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公开(公告)号：US09586827B2
公开(公告)日：2017-03-07
申请号：US14480582
申请日：2014-09-08
申请人： David Leroy Hagen
发明人： David Leroy Hagen
摘要： A system to calcine crushed carbonate, discharge alkaline oxide, and deliver an enhancing fluid having CO2, comprising: a pressurized insulated calciner having descendingly, a crushed alkaline carbonate feeder, a calciner fluid outlet manifold, a heated sideflow calciner fluid intake manifold, a preheated sideflow calciner fluid outtake manifold, a fluid inlet manifold to recirculate calciner fluid from the outlet manifold, and an alkaline oxide discharger; a pressurizer to repressurize sideflow calciner fluid, connected to intake and outtake manifolds; pressurizers to recirculate calciner outlet fluid to the inlet manifold, pressurize the calciner and deliver enhancing fluid comprising CO2; delivery and combustion systems to form a combustion fluid; a recuperating or regenerating refractory heat exchanger to heat sideflow calciner fluid with combustion fluid connected to the sideflow pressurizer, and fluid outtake and intake manifolds; and a controller operable to control combustion, heat exchange, calciner fluid formation and delivery, carbonate feed and oxide discharge.
摘要翻译： 一种用于煅烧粉碎的碳酸盐，排出碱性氧化物并输送具有CO 2的增强流体的系统，包括：具有下降的加压绝热煅烧炉，压碎的碱性碳酸盐进料器，煅烧液流体出口歧管，加热的侧流式煅烧液流体进气歧管，预热的 侧流煅烧液流出歧管，使来自出口歧管的煅烧液再循环的流体入口歧管和碱性氧化物排放器; 加压器，用于再加压侧流式煅烧液，连接到进气歧管和出口歧管; 加压器将煅烧炉出口流体再循环到入口歧管，对煅烧炉加压并输送包含CO 2的增强流体; 输送和燃烧系统以形成燃烧流体; 一种回热或再生的耐火热交换器，用于连接到侧流加压器的燃烧流体加热侧流煅烧流体，以及流体输出和进气歧管; 以及可操作以控制燃烧，热交换，煅烧液形成和输送，碳酸盐进料和氧化物排放的控制器。
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公开(公告)号：US20160258263A1
公开(公告)日：2016-09-08
申请号：US14641275
申请日：2015-03-06
申请人： David LeRoy Hagen
发明人： David LeRoy Hagen
CPC分类号： E21B43/164 , C01B32/50 , C01D1/02 , C04B2/10 , C09K8/594 , E21B43/34 , Y02P40/42 , Y02P90/70
摘要： A method of supplying crushed alkaline carbonate from a carbonate resource to a first calcining site having a design calcining capacity; solar calcining crushed carbonate within a prescribed carbon dioxide (CO2) delivery distance from a first enhancement location within a first hydrocarbon resource, whereby generating CO2 with a local CO2 generating capacity and an alkaline oxide; forming a first enhancing fluid comprising generated CO2 and delivering it into the first enhancement site having an injector well weighted first enhancement location, whereby mobilizing hydrocarbon in the first enhancement site; producing a produced fluid comprising mobilized hydrocarbon and enhancing fluid; recovering liquid hydrocarbon from the produced fluid; wherein the prescribed CO2 delivery distance is less than 67% of a remote CO2 delivery distance, to the first enhancement location from a remote calcining site having an equal or greater design calcined CO2 generating capacity. Then solar calcining CO2 to enhance a second site.
摘要翻译： 一种从碳酸盐资源将粉碎的碱性碳酸盐供给具有设计煅烧能力的第一煅烧部位的方法; 太阳能煅烧粉碎的碳酸盐在规定的二氧化碳（CO 2）输送距离内从第一烃类资源内的第一增强位置，从而产生具有局部CO 2发生能力的CO 2和碱性氧化物; 形成第一增强流体，其包括产生的CO 2并将其输送到具有喷射器良好加权的第一增强位置的第一增强位置，由此在第一增强位点中移动烃; 产生包含动员的烃和增强流体的产生的流体; 从产生的流体中回收液态烃; 其中规定的CO 2输送距离小于远程CO 2输送距离的67％，距离具有相同或更高设计的煅烧CO 2生成能力的远程煅烧部位的第一增强位置。 然后太阳能煅烧二氧化碳，以增强第二站点。
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公开(公告)号：US20090283632A1
公开(公告)日：2009-11-19
申请号：US12507573
申请日：2009-07-22
IPC分类号： B64C9/00
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a plurality of thrusters mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of a first thruster to enable a first vector force to be generated by a portion of the thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft at a position downstream of a second thruster, the first and the second control surfaces being displaced symmetrically on opposite sides of a longitudinal axis of the aircraft, the second control surface being configured to be independently and differentially movable with respect to the first control surface to enable a second vector force to be generated by a portion of the thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上用于推动空气的多个推进器，第一控制表面，其在第一推进器下游的位置处运动学地联接到飞行器，以使第一矢量力由推动的一部分产生 来自第一控制表面上的第一推进器的空气和在第二推进器下游的位置处运动学地联接到飞行器的第二控制表面，第一和第二控制表面在飞行器的纵向轴线的相对侧对称移位 所述第二控制表面被配置为相对于所述第一控制表面独立且可差分移动，以使第二向量力由所述第二控制表面上的来自所述第二推进器的被推动空气的一部分产生。
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公开(公告)号：US07911406B2
公开(公告)日：2011-03-22
申请号：US11731132
申请日：2007-03-31
IPC分类号： H01Q19/00
CPC分类号： H01Q19/30 , H01Q1/1228 , H01Q11/10 , H01Q19/04
摘要： The invention relates to Radio Frequency (RF) antennas suitable for receiving and/or transmitting digital signals in the Ultra High Frequency (UHF) and/or Very High Frequency (VHF) ranges. The invention comprises a modular driven DUV antenna comprising a driven DUV element, an RF signal line RF communicatively connected to the driven DUV element, and an antenna mount supporting the DUV element; and a modular RF signal enhancer, supported by the antenna mount and selected from: an RF amplifier and a passive RF enhancer positioned to enhance the RF performance of the DUV antenna and comprising one of: an RF director, an RF reflector, and an RF booster.
摘要翻译： 本发明涉及适用于在超高频（UHF）和/或超高频（VHF）范围内接收和/或发射数字信号的射频（RF）天线。 本发明包括一个模块化驱动的DUV天线，包括驱动的DUV元件，与驱动的DUV元件通信地连接的RF信号线RF以及支持DUV元件的天线安装座; 以及模块化RF信号增强器，由天线安装支撑并且选自：RF放大器和无源RF增强器，其被定位以增强DUV天线的RF性能，并且包括以下之一：RF导向器，RF反射器和RF 助推器。
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公开(公告)号：US08302903B2
公开(公告)日：2012-11-06
申请号：US13324713
申请日：2011-12-13
IPC分类号： B64C5/10
摘要： Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes thrusters mounted to an aircraft, a first control surface kinematically coupled to the aircraft downstream of a first thruster to enable a first vector force to be generated by a portion of thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft of a second thruster. The control surfaces are displaced symmetrically a longitudinal axis of the aircraft. The control surfaces are independently and differentially movable with respect to each other to enable generation of a second vector force by a portion of thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置中的控制面在悬停或低空速条件下为飞机提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上的推进器，第一控制表面，其运动学耦合到第一推进器下游的飞行器，以使第一矢量力能够由第一推进器在第一控制表面上的一部分推动空气产生 以及与第二推进器的飞行器运动耦合的第二控制表面。 控制表面对称地移动飞行器的纵向轴线。 控制表面可相对于彼此独立且可差分地移动，从而能够通过来自第二控制表面上的第二推进器的推动空气的一部分产生第二向量力。
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公开(公告)号：US20120145834A1
公开(公告)日：2012-06-14
申请号：US13324713
申请日：2011-12-13
摘要： Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes thrusters mounted to an aircraft, a first control surface kinematically coupled to the aircraft downstream of a first thruster to enable a first vector force to be generated by a portion of thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft of a second thruster. The control surfaces are displaced symmetrically a longitudinal axis of the aircraft. The control surfaces are independently and differentially movable with respect to each other to enable generation of a second vector force by a portion of thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置中的控制面在悬停或低空速条件下为飞机提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上的推进器，第一控制表面，其运动学耦合到第一推进器下游的飞行器，以使第一矢量力能够由第一推进器在第一控制表面上的一部分推动空气产生 以及与第二推进器的飞行器运动耦合的第二控制表面。 控制表面对称地移动飞行器的纵向轴线。 控制表面可相对于彼此独立且可差分地移动，从而能够通过来自第二控制表面上的第二推进器的推动空气的一部分产生第二向量力。
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公开(公告)号：US08074925B2
公开(公告)日：2011-12-13
申请号：US12507573
申请日：2009-07-22
IPC分类号： B64C5/10
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a plurality of thrusters mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of a first thruster to enable a first vector force to be generated by a portion of the thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft at a position downstream of a second thruster, the first and the second control surfaces being displaced symmetrically on opposite sides of a longitudinal axis of the aircraft, the second control surface being configured to be independently and differentially movable with respect to the first control surface to enable a second vector force to be generated by a portion of the thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上用于推动空气的多个推进器，第一控制表面，其在第一推进器下游的位置处运动学地联接到飞行器，以使第一矢量力由推动的一部分产生 来自第一控制表面上的第一推进器的空气和在第二推进器下游的位置处运动学地联接到飞行器的第二控制表面，第一和第二控制表面在飞行器的纵向轴线的相对侧对称移位 所述第二控制表面被配置为相对于所述第一控制表面独立且可差分移动，以使第二向量力由所述第二控制表面上的来自所述第二推进器的被推动空气的一部分产生。
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公开(公告)号：US07581696B2
公开(公告)日：2009-09-01
申请号：US11595525
申请日：2006-11-09
IPC分类号： B64C5/10
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a thruster mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of the thruster, and a second control surface kinematically coupled to the aircraft at a position downstream of the thruster, the second control surface being differentially movable with respect to the first control surface such that a portion of the thrusted air from the thruster generates a first vector force on the first control surface and another portion of the thrusted air generates a second vector force on the second control surface, so that the first and the second vector forces provide a net roll moment about the Y-Roll axis.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制构型包括安装在飞行器上用于推动空气的推进器，在推进器下游的位置运动地联接到飞行器的第一控制表面，以及在推进器下游的位置运动地联接到飞行器的第二控制表面 所述第二控制表面可相对于所述第一控制表面差异移动，使得来自所述推进器的所述推动空气的一部分在所述第一控制表面上产生第一向量力，并且所述推动空气的另一部分在所述第二控制表面上产生第二向量力 第二控制表面，使得第一和第二向量力围绕Y-辊轴提供净滚动力矩。
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公开(公告)号：US20160083258A1
公开(公告)日：2016-03-24
申请号：US14480582
申请日：2014-09-08
申请人： DAVID LEROY HAGEN
发明人： DAVID LEROY HAGEN
摘要： A system to calcine crushed carbonate, discharge alkaline oxide, and deliver an enhancing fluid having CO2, comprising: a pressurized insulated calciner having descendingly, a crushed alkaline carbonate feeder, a calciner fluid outlet manifold, a heated sideflow calciner fluid intake manifold, a preheated sideflow calciner fluid outtake manifold, a fluid inlet manifold to recirculate calciner fluid from the outlet manifold, and an alkaline oxide discharger; a pressurizer to repressurize sideflow calciner fluid, connected to intake and outtake manifolds; pressurizers to recirculate calciner outlet fluid to the inlet manifold, pressurize the calciner and deliver enhancing fluid comprising CO2; delivery and combustion systems to form a combustion fluid; a recuperating or regenerating refractory heat exchanger to heat sideflow calciner fluid with combustion fluid connected to the sideflow pressurizer, and fluid outtake and intake manifolds; and a controller operable to control combustion, heat exchange, calciner fluid formation and delivery, carbonate feed and oxide discharge.
摘要翻译： 一种用于煅烧粉碎的碳酸盐，排出碱性氧化物并输送具有CO 2的增强流体的系统，包括：具有下降的加压绝热煅烧炉，压碎的碱性碳酸盐进料器，煅烧液流体出口歧管，加热的侧流式煅烧液流体进气歧管，预热的 侧流煅烧液流出歧管，使来自出口歧管的煅烧液再循环的流体入口歧管和碱性氧化物排放器; 加压器，用于再加压侧流式煅烧液，连接到进气歧管和出口歧管; 加压器将煅烧炉出口流体再循环到入口歧管，对煅烧炉加压并输送包含CO 2的增强流体; 输送和燃烧系统以形成燃烧流体; 一种回热或再生的耐火热交换器，用于连接到侧流加压器的燃烧流体加热侧流煅烧流体，以及流体输出和进气歧管; 以及可操作以控制燃烧，热交换，煅烧液形成和输送，碳酸盐进料和氧化物排放的控制器。
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公开(公告)号：US20150129208A1
公开(公告)日：2015-05-14
申请号：US14480271
申请日：2014-09-08
申请人： David LeRoy Hagen
发明人： David LeRoy Hagen
CPC分类号： E21B43/164 , C01B32/50 , C01D1/02 , C04B2/10 , C09K8/594 , E21B43/34 , Y02P40/42 , Y02P90/70
摘要： A method of supplying crushed alkaline carbonate from a carbonate resource to a first calcining site having a design calcining capacity; calcining the crushed carbonate within a prescribed carbon dioxide (CO2) delivery distance from a first enhancement location within a first hydrocarbon resource, whereby generating CO2 with a local CO2 generating capacity and an alkaline oxide; forming a first enhancing fluid comprising generated CO2 and delivering it into the first enhancement site having an injector well weighted first enhancement location, whereby mobilizing hydrocarbon in the first enhancement site; producing a produced fluid comprising mobilized hydrocarbon and enhancing fluid; recovering liquid hydrocarbon from the produced fluid; wherein the prescribed CO2 delivery distance is less than 67% of a remote CO2 delivery distance, to the first enhancement location from a remote calcining site having an equal or greater design calcined CO2 generating capacity. Then calcining CO2 to enhance a second larger site.
摘要翻译： 一种从碳酸盐资源将粉碎的碱性碳酸盐供给具有设计煅烧能力的第一煅烧部位的方法; 在第一烃类资源内的第一增强位置的规定的二氧化碳（CO 2）输送距离内煅烧所述粉碎的碳酸盐，由此产生具有局部CO 2生成能力的CO 2和碱性氧化物; 形成第一增强流体，其包括产生的CO 2并将其输送到具有喷射器良好加权的第一增强位置的第一增强位置，由此在第一增强位点中移动烃; 产生包含动员的烃和增强流体的产生的流体; 从产生的流体中回收液态烃; 其中规定的CO 2输送距离小于远程CO 2输送距离的67％，距离具有相同或更高设计的煅烧CO 2生成能力的远程煅烧部位的第一增强位置。 然后煅烧二氧化碳以增强第二个较大的场地。
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