The invention relates to a method for cleaning an aircraft engine. A cleaning agent and/or a cleaning tool are introduced directly into a rear compression step, a combustion chamber and/or a turbine of a gas turbine.
申请公布号
WO2009129788(A2)
申请公布日期
2009.10.29
申请号
WO2009DE00531
申请日期
2009.04.18
申请人
MTU AERO ENGINES GMBH;SEIDEL, FRANK;OLFE, JUERGEN;WINKLER, LUTZ
