Patents by Inventor Seyed Gholamali Saddoughi

Seyed Gholamali Saddoughi 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).

  • Patent number: 7204615
    Abstract: An LED light assembly includes a housing, an LED disposed in the housing, a heat dissipating structure and a fluid current generator. The LED is in thermal communication with the heat dissipating structure and includes a flow path surface. The fluid current generator is disposed in the housing to create a current over the flow path surface.
    Type: Grant
    Filed: December 3, 2003
    Date of Patent: April 17, 2007
    Assignee: Lumination LLC
    Inventors: Mehmet Arik, Todd Garrett Wetzel, Seyed Gholamali Saddoughi, Matthew Patrick Boespflug, James T. Petroski
  • Patent number: 7198234
    Abstract: An apparatus comprising: an aerodynamic surface adapted for producing an adverse pressure gradient in a fluid flow; and a first pulse detonation actuator disposed adjacent the aerodynamic surface and adapted for impulsively detonating a fuel/air mixture to produce a pressure rise and velocity increase of combustion products therein, the aerodynamic surface having a plurality of separation control holes adapted for communicating combustion product flows from the first pulse detonation actuator to the aerodynamic surface for modulating separation of the fluid flow from the aerodynamic surface.
    Type: Grant
    Filed: January 5, 2005
    Date of Patent: April 3, 2007
    Assignee: General Electric Company
    Inventor: Seyed Gholamali Saddoughi
  • Patent number: 7055329
    Abstract: A method enables a gas turbine engine to be operated. The method comprises channeling exhaust gases from a core engine through an exhaust assembly and past at least one flow boundary surface, and selectively operating a noise suppression system extending from the at least one flow boundary surface to facilitate attenuating noise generated during engine operation.
    Type: Grant
    Filed: March 31, 2003
    Date of Patent: June 6, 2006
    Assignee: General Electric Company
    Inventors: Steven Martens, Seyed Gholamali Saddoughi, Kevin Sean Early
  • Patent number: 6869049
    Abstract: An apparatus comprising: an aerodynamic surface adapted for producing an adverse pressure gradient in a fluid flow; and a first pulse detonation actuator disposed adjacent the aerodynamic surface and adapted for impulsively detonating a fuel/air mixture to produce a pressure rise and velocity increase of combustion products therein, the aerodynamic surface having a plurality of separation control holes adapted for communicating combustion product flows from the first pulse detonation actuator to the aerodynamic surface for modulating separation of the fluid flow from the aerodynamic surface.
    Type: Grant
    Filed: July 24, 2002
    Date of Patent: March 22, 2005
    Assignee: General Electric Company
    Inventor: Seyed Gholamali Saddoughi
  • Publication number: 20040187474
    Abstract: A method enables a gas turbine engine to be operated. The method comprises channeling exhaust gases from a core engine through an exhaust assembly and past at least one flow boundary surface, and selectively operating a noise suppression system extending from the at least one flow boundary surface to facilitate attenuating noise generated during engine operation.
    Type: Application
    Filed: March 31, 2003
    Publication date: September 30, 2004
    Inventors: Steven Martens, Seyed Gholamali Saddoughi, Kevin Sean Early
  • Publication number: 20040190305
    Abstract: An LED light assembly includes a housing, an LED disposed in the housing, a heat dissipating structure and a fluid current generator. The LED is in thermal communication with the heat dissipating structure and includes a flow path surface. The fluid current generator is disposed in the housing to create a current over the flow path surface.
    Type: Application
    Filed: December 3, 2003
    Publication date: September 30, 2004
    Applicants: General Electric Company, GELcore LLC
    Inventors: Mehmet Arik, Todd Garrett Wetzel, Seyed Gholamali Saddoughi, Matthew Patrick Boespflug, James T. Petroski
  • Publication number: 20040016853
    Abstract: An apparatus comprising: an aerodynamic surface adapted for producing an adverse pressure gradient in a fluid flow; and a first pulse detonation actuator disposed adjacent the aerodynamic surface and adapted for impulsively detonating a fuel/air mixture to produce a pressure rise and velocity increase of combustion products therein, the aerodynamic surface having a plurality of separation control holes adapted for communicating combustion product flows from the first pulse detonation actuator to the aerodynamic surface for modulating separation of the fluid flow from the aerodynamic surface.
    Type: Application
    Filed: July 24, 2002
    Publication date: January 29, 2004
    Applicant: General Electric Company
    Inventor: Seyed Gholamali Saddoughi
  • Patent number: 6629674
    Abstract: An apparatus comprising: an airfoil adapted for generating a lift force; and a first pulse detonation actuator disposed inside the airfoil and adapted for impulsively detonating a fuel/air mixture to produce a pressure rise and velocity increase of combustion products therein, the airfoil having a plurality of lift control holes adapted for communicating combustion product flows from the first pulse detonation actuator to an airfoil surface to modulate the lift force.
    Type: Grant
    Filed: July 24, 2002
    Date of Patent: October 7, 2003
    Assignee: General Electric Company
    Inventors: Seyed Gholamali Saddoughi, Ivett Alejandra Leyva, Anthony John Dean, Bernard Francois Robic, Lawrence Butler