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    • 33. 发明申请
    • PERFORMANCE ENHANCED GAS TURBINE POWERPLANTS
    • 性能增强的气体涡轮发电机
    • WO1995011375A2
    • 1995-04-27
    • PCT/US1994011830
    • 1994-10-18
    • STATE OF CALIFORNIA ENERGY RESOURCES CONSERVATION AND DEVELOPMENT COMMISSION
    • STATE OF CALIFORNIA ENERGY RESOURCES CONSERVATION AND DEVELOPMENT COMMISSIONJANES, Clarence, W.
    • F02C07/18
    • F01D13/00F01D1/00F01D1/023F01K21/047F02C1/06F02C3/28F02C6/003F02C7/143F02C7/18F02C7/185F02C7/224F05D2260/10Y02E20/14Y02E20/16Y02T50/675
    • A gas turbine driven powerplant (10) having one or more compressors (20, 22) for producing a down stream air flow, a compressor heat exchanger (34) positioned down stream of the compressors (20, 22) followed by a side stream flow coolant line (50), a regenerator (58) positioned down stream of the heat exchanger (34) and side stream coolant line (50), a combustor (48) positioned down stream of the regenerator (58), one or more turbines (24, 28) positioned down stream of the combustor (48) and mechanically coupled to the compressors (20, 22), and a power turbine (32) positioned down stream of the turbines (24, 28). Combustible effluent flows through heat exchanger (34) and to combustor (48), and air discharged from the compressors (20, 22) flows through heat exchanger (34) and to coolant line (50) and regenerator (58). Heat is transferred from the compressor discharge air to the combustible effluent, thereby producing cooling air and heating the combustible effluent. Heat exchanger (34) can be a heat exchanger or a methane/steam reformer which produces a hydrogen-rich, low NOx, steam diluted combustible effluent. In alternative embodiments, power output is augmented by injecting cooled compressed air directly into the combustor (48) to increase the mass flow through the turbines (24, 28, 32), and exhaust heat is recuperated with a counter-current flow of combustible and water, or water and air, in a conventional once-through heat recovery unit (118). In further embodiments, a small portion of the cool air is combined with the recuperation water in the heat recovery unit (118) to allow vaporization of the water throughout the initial portion of the heat exchange path and form a two-phased feed of water and air to the combustor (48). Additionally, in all embodiments a portion of the cooled compressed air can be processed by a compressor/expander for providing coolant to the turbines, compressors, and auxiliary equipment.
    • 一种具有一个或多个用于产生下游气流的压缩机(20,22)的燃气轮机驱动动力装置(10),位于压缩机(20,22)下游的压缩机热交换器(34),随后是侧流 冷却剂管线(50),位于热交换器(34)下游的再生器(58)和侧流冷却剂管线(50),位于再生器(58)下游的燃烧器(48),一个或多个涡轮机 位于燃烧器(48)下游并机械地联接到压缩机(20,22)的动力涡轮机(32,28),以及定位在涡轮机(24,28)下游的动力涡轮机(32)。 可燃流出物流过热交换器(34)和燃烧器(48),并且从压缩机(20,22)排出的空气流过热交换器(34)和冷却剂管线(50)和再生器(58)。 热量从压缩机排放空气传递到可燃性流出物,从而产生冷却空气并加热可燃性流出物。 热交换器(34)可以是热交换器或甲烷/蒸汽重整器,其产生富含氢的低NOx,蒸汽稀释的可燃性流出物。 在替代实施例中,通过将冷却的压缩空气直接喷射到燃烧器(48)中以增加通过涡轮机(24,28,32)的质量流量来增加功率输出,并且排气热量通过可逆的逆流和 水或水和空气,在常规的直通热回收单元(118)中。 在另外的实施例中,一小部分冷空气与热回收单元(118)中的回收水相结合,以允许水在热交换路径的整个初始部分蒸发并形成两相供水和 空气到燃烧器(48)。 此外,在所有实施例中,冷却的压缩空气的一部分可以由压缩机/膨胀机来处理,以向涡轮机,压缩机和辅助设备提供冷却剂。