Title:
STAGNATION POINT REVERSE FLOW COMBUSTOR FOR A COMBUSTION SYSTEM
Document Type and Number:
WIPO Patent Application WO2006085922
Kind Code:
A9
Abstract:
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.
Inventors:
ZINN BEN T (US)
NEUMEIER YEDIDIA (US)
SEITZMAN JERRY M (US)
JAGODA JECHIEL (US)
HASHMONAY BEN-AMI (IL)
WEKSLER YOAV (IL)
NEUMEIER YEDIDIA (US)
SEITZMAN JERRY M (US)
JAGODA JECHIEL (US)
HASHMONAY BEN-AMI (IL)
WEKSLER YOAV (IL)
Application Number:
PCT/US2005/020389
Publication Date:
October 05, 2006
Filing Date:
June 09, 2005
Export Citation:
Assignee:
GEORGIA TECH RES INST (US)
ZINN BEN T (US)
NEUMEIER YEDIDIA (US)
SEITZMAN JERRY M (US)
JAGODA JECHIEL (US)
HASHMONAY BEN-AMI (IL)
WEKSLER YOAV (IL)
ZINN BEN T (US)
NEUMEIER YEDIDIA (US)
SEITZMAN JERRY M (US)
JAGODA JECHIEL (US)
HASHMONAY BEN-AMI (IL)
WEKSLER YOAV (IL)
International Classes:
F23M3/00; F23C5/24; F23C9/00; F23L1/00; F23R3/42; F23R3/54
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