发明名称 Changing combustion modes in gas turbine engine
摘要 In a first mode fuel for diffuse combustion is supplied through a first injection nozzle 4, while in a second mode fuel for premixed combustion is supplied through a second nozzle 5. The change from one mode to the other (and vice versa) is controlled by electronic control means 1, in accordance with engine speed and/or load. The control means also controls a purge air switch portion 6, and a fuel supply portion 2, to provide air purge of the nozzle to which fuel supply has been terminated, during the mode change, and to temporarily restrict the maximum fuel flow rate to the nozzle to which the fuel supply has been initiated. These measures minimise speed variation during the mode change.
申请公布号 GB2348675(A) 申请公布日期 2000.10.11
申请号 GB20000004694 申请日期 2000.02.28
申请人 * HONDA GIKEN KOGYO KABUSHIKI KAISHA 发明人 HINONORI * MURAMATSU;MASAAKI * ENDOU
分类号 F02C9/28;F02C7/228;F02C7/232;F02C9/34;F23R3/28;F23R3/30;(IPC1-7):F02C7/228;F02C9/26 主分类号 F02C9/28
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