专利名称：CLOSED-LOOP CONTROL FOR A GAS
TURBINE WITH ACTIVELY STABILIZEDCOMPRESSOR
发明人：HORN, WOLFGANG,SCHMIDT, KLAUS-JUERGEN
申请号：EP08784357.9申请日：20080717公开号：EP2171216B1公开日：20130911
摘要：A closed-loop control system for a gas turbine, in particular an aircraft engine,has devices for blade-tip blowing-in (ASC) in order to improve the compressor stability,which devices are activated when required. The closed-loop control system is
characterized in that it has devices for active gap control (ACC), preferably in the high-pressure compressor, by which means the radial gap in the high-pressure compressor iskept in an optimum operating range, and wherein the control system has a commonengine regulator (1) for both devices (ASC, ACC). The invention avoids the technicalproblems of the prior art and provides a better closed-loop control system for a gasturbine, in particular an aircraft engine, for active stabilization of the compressor.
申请人：MTU AERO ENGINES GMBH,MTU AERO ENGINES GMBH,MTU AERO ENGINESGMBH
地址：DE
国籍：DE
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