发明名称 |
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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申请公布号 |
US2006029894(A1) |
申请公布日期 |
2006.02.09 |
申请号 |
US20050127038 |
申请日期 |
2005.05.11 |
申请人 |
ZINN BEN T;NEUMEIER YEDIDIA;SEITZMAN JERRY M;JAGODA JECHIEL;HASHMONAY BEN-AMI |
发明人 |
ZINN BEN T.;NEUMEIER YEDIDIA;SEITZMAN JERRY M.;JAGODA JECHIEL;HASHMONAY BEN-AMI |
分类号 |
F23M3/00;F23C5/24;F23C9/00;F23D11/44;F23L1/00;F23R3/42;F23R3/54 |
主分类号 |
F23M3/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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