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公开(公告)号：US4369624A
公开(公告)日：1983-01-25
申请号：US222093
申请日：1981-01-02
申请人： James R. Hamm , William E. Young
发明人： James R. Hamm , William E. Young
摘要： High temperature gas turbine generation systems utilizing multiple heating stages between the primary compressor and expander, including coal based reactors and direct fired combustors.
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公开(公告)号：US4499722A
公开(公告)日：1985-02-19
申请号：US420668
申请日：1982-09-21
申请人： James R. Hamm , William E. Young
发明人： James R. Hamm , William E. Young
摘要： High temperature gas turbine generation systems utilizing multiple heating stages between the primary compressor and expander, including coal based reactors and direct fired combustors.
摘要翻译： 利用主压缩机和膨胀机之间的多个加热阶段的高温燃气轮机发电系统，包括煤基反应堆和直接燃烧的燃烧器。
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公开(公告)号：US4067190A
公开(公告)日：1978-01-10
申请号：US749594
申请日：1976-12-10
申请人： James R. Hamm , Prith P. Singh
发明人： James R. Hamm , Prith P. Singh
CPC分类号： F23R3/40
摘要： A combustor for a gas turbine is shown having a catalytic reactor element to promote low temperature combustion of the fuel. An air-fuel premix chamber is provided in the upstream end of the combustor arrangement to produce a mixture which is substantially uniform throughout a plane transverse to the direction of flow of the mixture just prior to the catalytic element. The premix chamber comprises a short cylindrical member of less diameter than the shell of the combustor and closed at the upstream end, with the opposite end discharging directly to the catalytic element. The upstream portion of the walls of the cylinder contain apertures so that the air and fuel introduced into the upstream end of the combustor must flow axially into the annular space between the shell and the chamber, then the flow is abruptly changed to a somewhat radial component to enter the apertures and then the flow is again abruptly changed to an axial direction to enter the catalytic reactor. This provides a sufficiently tortuous path to uniformly mix the air-fuel components prior to entering the catalytic elements.
摘要翻译： 示出了用于燃气轮机的燃烧器具有催化反应器元件以促进燃料的低温燃烧。 空气燃料预混合室设置在燃烧器装置的上游端，以产生在刚好在催化元件之前横穿于混合物流动方向的整个平面内基本均匀的混合物。 预混合室包括一个直径小于燃烧器外壳的短圆柱形构件，在上游端封闭，相反的端部直接排放到催化元件上。 气缸的壁的上游部分包含孔，使得引入燃烧器的上游端的空气和燃料必须轴向地流入壳体和室之间的环形空间，然后流动突然改变为稍微径向的部件 进入孔，然后将流动再次突然改变为轴向以进入催化反应器。 这提供了在进入催化元件之前均匀混合空气燃料组分的足够曲折的途径。
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公开(公告)号：US4667467A
公开(公告)日：1987-05-26
申请号：US741091
申请日：1985-06-04
申请人： David H. Archer , James R. Hamm , Edward J. Vidt
发明人： David H. Archer , James R. Hamm , Edward J. Vidt
摘要： A method for electric power production or cogeneration of electrical power and process heat and/or steam that integrates a solid carbonaceous fuel gasification system and gas turbine system. Fuel gas produced in the gasification system is combusted and the combustion gases used in the gas turbine system. The gas turbine system uses water spray intercooling of the compressor or compressors, with air-water mixture from the compressor used in the gasification system, while hot exhaust gas from the turbine system has heat recuperated therefrom and is used to produce steam, which is also used in the gasification system.
摘要翻译： 一种将固体碳质燃料气化系统和燃气轮机系统集成在一起的用于电力生产或热电联产的电力和工艺热和/或蒸汽的方法。 在气化系统中产生的燃料气体被燃烧并且在燃气轮机系统中使用燃烧气体。 燃气轮机系统使用压缩机或压缩机的喷水中间冷却，使用来自气化系统中使用的压缩机的空气 - 水混合物，而来自涡轮机系统的热废气具有热回收并用于产生蒸汽，其也是 用于气化系统。
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