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公开(公告)号：US20100092896A1
公开(公告)日：2010-04-15
申请号：US12250875
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
CPC分类号： F23R3/04 , F23L7/005 , F23L2900/07002 , F23L2900/07003 , F23L2900/07009 , F23R3/283 , F23R3/44 , F23R3/60 , F23R2900/00017 , Y02E20/342
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. At least one shroud is secured to the baffle plate and includes at least one piston ring disposed at the shroud. The at least one piston ring is configured to meter a flow of diluent between the at least one shroud and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a piston ring gap defined by at least one piston ring disposed at a baffle plate and a fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the piston ring gap toward at least one airflow hole in the fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 至少一个护罩固定在挡板上并且包括设置在护罩上的至少一个活塞环。 所述至少一个活塞环构造成测量所述至少一个护罩和所述至少一个燃料喷嘴之间的稀释剂流。 还公开了一种向燃烧器提供稀释剂的方法，包括提供由设置在挡板上的至少一个活塞环限定的活塞环间隙和延伸穿过挡板中的通孔的燃料喷嘴。 稀释剂通过活塞环间隙朝向燃料喷嘴中的至少一个气流孔流动。
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公开(公告)号：US20100089020A1
公开(公告)日：2010-04-15
申请号：US12250933
申请日：2008-10-14
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A circumferentially adjustable collar is located at the at least one baffle hole between the baffle plate and the at least one fuel nozzle. A plurality of openings at the collar are configured to meter a flow of diluent between the baffle hole and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings disposed at a circumferentially adjustable collar between a baffle plate and at least one fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow hole in the at least one fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 一个可周向调节的套环位于挡板和至少一个燃料喷嘴之间的至少一个挡板孔处。 在轴环处的多个开口被配置成测量在挡板孔和至少一个燃料喷嘴之间的稀释剂流。 还公开了一种用于向燃烧器提供稀释剂的方法，包括提供设置在挡板和至少一个延伸穿过挡板中的通孔的燃料喷嘴之间的周向可调环圈处的多个开口。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流孔流动。
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公开(公告)号：US09121609B2
公开(公告)日：2015-09-01
申请号：US12250875
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
CPC分类号： F23R3/04 , F23L7/005 , F23L2900/07002 , F23L2900/07003 , F23L2900/07009 , F23R3/283 , F23R3/44 , F23R3/60 , F23R2900/00017 , Y02E20/342
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. At least one shroud is secured to the baffle plate and includes at least one piston ring disposed at the shroud. The at least one piston ring is configured to meter a flow of diluent between the at least one shroud and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a piston ring gap defined by at least one piston ring disposed at a baffle plate and a fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the piston ring gap toward at least one airflow hole in the fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 至少一个护罩固定在挡板上并且包括设置在护罩上的至少一个活塞环。 所述至少一个活塞环构造成测量所述至少一个护罩和所述至少一个燃料喷嘴之间的稀释剂流。 还公开了一种向燃烧器提供稀释剂的方法，包括提供由设置在挡板上的至少一个活塞环限定的活塞环间隙和延伸穿过挡板中的通孔的燃料喷嘴。 稀释剂通过活塞环间隙朝向燃料喷嘴中的至少一个气流孔流动。
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公开(公告)号：US08567199B2
公开(公告)日：2013-10-29
申请号：US12250995
申请日：2008-10-14
IPC分类号： F02C3/20
CPC分类号： F23R3/28 , F23L7/00 , F23L2900/07002 , F23L2900/07009
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A plurality of injection holes extend through the at least one fuel nozzle and are configured to meter a flow of diluent into the combustor. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings located at at least one fuel nozzle extending through a through hole in a baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 多个喷射孔延伸穿过至少一个燃料喷嘴，并被配置成计量稀释剂流入燃烧器的流量。 还公开了一种用于向燃烧器提供稀释剂的方法，包括提供多个位于至少一个延伸穿过挡板中的通孔的燃料喷嘴的开口。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。
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5.发明申请METHOD AND FLOW SLEEVE PROFILE REDUCTION TO EXTEND COMBUSTOR LINER LIFE 审中-公开方法和流程套件减少扩展COMBUSTOR LINER LIFE公开(公告)号：US20100300107A1
公开(公告)日：2010-12-02
申请号：US12474371
申请日：2009-05-29
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , James Thomas Brown , Mark Allan Hadley , Patrick Benedict Melton , Svetlana Yakubova
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , James Thomas Brown , Mark Allan Hadley , Patrick Benedict Melton , Svetlana Yakubova
摘要： A gas turbine includes a combustor liner having at least one hole formed therein. The gas turbine also includes a flow sleeve that at least partially surrounds the liner thereby forming a plenum between the flow sleeve and the liner, the plenum having an airflow therethrough, a portion of the airflow passing through the at least one hole in the liner and into the liner thereby reducing the mass of the airflow in the plenum. The flow sleeve has an axial profile that is reduced in cross section dimension at a predetermined axial location of the flow sleeve, thereby reducing a width of the plenum at the predetermined axial location. The reduction at the cross section dimension in the flow sleeve increases a velocity of the airflow in the plenum at the predetermined axial location, the increased velocity airflow increasing transfer of heat away from the liner.
摘要翻译： 燃气轮机包括其中形成有至少一个孔的燃烧器衬套。 燃气轮机还包括至少部分地围绕衬套的流动套管，从而在流动套筒和衬套之间形成一个气室，气室具有穿过其中的气流，一部分气流穿过衬套中的至少一个孔， 进入衬里，从而减小了气室中气流的质量。 流动套筒具有在流动套筒的预定轴向位置处的横截面尺寸减小的轴向轮廓，从而减小了在预定轴向位置处的增压室的宽度。 流动套管中的横截面尺寸的减小增加了在预定轴向位置处的增压室中的气流的速度，增加的速度气流增加了热量从衬套的转移。
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公开(公告)号：US20100089022A1
公开(公告)日：2010-04-15
申请号：US12251050
申请日：2008-10-14
IPC分类号： F02C3/30
CPC分类号： F23R3/04 , F23L7/005 , F23L2900/07002 , F23R3/10 , F23R3/283 , F23R2900/00012
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A shroud is disposed between the baffle plate and the at least one fuel nozzle and is affixed to the baffle plate. A plurality of openings in the shroud are configured to meter a flow of diluent between the baffle hole and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings disposed in a shroud affixed to a baffle plate and disposed between the baffle plate and at least one fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 挡板布置在挡板和至少一个燃料喷嘴之间并且固定到挡板上。 护罩中的多个开口构造成测量在挡板孔和至少一个燃料喷嘴之间的稀释剂流。 还公开了一种用于向燃烧器提供稀释剂的方法，包括提供设置在固定到挡板上的护罩中的多个开口，并设置在挡板和延伸穿过挡板中的通孔的至少一个燃料喷嘴之间。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。
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公开(公告)号：US20100089021A1
公开(公告)日：2010-04-15
申请号：US12250995
申请日：2008-10-14
CPC分类号： F23R3/28 , F23L7/00 , F23L2900/07002 , F23L2900/07009
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A plurality of injection holes extend through the at least one fuel nozzle and are configured to meter a flow of diluent into the combustor. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings located at at least one fuel nozzle extending through a through hole in a baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.
摘要翻译： 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 多个喷射孔延伸穿过至少一个燃料喷嘴，并被配置成计量稀释剂流入燃烧器的流量。 还公开了一种用于向燃烧器提供稀释剂的方法，包括提供多个位于至少一个延伸穿过挡板中的通孔的燃料喷嘴的开口。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。
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公开(公告)号：US20100281872A1
公开(公告)日：2010-11-11
申请号：US12436524
申请日：2009-05-06
摘要： A fuel nozzle tip for use with a combustor and a method of assembling the fuel nozzle tip are provided. The fuel nozzle tip includes a fuel tube and an air collar coupled to the fuel tube. The fuel tube includes a first plurality of circumferentially-spaced fuel openings and a second plurality of circumferentially-spaced fuel openings. The fuel tube is configured to channel fuel into a mixing zone defined within the combustor. The air collar includes a plurality of circumferentially-spaced air openings configured to discharge air into the mixing zone. At least one of the plurality of air openings is oriented to facilitate generating a swirl number of greater than 0.6 within the mixing zone.
摘要翻译： 提供了一种用于燃烧器的燃料喷嘴头和组装燃料喷嘴头的方法。 燃料喷嘴尖端包括燃料管和联接到燃料管的空气环。 燃料管包括第一多个周向间隔开的燃料开口和第二多个周向间隔开的燃料开口。 燃料管构造成将燃料引导到限定在燃烧器内的混合区域中。 空气环包括多个周向间隔开的空气开口，其构造成将空气排放到混合区中。 多个空气开口中的至少一个被定向以便于在混合区域内产生大于0.6的涡旋数。
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公开(公告)号：US20100281871A1
公开(公告)日：2010-11-11
申请号：US12436445
申请日：2009-05-06
摘要： A fuel nozzle tip for use with a combustor and a method of assembling the fuel nozzle tip are provided. The fuel nozzle tip includes a fuel tube and an air collar coupled to the fuel tube. The fuel tube includes a first plurality of circumferentially-spaced fuel openings and a second plurality of circumferentially-spaced fuel openings. The fuel tube is configured to channel fuel into a mixing zone defined within the combustor. The air collar includes a plurality of circumferentially-spaced air openings configured to discharge air into the mixing zone.
摘要翻译： 提供了一种用于燃烧器的燃料喷嘴头和组装燃料喷嘴头的方法。 燃料喷嘴尖端包括燃料管和联接到燃料管的空气环。 燃料管包括第一多个周向间隔开的燃料开口和第二多个周向间隔开的燃料开口。 燃料管构造成将燃料引导到限定在燃烧器内的混合区域中。 空气环包括多个周向间隔开的空气开口，其构造成将空气排放到混合区中。
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公开(公告)号：US08607570B2
公开(公告)日：2013-12-17
申请号：US12436445
申请日：2009-05-06
IPC分类号： F23R3/28
摘要： A fuel nozzle tip for use with a combustor and a method of assembling the fuel nozzle tip are provided. The fuel nozzle tip includes a fuel tube and an air collar coupled to the fuel tube. The fuel tube includes a first plurality of circumferentially-spaced fuel openings and a second plurality of circumferentially-spaced fuel openings. The fuel tube is configured to channel fuel into a mixing zone defined within the combustor. The air collar includes a plurality of circumferentially-spaced air openings configured to discharge air into the mixing zone.
摘要翻译： 提供了一种用于燃烧器的燃料喷嘴头和组装燃料喷嘴头的方法。 燃料喷嘴尖端包括燃料管和联接到燃料管的空气环。 燃料管包括第一多个周向间隔开的燃料开口和第二多个周向间隔开的燃料开口。 燃料管构造成将燃料引导到限定在燃烧器内的混合区域中。 空气环包括多个周向间隔开的空气开口，其构造成将空气排放到混合区中。
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