Patents by Inventor Georges Broers

Georges Broers 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: 8899917
    Abstract: The invention relates to a gas flow separator dividing the flow into a primary and a secondary stream, especially for a dual rotor axial turbomachine. The separator comprises a splitter nose of the turbomachine and includes a generally wedge-shaped leading edge in the gas flow to be split. The flow separator also comprises a metal blade having a longitudinal section in the form of an ā€œSā€ and located in the nose in contact with the back of the leading edge and extending from the leading edge to a rear end of the separator at some distance from the leading edge, so as to be in contact with a heat source, such as a heat exchanger, located at some distance from the leading edge.
    Type: Grant
    Filed: March 26, 2012
    Date of Patent: December 2, 2014
    Assignee: Techspace Aero S.A.
    Inventors: Denis Bajusz, Nicholas Raimarckers, Antoine Stephany, Georges Broers, Yves Culot, Marc Strengnart, Albert Cornet, David Depaepe
  • Publication number: 20120251373
    Abstract: The invention relates to a gas flow separator dividing the flow into a primary and a secondary stream, especially for a dual rotor axial turbomachine. The separator comprises a splitter nose of the turbomachine and includes a generally wedge-shaped leading edge in the gas flow to be split. The flow separator also comprises a metal blade having a longitudinal section in the form of an ā€œSā€ and located in the nose in contact with the back of the leading edge and extending from the leading edge to a rear end of the separator at some distance from the leading edge, so as to be in contact with a heat source, such as a heat exchanger, located at some distance from the leading edge.
    Type: Application
    Filed: March 26, 2012
    Publication date: October 4, 2012
    Applicant: TECHSPACE AERO S.A.
    Inventors: Denis Bajusz, Yves Culot, Marc Strengnart, Antoine Stephany, David Depaepe, Albert Cornet, Nicolas Raimarckers, Georges Broers
  • Patent number: 7722321
    Abstract: A turbo-engine stator blading is disclosed. The turbo-engine stator blading includes a crown of fixed blades mounted on a ring. Each blade includes a platform and each blade is fastened to the ring. The ring includes a plurality of individual receptacles for the each of the platforms, the receptacles being machined in the thickness of the ring, the form of each receptacle being complementary to that of the corresponding platform. By means of the receptacles, the mounting of the blades within the blading is both simple and accurate.
    Type: Grant
    Filed: December 20, 2006
    Date of Patent: May 25, 2010
    Assignee: Techspace Aero
    Inventors: Andre Lhoest, Georges Broers, Thomas Colmant, Georges Duchaine, Xavier Wery
  • Publication number: 20070147993
    Abstract: The turbo-engine stator blading of the invention comprises a crown of fixed blades mounted on a ring, each blade comprising a platform intended to be fastened to the ring. The blading is characterized in that the ring comprises a plurality of individual receptacles for the platforms, the said receptacles being machined in the thickness of the ring, the form of each receptacle being complementary to that of the corresponding platform. By means of the receptacles, the mounting of the blades within the blading is both simple and accurate.
    Type: Application
    Filed: December 20, 2006
    Publication date: June 28, 2007
    Applicant: TECHSPACE AERO
    Inventors: Andre Lhoest, Georges Broers, Thomas Colmant, Georges Duchaine, Xavier Wery