Patent ID: 10415425

Abstract:
The invention relates to a turbomachine including:a guide baffle, whose sv guide blades are situated on c guide blade carriers; andan adjacent moving baffle including sb moving blades;the guide baffle nv including impulse bodies which are situated in a cavity system of the guide baffle with movement play with respect to the impulse contact; the moving baffle nb including impulse bodies which are situated in a cavity system of the moving baffle with movement play with respect to the impulse contact; and quotient of sum  of the masses of all impulse bodies of the guide baffle divided by the difference (sv−c) of the number sv of all guide blades minus the number c of all guide blade carriers amounts to at least 1.5 times quotient  of sum  of the masses of all impulse bodies of the moving baffle divided by the number sb of all moving blades