Patents by Inventor Dario Iannucci

Dario Iannucci 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).

  • Aircraft capable of hovering, aircraft maneuvering assist method, and interface
    Patent number: 9214089
    Abstract: An aircraft capable of hovering, and characterized by having at least one sensor, which has a plane sweep region and is designed to acquire, when the aircraft is maneuvering, values of respective distances between first points on an obstacle within the plane sweep region, and a second point on the aircraft; and a control unit designed to generate an alarm signal when at least one of the first points lies within a safety region containing the second point on the aircraft.
    Type: Grant
    Filed: May 20, 2011
    Date of Patent: December 15, 2015
    Assignee: Agusta S.P.A.
    Inventors: Massimo Brunetti, Simone Gobbi, Dario Iannucci, Emilio Majori
  • Aircraft capable of hovering having an exhaust duct with thermoelectric conversion circuit
    Patent number: 8939397
    Abstract: An aircraft, capable of hovering, having drive means; and at least one exhaust duct connected to an outlet of the drive means to expel the exhaust gas, produced by fuel combustion, from the aircraft. At least part of the exhaust duct has a thermoelectric conversion circuit for Seebeck-effect converting to electric energy the thermal gradient produced between the inside and outside of the exhaust duct by flow of the exhaust gas.
    Type: Grant
    Filed: March 16, 2012
    Date of Patent: January 27, 2015
    Assignee: Agustawestland S.p.A.
    Inventors: Massimo Brunetti, Andrea Cogliati, Dario Iannucci, Alessandro Scandroglio
  • AIRCRAFT CAPABLE OF HOVERING
    Publication number: 20120233988
    Abstract: An aircraft, capable of hovering, having drive means; and at least one exhaust duct connected to an outlet of the drive means to expel the exhaust gas, produced by fuel combustion, from the aircraft. At least part of the exhaust duct has a thermoelectric conversion circuit for Seebeck-effect converting to electric energy the thermal gradient produced between the inside and outside of the exhaust duct by flow of the exhaust gas.
    Type: Application
    Filed: March 16, 2012
    Publication date: September 20, 2012
    Inventors: Massimo Brunetti, Andrea Cogliati, Dario Iannucci, Alessandro Scandroglio
  • AIRCRAFT CAPABLE OF HOVERING, AIRCRAFT MANEUVERING ASSIST METHOD, AND INTERFACE
    Publication number: 20120029738
    Abstract: An aircraft capable of hovering, and characterized by having at least one sensor, which has a plane sweep region and is designed to acquire, when the aircraft is manoeuvring, values of respective distances between first points on an obstacle within the plane sweep region, and a second point on the aircraft; and a control unit designed to generate an alarm signal when at least one of the first points lies within a safety region containing the second point on the aircraft.
    Type: Application
    Filed: May 20, 2011
    Publication date: February 2, 2012
    Inventors: Massimo Brunetti, Simone Gobbi, Dario Iannucci, Emilio Majori