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    • 45. 发明公开
    • POWER PLANT WITH STEAM GENERATION VIA COMBUSTOR GAS EXTRACTION
    • 通过燃烧器提取蒸汽的电厂
    • EP3181858A1
    • 2017-06-21
    • EP16201721.4
    • 2016-12-01
    • General Electric Company
    • KLOSINSKI, Joseph PhilipSCIPIO, Alston IlfordEKANAYAKE, Sanji
    • F02C1/06F02C3/30F02C6/18F02C9/18F22B1/18
    • F02C6/06F01D25/305F01K7/16F01K23/10F02C1/06F02C3/04F02C3/30F02C6/18F02C9/18F05D2220/31F05D2260/212H02K7/1823Y02E20/14Y02E20/16
    • A power plant (10) includes a gas turbine (100) having a combustor (104) downstream from a compressor (102), a turbine (106) disposed downstream from the combustor (104) and an exhaust duct (120) downstream from an outlet of the turbine (106). The combustor (104) includes an extraction port (140) that is in fluid communication with a hot gas path (138) of the combustor (104). The extraction port (140) defines a flow path for a stream of combustion gas (114) to flow out of the hot gas path (138). The exhaust duct (120) receives exhaust gas (118) from the turbine outlet. A coolant injection system (148) injects a coolant (150) into the stream of combustion gas (114) upstream from the exhaust duct (120) such that the stream of combustion gas (114) blends with the exhaust gas (118) from the turbine (106) within the exhaust duct (120) and forms an exhaust gas mixture (156) within the exhaust duct (120). A heat exchanger (122) is disposed downstream from the exhaust duct (120) and receives the exhaust gas mixture (156) from the exhaust duct (120).
    • 发电设备(10)包括具有位于压缩机(102)下游的燃烧器(104),设置在燃烧器(104)下游的涡轮机(106)和位于燃烧器(104)下游的排气管道(120)的燃气轮机 涡轮机(106)的出口。 燃烧器(104)包括与燃烧器(104)的热气体路径(138)流体连通的抽取端口(140)。 提取端口(140)限定用于燃烧气体流(114)流出热气体路径(138)的流动路径。 排气管(120)接收来自涡轮机出口的排气(118)。 冷却剂喷射系统(148)将冷却剂(150)喷射到排气管道(120)上游的燃烧气体流(114)中,使得燃烧气体(114)流与排气(118) 涡轮机(106)在排气管道(120)内并且在排气管道(120)内形成排气混合物(156)。 热交换器(122)设置在排气管道(120)的下游并从排气管道(120)接收排气混合物(156)。
    • 50. 发明公开
    • HEAVY DUTY GAS TURBINE INLET SYSTEM
    • 工业石膏纤维系统
    • EP3064742A1
    • 2016-09-07
    • EP16158298.6
    • 2016-03-02
    • General Electric Company
    • PONYAVIN, Valery IvanovichZHANG, HuaMERCHANT, LaxmikantVENUGOPAL SETTY, Dinesh
    • F02C3/30F02C7/045F02C7/047
    • F02C7/045B64D29/00F02C3/30F02C7/047F05D2260/96
    • A silencer apparatus for a gas turbine inlet system ducting is disclosed. The inlet ducting contains a main silencer 42 and a pre-silencer 45, and Inlet Bleed Heat ("IBH") 43 located between the silencers. The pre-silencer decreases the noise level from the turbine compressor and makes the air flow/temperature profiles more uniform. The main silencer reduces noise from the IBH and the remaining noise from the compressor to an appropriate level. The main silencer is comprised of a first plurality of sound-absorbing splitters disposed along the gas flow direction. The pre-silencer is comprised of a second plurality of sound-absorbing splitters disposed along the gas flow direction, but staggered with respect to the first plurality of splitters to thereby block a direct line of travel for noise acoustical waves from the compressor travelling opposite the gas flow direction in the inlet ducting.
    • 公开了一种用于燃气轮机入口系统管道的消声器装置。 入口管道包含主消音器42和预消音器45,以及位于消音器之间的入口放热(“IBH”)43。 预消音器降低了涡轮压缩机的噪音水平,使空气流量/温度曲线更加均匀。 主消声器将IBH的噪音和压缩机的噪音降低到适当的水平。 主消声器由沿着气体流动方向设置的第一多个吸声分离器构成。 预消声器包括沿着气体流动方向设置的第二组多个吸声分离器,但是相对于第一多个分离器交错,从而阻挡来自压缩机的噪声声波的直接行进线 入口管道中的气体流动方向。