Patents by Inventor Jechiel Jagoda

Jechiel Jagoda has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Stagnation point reverse flow combustor
    Patent number: 7425127
    Abstract: A method for combusting a combustible fuel includes providing a vessel having an opening near a proximate end and a closed distal end defining a combustion chamber. A combustible reactants mixture is presented into the combustion chamber. The combustible reactants mixture is ignited creating a flame and combustion products. The closed end of the combustion chamber is utilized for directing combustion products toward the opening of the combustion chamber creating a reverse flow of combustion products within the combustion chamber. The reverse flow of combustion products is intermixed with combustible reactants mixture to maintain the flame.
    Type: Grant
    Filed: August 26, 2004
    Date of Patent: September 16, 2008
    Assignee: Georgia Tech Research Corporation
    Inventors: Ben T. Zinn, Yedidia Neumeier, Jerry M. Seitzman, Jechiel Jagoda, Yoav Weksler
  • Stagnation point reverse flow combustor for a combustion system
    Patent number: 7168949
    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.
    Type: Grant
    Filed: May 11, 2005
    Date of Patent: January 30, 2007
    Assignee: Georgia Tech Research Center
    Inventors: Ben T. Zinn, Yedidia Neumeier, Jerry M. Seitzman, Jechiel Jagoda, Ben-Ami Hashmonay
  • Stagnation point reverse flow combustor for a combustion system
    Publication number: 20060029894
    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.
    Type: Application
    Filed: May 11, 2005
    Publication date: February 9, 2006
    Inventors: Ben Zinn, Yedidia Neumeier, Jerry Seitzman, Jechiel Jagoda, Ben-Ami Hashmonay
  • Stagnation point reverse flow combustor
    Publication number: 20050277074
    Abstract: A method for combusting a combustible fuel includes providing a vessel having an opening near a proximate end and a closed distal end defining a combustion chamber. A combustible reactants mixture is presented into the combustion chamber. The combustible reactants mixture is ignited creating a flame and combustion products. The closed end of the combustion chamber is utilized for directing combustion products toward the opening of the combustion chamber creating a reverse flow of combustion products within the combustion chamber. The reverse flow of combustion products is intermixed with combustible reactants mixture to maintain the flame.
    Type: Application
    Filed: August 26, 2004
    Publication date: December 15, 2005
    Inventors: Ben Zinn, Yedidia Neumeier, Jerry Seitzman, Jechiel Jagoda, Yoav Weksler