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公开(公告)号：US20070163438A1
公开(公告)日：2007-07-19
申请号：US11334126
申请日：2006-01-18
申请人： Louis Chiappetta , Louis Spadaccini , He Huang , Mallika Gummalla , Dochul Choi
发明人： Louis Chiappetta , Louis Spadaccini , He Huang , Mallika Gummalla , Dochul Choi
IPC分类号： B01D53/22
CPC分类号： B01D19/0042 , B01D19/0031
摘要： A fuel system for an energy conversion device includes a deoxygenator system with a multitude of flow impingement elements which are interleaved to provide a fuel channel with intricate two-dimensional flow characteristics. The flow impingement elements break up the boundary layers and enhance the transport of oxygen from the core of the of the fuel flow within the fuel channel to the oxygen permeable membrane surfaces by directing the fuel flow in a direction normal to the oxygen permeable membrane. The rapid mixing of the relatively rich oxygen core of the fuel with the relatively oxygen-poor flow near the oxygen permeable membrane enhances the overall removal rate of oxygen from the fuel. Because this process can be accomplished in fuel channels of relatively larger flow areas while maintaining laminar flow, the pressure drop sustained is relatively low.
摘要翻译： 用于能量转换装置的燃料系统包括具有多个流动冲击元件的脱氧器系统，其被交错以提供具有复杂二维流动特性的燃料通道。 流动冲击元件通过沿着与透氧膜垂直的方向引导燃料流而分解边界层并增强氧从燃料通道内的燃料流的核心输送到氧气渗透膜表面。 燃料的相对富氧核心与氧气渗透膜附近的相对贫氧流的快速混合提高了氧气从燃料中的总体去除速率。 因为该过程可以在维持层流的同时在相对较大的流动区域的燃料通道中实现，所以压力下降相对较低。
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公开(公告)号：US07824470B2
公开(公告)日：2010-11-02
申请号：US11334126
申请日：2006-01-18
IPC分类号： B01D53/22
CPC分类号： B01D19/0042 , B01D19/0031
摘要： A fuel system for an energy conversion device includes a deoxygenator system with a multitude of flow impingement elements which are interleaved to provide a fuel channel with intricate two-dimensional flow characteristics. The flow impingement elements break up the boundary layers and enhance the transport of oxygen from the core of the of the fuel flow within the fuel channel to the oxygen permeable membrane surfaces by directing the fuel flow in a direction normal to the oxygen permeable membrane. The rapid mixing of the relatively rich oxygen core of the fuel with the relatively oxygen-poor flow near the oxygen permeable membrane enhances the overall removal rate of oxygen from the fuel. Because this process can be accomplished in fuel channels of relatively larger flow areas while maintaining laminar flow, the pressure drop sustained is relatively low.
摘要翻译： 用于能量转换装置的燃料系统包括具有多个流动冲击元件的脱氧器系统，其被交错以提供具有复杂二维流动特性的燃料通道。 流动冲击元件通过沿着与透氧膜垂直的方向引导燃料流而分解边界层并增强氧从燃料通道内的燃料流的核心输送到氧气渗透膜表面。 燃料的相对富氧核心与氧气渗透膜附近的相对贫氧流的快速混合提高了氧气从燃料中的总体去除速率。 因为该过程可以在维持层流的同时在相对较大的流动区域的燃料通道中实现，所以压力下降相对较低。
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3.发明申请公开(公告)号：US20070163433A1
公开(公告)日：2007-07-19
申请号：US11334587
申请日：2006-01-18
IPC分类号： B01D53/22
CPC分类号： B01D69/06 , B01D19/0031 , B01D19/0042 , B01D63/082 , B01D65/08 , B01D67/0006 , B01D67/0037 , B01D69/00 , B01D69/10 , B01D69/12 , B01D69/125 , B01D71/36 , B01D2321/2008 , B01D2321/2016 , B01D2323/40 , B01D2325/06 , B64D37/32 , Y02T50/44
摘要： A device for use in a fluid system includes a flow perturbation element within a fluid channel. The flow perturbation element has a gas permeable surface for removing dissolved gas from passing fluid. A gas permeable membrane is coated on the gas permeable surface and allows the dissolved gas transport out of passing fluid into a gas-removal channel. The gas permeable membrane may be coated on the fuel perturbation elements using any of a variety of methods.
摘要翻译： 用于流体系统的装置包括流体通道内的流动扰动元件。 流动扰动元件具有用于从流过的流体中除去溶解气体的气体透过表面。 气体渗透膜被涂覆在透气表面上，并允许溶解的气体从通过的流体输送到排气通道中。 气体渗透膜可以使用各种方法中的任何一种涂覆在燃料扰动元件上。
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公开(公告)号：US20060254422A1
公开(公告)日：2006-11-16
申请号：US11128571
申请日：2005-05-13
申请人： Louis Spadaccini , Harry Cordatos , Thomas Tillman , Alexander Chen , Louis Chiappetta , James Irish , Foster Lamm , Stephen Jones
发明人： Louis Spadaccini , Harry Cordatos , Thomas Tillman , Alexander Chen , Louis Chiappetta , James Irish , Foster Lamm , Stephen Jones
IPC分类号： B01D53/22
CPC分类号： B64D37/32 , B01D19/0031 , B01D19/0036 , B01D61/00 , B01D63/10 , Y02T50/44
摘要： A deoxygenator includes a plurality of permeable membranes spirally wound about an exhaust tube for removing dissolved oxygen from a hydrocarbon fuel. The permeable membrane is spirally wrapped about the exhaust tube and defines fuel passages and exhaust passages. The fuel passages and exhaust passages alternate such that each fuel passage is bounded on each adjacent side by an exhaust passage. An oxygen partial pressure differential is generated across the permeable membrane to draw dissolved oxygen from fuel in the fuel passage. The dissolved oxygen is then communicated through openings about the circumference of the exhaust tube and out the deoxygenator.
摘要翻译： 脱氧器包括围绕排气管螺旋地缠绕以从烃燃料中除去溶解氧的多个可渗透膜。 可渗透膜围绕排气管螺旋缠绕并限定燃料通道和排气通道。 燃料通道和排气通道交替使得每个燃料通道在每个相邻侧由排气通道限定。 在渗透膜上产生氧分压，以从燃料通道中的燃料中抽出溶解氧。 然后将溶解的氧气通过围绕排气管的圆周的开口连通并脱出脱氧器。
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公开(公告)号：US20100218921A1
公开(公告)日：2010-09-02
申请号：US11516402
申请日：2006-09-06
申请人： Daniel R. Sabatino , Scott F. Kaslusky , Hayden M. Reeve , Louis J. Spadaccini , Louis Chiappetta , He Huang , David R. Sobel
发明人： Daniel R. Sabatino , Scott F. Kaslusky , Hayden M. Reeve , Louis J. Spadaccini , Louis Chiappetta , He Huang , David R. Sobel
CPC分类号： F28F13/003
摘要： A heat exchanger includes one or more passages and one or more metal foam sections adjacent the passage to promote an exchange of heat relative to the passage. The metal foam section includes a nominal thermal conductivity gradient there though to provide a desirable balance of heat exchange properties within the metal foam section.
摘要翻译： 热交换器包括一个或多个通道和邻近通道的一个或多个金属泡沫部分，以促进相对于通道的热交换。 金属泡沫部分包括标称的热导率梯度，尽管在金属泡沫部分内提供期望的热交换性质的平衡。
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公开(公告)号：US08127829B2
公开(公告)日：2012-03-06
申请号：US11516402
申请日：2006-09-06
申请人： Daniel R. Sabatino , Scott F. Kaslusky , Hayden M. Reeve , Louis J. Spadaccini , Louis Chiappetta , He Huang , David R. Sobel
发明人： Daniel R. Sabatino , Scott F. Kaslusky , Hayden M. Reeve , Louis J. Spadaccini , Louis Chiappetta , He Huang , David R. Sobel
CPC分类号： F28F13/003
摘要： A heat exchanger includes one or more passages and one or more metal foam sections adjacent the passage to promote an exchange of heat relative to the passage. The metal foam section includes a nominal thermal conductivity gradient there though to provide a desirable balance of heat exchange properties within the metal foam section.
摘要翻译： 热交换器包括一个或多个通道和邻近通道的一个或多个金属泡沫部分，以促进相对于通道的热交换。 金属泡沫部分包括标称的热导率梯度，尽管在金属泡沫部分内提供期望的热交换性质的平衡。
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7.发明申请Racetrack Carryover Design for Multi-Burner Ignition in Induced Draft Heating System 有权引风加热系统中多燃烧器点火赛马场设计公开(公告)号：US20120052452A1
公开(公告)日：2012-03-01
申请号：US13196418
申请日：2011-08-02
CPC分类号： F23D14/08 , F23D14/045 , F23D2207/00 , F23D2900/14021 , F24H3/105
摘要： An ignition system for a multi-burner heat exchanger assembly, a furnace, and a method using same are disclosed. The assembly may include a plurality of adjacent heat exchanger tubes, with a burner associated with each tube. All the burners may be lit with a single igniter and no source of secondary air. To do so, each of the burners may be provided so as to generate a swirling exit flow of combustion gases. One or more carryover tubes may also be connected between adjacent pairs of heat exchanger tubes or adjacent pairs of burners. The swirling flow generated by the burners causes hot combustion gases to move through the carryover tubes to thus carry the flame from one burner to the next. Not only can a single igniter be used, but a single flame sensor as well, while at the same time reducing nitrogen oxide emissions.
摘要翻译： 公开了一种用于多燃烧器热交换器组件，炉和其使用方法的点火系统。 组件可以包括多个相邻的热交换器管，其具有与每个管相关联的燃烧器。 所有的燃烧器可能会点燃一个点火器，没有二次空气源。 为了这样做，可以提供每个燃烧器以产生涡流的燃烧气体的出口流。 一个或多个携带管也可以连接在相邻的热交换器管对或相邻的燃烧器对之间。 由燃烧器产生的旋流使得热的燃烧气体移动通过排出管，从而将火焰从一个燃烧器运送到下一个燃烧器。 不仅可以使用单个点火器，还可以使用单个火焰传感器，同时减少氮氧化物排放。
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公开(公告)号：US07393388B2
公开(公告)日：2008-07-01
申请号：US11128571
申请日：2005-05-13
申请人： Louis J. Spadaccini , Harry Cordatos , Thomas Gregory Tillman , Alexander G. Chen , Louis Chiappetta , James R. Irish , Foster Phillip Lamm , Stephen R. Jones
发明人： Louis J. Spadaccini , Harry Cordatos , Thomas Gregory Tillman , Alexander G. Chen , Louis Chiappetta , James R. Irish , Foster Phillip Lamm , Stephen R. Jones
CPC分类号： B64D37/32 , B01D19/0031 , B01D19/0036 , B01D61/00 , B01D63/10 , Y02T50/44
摘要： A deoxygenator includes a plurality of permeable membranes spirally wound about an exhaust tube for removing dissolved oxygen from a hydrocarbon fuel. The permeable membrane is spirally wrapped about the exhaust tube and defines fuel passages and exhaust passages. The fuel passages and exhaust passages alternate such that each fuel passage is bounded on each adjacent side by an exhaust passage. An oxygen partial pressure differential is generated across the permeable membrane to draw dissolved oxygen from fuel in the fuel passage. The dissolved oxygen is then communicated through openings about the circumference of the exhaust tube and out the deoxygenator.
摘要翻译： 脱氧器包括围绕排气管螺旋地缠绕以从烃燃料中除去溶解氧的多个可渗透膜。 可渗透膜围绕排气管螺旋缠绕并限定燃料通道和排气通道。 燃料通道和排气通道交替使得每个燃料通道在每个相邻侧由排气通道限定。 在渗透膜上产生氧分压，以从燃料通道中的燃料中抽出溶解氧。 然后将溶解的氧气通过围绕排气管的圆周的开口连通并脱出脱氧器。
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9.发明授权Racetrack carryover design for multi-burner ignition in induced draft heating system 有权引风加热系统中多燃烧器点火的跑道残留设计公开(公告)号：US08668489B2
公开(公告)日：2014-03-11
申请号：US13196418
申请日：2011-08-02
IPC分类号： F24H3/02
CPC分类号： F23D14/08 , F23D14/045 , F23D2207/00 , F23D2900/14021 , F24H3/105
摘要： An ignition system for a multi-burner heat exchanger assembly, a furnace, and a method using same are disclosed. The assembly may include a plurality of adjacent heat exchanger tubes, with a burner associated with each tube. All the burners may be lit with a single igniter and no source of secondary air. To do so, each of the burners may be provided so as to generate a swirling exit flow of combustion gases. One or more carryover tubes may also be connected between adjacent pairs of heat exchanger tubes or adjacent pairs of burners. The swirling flow generated by the burners causes hot combustion gases to move through the carryover tubes to thus carry the flame from one burner to the next. Not only can a single igniter be used, but a single flame sensor as well, while at the same time reducing nitrogen oxide emissions.
摘要翻译： 公开了一种用于多燃烧器热交换器组件，炉和其使用方法的点火系统。 组件可以包括多个相邻的热交换器管，其具有与每个管相关联的燃烧器。 所有的燃烧器可能会点燃一个点火器，没有二次空气源。 为了这样做，可以提供每个燃烧器以产生涡流的燃烧气体的出口流。 一个或多个携带管也可以连接在相邻的热交换器管对或相邻的燃烧器对之间。 由燃烧器产生的旋流使得热的燃烧气体移动通过排出管，从而将火焰从一个燃烧器运送到下一个燃烧器。 不仅可以使用单个点火器，还可以使用单个火焰传感器，同时减少氮氧化物排放。
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10.发明授权公开(公告)号：US07582137B2
公开(公告)日：2009-09-01
申请号：US11334587
申请日：2006-01-18
IPC分类号： B01D53/22
CPC分类号： B01D69/06 , B01D19/0031 , B01D19/0042 , B01D63/082 , B01D65/08 , B01D67/0006 , B01D67/0037 , B01D69/00 , B01D69/10 , B01D69/12 , B01D69/125 , B01D71/36 , B01D2321/2008 , B01D2321/2016 , B01D2323/40 , B01D2325/06 , B64D37/32 , Y02T50/44
摘要： A device for use in a fluid system includes a flow perturbation element within a fluid channel. The flow perturbation element has a gas permeable surface for removing dissolved gas from passing fluid. A gas permeable membrane is coated on the gas permeable surface and allows the dissolved gas transport out of passing fluid into a gas-removal channel. The gas permeable membrane may be coated on the fuel perturbation elements using any of a variety of methods.
摘要翻译： 用于流体系统的装置包括流体通道内的流动扰动元件。 流动扰动元件具有用于从流过的流体中除去溶解气体的气体透过表面。 气体渗透膜被涂覆在透气表面上，并允许溶解的气体从通过的流体输送到排气通道中。 气体渗透膜可以使用各种方法中的任何一种涂覆在燃料扰动元件上。
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