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公开(公告)号：EP2562383A3
公开(公告)日：2018-01-03
申请号：EP12180613.7
申请日：2012-08-16
发明人： Wichmann, Lisa Anne , Snook, Daniel David , Draper, Samuel David , Ouellett, Noemie Dion , Rittenhouse, Scott Allen
CPC分类号： F02C6/06 , F02C3/34 , F02C9/18 , F05D2260/85 , F05D2270/301
摘要： At least one main air compressor (12) makes a compressed ambient gas flow (26). The compressed ambient gas flow (26) is delivered to a turbine combustor (32) at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor (32) from a turbine compressor (30) as at least a first portion of a recirculated gas flow (50). A fuel stream (28) is delivered to the turbine combustor (32), and a combustible mixture is formed and burned, forming the recirculated gas flow (50). A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor (30). At least a portion of the recirculated gas flow (50) is recirculated through a recirculation loop (52). An excess portion of the recirculated gas flow (50) is vented or a portion of the turbine compressor exhaust (44) bypasses the turbine combustor (32) or both.
摘要翻译： 至少一个主空气压缩机（12）产生压缩的环境气流（26）。 压缩的环境气流（26）以大于或基本上等于从涡轮压缩机（30）输送到涡轮机燃烧器（32）的输出压力的压力被输送到涡轮燃烧器（32），作为至少一个 再循环气流（50）的第一部分。 燃料物流（28）被输送到涡轮机燃烧室（32），并且形成并燃烧可燃混合物，形成再循环气流（50）。 产生的涡轮功率基本上等于旋转涡轮压缩机（30）所需的至少一个动力。 再循环气流（50）的至少一部分再循环通过再循环回路（52）。 再循环气流（50）的过量部分被排空或者涡轮压缩机排气（44）的一部分绕过涡轮燃烧室（32）或两者。
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公开(公告)号：EP2562383B1
公开(公告)日：2020-11-25
申请号：EP12180613.7
申请日：2012-08-16
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公开(公告)号：EP2562383A2
公开(公告)日：2013-02-27
申请号：EP12180613.7
申请日：2012-08-16
发明人： Wichmann, Lisa Anne , Snook, Daniel David , Draper, Samuel David , Ouellett, Noemie Dion , Rittenhouse, Scott Allen
CPC分类号： F02C6/06 , F02C3/34 , F02C9/18 , F05D2260/85 , F05D2270/301
摘要： At least one main air compressor (12) makes a compressed ambient gas flow (26). The compressed ambient gas flow (26) is delivered to a turbine combustor (32) at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor (32) from a turbine compressor (30) as at least a first portion of a recirculated gas flow (50). A fuel stream (28) is delivered to the turbine combustor (32), and a combustible mixture is formed and burned, forming the recirculated gas flow (50). A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor (30). At least a portion of the recirculated gas flow (50) is recirculated through a recirculation loop (52). An excess portion of the recirculated gas flow (50) is vented or a portion of the turbine compressor exhaust (44) bypasses the turbine combustor (32) or both.
摘要翻译： 至少一个主空气压缩机（12）形成压缩的环境气流（26）。 压缩的环境气体流（26）以大于或基本等于从涡轮压缩机（30）输送到涡轮机燃烧器（32）的输出压力的压力被输送到涡轮机燃烧器（32），至少至少 循环气流（50）的第一部分。 燃料流（28）被输送到涡轮机燃烧器（32），并且形成并燃烧可燃混合物，形成再循环的气流（50）。 产生涡轮机功率，其大致等于至少旋转涡轮压缩机（30）所需的功率。 再循环气体流（50）的至少一部分通过循环回路（52）再循环。 排出再循环气体流（50）的一部分，或涡轮压缩机排气（44）的一部分绕过涡轮机燃烧室（32）或两者。
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