Gas turbine and method for damping oscillations of an...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S779000, C060S725000, C060S039091

Reexamination Certificate

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06988366

ABSTRACT:
A gas turbine includes an annular combustion chamber and an outer wall of an annular combustion chamber. A straining ring is arranged on the outer wall of the annular combustion chamber and enables oscillations of the outer wall to be damped via friction. The effects of combustion oscillations produced by damaging vibrations of the annular combustion chamber are thus reduced. A method is further for damping an oscillation of an outer wall of an annular combustion chamber.

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