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Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
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机译:具有第一会聚体积和第二会聚体积的燃气轮机环形燃烧器,其渐缩程度小于第一会聚体积
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摘要
A gas turbine engine combustor has inboard and outboard walls. A forward bulkhead extends between the walls and cooperates therewith to define a combustor interior volume. In longitudinal section, a first portion of the combustor interior volume converges from fore to aft and a second portion, aft of the first portion converges from fore to aft more gradually than the first portion.
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