Patents by Inventor Nicolas Picco

Nicolas Picco 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: 9784394
    Abstract: Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
    Type: Grant
    Filed: July 6, 2016
    Date of Patent: October 10, 2017
    Assignee: Zodiac Aerosafety Systems
    Inventors: Amine Sannadi, Nicolas Picco
  • Publication number: 20160312938
    Abstract: Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
    Type: Application
    Filed: July 6, 2016
    Publication date: October 27, 2016
    Inventors: Amine Sannadi, Nicolas Picco
  • Patent number: 9404610
    Abstract: Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
    Type: Grant
    Filed: January 14, 2014
    Date of Patent: August 2, 2016
    Assignee: Zodiac Aerosafety Systems
    Inventors: Amine Sannadi, Nicolas Picco
  • Patent number: 9309003
    Abstract: Systems for improved access door assemblies. In particular, disclosed are boltless/screwless access door assemblies with a radial sealing mechanism. In some embodiments, the access door assembly includes a shoulder configured to withstand interior stresses and a retaining strip configured to withstand exterior stresses. The access door assembly is also configured to be opened when the retaining strip is released.
    Type: Grant
    Filed: January 14, 2014
    Date of Patent: April 12, 2016
    Assignee: Zodiac Aerosafety Systems
    Inventors: Amine Sannadi, Nicolas Picco
  • Publication number: 20140217723
    Abstract: Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
    Type: Application
    Filed: January 14, 2014
    Publication date: August 7, 2014
    Applicant: Aerazur S.A.
    Inventors: Amine Sannadi, Nicolas Picco
  • Publication number: 20140196378
    Abstract: Systems for improved access door assemblies. In particular, disclosed are boltless/screwless access door assemblies with a radial sealing mechanism. In some embodiments, the access door assembly includes a shoulder configured to withstand interior stresses and a retaining strip configured to withstand exterior stresses. The access door assembly is also configured to be opened when the retaining strip is released.
    Type: Application
    Filed: January 14, 2014
    Publication date: July 17, 2014
    Applicant: Aerazur S.A.
    Inventors: Amine Sannadi, Nicolas Picco
  • Publication number: 20140131999
    Abstract: Embodiments of the present invention relate generally to a claw quick disconnect intercom fitting. The intercom fitting has a locking fit that features two independent locking systems that are generally operable together, without tools and with one hand. A claw ring and a clutch ring are configured to be assembled together and to move together, although they separately activate a claw lock and a clutch lock.
    Type: Application
    Filed: July 10, 2013
    Publication date: May 15, 2014
    Applicant: AERAZUR S. A.
    Inventors: Amine Sannadi, Nicolas Picco
  • Patent number: 8485473
    Abstract: According to the invention, the method comprises exposing a surface (3) sensitive to relative wind and monitoring the thermal flow variations between the surface (3) and the aerodynamic flow, said variations resulting from that of the forced-convection thermal exchange coefficient between the surface (3) and the aerodynamic flow depending on the rime or ice build-up, using the temperature sensor (12) under the surface (3), considering that stripping occurs by the flow of an ice layer formed on the surface (3) if it is detected, preferably after heating by at least one heater (4), that there is a brisk rise of the flow at a temperature close to 0° C., and supplying after the detection of ice stripping, a signal indicating the presence of rime or rime conditions. A cooler (5) may cool the surface (3) for anticipating the formation of ice with a heating process. The invention can be used for detecting rime and/or rime conditions on a flying aircraft.
    Type: Grant
    Filed: April 9, 2008
    Date of Patent: July 16, 2013
    Assignee: Intertechnique
    Inventors: Nicolas Picco, Bruno Thillays, Philippe Portier, Francois Larue
  • Publication number: 20100116940
    Abstract: According to the invention, the method comprises exposing a surface (3) sensitive to relative wind and monitoring the thermal flow variations between the surface (3) and the aerodynamic flow, said variations resulting from that of the forced-convection thermal exchange coefficient between the surface (3) and the aerodynamic flow depending on the rime or ice build-up, using the temperature sensor (12) under the surface (3), considering that stripping occurs by the flow of an ice layer formed on the surface (3) if it is detected, preferably after heating by at least one heater (4), that there is a brisk rise of the flow at a temperature close to 0° C., and supplying after the detection of ice stripping, a signal indicating the presence of rime or rime conditions. A cooler (5) may cool the surface (3) for anticipating the formation of ice with a heating process. The invention can be used for detecting rime and/or rime conditions on a flying aircraft.
    Type: Application
    Filed: April 9, 2008
    Publication date: May 13, 2010
    Inventors: Nicolas Picco, Bruno Thillays, Philippe Portier, Francois Larue