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1. 发明授权

US08375696B2 Independent manifold dual gas turbine fuel system 有权
标题翻译：独立歧管双燃气轮机燃油系统
公开(公告)号：US08375696B2
公开(公告)日：2013-02-19
申请号：US12114899
申请日：2008-05-05
申请人： William J. Lawson , Rahul Mohan Joshi
发明人： William J. Lawson , Rahul Mohan Joshi
IPC分类号： F02C3/20
CPC分类号： F02C9/40 , F02C3/22 , F02C3/28 , F02C7/222
摘要： The present application provides a dual gas fuel delivery system and a method of delivering two gas fuels. The system may include (a) a low energy gas delivery system comprising a low energy gas inlet, a gas split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet; (b) a high energy gas delivery system comprising a high energy gas inlet and a high energy gas primary manifold outlet; (c) a primary manifold; and (d) a secondary manifold, wherein the low energy gas primary manifold outlet and the high energy gas primary manifold outlet are coupled to the primary manifold, wherein the low energy gas secondary manifold outlet is coupled to the secondary manifold, and wherein the low energy gas delivery system further comprises a primary low energy gas stop and pressure control valve between the gas split and the low energy gas primary manifold outlet.
摘要翻译：本申请提供了双气体燃料输送系统和递送两种气体燃料的方法。该系统可以包括（a）低能量气体输送系统，其包括低能气体入口，气体分离器，低能量气体主歧管出口和低能气体二次歧管出口; （b）高能量气体输送系统，其包括高能气体入口和高能气体主歧管出口; （c）主歧管; 和（d）次级歧管，其中所述低能量气体主歧管出口和所述高能量气体主歧管出口联接到所述主歧管，其中所述低能量气体次级歧管出口联接到所述次级歧管，并且其中所述低能量气体输送系统还包括在气体分配和低能量气体主歧管出口之间的初级低能气体停止和压力控制阀。

2. 发明申请

US20090272097A1 Independent Manifold Dual Gas Turbine Fuel System 有权
标题翻译：独立歧管双燃气轮机燃油系统
公开(公告)号：US20090272097A1
公开(公告)日：2009-11-05
申请号：US12114899
申请日：2008-05-05
申请人： William J. Lawson , Rahul Mohan Joshi
发明人： William J. Lawson , Rahul Mohan Joshi
IPC分类号： F02C3/20
CPC分类号： F02C9/40 , F02C3/22 , F02C3/28 , F02C7/222
摘要： The present application provides a dual gas fuel delivery system and a method of delivering two gas fuels. The system may include (a) a low energy gas delivery system comprising a low energy gas inlet, a gas split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet; (b) a high energy gas delivery system comprising a high energy gas inlet and a high energy gas primary manifold outlet; (c) a primary manifold; and (d) a secondary manifold, wherein the low energy gas primary manifold outlet and the high energy gas primary manifold outlet are coupled to the primary manifold, wherein the low energy gas secondary manifold outlet is coupled to the secondary manifold, and wherein the low energy gas delivery system further comprises a primary low energy gas stop and pressure control valve between the gas split and the low energy gas primary manifold outlet.
摘要翻译：本申请提供了双气体燃料输送系统和递送两种气体燃料的方法。该系统可以包括（a）低能量气体输送系统，其包括低能气体入口，气体分离器，低能量气体主歧管出口和低能气体二次歧管出口; （b）高能量气体输送系统，其包括高能气体入口和高能气体主歧管出口; （c）主歧管; 和（d）次级歧管，其中所述低能量气体主歧管出口和所述高能量气体主歧管出口联接到所述主歧管，其中所述低能量气体次级歧管出口联接到所述次级歧管，并且其中所述低能量气体输送系统还包括在气体分配和低能量气体主歧管出口之间的初级低能气体停止和压力控制阀。

3. 发明申请

US20090272096A1 Single Manifold Dual Gas Turbine Fuel System 审中-公开
标题翻译：单歧管双燃气轮机燃油系统
公开(公告)号：US20090272096A1
公开(公告)日：2009-11-05
申请号：US12114893
申请日：2008-05-05
申请人： William J. Lawson , Rahul Mohan Joshi
发明人： William J. Lawson , Rahul Mohan Joshi
IPC分类号： F02C3/20
CPC分类号： F02C7/22 , F02C7/222 , F02C9/40
摘要： The present application provides a dual gas fuel delivery system and a method of delivering two gas fuels to a turbine. The dual gas fuel delivery system may include (a) a low energy gas delivery system comprising a low energy gas inlet and a low energy gas primary manifold outlet; (b) a high energy gas delivery system comprising a high energy gas inlet and a high energy gas primary manifold outlet; and (c) a primary manifold, wherein the low energy gas primary manifold outlet and the high energy gas primary manifold outlet are coupled to the primary manifold.
摘要翻译：本申请提供了双气体燃料输送系统和将两种气体燃料输送到涡轮机的方法。双气体燃料输送系统可以包括（a）低能量气体输送系统，其包括低能量气体入口和低能量气体主歧管出口; （b）高能量气体输送系统，其包括高能气体入口和高能气体主歧管出口; 和（c）主歧管，其中低能量气体主歧管出口和高能气体主歧管出口联接到主歧管。

4. 发明授权

US08438830B2 Primary manifold dual gas turbine fuel system 有权
标题翻译：主歧管双燃气轮机燃油系统
公开(公告)号：US08438830B2
公开(公告)日：2013-05-14
申请号：US12114905
申请日：2008-05-05
申请人： William J. Lawson , Rahul Mohan Joshi , Danny Lawing , Jitendra Morankar , Robert J. Iasillo
发明人： William J. Lawson , Rahul Mohan Joshi , Danny Lawing , Jitendra Morankar , Robert J. Iasillo
IPC分类号： F02C3/20
CPC分类号： F02C7/222 , F02C3/22 , F02C3/28 , F02C9/40
摘要： The present application provides a dual gas fuel delivery system and a method of delivering two gas fuels. The dual gas fuel delivery system may include (a) a low energy gas delivery system comprising a low energy gas inlet, a gas split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet; (b) a high energy gas delivery system comprising a high energy gas inlet and a high energy gas primary manifold outlet; (c) a primary manifold; and (d) a secondary manifold, wherein the low energy gas primary manifold outlet and the high energy gas primary manifold outlet are coupled to the primary manifold, and wherein the low energy gas secondary manifold outlet is coupled to the secondary manifold.
摘要翻译：本申请提供了双气体燃料输送系统和递送两种气体燃料的方法。双气体燃料输送系统可以包括（a）低能气体输送系统，其包括低能气体入口，气体分离，低能气体主歧管出口和低能气体二次歧管出口; （b）高能量气体输送系统，其包括高能气体入口和高能气体主歧管出口; （c）主歧管; 和（d）次级歧管，其中所述低能量气体主歧管出口和所述高能气体主歧管出口连接到所述主歧管，并且其中所述低能量气体次级歧管出口连接到所述次级歧管。

5. 发明申请

US20090272098A1 Primary Manifold Dual Gas Turbine Fuel System 有权
标题翻译：主歧管双燃气轮机燃油系统
公开(公告)号：US20090272098A1
公开(公告)日：2009-11-05
申请号：US12114905
申请日：2008-05-05
申请人： William J. Lawson , Rahul Mohan Joshi , Danny Lawing , Jitendra Morankar , Robert J. Iasillo
发明人： William J. Lawson , Rahul Mohan Joshi , Danny Lawing , Jitendra Morankar , Robert J. Iasillo
IPC分类号： F02C3/20
CPC分类号： F02C7/222 , F02C3/22 , F02C3/28 , F02C9/40
摘要： The present application provides a dual gas fuel delivery system and a method of delivering two gas fuels. The dual gas fuel delivery system may include (a) a low energy gas delivery system comprising a low energy gas inlet, a gas split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet; (b) a high energy gas delivery system comprising a high energy gas inlet and a high energy gas primary manifold outlet; (c) a primary manifold; and (d) a secondary manifold, wherein the low energy gas primary manifold outlet and the high energy gas primary manifold outlet are coupled to the primary manifold, and wherein the low energy gas secondary manifold outlet is coupled to the secondary manifold.
摘要翻译：本申请提供了双气体燃料输送系统和递送两种气体燃料的方法。双气体燃料输送系统可以包括（a）低能气体输送系统，其包括低能气体入口，气体分离，低能气体主歧管出口和低能气体二次歧管出口; （b）高能量气体输送系统，其包括高能气体入口和高能气体主歧管出口; （c）主歧管; 和（d）次级歧管，其中所述低能量气体主歧管出口和所述高能气体主歧管出口连接到所述主歧管，并且其中所述低能量气体次级歧管出口连接到所述次级歧管。

6. 发明申请

US20110154802A1 PARALLEL TURBINE FUEL CONTROL VALVES 审中-公开
标题翻译：并联涡轮燃油控制阀
公开(公告)号：US20110154802A1
公开(公告)日：2011-06-30
申请号：US13043015
申请日：2011-03-08
申请人： Rahul Mohan Joshi , William J. Lawson
发明人： Rahul Mohan Joshi , William J. Lawson
IPC分类号： F02C9/26
CPC分类号： F02C9/40 , F02C7/22 , F05D2220/722 , Y02E20/18
摘要： A fuel system for a turbine, including a plurality of fuel control valves connected to the turbine and in parallel with each other; and a controller for opening each of the control valves to pass a lower controllable fuel flow through each valve, and for further opening one of the control valves in response to a control signal for controlling the turbine.
摘要翻译：一种用于涡轮机的燃料系统，包括连接到涡轮机并且彼此并联的多个燃料控制阀; 以及控制器，用于打开每个控制阀，以通过每个阀的下部可控燃料流，并响应用于控制涡轮的控制信号进一步打开一个控制阀。

7. 发明申请

US20090025396A1 Parallel turbine fuel control valves 审中-公开
标题翻译：平行涡轮燃油控制阀
公开(公告)号：US20090025396A1
公开(公告)日：2009-01-29
申请号：US11880700
申请日：2007-07-24
申请人： Rahul Mohan Joshi , William J. Lawson
发明人： Rahul Mohan Joshi , William J. Lawson
IPC分类号： F02C9/00
CPC分类号： F02C9/40 , F02C7/22 , F05D2220/722 , Y02E20/18
摘要： A fuel system for a turbine, including a plurality of fuel control valves connected to the turbine and in parallel with each other, and a controller for opening each of the control valves to pass a lower controllable fuel flow through each valve, and for further opening one of the control valves in response to a control signal for controlling the turbine.
摘要翻译：一种用于涡轮机的燃料系统，包括连接到涡轮机并且彼此并联的多个燃料控制阀，以及用于打开每个控制阀以使下部可控燃料流通过每个阀并用于进一步打开的控制器一个控制阀响应用于控制涡轮机的控制信号。

8. 发明授权

US09261023B2 Systems and methods for monitoring fluid separation and/or monitoring the health of a valve 有权
标题翻译：用于监测流体分离和/或监测阀门健康的系统和方法
公开(公告)号：US09261023B2
公开(公告)日：2016-02-16
申请号：US13343243
申请日：2012-01-04
申请人： William J. Lawson , Brittany L. Sater
发明人： William J. Lawson , Brittany L. Sater
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F05D2270/3015 , F16K37/0091 , Y10T137/0318 , Y10T137/2931
摘要： The present subject matter is generally directed to fuel systems for a gas turbine and related methods for monitoring fluid separation in the fuel systems. More particularly, the systems and methods include measuring pressure differentials and comparing the measurements to a predetermined value.
摘要翻译：本发明主要涉及用于燃气轮机的燃料系统和用于监测燃料系统中的流体分离的相关方法。更具体地，系统和方法包括测量压差并将测量值与预定值进行比较。

9. 发明授权

US4253941A Controlled buoyancy separator apparatus and method 失效
标题翻译：控制浮力分离装置及方法
公开(公告)号：US4253941A
公开(公告)日：1981-03-03
申请号：US81311
申请日：1979-10-03
申请人： William J. Lawson
发明人： William J. Lawson
IPC分类号： B03B5/62 , B03B5/66
CPC分类号： B03B5/623
摘要： To avoid using salt in a costly flotation separator process for various products of differing specific gravities, a fresh water flotation system is employed having a controlled buoyancy zone in which an induced current or up-flow elevates the product component of lesser specific gravity causing it to overflow a product conveyor divider member and to settle on that side of the conveyor away from the product component of greater specific gravity. The separation of clam meat from clam shells is envisioned.
摘要翻译：为了避免在用于不同比重的各种产品的昂贵的浮选分离器方法中使用盐，使用具有受控浮力区域的淡水浮选系统，其中感应电流或上升流使提高较小比重的产物组分导致其溢出产品输送机分隔件，并将输送机的该侧定位在较大比重的产品部件上。蛤蜊肉与蛤壳分离是可以预见的。

10. 发明授权

US4057880A Method of producing snag resistant hosiery article 失效
标题翻译：生产防汗袜子制品的方法
公开(公告)号：US4057880A
公开(公告)日：1977-11-15
申请号：US725998
申请日：1976-09-23
申请人： Robert M. Matthews , William J. Lawson
发明人： Robert M. Matthews , William J. Lawson
IPC分类号： D04B1/26 , D02G1/00
CPC分类号： D04B1/26
摘要： The snag resistant leg portion of this hosiery article is knit of a composite self-crimping yarn including a series of mechanical crimps imparted thereto prior to knitting, and a series of crimps imparted to the composite yarn by development of the latent crimp in the composite yarn after knitting. The hosiery article knit of the composite self-comprising yarn having both types of crimp therein has much greater snag or pick resistance than either a hosiery article knit of the same type of composite yarn but including only the crimps imparted by development of the latent crimp in the yarn, or a hosiery article knit of yarn having mechanical crimp only. The knitting of a mechanically crimped composite yarn also produces a normal size greige hosiery article blank which may be processed in the usual manner to produce the finished hosiery article.
摘要翻译：该针织物的防滑腿部是编织前的一系列机械卷曲的复合自卷曲纱，并且通过在复合纱中形成潜在卷曲而赋予复合纱线的一系列卷曲针织后。具有两种类型的卷曲的复合自包纱的针织品编织比相同类型的复合纱线的针织品针织物具有更大的阻碍或抗拉强度，但是仅包括通过显影潜在卷曲而产生的卷曲纱线或仅具有机械卷曲的纱线针织品。机械卷曲复合纱线的编织也产生正常尺寸的粗针织物品坯料，其可以以常规方式加工以制造成品针织物品。

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