Patents by Inventor Guillaume Ring

Guillaume Ring 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).

  • Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
    Patent number: 9388767
    Abstract: An aircraft nacelle comprising a lip extended by an inner conduit forming an air intake, a front frame delimiting with said lip an annular channel within which hot air flows and a panel for acoustic treatment having, from outside inwardly, an acoustic resistive layer, at least one honeycomb structure and a reflective layer as well as ducts for channeling hot air, each including one inlet communicating with the annular channel and one outlet communicating with the inner conduit, wherein the panel for acoustic treatment comprises at least a stabilization chamber in the form of an annular channel with a cross-section larger than that of the ducts which extends over at least a portion of the nacelle circumference and which communicates with a plurality of ducts, the inlets and outlets not being aligned in the longitudinal direction.
    Type: Grant
    Filed: October 3, 2012
    Date of Patent: July 12, 2016
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Alain Porte, Grégory Albet, Guillaume Ring, Pascal Galletti
  • Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
    Publication number: 20140001284
    Abstract: An aircraft nacelle comprising a lip extended by an inner conduit forming an air intake, a front frame delimiting with said lip an annular channel within which hot air flows and a panel for acoustic treatment having, from outside inwardly, an acoustic resistive layer, at least one honeycomb structure and a reflective layer as well as ducts for channeling hot air, each including one inlet communicating with the annular channel and one outlet communicating with the inner conduit, wherein the panel for acoustic treatment comprises at least a stabilization chamber in the form of an annular channel with a cross-section larger than that of the ducts which extends over at least a portion of the nacelle circumference and which communicates with a plurality of ducts, the inlets and outlets not being aligned in the longitudinal direction.
    Type: Application
    Filed: October 3, 2012
    Publication date: January 2, 2014
    Applicant: AIRBUS OPERATIONS SAS
    Inventors: Alain Porte, Grégory Albet, Guillaume Ring, Pascal Galletti