Invention Grant
US08171740B2 Annular rich-quench-lean gas turbine combustors with plunged holes 有权
环状富稀燃气涡轮燃烧器,带有漏洞

Annular rich-quench-lean gas turbine combustors with plunged holes
Abstract:
A combustor may include an outer liner having a first group of air admission holes and defining a plurality of outer liner regions. The combustor may further include an inner liner having a second group of air admission holes and defining a plurality of inner liner regions. The first group of air admission holes within a respective outer liner region may include a first plunged air admission hole approximately axially aligned with the respective fuel injector, a second plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a first adjacent outer liner region, the first air admission hole being downstream of the second air admission hole, and a third plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a second adjacent outer liner region.
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