公开(公告)号：US20060005526A1

公开(公告)日：2006-01-12

申请号：US10528408

申请日：2003-10-09

申请人： Satoshi Tanaka ,  Fuminori Fuji ,  Naoki Ujiie ,  Kozo Toyama

发明人： Satoshi Tanaka ,  Fuminori Fuji ,  Naoki Ujiie ,  Kozo Toyama

IPC分类号： F02C9/50

CPC分类号： F02C9/00 ,  F02C7/228 ,  F02C9/34

摘要： A turbine inlet temperature operating section (15) determines the turbine inlet temperature T4 based on the flow rate Gf and temperature Tf of fuel being supplied to a combustor (3) and the flow rate G3 and temperature T3 of air. Based on the turbine inlet temperature T4, a pilot ratio operating section (16) sets a pilot ratio, and a bypass valve operating section (17) and an IGV opening operating section (18) generate a bypass valve control signal and an IGV control signal, respectively.

摘要翻译： 涡轮入口温度运行部分（15）基于供给到燃烧器（3）的燃料的流量Gf和温度Tf以及空气的流量G 3和温度T 3来确定涡轮机入口温度T 4。 基于涡轮机入口温度T 4，先导比操作部（16）设定先导比，旁通阀操作部（17）和IGV打开操作部（18）产生旁通阀控制信号和IGV控制 信号。

公开(公告)号：US07191588B2

公开(公告)日：2007-03-20

申请号：US10528408

申请日：2003-10-09

申请人： Satoshi Tanaka ,  Shinsuke Nakamura ,  Fuminori Fuji ,  Naoki Ujiie ,  Kozo Toyama

发明人： Satoshi Tanaka ,  Shinsuke Nakamura ,  Fuminori Fuji ,  Naoki Ujiie ,  Kozo Toyama

IPC分类号： F02C9/28 ,  F02C9/48

CPC分类号： F02C9/00 ,  F02C7/228 ,  F02C9/34

摘要： A turbine inlet temperature operating section (15) determines the turbine inlet temperature T4 based on the flow rate Gf and temperature Tf of fuel being supplied to a combustor (3) and the flow rate G3 and temperature T3 of air. Based on the turbine inlet temperature T4, a pilot ratio operating section (16) sets a pilot ratio, and a bypass valve operating section (17) and an IGV opening operating section (18) generate a bypass valve control signal and an IGV control signal, respectively.

摘要翻译： 涡轮入口温度运行部分（15）基于供给到燃烧器（3）的燃料的流量Gf和温度Tf以及空气的流量G 3和温度T 3来确定涡轮机入口温度T 4。 基于涡轮机入口温度T 4，先导比操作部（16）设定先导比，旁通阀操作部（17）和IGV打开操作部（18）产生旁通阀控制信号和IGV控制 信号。