Patents by Inventor Raymond Kulak

Raymond Kulak 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: 7377748
    Abstract: A component for use in a gas turbine engine is provided. The component has an airfoil portion with a plurality of internal cooling passages and a non-linear trailing edge. The component further has a non-linear array of teardrop shaped assemblies which form a plurality of injection slots for injecting a coolant fluid into a fluid passing over the airfoil portion. The teardrop shaped assemblies are designed to maximize thermal performance of the component by reducing a relative diffusion angle between the injected coolant flow and the streamline direction of the fluid passing over the airfoil portion.
    Type: Grant
    Filed: September 22, 2005
    Date of Patent: May 27, 2008
    Assignee: United Technologies Corporation
    Inventors: Dominic J. Mongillo, Jr., Young H. Chon, Eugene Kulak, legal representative, Raymond Kulak
  • Publication number: 20070224033
    Abstract: A component for use in a gas turbine engine is provided. The component has an airfoil portion with a plurality of internal cooling passages and a non-linear trailing edge. The component further has a non-linear array of teardrop shaped assemblies which form a plurality of injection slots for injecting a coolant fluid into a fluid passing over the airfoil portion. The teardrop shaped assemblies are designed to maximize thermal performance of the component by reducing a relative diffusion angle between the injected coolant flow and the streamline direction of the fluid passing over the airfoil portion.
    Type: Application
    Filed: September 22, 2005
    Publication date: September 27, 2007
    Inventors: Dominic Mongillo, Young Chon, Raymond Kulak
  • Patent number: 7021893
    Abstract: A component for use in a gas turbine engine is provided. The component has an airfoil portion with a plurality of internal cooling passages and a non-linear trailing edge. The component further has a non-linear array of teardrop shaped assemblies which form a plurality of injection slots for injecting a coolant fluid into a fluid passing over the airfoil portion. The teardrop shaped assemblies are designed to maximize thermal performance of the component by reducing a relative diffusion angle between the injected coolant flow and the streamline direction of the fluid passing over the airfoil portion.
    Type: Grant
    Filed: January 9, 2004
    Date of Patent: April 4, 2006
    Assignee: United Technologies Corporation
    Inventors: Dominic J. Mongillo, Jr., Young H. Chon, Eugene Kulak, legal representative, Raymond Kulak, deceased
  • Publication number: 20050191167
    Abstract: A component for use in a gas turbine engine is provided. The component has an airfoil portion with a plurality of internal cooling passages and a non-linear trailing edge. The component further has a non-linear array of teardrop shaped assemblies which form a plurality of injection slots for injecting a coolant fluid into a fluid passing over the airfoil portion. The teardrop shaped assemblies are designed to maximize thermal performance of the component by reducing a relative diffusion angle between the injected coolant flow and the streamline direction of the fluid passing over the airfoil portion.
    Type: Application
    Filed: January 9, 2004
    Publication date: September 1, 2005
    Inventors: Dominic Mongillo, Young Chon, Raymond Kulak, Eugene Kulak