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1. 发明授权

US06685903B2 Method of purifying and recycling argon 有权
标题翻译：氩气净化和回收方法
公开(公告)号：US06685903B2
公开(公告)日：2004-02-03
申请号：US09725778
申请日：2001-03-01
申请人： Kenneth K. Wong , Dante Patrick Bonaquist
发明人： Kenneth K. Wong , Dante Patrick Bonaquist
IPC分类号： C01B2300
CPC分类号： F25J3/0252 , B01D53/00 , B01D53/02 , B01D2251/202 , B01D2257/104 , B01D2257/2064 , B01D2257/2066 , C01B23/0094 , C01B2210/0006 , C01B2210/0014 , C01B2210/0045 , C01B2210/0046 , F25J3/0257 , F25J3/0285 , F25J3/08 , F25J2200/02 , F25J2200/04 , F25J2200/30 , F25J2200/50 , F25J2200/74 , F25J2205/60 , F25J2205/82 , F25J2215/04 , F25J2215/50 , F25J2215/58 , F25J2245/58 , F25J2270/12 , F25J2270/42 , F25J2290/62 , Y02C10/08 , Y02C10/12 , Y02P20/152 , Y02P20/154 , Y10S62/924
摘要： This invention is directed to a method for purifying argon from an impure argon stream. If the oxygen concentration in the impure argon is less than about 10 mole percent of oxygen, the invention is proceeded in the sequential steps of a) removing chlorine from the impure argon stream; b) adding hydrogen to the impure argon stream; c) removing carbon dioxide and water from the impure argon stream; d) removing hydrogen from the impure argon stream; and e) removing nitrogen from the impure argon stream to form a purified argon stream. If the oxygen concentration in the impure argon is greater than about 10 mole percent of oxygen, the method comprises the sequential steps of a) removing chlorine from the impure argon stream; b) removing carbon dioxide and water from the impure argon stream; c) removing nitrogen and oxygen from the impure argon stream; d) adding hydrogen to the impure argon stream; e) removing water from the impure argon stream; f) removing hydrogen from the impure argon stream; and g) removing nitrogen from the impure argon stream to form a purified stream.
摘要翻译：本发明涉及一种从不纯的氩气流中纯化氩气的方法。如果不纯的氩气中的氧气浓度小于约10摩尔％的氧气，则本发明按照以下顺序进行：a）从不纯的氩气流中除去氯气; b）向不纯的氩气流中加入氢气; c）从不纯的氩气流中除去二氧化碳和水; d）从不纯的氩气流中除去氢; 和e）从不纯的氩气流中除去氮气以形成纯化的氩气流。如果不纯的氩气中的氧气浓度大于约10摩尔％的氧气，则该方法包括以下顺序步骤：a）从不纯的氩气流中除去氯气; b）从不纯的氩气流中除去二氧化碳和水; c）从不纯的氩气流中除去氮气和氧气; d）向不纯的氩气流中加入氢气; e）从不纯的氩气流中除去水; f）从不纯的氩气流中除去氢; 和g）从不纯的氩气流中除去氮气以形成纯化的物流。

2. 发明授权

US07306646B2 Utilization of compressor surge control air in an aircraft on-board inert gas generating system 有权
标题翻译：利用压缩机喘振控制空气在飞机上的惰性气体发生系统
公开(公告)号：US07306646B2
公开(公告)日：2007-12-11
申请号：US10973374
申请日：2004-10-26
申请人： Kenneth K. Wong
发明人： Kenneth K. Wong
IPC分类号： B01D53/22
CPC分类号： B01D53/22 , B01D2257/104 , B64D37/32 , B64D2013/0677 , Y02T50/44
摘要： Improvements in aircraft on-board inert gas generating systems wherein generally excess or surplus compressed airflow from a radial flow centrifugal compressor, produced in order to keep the compressor from surging in predetermined “reduced speed/reduced pressure ratio” operating modes, is utilized for at least one of driving a turbofan for conditioning the air separator module inlet air, or warming up/heating an air separator module in the inert gas generating system, thereby utilizing at least some of the energy of this excess/surplus compressed air that would otherwise be wasted. Several preferential operational methods and structural systems are set forth.
摘要翻译：飞机机载惰性气体发生系统的改进，其中通常为了保持压缩机在预定的“减速/减压比”操作模式下的喘振而产生的来自径流式离心式压缩机的过量或过剩的压缩气流被用于至少一个驾驶涡轮风扇来调节空气分离器模块入口空气，或者加热/加热惰性气体发生系统中的空气分离器模块，从而利用这种过剩/过剩压缩空气的至少一些能量，否则这些能量将是浪费了阐述了若干优惠作业方法和结构体系。

3. 发明授权

US08979028B2 Anti-cross flow fuel vent system architecture 有权
标题翻译：反交叉燃油通风系统架构
公开(公告)号：US08979028B2
公开(公告)日：2015-03-17
申请号：US13819364
申请日：2011-10-12
申请人： Kenneth K. Wong , Stephen C. Metrulas , Rogerio Konig da Silva , Michel Loignon
发明人： Kenneth K. Wong , Stephen C. Metrulas , Rogerio Konig da Silva , Michel Loignon
IPC分类号： B64C17/10 , B64D37/10 , B60K15/035 , B64D37/06 , B64D37/32
CPC分类号： B60K15/035 , B60K2015/03523 , B60Y2200/51 , B64D37/06 , B64D37/32 , Y02T50/44 , Y10T137/86324
摘要： A venting system (10) in an aircraft (12), where the aircraft (12) is substantially symmetrical about a midline (14), has a pair of wings (16 and 18) extending outwardly on respective sides of the midline (14), a center fuel tank (20), a surge tank (22 and 24) at outer ends of each wing (16 and 18), and optionally one or more wing fuel tanks (26 and 28) interposed between the center fuel tank (20) and the respective surge tank (22 or 24). The venting system (10) for the center fuel tank (20) includes a main vent line (30) that extends across the midline (14) to vent openings (32 and 34) communicating with respective surge tanks (22 and 24). The main vent line (30) forms a linear flow path for fluid, generally air, flowing between opposite ends of the vent line (30). The venting system (10) also includes a branch vent line (36 and 38) extending from the main vent line (30) and opening on the center fuel tank (20). The branch line has at least one fuel tank opening (40 and 42) on each side of the midline (14).
摘要翻译：在飞行器（12）中的飞行器（12）围绕中线（14）基本对称的排气系统（10）具有在中线（14）的相应侧上向外延伸的一对翼（16和18），中心燃料箱（20），在每个翼（16和18）的外端处的缓冲罐（22和24），以及可选地一个或多个翼燃料箱（26和28），其插入在中心燃料箱）和相应的缓冲罐（22或24）。用于中心燃料箱（20）的排气系统（10）包括主通风管线（30），该主排气管线延伸穿过中线（14），以便与各个缓冲罐（22和24）连通的排气口（32和34）。主排气管线（30）形成在通气管线（30）的相对端之间流动的流体（通常是空气）的线性流动路径。排气系统（10）还包括从主排气管线（30）延伸并在中心燃料箱（20）上开口的分支排气管线（36和38）。分支线在中线（14）的每一侧具有至少一个燃料箱开口（40和42）。

4. 发明申请

US20130168111A1 FUEL TANK FLAMMABILITY-REDUCING GAS DISTRIBUTION ARCHITECTURE 审中-公开
标题翻译：燃油罐易燃气体分配架构
公开(公告)号：US20130168111A1
公开(公告)日：2013-07-04
申请号：US13819741
申请日：2011-10-12
申请人： Kenneth K. Wong , Stephen C. Metrulas
发明人： Kenneth K. Wong , Stephen C. Metrulas
IPC分类号： A62C2/04
CPC分类号： A62C2/04 , B64D37/32
摘要： A flammability-reducing gas distribution system (10) for an aircraft includes a conduit (20) for distributing flammability-reducing gas within the fuel tank (12) while preventing or minimizing the potential for the buildup of a column of liquid against a separating valve (24) that prevents the exit of liquid fuel from the fuel tank (12). The conduit (20) includes a trap (26) in which liquid that enters the conduit (20) will accumulate. The trap (26) includes a drain (30), such as a float drain valve, to drain liquid from the trap (26) back into the fuel tank (12). The trap (26) includes a section of the conduit (20) at a local minimum elevation between sections of conduit (20) with relatively higher elevations. Consequently, any liquid that enters the distribution conduit (20) can be captured in the trap (26), minimizing or eliminating the opportunity for a liquid column to form against the separating valve (24).
摘要翻译：一种用于飞行器的可燃性降低气体分配系统（10）包括用于在燃料箱（12）内分配易燃性气体的导管（20），同时防止或最小化一列液体积聚在分离阀（24），其防止来自燃料箱（12）的液体燃料的排出。导管（20）包括其中将进入导管（20）的液体将聚集的捕集器（26）。捕集器（26）包括排水口（30），例如浮子排水阀，以将液体从捕集器（26）排回到燃料箱（12）中。捕集器（26）包括导管（20）的在具有相对较高海拔的导管（20）的部分之间的局部最小高度处的部分。因此，进入分配管道（20）的任何液体都可以捕获在捕集器（26）中，从而最小化或消除液柱形成抵靠分离阀（24）的机会。

5. 发明申请

US20130161342A1 ANTI-CROSS FLOW FUEL VENT SYSTEM ARCHITECTURE 有权
标题翻译：反交叉燃油通风系统架构
公开(公告)号：US20130161342A1
公开(公告)日：2013-06-27
申请号：US13819364
申请日：2011-10-12
申请人： Kenneth K. Wong , Stephen C. Metrulas , Rogerio Konig da Silva , Michel Loignon
发明人： Kenneth K. Wong , Stephen C. Metrulas , Rogerio Konig da Silva , Michel Loignon
IPC分类号： B60K15/035
CPC分类号： B60K15/035 , B60K2015/03523 , B60Y2200/51 , B64D37/06 , B64D37/32 , Y02T50/44 , Y10T137/86324
摘要： A venting system (10) in an aircraft (12), where the aircraft (12) is substantially symmetrical about a midline (14), has a pair of wings (16 and 18) extending outwardly on respective sides of the midline (14), a center fuel tank (20), a surge tank (22 and 24) at outer ends of each wing (16 and 18), and optionally one or more wing fuel tanks (26 and 28) interposed between the center fuel tank (20) and the respective surge tank (22 or 24). The venting system (10) for the center fuel tank (20) includes a main vent line (30) that extends across the midline (14) to vent openings (32 and 34) communicating with respective surge tanks (22 and 24). The main vent line (30) forms a linear flow path for fluid, generally air, flowing between opposite ends of the vent line (30). The venting system (10) also includes a branch vent line (36 and 38) extending from the main vent line (30) and opening on the center fuel tank (20). The branch line has at least one fuel tank opening (40 and 42) on each side of the midline (14).
摘要翻译：在飞行器（12）中的飞行器（12）围绕中线（14）基本对称的排气系统（10）具有在中线（14）的相应侧上向外延伸的一对翼（16和18），中心燃料箱（20），在每个翼（16和18）的外端处的缓冲罐（22和24），以及可选地一个或多个翼燃料箱（26和28），其插入在中心燃料箱）和相应的缓冲罐（22或24）。用于中心燃料箱（20）的排气系统（10）包括主通风管线（30），该主排气管线延伸穿过中线（14），以便与各个缓冲罐（22和24）连通的排气口（32和34）。主排气管线（30）形成在通气管线（30）的相对端之间流动的流体（通常是空气）的线性流动路径。排气系统（10）还包括从主排气管线（30）延伸并在中心燃料箱（20）上开口的分支排气管线（36和38）。分支线在中线（14）的每一侧具有至少一个燃料箱开口（40和42）。

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