Patents by Inventor Oleg Morenko

Oleg Morenko 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: 7025566
    Abstract: A gas turbine engine diffuser comprises a bowl-shaped diffuser casing and a cover nested into the bowl-shaped diffuser casing and cooperating therewith in defining a diffuser passage having a channeled entry portion in fluid flow communication with a vaned exit portion via a vaneless intermediate portion. The channeled entry portion is divided into an array of inlet flowpaths by a first set of vanes. Likewise, the vaned exit portion is divided into an array of outlet flowpaths by a second set of vanes.
    Type: Grant
    Filed: November 4, 2003
    Date of Patent: April 11, 2006
    Assignee: Pratt & Whitney Canada Corp.
    Inventors: Ioan Sasu, Doug Roberts, Oleg Morenko
  • Patent number: 7024863
    Abstract: A gas turbine engine with: a compressor section; a turbine section; a combustor, disposed between the compressor and turbine sections, having at least one combustor mounting assembly connecting the combustor to the engine. Each combustor mounting assembly has: a longitudinal axis; and an articulating joint having a first and second portion constrained from relative translation transverse to the longitudinal axis, and where said first and second portion have a multiple rotational degrees of freedom relative to each other about axes transverse to the longitudinal axis.
    Type: Grant
    Filed: July 8, 2003
    Date of Patent: April 11, 2006
    Assignee: Pratt & Whitney Canada Corp.
    Inventor: Oleg Morenko
  • Publication number: 20060042271
    Abstract: An improved gas turbine engine combustor includes a planar region in which manufacturing tolerances are improved and thus cost of the combustor can be reduced.
    Type: Application
    Filed: August 27, 2004
    Publication date: March 2, 2006
    Inventors: Oleg Morenko, Bhawan Patel
  • Publication number: 20060042263
    Abstract: A gas turbine engine combustor includes an apparatus for directing air around the axis along which fuel is injected into the combustor to thereby improve the combustor.
    Type: Application
    Filed: August 27, 2004
    Publication date: March 2, 2006
    Inventors: Bhawan Patel, Oleg Morenko, Parthasarathy Sampath
  • Publication number: 20050095127
    Abstract: A gas turbine engine diffuser comprises a bowl-shaped diffuser casing and a cover nested into the bowl-shaped diffuser casing and cooperating therewith in defining a diffuser passage having a channeled entry portion in fluid flow communication with a vaned exit portion via a vaneless intermediate portion. The channeled entry portion is divided into an array of inlet flowpaths by a first set of vanes. Likewise, the vaned exit portion is divided into an array of outlet flowpaths by a second set of vanes.
    Type: Application
    Filed: November 4, 2003
    Publication date: May 5, 2005
    Inventors: Ioan Sasu, Doug Roberts, Oleg Morenko
  • Publication number: 20050016182
    Abstract: A gas turbine engine with: a compressor section; a turbine section; a combustor, disposed between the compressor and turbine sections, having at least one combustor mounting assembly connecting the combustor to the engine. Each combustor mounting assembly has: a longitudinal axis; and an articulating joint having a first and second portion constrained from relative translation transverse to the longitudinal axis, and where said first and second portion have a multiple rotational degrees of freedom relative to each other about axes transverse to the longitudinal axis.
    Type: Application
    Filed: July 8, 2003
    Publication date: January 27, 2005
    Inventor: Oleg Morenko