Invention Grant
US09194585B2 Cooling for combustor liners with accelerating channels 有权
用于具有加速通道的燃烧器衬套的冷却

Cooling for combustor liners with accelerating channels
Abstract:
A combustor liner which reduces cooling flow to a combustion chamber and augments pressure drop split between impingement holes and effusion holes is disclosed. The combustor liner may further include accelerating channels, trip strips, pedestals, and cone-shaped effusion holes to provide further cooling of the liner. The combustor liner may reduce NOx production and the temperature of the combustion chamber of a gas turbine engine or the like.
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