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公开(公告)号：US20180306109A1
公开(公告)日：2018-10-25
申请号：US15768187
申请日：2016-10-17
摘要： Disclosed herein is an integrated power generation and load driving system, comprising in combination a multi-shaft gas turbine engine comprising a high-pressure turbine mechanically coupled to an air compressor; and a low-pressure turbine, fluidly coupled to but mechanically separated from the high-pressure turbine and mechanically coupled to an output power shaft wherein the output power shaft is connected to a shaft line an electric generator, mechanically coupled to the shaft line and driven into rotation by the gas turbine engine a rotating load, mechanically coupled to the shaft line and driven into rotation by the gas turbine engine a load control arrangement, configured for controlling at least one operating parameter of the rotating load to adapt the operating condition of the rotating load to process requirements from a process, whereof the rotating load forms part, while the low-pressure turbine and the electric generator rotate at a substantially constant speed.
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公开(公告)号：US20180094585A1
公开(公告)日：2018-04-05
申请号：US15820933
申请日：2017-11-22
发明人： Tommaso BETTI , Antonio BALDASSARRE , Filippo VITI , Stefano MEUCCI , Marco LAZZERI , Roberto MERLO , Daniele MARCUCCI
IPC分类号： F02C7/18 , F02C7/26 , F01D17/14 , F04D29/66 , F04D25/14 , F01D25/12 , F01D19/02 , F02C7/04 , F01D25/34
摘要： An aeroderivative gas turbine including an air intake plenum; a compressor with a compressor air intake in fluid communication with the air intake plenum; a combustor; a high pressure turbine; a power turbine. A forced air-stream generator is arranged in fluid communication with the air intake plenum. A shutter arrangement is provided in a combustion-air flow path, arranged and controlled to close the combustion-air flow path for pressurizing said air intake plenum by means of the forced air-stream generator to a pressure sufficient to cause pressurized air to flow through the aeroderivative air turbine.
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