold is provided and includes a central nozzle and first and second side nozzles positioned at circumferential locations defined around a vessel, a connector, a first leg, to which the connector is connected, formed to define a tube extending from the central nozzle to the first side nozzle such that fuel is communicable between the connector, the central nozzle and the first side nozzle and a second leg. The second leg is formed to define a tube extending from the central nozzle to the second side nozzle such that the fuel is communicable between the central nozzle and the second side nozzle.
Abstract translation: 提供了一种后期稀薄注射（LLI）歧管，并且包括中心喷嘴和位于围绕容器限定的周向位置处的第一和第二侧面喷嘴，连接器，连接器连接的第一腿，形成为限定延伸的管 从中心喷嘴到第一侧喷嘴，使得燃料可在连接器，中心喷嘴和第一侧喷嘴与第二支管之间连通。 第二腿形成为限定从中心喷嘴延伸到第二侧喷嘴的管，使得燃料可在中心喷嘴和第二侧喷嘴之间连通。
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公开(公告)号：US20120102958A1
公开(公告)日：2012-05-03
申请号：US12914537
申请日：2010-10-28
Applicant: Lucas John Stoia , Jonathan Hale Kegley , Crystal McGee McConnaughhay , Bryan Wesley Romig
Inventor： Lucas John Stoia , Jonathan Hale Kegley , Crystal McGee McConnaughhay , Bryan Wesley Romig
IPC: F02C7/22
CPC classification number: F02C7/22 , F05D2270/07 , F05D2270/31
Abstract: A late lean injection (LLI) manifold is provided and includes a central nozzle and first and second side nozzles positioned at circumferential locations defined around a vessel, a connector, a first leg, to which the connector is connected, formed to define a tube extending from the central nozzle to the first side nozzle such that fuel is communicable between the connector, the central nozzle and the first side nozzle and a second leg. The second leg is formed to define a tube extending from the central nozzle to the second side nozzle such that the fuel is communicable between the central nozzle and the second side nozzle.
Abstract translation: 提供了一种后期稀薄注射（LLI）歧管，并且包括中心喷嘴和位于围绕容器限定的周向位置处的第一和第二侧面喷嘴，连接器，连接器连接的第一腿，形成为限定延伸的管 从中心喷嘴到第一侧喷嘴，使得燃料可在连接器，中心喷嘴和第一侧喷嘴与第二支管之间连通。 第二腿形成为限定从中心喷嘴延伸到第二侧喷嘴的管，使得燃料可在中心喷嘴和第二侧喷嘴之间连通。
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