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US08661822B2 Acoustically stiffened gas turbine combustor supply 有权
声学加强燃气轮机燃烧室供应

Acoustically stiffened gas turbine combustor supply
Abstract:
In one embodiment, a system includes a variable geometry resonator configured to couple to a fluid path upstream from a combustor of a turbine engine. The variable geometry resonator is configured to dampen pressure oscillations in the fluid path and the combustor.
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