Patents by Inventor Joseph Taglialavore

Joseph Taglialavore 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).

  • Fire resistance device intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment
    Patent number: 11480107
    Abstract: A fire resistance device is intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment.
    Type: Grant
    Filed: February 14, 2019
    Date of Patent: October 25, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Bruno Alexandre Didier Jacon, Baghdad Achbari, Thomas Claude Broage, Hervé Simonotti, Soufien Akachkachy, Charles Maurice Jean-Louis Cheret, Joseph Taglialavore
  • FIRE RESISTANCE DEVICE INTENDED TO BE INTERPOSED BETWEEN AN UPSTREAM END OF AN AIRCRAFT TURBINE ENGINE MOUNTING STRUCTURE AND A COWLING OF THE TURBINE ENGINE DELIMITING AN INTER-FLOW COMPARTMENT
    Publication number: 20210095569
    Abstract: A fire resistance device is intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment.
    Type: Application
    Filed: February 14, 2019
    Publication date: April 1, 2021
    Inventors: Bruno Alexander Didier JACON, Baghdad ACHBARI, Thomas Claude BROAGE, Hervé SIMONOTTI, Soufien AKACHKACHY, Charles Maurice Jean-Louis CHERET, Joseph TAGLIALAVORE
  • Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm
    Patent number: 7661272
    Abstract: A turbofan jet engine includes an external easing, connected by radial arms to an annular internal device, downstream of which is mounted, opposite to the external casing, a shell forming a fairing, ancillaries on the outside of the external casing, and ancillaries on the inside of the shell. The turbofan jet engine further includes at least one monoblock arm for the connection of ancillaries between the outside of the external casing and the inside of the shell, placed parallel to a radial arm.
    Type: Grant
    Filed: September 15, 2005
    Date of Patent: February 16, 2010
    Assignee: Snecma
    Inventors: Pierre Gagneux, Lionel Jean Leon Lefranc, Johnny Letache, Joseph Taglialavore
  • Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm
    Publication number: 20070234706
    Abstract: The invention concerns a turbofan jet engine that includes an external casing, connected by radial arms to an annular internal device, downstream of which is mounted, opposite to the external casing, a shell forming a fairing, ancillaries on the outside of the external casing, and ancillaries on the inside of the shell. It is characterised by the fact that the turbofan jet engine includes at least one monoblock arm for the connection of ancillaries between the outside of the external casing and the inside of the shell, placed parallel to a radial arm. The invention applies to double-flow turbofan jet engines.
    Type: Application
    Filed: September 15, 2005
    Publication date: October 11, 2007
    Applicant: SNECMA
    Inventors: Pierre Gagneux, Lionel Jean Lefranc, Johnny Letache, Joseph Taglialavore