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1. 发明申请

WO2006118693A1 HIGH PRESSURE DRY COAL SLURRY EXTRUSION PUMP 审中-公开
标题翻译：高压干燥煤浆挤压泵
公开(公告)号：WO2006118693A1
公开(公告)日：2006-11-09
申请号：PCT/US2006/010707
申请日：2006-03-22
申请人： THE BOEING COMPANY , SPROUSE, Kenneth, M. , MATTHEWS, David, R.
发明人： SPROUSE, Kenneth, M. , MATTHEWS, David, R.
IPC分类号： C10J3/50
CPC分类号： F27D3/18 , B01J8/003 , B01J8/0045 , B01J2208/00752 , C10J3/50 , C10J3/506 , C10J2300/0906 , C10J2300/093 , C21B11/08 , C21B13/143 , C21C7/0025 , Y02P10/136
摘要： A system for providing highly pressurized raw fuel to a pressure reactor. The system includes an inlet (33) for receiving the raw fuel (8) and a roller system (36) communicating with the inlet (33) . The roller system (36) includes a plurality of independent rollers (44) arranged in two converging planes. The rollers (44) of the roller system (36) successively compress the raw fuel (8) as the raw fuel passes through the roller system between the rollers, such that the fuel is highly pressurized when it reaches an output end of the roller system ( 36) . An outlet (42) is located adjacent the output end of the roller system (36) to dispense the pressurized raw fuel (8) to the pressure reactor.
摘要翻译：一种用于向压力反应器提供高加压原料燃料的系统。该系统包括用于接收原燃料（8）的入口（33）和与入口（33）连通的辊系统（36）。辊系统（36）包括布置在两个会聚平面中的多个独立的辊（44）。当原料燃料通过辊之间的辊系统时，辊系统（36）的辊（44）连续地压缩原燃料（8），使得当燃料到达辊系统的输出端时高度加压（36）。出口（42）位于邻近辊系统（36）的输出端，以将加压的原料燃料（8）分配到压力反应器。

2. 发明申请

WO2006101642A1 COMPACT HIGH EFFICIENCY GASIFIER 审中-公开
标题翻译：紧凑高效气化器
公开(公告)号：WO2006101642A1
公开(公告)日：2006-09-28
申请号：PCT/US2006/005968
申请日：2006-02-21
申请人： THE BOEING COMPANY , FARHANGI, Shahram , SPROUSE, Kenneth, M. , MATTHEWS, David, R.
发明人： FARHANGI, Shahram , SPROUSE, Kenneth, M. , MATTHEWS, David, R.
IPC分类号： C10J3/48
CPC分类号： C10J3/485 , C10J2200/09 , C10J2300/093 , C10J2300/0943 , C10J2300/0959 , C10J2300/0969 , C10J2300/0973 , C10J2300/1823 , Y02P20/129
摘要： A gasifier system (10) is provided that includes a gasification chamber spool (18) that has a ceramic matrix composite (CMC) liner adapted to form a solidified slag protective layer on an interior surface of the liner from molten slag flowing through the gasification chamber spool. The gasification system (10) additionally includes a heat exchanger (HEX) quench spool (26) that also includes a CMC liner adapted to form a solidified slag protective layer on an interior surface of the liner from molten slag flowing through the HEX quench spool (26) . Additionally, the HEX quench spool (26) includes a parallel plate HEX core having a plurality of CMC panels. The CMC panels are adapted to form a solidified slag protective layer on exterior surfaces of each respective CMC panel from molten slag flowing through the HEX quench spool (26) . Furthermore, each CMC panel includes a plurality of internal coolant channels adapted to exchange sensible waste heat from the hot product flowing through the HEX quench spool (26) with a coolant flowing through the internal coolant channels. The sensible waste heat absorbed by the coolant is recovered by the gasification system by utilizing the heated coolant in various operational phases of the gasification system.
摘要翻译：提供了一种气化器系统（10），其包括气化室阀芯（18），该气化室阀芯（18）具有陶瓷基体复合材料（CMC）衬垫，其适用于在衬套的内表面上形成固化的炉渣保护层，阀芯。气化系统（10）还包括热交换器（HEX）骤冷阀芯（26），该换热器（HEX）骤冷阀芯（26）还包括CMC衬套，其适用于在流经HEX骤冷阀芯的熔渣中在衬套的内表面上形成凝固的渣保护层 26）。此外，HEX骤冷线轴（26）包括具有多个CMC板的平行板HEX芯。 CMC板适于在每个相应的CMC板的外表面上形成流过HEX骤冷线轴（26）的熔渣的凝固的渣保护层。此外，每个CMC面板包括多个内部冷却剂通道，其适于通过流过HEX骤冷线轴（26）的热产物与流过内部冷却剂通道的冷却剂交换明显的废热。通过在气化系统的各种操作阶段利用加热的冷却剂，由气化系统回收由冷却剂吸收的明显的废热。

3. 发明申请

WO2008091589A1 CONTINUOUS PRESSURE LETDOWN SYSTEM 审中-公开
标题翻译：连续压力系统
公开(公告)号：WO2008091589A1
公开(公告)日：2008-07-31
申请号：PCT/US2008/000803
申请日：2008-01-22
申请人： PRATT & WHITNEY ROCKETDYNE, INC. , SPROUSE, Kenneth, M. , MATTHEWS, David, R. , LANGOWSKI, Terry
发明人： SPROUSE, Kenneth, M. , MATTHEWS, David, R. , LANGOWSKI, Terry
IPC分类号： B01D45/00
CPC分类号： B01D45/12 , B01D46/02 , B01D46/2407
摘要： A continuous pressure letdown system (10) connected to a hopper decreases a pressure of a 2-phase (gas and solid) dusty gas stream flowing through the system. The system (10) includes a discharge line (18) for receiving the dusty gas from the hopper (14), a valve (16), a cascade nozzle assembly (28) positioned downstream of the discharge line (18), a purge ring (20), an inert gas supply (24) connected to the purge ring (20), an inert gas throttle (26), and a filter (32). The valve connects the hopper (14) to the discharge line (18) and controls introduction of the dusty gas stream into the discharge line (18). The purge ring (20) is connected between the discharge line (18) and the cascade nozzle assembly (28). The inert gas throttle (26) controls a flow rate of an inert gas into the cascade nozzle assembly (28). The filter (32) is connected downstream of the cascade nozzle assembly (28).
摘要翻译：连接到料斗的连续压力降低系统（10）降低了流过系统的两相（气体和固体）多尘气流的压力。系统（10）包括用于从料斗（14）接收灰尘气体的排出管线（18），位于排放管线（18）下游的阀门（16），级联喷嘴组件（28）（20），连接到清洗环（20）的惰性气体供应源（24），惰性气体节流阀（26）和过滤器（32）。阀将料斗（14）连接到排出管（18），并控制将多尘的气流引入排出管线（18）。清洗环（20）连接在排出管线（18）和级联喷嘴组件（28）之间。惰性气体节气门（26）控制进入级联喷嘴组件（28）的惰性气体的流量。过滤器（32）连接在级联喷嘴组件（28）的下游。

4. 发明申请

WO2013009950A2 AGGLOMERATOR WITH CERAMIC MATRIX COMPOSITE OBSTACLES 审中-公开
标题翻译：具有陶瓷基体复合材料的AGGLOMERATOR
公开(公告)号：WO2013009950A2
公开(公告)日：2013-01-17
申请号：PCT/US2012/046397
申请日：2012-07-12
申请人： UNITED TECHNOLOGIES CORPORATION , SPROUSE, Kenneth, M. , MATTHEWS, David, R.
发明人： SPROUSE, Kenneth, M. , MATTHEWS, David, R.
IPC分类号： C10J3/52 , B09B5/00 , C10J3/72
CPC分类号： C10J3/84 , C10J3/00 , C10J3/74 , C10J3/76 , C10J2300/1884 , C10J2300/1892 , C10K1/022 , C10K1/026
摘要： A slag agglomerator includes an inlet, an outlet and a plurality of obstacles. The inlet receives a flow of gas and slag droplets and the outlet allows the flow of gas and slag droplets to exit the agglomerator. The obstacles are oblique or perpendicular to the flow of gas and slag droplets and have an exterior surface containing a ceramic matrix composite.
摘要翻译：渣团聚器包括入口，出口和多个障碍物。入口接收气体和熔渣液滴的流动，并且出口允许气体和熔渣液滴的流动离开凝聚器。障碍物倾斜或垂直于气体和熔渣液滴的流动并且具有包含陶瓷基质复合材料的外表面。

5. 发明申请

WO2006026046A1 METHOD AND APPARATUS FOR A COAL GASIFIER 审中-公开
标题翻译：煤气化炉的方法和装置
公开(公告)号：WO2006026046A1
公开(公告)日：2006-03-09
申请号：PCT/US2005/027611
申请日：2005-08-03
申请人： THE BOEING COMPANY , SPROUSE, Kenneth, M.
发明人： SPROUSE, Kenneth, M.
IPC分类号： C10J3/54 , C10J3/78
CPC分类号： C10J3/721 , C10J3/54 , C10J3/78 , C10J2200/09 , C10J2200/15 , C10J2300/093 , C10J2300/0943 , C10J2300/0956 , C10J2300/0959 , C10J2300/0969 , C10J2300/0973 , C10J2300/1634 , C10J2300/1687 , C10J2300/1807 , C10J2300/1838 , C10J2300/1846 , C10J2300/1884 , C10J2300/1892 , C10K1/026 , C10K1/101
摘要： A method and apparatus for efficiently forming a gaseous material from a solid starting material (116). The produced gaseous material includes a CGE HHV having a high percentage of an original HHV of the starting material (54). The gaseous product (116) may be used to form a plurality of materials for various purposes.
摘要翻译：一种用于从固体原料（116）有效地形成气态物质的方法和装置。产生的气态材料包括具有起始材料（54）的原始HHV的高百分比的CGE HHV。气态产物（116）可以用于形成用于各种目的的多种材料。

6. 发明申请

WO2009111092A3 REACTOR VESSEL AND LINER 审中-公开
公开(公告)号：WO2009111092A3
公开(公告)日：2009-09-11
申请号：PCT/US2009/030394
申请日：2009-01-08
申请人： PRATT & WHITNEY ROCKETDYNE, INC. , FUSSELMAN, Steven, P. , YOWS, Stephen Arthur , MCENERNEY, Bryan, William , SPROUSE, Kenneth, M.
发明人： FUSSELMAN, Steven, P. , YOWS, Stephen Arthur , MCENERNEY, Bryan, William , SPROUSE, Kenneth, M.
IPC分类号： B01J19/00 , C01B3/36 , C10J3/74
摘要： A reactor vessel liner system includes a liner having a plurality of first conduits and a plurality of second conduits for conveying a coolant. The plurality of second conduits is located at least partially within corresponding ones of the plurality of first conduits.

7. 发明申请

WO2012166118A1 INJECTOR MIXER FOR A COMPACT GASIFICATION REACTOR SYSTEM 审中-公开
标题翻译：用于紧凑气化反应器系统的喷射器混合器
公开(公告)号：WO2012166118A1
公开(公告)日：2012-12-06
申请号：PCT/US2011/038600
申请日：2011-05-31
申请人： PRATT & WHITNEY ROCKETDYNE, INC. , SONWANE, Chandrashekhar , SPROUSE, Kenneth, M.
发明人： SONWANE, Chandrashekhar , SPROUSE, Kenneth, M.
IPC分类号： C10J3/30 , C10J3/50 , F23D1/00 , C10J3/72
CPC分类号： F23D1/005 , B01F5/04 , C10J3/506 , C10J2200/152 , F23D1/00
摘要： An injector mixer for a gasification reactor system that utilizes reactants includes an injector body that extends between a first face and a second face. The injector body includes a first passage that extends between the first face and the second face and has a first central axis. At least one second, impinging passage extends between the first face and second face and has an associated second central axis that has an angle with the first axis. The angle satisfies mixing efficiency Equation (I) disclosed herein.
摘要翻译：利用反应物的气化反应器系统的注射器混合器包括在第一面和第二面之间延伸的注射器主体。喷射器主体包括在第一面和第二面之间延伸并具有第一中心轴线的第一通道。至少一个第二冲击通道在第一面和第二面之间延伸并且具有与第一轴线成角度的相关联的第二中心轴线。角度满足本文公开的混合效率等式（I）。

8. 发明申请

WO2004097299A2 AN APPARATUS AND METHOD FOR SELECTING A FLOW MIXTURE 审中-公开
标题翻译：选择流动混合物的装置和方法
公开(公告)号：WO2004097299A2
公开(公告)日：2004-11-11
申请号：PCT/US2004/009311
申请日：2004-03-25
申请人： THE BOEING COMPANY
发明人： SPROUSE, Kenneth, M. , VON ARX, Alan, V. , MATTHEWS, David, R.
IPC分类号： F23R
CPC分类号： F23L15/04 , F23C2900/13002 , F23R3/005 , F23R3/40 , Y02E20/348 , Y02T50/675
摘要： A counter-flow system for use in a turbine for selecting various mixtures of fluids for use with the system. The system may be used for a combustor for a gas powered turbine which employs a heat exchanger to combust a fuel without the emission of undesired chemical species. A gas powered turbine requires expanding gases to power the turbine blades. Fuel is combusted to produce the required gases. An oxidizer is introduced into the counter-flow system in a first direction before a first portion of fuel is introduced into the oxidizer. The fuel and oxidizer mixture is then flowed through a second pathway wherein the fuel and oxidizer mixture obtains a selected amount of thermal energy. Moreover, in a second pathway an equivalence ratio of the fuel and oxidizer mixture may be altered from the original fuel and oxidizer mixture.
摘要翻译：一种用于涡轮机的逆流系统，用于选择与系统一起使用的各种流体混合物。该系统可以用于燃气轮机的燃烧器，该燃气轮机采用热交换器燃烧燃料而不排放不期望的化学物质。燃气轮机需要膨胀气体来为涡轮机叶片供电。燃料燃烧以产生所需的气体。在将第一部分燃料引入氧化剂之前，将氧化剂沿第一方向引入逆流系统。燃料和氧化剂混合物然后流过第二路径，其中燃料和氧化剂混合物获得选定量的热能。此外，在第二路径中，燃料和氧化剂混合物的当量比可以从原始燃料和氧化剂混合物改变。

9. 发明申请

WO2003087672A1 A CATALYTIC COMBUSTION SYSTEM AND METHOD OF OPERATING A GAS TURBINE INCORPORATING SUCH A SYSTEM 审中-公开
标题翻译：一种催化燃烧系统和运行这种系统的气体涡轮机的方法
公开(公告)号：WO2003087672A1
公开(公告)日：2003-10-23
申请号：PCT/US2003/010365
申请日：2003-04-04
申请人： THE BOEING COMPANY
发明人： SPROUSE, Kenneth, M. , FARHANGI, Shahram , MORIARTY, Michael, P. , MATTHEWS, David, R.
IPC分类号： F23R3/40
CPC分类号： F23R3/40
摘要： A combustor for a gas powered turbine which employs a heat exchanger and a catalyst to combust a fuel without the emission of undesired chemical species. A gas powered turbine requires expanding gases to power the turbine blades. Fuel is combusted to produce the required gases. A catalyst is employed to lower the combustion temperature of the fuel. The catalyst is placed on a set of tubes in the heat exchanger such that a portion of the thermal energy may be transferred to the air before it engages the catalyst. After encountering the catalyst, the combusted fuel increases the temperature of the air to an auto-ignition temperature so that no other ignition source is needed to combust additional fuel.
摘要翻译：一种用于燃气动力涡轮机的燃烧器，其采用热交换器和催化剂燃烧燃料而不排放不期望的化学物质。燃气轮机需要膨胀气体来为涡轮机叶片供电。燃料燃烧以产生所需的气体。采用催化剂来降低燃料的燃烧温度。将催化剂放置在热交换器中的一组管上，使得一部分热能在其接合催化剂之前可以转移到空气中。在遇到催化剂之后，燃烧的燃料将空气的温度升高到自燃温度，从而不需要其它点火源来燃烧附加燃料。

10. 发明申请

WO2005108894A1 COOLED SYNTHESIS GAS GENERATOR 审中-公开
标题翻译：冷却合成气发生器
公开(公告)号：WO2005108894A1
公开(公告)日：2005-11-17
申请号：PCT/US2004/032347
申请日：2004-10-01
申请人： THE BOEING COMPANY
发明人： SPROUSE, Kenneth, M.
IPC分类号： F27D1/12
CPC分类号： C10J3/76 , C10J3/74 , C10J2200/09 , F23M5/08 , F23M2900/05004
摘要： A coolant liner for a carbonaceous fuel (coal or petcoke) gasification vessel (18) including a ceramic composite panel and a method of cooling a vessel. The panel includes at least two layers of woven yarns of fibrous material and walls (28) extending between the layers. Accordingly, the layers and the walls define coolant channels (30) that extend in a warp direction. Moreover, one of the layers may be less than about 0.08 inches thick. Materials used to create the composite panel may include alumina, chromia, silicon carbide, and carbon. Additionally, the liners may be shaped in an arc or have coolant channels which vary in diameter in the warp direction. Additionally, the liner may abut a structural closeout of the vessel. The coolant liner (28) provides a significantly more durable component than previously employed liners and is especially well suited to demanding service environnements.
摘要翻译：一种用于碳质燃料（煤或石油焦）气化容器（18）的冷却剂衬套，其包括陶瓷复合板和冷却容器的方法。面板包括至少两层纤维材料的编织纱线和在层之间延伸的壁（28）。因此，层和壁限定了沿翘曲方向延伸的冷却剂通道（30）。此外，其中一个层可以小于约0.08英寸厚。用于制造复合板的材料可包括氧化铝，氧化铬，碳化硅和碳。另外，衬垫可以成形为弧形或具有在经向方向上直径变化的冷却剂通道。此外，衬套可以邻接容器的结构性封闭。冷却剂衬套（28）提供比以前使用的衬垫更显着更耐用的部件，并且特别适合于要求苛刻的服务环境。

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