Patents Assigned to Hurel-Hispano Meudon
  • Patent number: 6516606
    Abstract: The invention discloses an aeroengine nacelle afterbody of the type comprising a common nozzle for exhausting the mixed hot and cold gases originating respectively from the fan duct and from the aeroengine combustion chamber, the said nozzle having a longitudinal axis more or less coincident with the axis of the said engine. The common exhaust nozzle consists of two half-nozzles which are more or less symmetric with respect to a plane containing the said longitudinal axis, the said half-nozzles being, on the one hand, individually hinged via one of their longitudinal edges to a support structure hanging down from the wing structure or from the fuselage of the aircraft and, on the other hand, lockable together along their opposite longitudinal edges.
    Type: Grant
    Filed: July 17, 2001
    Date of Patent: February 11, 2003
    Assignee: Hurel-Hispano Meudon
    Inventors: Alain Fournier, Bernard Laboure
  • Publication number: 20020006333
    Abstract: The invention discloses an aeroengine nacelle afterbody of the type comprising a common nozzle for exhausting the mixed hot and cold gases originating respectively from the fan duct and from the aeroengine combustion chamber, the said nozzle having a longitudinal axis more or less coincident with the axis of the said engine. The common exhaust nozzle consists of two half-nozzles which are more or less symmetric with respect to a plane containing the said longitudinal axis, the said half-nozzles being, on the one hand, individually hinged via one of their longitudinal edges to a support structure hanging down from the wing structure or from the fuselage of the aircraft and, on the other hand, lockable together along their opposite longitudinal edges.
    Type: Application
    Filed: July 17, 2001
    Publication date: January 17, 2002
    Applicant: HUREL-HISPANO MEUDON
    Inventors: Alain Fournier, Bernard Laboure