Gas turbine for use as turbofan engine, for aircraft in e.g. hot countries, has heat insulating layer provided on surface of blades of guide vane ring along flowing direction of working gas downstream behind profile center of gravity
SEITZ, THILO, KRAFT, JOERN, LUEBCKE, TIM, DEPPE, ANDREAS, SCHLOESSER, MARCEL, CZERNER, STEFAN
Year of Publication 09.02.2012
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Year of Publication 09.02.2012
Patent