| 摘要 |
The present invention relates to a method for operating a combustion system (10) of a combustion section (12) of a gas turbine engine (14) comprising at least one main burner arrangement (16) and at least one pilot burner arrangement (18), wherein the at least one main burner arrangement (16) and the at least one pilot burner arrangement (18) are operated with an air-fuel mixture (20), wherein the method comprises the step(s) of: Enriching an air (22) of the air-fuel mixture (20) of the at least one pilot burner arrangement (18) and/or a fuel (24) of the air-fuel mixture (20) of the at least one pilot burner arrangement (18) and/or the air-fuel mixture (20) of the at least one pilot burner arrangement (18) with oxygen (26) and preferably with pure oxygen (26). |
