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61. 发明申请

WO1997006386A1 OXY-LIQUID FUEL COMBUSTION PROCESS AND APPARATUS 审中-公开
标题翻译：氧气燃料燃烧过程和装置
公开(公告)号：WO1997006386A1
公开(公告)日：1997-02-20
申请号：PCT/US1996012586
申请日：1996-07-31
申请人： COMBUSTION TEC, INC.
发明人： COMBUSTION TEC, INC. , JOSHI, Mahendra, L. , BROADWAY, Lee , MOHR, Patrick, J. , NITZMAN, Jack, L.
IPC分类号： F23D11/10
CPC分类号： F23D14/22 , F23C2201/20 , F23D11/106 , F23D14/56 , F23D14/84 , F23D2900/00006 , F23D2900/00013 , F23L7/007 , F23M5/025 , Y02E20/344
摘要： An oxy-liquid fuel burner comprising: a liquid fuel conduit (12) having a liquid fuel inlet (17) end and a liquid fuel discharge end; an oxygen conduit (13) disposed around said liquid fuel conduit and forming an annular region between an exterior surface of said liquid fuel conduit and an interior surface of said oxygen conduit; said liquid fuel conduit comprising atomization means for atomization of a liquid fuel and shaping means for discharging said liquid fuel from said liquid fuel discharge end in an outwardly divergent, fishtail configuration; and said oxygen conduit comprising means for discharging oxygen in an outwardly divergent, fishtail configuration corresponding to said liquid fuel configuration and substantially encircling said liquid fuel.
摘要翻译：一种氧液体燃料燃烧器，包括：具有液体燃料入口（17）端和液体燃料排出端的液体燃料管道（12）设置在所述液体燃料管道周围的氧气导管（13），并且在所述液体燃料管道的外表面和所述氧气导管的内表面之间形成环形区域; 所述液体燃料管道包括用于雾化液体燃料的雾化装置和用于以向外发散的鱼尾构型从所述液体燃料排放端排出所述液体燃料的成形装置; 并且所述氧气导管包括用于以对应于所述液体燃料构造并基本上环绕所述液体燃料的向外发散的鱼尾构型排出氧气的装置。

62. 发明申请

WO9621823A3 METHOD AND APPARATUS FOR DISPENSING FUEL AND OXIDANT FROM A BURNER 审中-公开
标题翻译：用于从燃烧器分配燃料和氧化物的方法和装置
公开(公告)号：WO9621823A3
公开(公告)日：1996-08-22
申请号：PCT/US9517069
申请日：1995-12-29
申请人： COMBUSTION TEC INC , JOSHI MAHENDRA L , BROADWAY LEE , MOHR PATRICK J
发明人： JOSHI MAHENDRA L , BROADWAY LEE , MOHR PATRICK J
IPC分类号： F23D14/22 , F23D14/56 , F23D14/58
CPC分类号： F23D14/22 , F23C2201/20 , F23D14/56 , F23D2900/00006 , F23D2900/00013
摘要： A method and apparatus for injecting fuel and oxidant into a combustion burner. At a fuel exit plane of a fuel discharge nozzle (15), fuel is discharged in a generally planar fuel layer which has an upper boundary and a lower boundary. At an oxidant exit plane (25), oxidant is preferably discharged in both a top layer along the upper boundary of the fuel layer and a bottom layer along the lower boundary of the fuel layer. In a downstream flow direction, the fuel and oxidant preferably converge in a generally vertical plane and diverge in a generally horizontal plane. The discharged fuel and oxidant form a fishtail or fan-shaped flame configuration. The fuel exit plane (116; Fig. 9 + 10) can be moved upstream or downstream with respect to the oxidant exit plane (126; Fig. 9 + 10) to vary the flame characteristics and the flame shape. A refractory manifold (47) can be used to further enhance the fishtail or fan-shaped flame configuration.

63. 发明申请

WO1995016880A2 OXYGEN-FUEL BURNER WITH INTEGRAL STAGED OXYGEN SUPPLY 审中-公开
标题翻译：氧气燃烧器具有整体标准氧气供应
公开(公告)号：WO1995016880A2
公开(公告)日：1995-06-22
申请号：PCT/US1994012638
申请日：1994-11-02
申请人： MAXON CORPORATION
发明人： MAXON CORPORATION , TAYLOR, Curtis, L.
IPC分类号： F23D00/00
CPC分类号： F23D11/102 , F23C6/045 , F23C7/02 , F23C2201/20 , F23D11/106 , F23D14/32 , F23D2900/00006 , F23D2900/00013
摘要： A burner assembly (10) is provided for combining oxygen and fuel to produce a flame (44). The burner assembly (10) includes a burner block (12) formed to include a flame chamber (32) having inlet and outlet openings (34, 36), a bypass passage (126) for conducting oxygen outside of the flame chamber (32), and a mechanism (20) for discharging fuel into the flame chamber (32) formed in the burner block. An oxygen-supply housing (16) includes a base wall (52) adjacent to the burner block (12) and a chamber (56) for receiving a supply of oxygen. The base wall (52) is formed to include a first aperture (66) for discharging oxygen from the chamber into the flame chamber and at least one second aperture (68) for discharging oxygen from the chamber (56) into the bypass passage (126).
摘要翻译：提供燃烧器组件（10），用于组合氧气和燃料以产生火焰（44）。燃烧器组件（10）包括形成为包括具有入口和出口开口（34,36）的火焰室（32）的燃烧器组件（12），用于在火焰室（32）外部传导氧气的旁路通道（126）以及用于将燃料排放到形成在燃烧器块中的火焰室（32）中的机构（20）。供氧壳体（16）包括邻近燃烧器块（12）的底壁（52）和用于接收氧气供应的腔室（56）。基壁（52）形成为包括用于将氧气从腔室排放到火焰室中的第一孔（66）和用于将氧从室（56）排出到旁路通道（126）中的至少一个第二孔）。

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