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公开(公告)号：US20120023963A1
公开(公告)日：2012-02-02
申请号：US13217713
申请日：2011-08-25
摘要： At least one main air compressor makes a compressed ambient gas flow. The compressed ambient gas flow is delivered to both master and slave turbine combustors at a pressure that is greater than or substantially equal to an output pressure delivered to each turbine combustor from each turbine compressor as at least a first portion of a recirculated gas flow. A fuel stream is delivered to each turbine combustor, and combustible mixtures are formed and burned, forming the recirculated gas flows. A master and slave turbine power are produced, and each is substantially equal to at least a power required to rotate each turbine compressor. At least a portion of the recirculated gas flow is recirculated through recirculation loops. At least a second portion of the recirculated gas flow bypasses the combustors or an excess portion of each recirculated gas flow is vented or both.
摘要翻译： 至少一个主要空气压缩机使压缩的环境气体流动。 压缩的环境气体流以大于或基本上等于从每个涡轮压缩机作为再循环气流的至少第一部分输送到每个涡轮机燃烧器的输出压力的压力被输送到主涡轮燃烧器和从属涡轮机燃烧器。 燃料流被输送到每个涡轮机燃烧器，并且形成并燃烧可燃混合物，形成再循环的气体流。 制造主和从属涡轮机功率，并且每个主要和从属涡轮机功率基本上等于旋转每个涡轮压缩机所需的至少一个功率。 再循环气体的至少一部分通过再循环回路再循环。 再循环气体流的至少第二部分绕过燃烧器，或者每个再循环气体流的多余部分被排出或两者。
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公开(公告)号：US20120023962A1
公开(公告)日：2012-02-02
申请号：US13217658
申请日：2011-08-25
申请人： Lisa Anne Wichmann , Daniel David Snook , Samuel David Draper , Noémie Dion Ouellet , Scott Allen Rittenhouse
发明人： Lisa Anne Wichmann , Daniel David Snook , Samuel David Draper , Noémie Dion Ouellet , Scott Allen Rittenhouse
IPC分类号： F02C9/00
CPC分类号： F02C6/06 , F02C3/34 , F02C9/18 , F05D2260/85 , F05D2270/301
摘要： At least one main air compressor makes a compressed ambient gas flow. The compressed ambient gas flow is delivered to a turbine combustor at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor from a turbine compressor as at least a first portion of a recirculated gas flow. A fuel stream is delivered to the turbine combustor, and a combustible mixture is formed and burned, forming the recirculated gas flow. A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor. At least a portion of the recirculated gas flow is recirculated through a recirculation loop. An excess portion of the recirculated gas flow is vented or a portion of the recirculated gas flow bypasses the turbine combustor or both.
摘要翻译： 至少一个主要空气压缩机使压缩的环境气体流动。 压缩的环境气体流以大于或基本上等于从涡轮压缩机作为再循环气流的至少第一部分输送到涡轮机燃烧器的输出压力的压力被输送到涡轮机燃烧器。 燃料流被输送到涡轮机燃烧器，并且形成并燃烧可燃混合物，形成再循环气体流。 产生的涡轮功率基本上等于至少旋转涡轮压缩机所需的功率。 再循环气流的至少一部分通过循环回路再循环。 再循环气流的一部分被排出，或者再循环气流的一部分绕过涡轮机燃烧室或两者。
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公开(公告)号：US20120023966A1
公开(公告)日：2012-02-02
申请号：US13217646
申请日：2011-08-25
申请人： Noémie Dion Ouellet , Daniel David Snook , Lisa Anne Wichmann , Samuel David Draper , Scott Allen Rittenhouse
发明人： Noémie Dion Ouellet , Daniel David Snook , Lisa Anne Wichmann , Samuel David Draper , Scott Allen Rittenhouse
IPC分类号： F02C7/26
CPC分类号： F02C7/277 , F01D13/02 , F01D19/00 , F02C3/36 , F02C7/18 , F02C9/52 , F05D2220/76 , F05D2260/85 , F05D2270/061 , F05D2270/082 , Y02T50/675 , Y02T50/677
摘要： Ambient air is compressed into a compressed ambient gas flow and delivered to a turbine combustor. At least one of an exhaust port, a bypass conduit, or an extraction conduit is opened to vent the power plant. A turbine shaft is rotated at an ignition speed and a fuel stream is delivered to the turbine combustor for mixing with the compressed ambient gas flow to form a combustible mixture. The combustible mixture is burned and forms a recirculated gas flow that drives the turbine. The recirculated gas flow is recirculated using the recirculation loop. The turbine is operated at a target operating speed and then reaches substantially stoichiometric combustion. At least a portion of the recirculated gas flow is extracted using an extraction conduit that is fluidly connected to the turbine compressor.
摘要翻译： 环境空气被压缩成压缩的环境气流并输送到涡轮机燃烧器。 打开排气口，旁通管道或抽取管道中的至少一个以排放发电厂。 涡轮轴以点火速度旋转，并且燃料流被输送到涡轮机燃烧器以与压缩的环境气流混合以形成可燃混合物。 可燃混合物被燃烧并形成驱动涡轮机的再循环气流。 再循环气体循环使用再循环回路。 涡轮机以目标操作速度运行，然后达到基本上化学计量的燃烧。 使用流体连接到涡轮压缩机的抽出管道提取至少一部分再循环的气流。
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4.发明授权公开(公告)号：US08453462B2
公开(公告)日：2013-06-04
申请号：US13217658
申请日：2011-08-25
申请人： Lisa Anne Wichmann , Daniel David Snook , Samuel David Draper , Noémie Dion Ouellet , Scott Allen Rittenhouse
发明人： Lisa Anne Wichmann , Daniel David Snook , Samuel David Draper , Noémie Dion Ouellet , Scott Allen Rittenhouse
CPC分类号： F02C6/06 , F02C3/34 , F02C9/18 , F05D2260/85 , F05D2270/301
摘要： At least one main air compressor makes a compressed ambient gas flow. The compressed ambient gas flow is delivered to a turbine combustor at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor from a turbine compressor as at least a first portion of a recirculated gas flow. A fuel stream is delivered to the turbine combustor, and a combustible mixture is formed and burned, forming the recirculated gas flow. A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor. At least a portion of the recirculated gas flow is recirculated through a recirculation loop. An excess portion of the recirculated gas flow is vented or a portion of the recirculated gas flow bypasses the turbine combustor or both.
摘要翻译： 至少一个主要空气压缩机使压缩的环境气体流动。 压缩的环境气体流以大于或基本上等于从涡轮压缩机作为再循环气流的至少第一部分输送到涡轮机燃烧器的输出压力的压力被输送到涡轮机燃烧器。 燃料流被输送到涡轮机燃烧器，并且形成并燃烧可燃混合物，形成再循环气体流。 产生的涡轮功率基本上等于至少旋转涡轮压缩机所需的功率。 再循环气流的至少一部分通过循环回路再循环。 再循环气流的一部分被排出，或者再循环气流的一部分绕过涡轮机燃烧室或两者。
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公开(公告)号：US08347600B2
公开(公告)日：2013-01-08
申请号：US13217713
申请日：2011-08-25
IPC分类号： F02C6/00
摘要： At least one main air compressor makes a compressed ambient gas flow. The compressed ambient gas flow is delivered to both master and slave turbine combustors at a pressure that is greater than or substantially equal to an output pressure delivered to each turbine combustor from each turbine compressor as at least a first portion of a recirculated gas flow. A fuel stream is delivered to each turbine combustor, and combustible mixtures are formed and burned, forming the recirculated gas flows. A master and slave turbine power are produced, and each is substantially equal to at least a power required to rotate each turbine compressor. At least a portion of the recirculated gas flow is recirculated through recirculation loops. At least a second portion of the recirculated gas flow bypasses the combustors or an excess portion of each recirculated gas flow is vented or both.
摘要翻译： 至少一个主要空气压缩机使压缩的环境气体流动。 压缩的环境气体流以大于或基本上等于从每个涡轮压缩机作为再循环气流的至少第一部分输送到每个涡轮机燃烧器的输出压力的压力被输送到主涡轮燃烧器和从属涡轮机燃烧器。 燃料流被输送到每个涡轮机燃烧器，并且形成并燃烧可燃混合物，形成再循环的气体流。 制造主和从属涡轮机功率，并且每个主要和从属涡轮机功率基本上等于旋转每个涡轮压缩机所需的至少一个功率。 再循环气体的至少一部分通过再循环回路再循环。 再循环气体流的至少第二部分绕过燃烧器，或者每个再循环气体流的多余部分被排出或两者。
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公开(公告)号：US08266883B2
公开(公告)日：2012-09-18
申请号：US13217646
申请日：2011-08-25
申请人： Noémie Dion Ouellet , Daniel David Snook , Lisa Anne Wichmann , Samuel David Draper , Scott Allen Rittenhouse
发明人： Noémie Dion Ouellet , Daniel David Snook , Lisa Anne Wichmann , Samuel David Draper , Scott Allen Rittenhouse
CPC分类号： F02C7/277 , F01D13/02 , F01D19/00 , F02C3/36 , F02C7/18 , F02C9/52 , F05D2220/76 , F05D2260/85 , F05D2270/061 , F05D2270/082 , Y02T50/675 , Y02T50/677
摘要： Ambient air is compressed into a compressed ambient gas flow and delivered to a turbine combustor. At least one of an exhaust port, a bypass conduit, or an extraction conduit is opened to vent the power plant. A turbine shaft is rotated at an ignition speed and a fuel stream is delivered to the turbine combustor for mixing with the compressed ambient gas flow to form a combustible mixture. The combustible mixture is burned and forms a recirculated gas flow that drives the turbine. The recirculated gas flow is recirculated using the recirculation loop. The turbine is operated at a target operating speed and then reaches substantially stoichiometric combustion. At least a portion of the recirculated gas flow is extracted using an extraction conduit that is fluidly connected to the turbine compressor.
摘要翻译： 环境空气被压缩成压缩的环境气流并输送到涡轮机燃烧器。 打开排气口，旁通管道或抽取管道中的至少一个以排放发电厂。 涡轮轴以点火速度旋转，并且燃料流被输送到涡轮机燃烧器以与压缩的环境气流混合以形成可燃混合物。 可燃混合物被燃烧并形成驱动涡轮机的再循环气流。 再循环气体循环使用再循环回路。 涡轮机以目标操作速度运行，然后达到基本上化学计量的燃烧。 使用流体连接到涡轮压缩机的抽出管道提取至少一部分再循环的气流。
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