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公开(公告)号:US20070021899A1
公开(公告)日:2007-01-25
申请号:US11447893
申请日:2006-06-07
申请人: Ian Griffin , Arthur Rowe , Andrew Stevenson , Jean-Francois Lebel , Caroline Mohamed , Timofei Breikin , David Sherwood
发明人: Ian Griffin , Arthur Rowe , Andrew Stevenson , Jean-Francois Lebel , Caroline Mohamed , Timofei Breikin , David Sherwood
CPC分类号: F02C9/34 , F05D2270/303 , F23R3/346
摘要: A method for operating a multi-stage combustor of a gas turbine engine comprises: (a) determining a combustor air entry temperature; (b) determining the combustor air entry flow rate; and (c) controlling the fuel split ratio to stages of the combustor on the basis of the combustor air entry flow rate and the combustor air entry temperature.
摘要翻译: 一种用于操作燃气涡轮发动机的多级燃烧器的方法包括:(a)确定燃烧器空气入口温度; (b)确定燃烧器空气入口流量; 以及(c)基于燃烧器空气进入流量和燃烧器空气进入温度来控制燃料分配比与燃烧器的各阶段。