发明申请
US20060029894A1 Stagnation point reverse flow combustor for a combustion system 有权
用于燃烧系统的停滞点反流燃烧器

Stagnation point reverse flow combustor for a combustion system
摘要:
A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end.
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