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公开(公告)号：US20080170948A1
公开(公告)日：2008-07-17
申请号：US11622338
申请日：2007-01-11
Applicant: Bobby D. Martinez , John R. Wolflick , Jaleel Valappil
Inventor： Bobby D. Martinez , John R. Wolflick , Jaleel Valappil
CPC classification number: F04C23/001 , F04D27/0269 , F25J1/0022 , F25J1/0283 , F25J1/0298 , F25J2280/10
Abstract: An improved system and methodology for starting up a gas-turbine driven multi-stage compressor. The improvement involves isolating individual compression stages and creating positive pressure in each stage prior to initiating rotation of the compressor/driver system. The isolation of individual compression stages allows the turbine to reach normal operating speeds with substantially no supplemental power from an auxiliary source.
Abstract translation: 一种用于启动燃气轮机驱动的多级压缩机的改进的系统和方法。 该改进涉及在启动压缩机/驱动器系统的旋转之前在每个阶段隔离各个压缩级并产生正压。 单独的压缩级的隔离允许涡轮达到正常的运行速度，基本上没有来自辅助源的补充功率。
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公开(公告)号：US20080056910A1
公开(公告)日：2008-03-06
申请号：US11470010
申请日：2006-09-05
Applicant: John R. Wolflick , Megan V. Evans , Jaleel Valappil , Bobby D. Martinez , Marc Bellomy
Inventor： John R. Wolflick , Megan V. Evans , Jaleel Valappil , Bobby D. Martinez , Marc Bellomy
IPC: F04B49/00
CPC classification number: F04D27/0261 , F04D25/04 , F25J1/0022 , F25J1/0283 , F25J1/0298 , F25J2280/20
Abstract: An anti-bogdown control system monitors and regulates operation of a turbine and a compressor to prevent underspeed trip of the turbine while avoiding surge of the compressor. A turbine speed controller receives a turbine speed signal and a turbine temperature signal, generates a surge margin setpoint, and regulates overfiring of the turbine. A surge margin controller associated with the compressor receives the surge margin setpoint from the turbine speed controller and receives a load signal from one or more sensors and modulates a compressor throttle valve so that the compressor operates at a surge margin that is approximately equal to the surge margin setpoint. In a system with multiple compressors driven by a single turbine, a surge margin controller is associated with each compressor.
Abstract translation: 防倒档控制系统监测和调节涡轮机和压缩机的操作，以防止涡轮机的低速跳闸，同时避免压缩机的浪涌。 涡轮转速控制器接收涡轮转速信号和涡轮温度信号，产生浪涌余量设定点，并调节涡轮机过热。 与压缩机相关联的浪涌余量控制器接收来自涡轮转速控制器的喘振余量设定值，并接收来自一个或多个传感器的负载信号并调制压缩机节流阀，使得压缩机以大约等于浪涌的喘振裕度 余量设定值 在具有由单个涡轮机驱动的多个压缩机的系统中，喘振裕度控制器与每个压缩机相关联。
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公开(公告)号：US06172124B2
公开(公告)日：2001-01-09
申请号：US08950312
申请日：1997-10-14
Applicant: John R. Wolflick , Gary L. Beer , Richard L. Payne
Inventor： John R. Wolflick , Gary L. Beer , Richard L. Payne
IPC: C07C2700
CPC classification number: C10G2/32 , C01B3/382 , C01B2203/142 , C01B2203/82 , C07C1/0485 , Y02P20/123 , Y02P20/129
Abstract: A process for converting a hydrocarbon gas (e.g. natural gas) to syngas which, in turn, is converted into a liquid hydrocarbon product wherein a substantial amount of the heat generated in the process is recovered for use in generating steam needed in the process or for conversion into mechanical energy. Further, tail gas produced by the process is used to fuel the gas turbine which, in turn, is used power the compressors needed for compressing the air used in the process. By using tail gas to fuel the gas turbine, less of the compressed combustion-air is needed to cool the combustion gases in the turbine and, instead, can be used to provide a portion of the process-air required in the process; thereby possibly saving up to 20 to 30 percent of the horsepower otherwise needed to compress the required volume of process-air.
Abstract translation: 将烃气体（例如天然气）转化为合成气的方法，合成气又转化为液体烃产物，其中回收在该过程中产生的大量热量用于产生该方法中所需的蒸汽或用于 转化为机械能。 此外，由该方法产生的尾气被用于燃料燃气轮机，燃气轮机又被用于压缩在该过程中使用的空气所需的压缩机。 通过使用尾气来燃料燃气轮机，需要较少的压缩燃烧空气来冷却涡轮机中的燃烧气体，并且可以用来提供该方法中所需的一部分过程空气; 从而可能节省高达20％至30％的马力，否则需要压缩所需体积的加工空气。
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4.发明授权Method for increasing oil production from an oil well producing a mixture of oil and gas 失效从油井生产石油和天然气的混合物提高石油生产的方法
公开(公告)号：US5794697A
公开(公告)日：1998-08-18
申请号：US757857
申请日：1996-11-27
Applicant: John R. Wolflick , James L. Cawvey , Jerry L. Brady , John R. Whitworth , David D. Hearn
Inventor： John R. Wolflick , James L. Cawvey , Jerry L. Brady , John R. Whitworth , David D. Hearn
CPC classification number: E21B43/18 , E21B43/385
Abstract: A system and a method for producing increased quantities of oil from an oil well producing a mixture of oil and gas through a well bore penetrating an oil bearing formation containing a gas cap zone and an oil bearing zone by separating at least a portion of the gas from the mixture of oil and gas downhole in an auger separator to produce a separated gas and an oil enriched mixture; compressing at least a portion of the separated gas downhole to a pressure greater than the pressure in the gas cap zone to produce a compressed gas; and, injecting the compressed gas into the gas cap and, recovering at least a major portion of the oil enriched mixture.
Abstract translation: 一种用于从油井产生更多量的油的系统和方法，其产生油和气体的混合物，穿过穿透含有气帽区域和含油区域的含油地层的井眼，通过分离至少一部分气体 从螺旋分离器中的井下油和油的混合物产生分离的气体和富含油的混合物; 将井下的分离气体的至少一部分压缩至大于气帽区域中的压力的压力以产生压缩气体; 并且将压缩气体注入气帽并回收至少大部分富油混合物。
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5.发明授权公开(公告)号：US08323000B2
公开(公告)日：2012-12-04
申请号：US12144196
申请日：2008-06-23
Applicant: Saul Mirsky , Jeff McWhirter , John R. Wolflick
Inventor： Saul Mirsky , Jeff McWhirter , John R. Wolflick
IPC: F04B49/03
CPC classification number: F04D27/0253 , F01D15/08 , F02C6/12
Abstract: A control method and apparatus for simultaneously protecting a compression system from driver overpowering and turbocompressor surge. When overpowering is detected, flow rate through the each compressor in the turbocompressor train is reduced by closing an inlet throttling valve at the inlet of each respective compressor stage unless a compressor operating point is sufficiently near surge. In this latter case, the inlet throttling valve is not closed. In this way, overall flow rate through the compressor train is reduced while maintaining adequate flow through compromised stages to avoid surge.
Abstract translation: 一种用于同时保护压缩系统免受驾驶员超车和涡轮压缩机喘振的控制方法和装置。 当检测到超压时，通过在每个相应的压缩机级的入口处关闭入口节流阀来减少通过涡轮压缩机列中的每个压缩机的流量，除非压缩机工作点充分接近喘振。 在后一种情况下，入口节流阀不关闭。 以这种方式，通过压缩机系统的整个流量被减小，同时通过受损阶段保持足够的流量以避免浪涌。
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Patent Agency Ranking
公开(公告)号：US6156234A
公开(公告)日：2000-12-05
申请号：US405431
申请日：1999-09-23
Applicant: Michael D. Briscoe , Kernan J. McHugh , John R. Wolflick
Inventor： Michael D. Briscoe , Kernan J. McHugh , John R. Wolflick
CPC classification number: C01B3/382
Abstract: An improved process for the compression and heating of air or oxygen-enriched air for charging to an autothermal reactor by using a single high compression ratio compressor to produce a high-pressure, high-temperature air or oxygen-enriched air stream for mixture with a hydrocarbon gas stream to produce a charge stream to an autothermal reactor at an elevated pressure above about 350 psig and at an elevated temperature from about 700 to about 900.degree. F.
Abstract translation: 一种用于压缩和加热空气或富氧空气的改进方法，用于通过使用单个高压缩比压缩机来产生用于混合的高压，高温空气或富氧空气流到自热反应器 烃气流以在高于约350psig的升高的压力和约700至约900°F的升高的温度下产生进入自热反应器的进料流。
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公开(公告)号：US08591199B2
公开(公告)日：2013-11-26
申请号：US11622338
申请日：2007-01-11
Applicant: Bobby D. Martinez , John R. Wolflick , Jaleel Valappil
Inventor： Bobby D. Martinez , John R. Wolflick , Jaleel Valappil
IPC: F04B23/04
CPC classification number: F04C23/001 , F04D27/0269 , F25J1/0022 , F25J1/0283 , F25J1/0298 , F25J2280/10
Abstract: An improved system and methodology for starting up a gas-turbine driven multi-stage compressor. The improvement involves isolating individual compression stages and creating positive pressure in each stage prior to initiating rotation of the compressor/driver system. The isolation of individual compression stages allows the turbine to reach normal operating speeds with substantially no supplemental power from an auxiliary source.
Abstract translation: 一种用于启动燃气轮机驱动的多级压缩机的改进的系统和方法。 该改进涉及在启动压缩机/驱动器系统的旋转之前在每个阶段隔离各个压缩级并产生正压。 单独的压缩级的隔离允许涡轮达到正常的运行速度，基本上没有来自辅助源的补充功率。
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公开(公告)号：US07712299B2
公开(公告)日：2010-05-11
申请号：US11470010
申请日：2006-09-05
Applicant: John R. Wolflick , Megan V. Evans , Jaleel Valappil , Bobby D. Martinez , Marc Bellomy
Inventor： John R. Wolflick , Megan V. Evans , Jaleel Valappil , Bobby D. Martinez , Marc Bellomy
IPC: F02G3/00
CPC classification number: F04D27/0261 , F04D25/04 , F25J1/0022 , F25J1/0283 , F25J1/0298 , F25J2280/20
Abstract: An anti-bogdown control system monitors and regulates operation of a turbine and a compressor to prevent underspeed trip of the turbine while avoiding surge of the compressor. A turbine speed controller receives a turbine speed signal and a turbine temperature signal, generates a surge margin setpoint, and regulates overfiring of the turbine. A surge margin controller associated with the compressor receives the surge margin setpoint from the turbine speed controller and receives a load signal from one or more sensors and modulates a compressor throttle valve so that the compressor operates at a surge margin that is approximately equal to the surge margin setpoint. In a system with multiple compressors driven by a single turbine, a surge margin controller is associated with each compressor.
Abstract translation: 防倒档控制系统监测和调节涡轮机和压缩机的操作，以防止涡轮机的低速跳闸，同时避免压缩机的浪涌。 涡轮转速控制器接收涡轮转速信号和涡轮温度信号，产生浪涌余量设定点，并调节涡轮机过热。 与压缩机相关联的浪涌余量控制器接收来自涡轮转速控制器的喘振余量设定值，并接收来自一个或多个传感器的负载信号并调制压缩机节流阀，使得压缩机以大约等于浪涌的浪涌裕度 余量设定值 在具有由单个涡轮机驱动的多个压缩机的系统中，喘振裕度控制器与每个压缩机相关联。
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公开(公告)号：US20090317260A1
公开(公告)日：2009-12-24
申请号：US12144196
申请日：2008-06-23
Applicant: Saul Mirsky , Jeff McWhirter , John R. Wolflick
Inventor： Saul Mirsky , Jeff McWhirter , John R. Wolflick
IPC: F04B49/00
CPC classification number: F04D27/0253 , F01D15/08 , F02C6/12
Abstract: A control method and apparatus for simultaneously protecting a compression system from driver overpowering and turbocompressor surge. When overpowering is detected, flow rate through the each compressor in the turbocompressor train is reduced by closing an inlet throttling valve at the inlet of each respective compressor stage unless a compressor operating point is sufficiently near surge. In this latter case, the inlet throttling valve is not closed. In this way, overall flow rate through the compressor train is reduced while maintaining adequate flow through compromised stages to avoid surge.
Abstract translation: 一种用于同时保护压缩系统免受驾驶员超车和涡轮压缩机喘振的控制方法和装置。 当检测到超压时，通过在每个相应的压缩机级的入口处关闭入口节流阀来减少通过涡轮压缩机列中的每个压缩机的流量，除非压缩机工作点充分接近喘振。 在后一种情况下，入口节流阀不关闭。 以这种方式，通过压缩机系统的整个流量被减小，同时通过受损阶段保持足够的流量以避免浪涌。
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公开(公告)号：US5442934A
公开(公告)日：1995-08-22
申请号：US226918
申请日：1994-04-13
Applicant: John R. Wolflick
Inventor： John R. Wolflick
Abstract: Gas compression and chilling systems, particularly adapted for compressing and chilling gas for transmission through arctic pipelines are provided with a cross heat exchanger for transferring heat from gas compressed to the inlet gas to the compressor. The heat exchanger is disposed upstream of an expander which may comprise a mechanical expander or a throttling valve, or both, to achieve a predetermined final output pressure and temperature. An aerial heat exchanger is interposed between the compression and expansion stages upstream of the inlet gas heat exchanger. One embodiment of the system uses two stages of compression, aerial cooling and expansion to the final temperature and pressure.
Abstract translation: 特别适用于压缩和冷却通过北极管线传输的气体的气体压缩和冷却系统设置有用于将热量从压缩到入口气体的气体传递到压缩机的交叉热交换器。 热交换器设置在可以包括机械膨胀机或节流阀或两者的膨胀机的上游，以实现预定的最终输出压力和温度。 空气热交换器插入入口气体热交换器上游的压缩级和膨胀级之间。 该系统的一个实施例使用两个阶段的压缩，空中冷却和膨胀到最终的温度和压力。
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