Patents by Inventor Sophie ESSAYAN

Sophie ESSAYAN 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).

  • Publication number: 20220266584
    Abstract: A method of adhesively bonding a first substrate on a second substrate in an adhesive bonding zone by an adhesive joint integrating a support mesh, wherein surplus adhesive joint is folded over onto one or the other of the first or second substrates so that the support mesh is present over the entire adhesively bonded zone after curing.
    Type: Application
    Filed: June 18, 2020
    Publication date: August 25, 2022
    Inventors: Pierre Antoine BOSSAN, Sophie ESSAYAN, Allison GLUGLA, Jordan KUSCH, Benjamin SAMSON
  • Patent number: 10641178
    Abstract: Method (S) for protecting against fire a fan casing (1) comprising a roughly cylindrical barrel (10) having a main direction extending along a longitudinal axis (X) and an upstream flange (20) extending radially with respect to the longitudinal axis (X) from an upstream end of the barrel (10), the fan casing (1) being made of a composite comprising a fibrous reinforcement densified by a matrix, said matrix being polymerized, the protection method(S) comprising the following steps:?—laying (SI) widths containing glass fibre pre-impregnated with a resin capable of affording the fan casing with thermal protection against fire on an upstream radial face (22) of the upstream flange (20), and ?—polymerizing (S2) the resin in order to obtain a protective layer (2).
    Type: Grant
    Filed: January 8, 2015
    Date of Patent: May 5, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Sylvain Corradini, Timothee Elisseeff, Sophie Essayan
  • Publication number: 20160333789
    Abstract: Method (S) for protecting against fire a fan casing (1) comprising a roughly cylindrical barrel (10) having a main direction extending along a longitudinal axis (X) and an upstream flange (20) extending radially with respect to the longitudinal axis (X) from an upstream end of the barrel (10), the fan casing (1) being made of a composite comprising a fibrous reinforcement densified by a matrix, said matrix being polymerized, the protection method(S) comprising the following steps:•—laying (SI) widths containing glass fibre pre-impregnated with a resin capable of affording the fan casing with thermal protection against fire on an upstream radial face (22) of the upstream flange (20), and•—polymerizing (S2) the resin in order to obtain a protective layer (2).
    Type: Application
    Filed: January 8, 2015
    Publication date: November 17, 2016
    Applicants: SNECMA, SNECMA
    Inventors: Sylvain CORRADINI, Timothee ELISSEEFF, Sophie ESSAYAN