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1. 发明授权

US07841180B2 Method and apparatus for controlling combustor operability 有权
标题翻译：用于控制燃烧器可操作性的方法和装置
公开(公告)号：US07841180B2
公开(公告)日：2010-11-30
申请号：US11613049
申请日：2006-12-19
申请人： Gilbert O. Kraemer , John Joseph Lipinski , Jonathan Lloyd Male
发明人： Gilbert O. Kraemer , John Joseph Lipinski , Jonathan Lloyd Male
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F02C7/22 , F05D2270/082 , F05D2300/2118 , F23R3/286 , F23R3/40 , F23R2900/00017 , Y10T29/49229
摘要： A method for assembling a gas turbine engine includes providing at least one combustor assembly defining a combustion chamber. At least one fuel nozzle is positioned at a forward end of the combustion chamber. The at least one fuel nozzle is configured to inject a premixed fuel/air mixture into the combustion chamber. A catalytic material is applied to at least a portion of the at least one fuel nozzle.
摘要翻译：一种用于组装燃气涡轮发动机的方法包括提供限定燃烧室的至少一个燃烧器组件。至少一个燃料喷嘴位于燃烧室的前端。至少一个燃料喷嘴构造成将预混燃料/空气混合物注入燃烧室。催化材料被施加到至少一个燃料喷嘴的至少一部分。

2. 发明授权

US07810333B2 Method and apparatus for operating a turbine engine 有权
标题翻译：用于操作涡轮发动机的方法和装置
公开(公告)号：US07810333B2
公开(公告)日：2010-10-12
申请号：US11537730
申请日：2006-10-02
申请人： Gilbert O. Kraemer , Benjamin Lacy , John Joseph Lipinski
发明人： Gilbert O. Kraemer , Benjamin Lacy , John Joseph Lipinski
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/286 , F23D2900/00002 , F23D2900/00018 , F23D2900/14241 , F23R3/02 , F23R3/12 , F23R3/34
摘要： A method of operating a turbine engine includes providing at least one combustor having a chamber defined therein. The assembly includes at least one combustor wall defining the chamber and a first fluid passage defining a first fluid inlet within the wall. The first fluid passage is coupled in flow communication with the chamber and is configured to inject a first fluid stream. The assembly further includes at least one second fluid passage defining at least one second fluid inlet within the wall. The second fluid inlet is adjacent to the first fluid inlet and is coupled in flow communication with the chamber. The method also includes injecting the first fluid stream and injecting the second fluid stream into the chamber at an oblique angle with respect to the first fluid stream, thereby intersecting and mixing the second fluid stream with the first fluid stream.
摘要翻译：一种操作涡轮发动机的方法包括提供至少一个具有限定在其中的室的燃烧器。组件包括限定腔室的至少一个燃烧器壁和限定壁内的第一流体入口的第一流体通道。第一流体通道与室流动连通地联接并且被配置为注入第一流体流。组件还包括限定壁内的至少一个第二流体入口的至少一个第二流体通道。第二流体入口与第一流体入口相邻并且与腔室流动连通地联接。该方法还包括注射第一流体流并将第二流体流以相对于第一流体流倾斜的角度注入到腔室中，从而将第二流体流与第一流体流交叉并混合。

3. 发明申请

US20080078160A1 METHOD AND APPARATUS FOR OPERATING A TURBINE ENGINE 有权
标题翻译：用于运行涡轮发动机的方法和装置
公开(公告)号：US20080078160A1
公开(公告)日：2008-04-03
申请号：US11537730
申请日：2006-10-02
申请人： Gilbert O Kraemer , Benjamin Lacy , John Joseph Lipinski
发明人： Gilbert O Kraemer , Benjamin Lacy , John Joseph Lipinski
IPC分类号： B64G1/40
CPC分类号： F23R3/286 , F23D2900/00002 , F23D2900/00018 , F23D2900/14241 , F23R3/02 , F23R3/12 , F23R3/34
摘要： A method of operating a turbine engine includes providing at least one combustor having a chamber defined therein. The assembly includes at least one combustor wall defining the chamber and a first fluid passage defining a first fluid inlet within the wall. The first fluid passage is coupled in flow communication with the chamber and is configured to inject a first fluid stream. The assembly further includes at least one second fluid passage defining at least one second fluid inlet within the wall. The second fluid inlet is adjacent to the first fluid inlet and is coupled in flow communication with the chamber. The method also includes injecting the first fluid stream and injecting the second fluid stream into the chamber at an oblique angle with respect to the first fluid stream, thereby intersecting and mixing the second fluid stream with the first fluid stream.
摘要翻译：一种操作涡轮发动机的方法包括提供至少一个具有限定在其中的室的燃烧器。组件包括限定腔室的至少一个燃烧器壁和限定壁内的第一流体入口的第一流体通道。第一流体通道与室流动连通地联接并且被配置为注入第一流体流。组件还包括限定壁内的至少一个第二流体入口的至少一个第二流体通道。第二流体入口与第一流体入口相邻并且与腔室流动连通地联接。该方法还包括注射第一流体流并将第二流体流以相对于第一流体流倾斜的角度注入到腔室中，从而将第二流体流与第一流体流交叉并混合。

4. 发明申请

US20090223225A1 METHOD AND APPARATUS FOR CONTROLLING COMBUSTOR OPERABILITY 有权
标题翻译：控制组合机操作性的方法和装置
公开(公告)号：US20090223225A1
公开(公告)日：2009-09-10
申请号：US11613049
申请日：2006-12-19
申请人： Gilbert O. Kraemer , John Joseph Lipinski , Jonsthan Lloyd Male
发明人： Gilbert O. Kraemer , John Joseph Lipinski , Jonsthan Lloyd Male
IPC分类号： F23R3/40 , B23P11/00 , F23R3/28 , F02C7/22
CPC分类号： F02C7/22 , F05D2270/082 , F05D2300/2118 , F23R3/286 , F23R3/40 , F23R2900/00017 , Y10T29/49229
摘要： A method for assembling a gas turbine engine includes providing at least one combustor assembly defining a combustion chamber. At least one fuel nozzle is positioned at a forward end of the combustion chamber. The at least one fuel nozzle is configured to inject a premixed fuel/air mixture into the combustion chamber. A catalytic material is applied to at least a portion of the at least one fuel nozzle.
摘要翻译：一种用于组装燃气涡轮发动机的方法包括提供限定燃烧室的至少一个燃烧器组件。至少一个燃料喷嘴位于燃烧室的前端。至少一个燃料喷嘴构造成将预混燃料/空气混合物注入燃烧室。催化材料被施加到至少一个燃料喷嘴的至少一部分。

5. 发明申请

US20100101204A1 DILUENT SHROUD FOR COMBUSTOR 有权
标题翻译：公司的DILUENT SHROUD
公开(公告)号：US20100101204A1
公开(公告)日：2010-04-29
申请号：US12260545
申请日：2008-10-29
申请人： Jonathan Dwight Berry , John Joseph Lipinski , Girard Albert Simons , Abhijit Som
发明人： Jonathan Dwight Berry , John Joseph Lipinski , Girard Albert Simons , Abhijit Som
IPC分类号： F02C3/30
CPC分类号： F23R3/10 , F23R3/28
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 through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.
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通过挡板孔的燃料喷嘴。至少一个稀释剂护罩固定在所述至少一个挡板上，并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法，包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。稀释剂流通过多个空气旋流器孔流入混合室。

6. 发明授权

US07546743B2 Bolting configuration for joining ceramic combustor liner to metal mounting attachments 有权
标题翻译：将陶瓷燃烧器衬套连接到金属安装附件的螺栓结构
公开(公告)号：US07546743B2
公开(公告)日：2009-06-16
申请号：US11247129
申请日：2005-10-12
申请人： David Edward Bulman , Toby George Darkins, Jr. , Mark Stewart Schroder , John Joseph Lipinski
发明人： David Edward Bulman , Toby George Darkins, Jr. , Mark Stewart Schroder , John Joseph Lipinski
IPC分类号： F23R3/60
CPC分类号： F23R3/60 , F23R3/007
摘要： A gas turbine combustor includes a substantially cylindrical combustor liner located substantially concentrically within a flow sleeve, the combustor liner composed through a ceramic matrix composite material, a forward end of the combustor liner provided with a plurality of circumferentially arranged bolt holes. An inner metal ring is located about an outside surface of the forward end of the combustor liner, the inner metal ring provided with a second plurality of circumferentially spaced bolt holes, with a plurality of bolts extending through the first and second pluralities of bolt holes and secured by self-locking nuts. An outer metal ring is spaced radially outwardly of the inner metal ring, with a plurality of circumferentially spaced struts extending between the inner and outer rings.
摘要翻译：燃气轮机燃烧器包括基本上圆柱形的燃烧器衬套，其基本上同心地位于流动套管内，燃烧器衬套通过陶瓷基体复合材料构成，燃烧器衬套的前端设有多个周向布置的螺栓孔。内金属环位于燃烧器衬套的前端的外表面周围，内金属环设置有第二多个周向间隔开的螺栓孔，多个螺栓延伸穿过第一和第二多个螺栓孔，由自锁螺母固定。外金属环与内金属环径向向外间隔开，多个周向隔开的支柱在内环和外环之间延伸。

7. 发明授权

US07707835B2 Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air 有权
标题翻译：用于涡轮机燃烧器的轴流套筒和引入流动套管空气的方法
公开(公告)号：US07707835B2
公开(公告)日：2010-05-04
申请号：US11152234
申请日：2005-06-15
申请人： John Joseph Lipinski , Thomas Edward Johnson , Robert Paul Ziegler , Mark Stewart Schroder
发明人： John Joseph Lipinski , Thomas Edward Johnson , Robert Paul Ziegler , Mark Stewart Schroder
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/04
摘要： A combustor has a flow sleeve and a flow liner defining a generally axial flow direction of compressor discharge air toward combustor burners. A casing is secured to the forward end of the flow sleeve defining an annular plenum along the interior of the flow sleeve. Openings through the flow sleeve supply compressor discharge air into the plenum where the air changes direction for flow through apertures into and generally coaxially with the free air stream. The axial injection minimizes or eliminates energy losses due to cross flow injection within the axial air stream while continuing to cool the liner.
摘要翻译：燃烧器具有流动套筒和流动衬套，其限定压缩机向燃烧器燃烧器排出空气的大致轴向流动方向。壳体被固定到流动套筒的前端，沿着流动套管的内部限定环形增压室。通过流动套筒供应压缩机的开口将空气排放到空气室中，其中空气改变方向以通过孔流入并大体上与自由空气流同轴。轴向注射使轴向空气流内的横流注入最小化或消除能量损失，同时继续冷却衬套。

8. 发明申请

US20080034759A1 METHODS AND APPARATUS FOR RADIALLY COMPLIANT COMPONENT MOUNTING 有权
标题翻译：用于放射性合成元件安装的方法和装置
公开(公告)号：US20080034759A1
公开(公告)日：2008-02-14
申请号：US11463142
申请日：2006-08-08
申请人： David Edward Bulman , Toby George Darkins , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
发明人： David Edward Bulman , Toby George Darkins , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F02C3/14 , F05D2230/642 , F05D2300/21 , F05D2300/50212 , F05D2300/603 , F23R3/007
摘要： Methods and apparatus for a mounting assembly for a liner of a gas turbine engine combustor are provided. The combustor includes a combustor liner and a radially outer annular flow sleeve. The mounting assembly includes an inner ring surrounding a radially outer surface of the liner and including a plurality of axially extending fingers. The mounting assembly also includes a radially outer ring coupled to the inner ring through a plurality of spacers that extend radially from a radially outer surface of the inner ring to the outer ring.
摘要翻译：提供了一种用于燃气涡轮发动机燃烧器的衬套的安装组件的方法和装置。燃烧器包括燃烧器衬套和径向外部环形流动套筒。安装组件包括围绕衬套的径向外表面的内环，并且包括多个轴向延伸的指状物。安装组件还包括通过多个间隔件联接到内环的径向外环，其从内环的径向外表面径向延伸到外环。

9. 发明授权

US08454350B2 Diluent shroud for combustor 有权
标题翻译：用于燃烧器的稀释罩
公开(公告)号：US08454350B2
公开(公告)日：2013-06-04
申请号：US12260545
申请日：2008-10-29
申请人： Jonathan Dwight Berry , John Joseph Lipinski , Girard Albert Simons , Abhijit Som
发明人： Jonathan Dwight Berry , John Joseph Lipinski , Girard Albert Simons , Abhijit Som
IPC分类号： F23C5/00
CPC分类号： F23R3/10 , F23R3/28
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 through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.
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通过挡板孔的燃料喷嘴。至少一个稀释剂护罩固定在所述至少一个挡板上，并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法，包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。稀释剂流通过多个空气旋流器孔流入混合室。

10. 发明授权

US08141370B2 Methods and apparatus for radially compliant component mounting 有权
标题翻译：用于径向兼容部件安装的方法和装置
公开(公告)号：US08141370B2
公开(公告)日：2012-03-27
申请号：US11463142
申请日：2006-08-08
申请人： David Edward Bulman , Toby George Darkins, Jr. , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
发明人： David Edward Bulman , Toby George Darkins, Jr. , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F02C3/14 , F05D2230/642 , F05D2300/21 , F05D2300/50212 , F05D2300/603 , F23R3/007
摘要： Methods and apparatus for a mounting assembly for a liner of a gas turbine engine combustor are provided. The combustor includes a combustor liner and a radially outer annular flow sleeve. The mounting assembly includes an inner ring surrounding a radially outer surface of the liner and including a plurality of axially extending fingers. The mounting assembly also includes a radially outer ring coupled to the inner ring through a plurality of spacers that extend radially from a radially outer surface of the inner ring to the outer ring.
摘要翻译：提供了一种用于燃气涡轮发动机燃烧器的衬套的安装组件的方法和装置。燃烧器包括燃烧器衬套和径向外部环形流动套筒。安装组件包括围绕衬套的径向外表面的内环，并且包括多个轴向延伸的指状物。安装组件还包括通过多个间隔件联接到内环的径向外环，其从内环的径向外表面径向延伸到外环。

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