Patents by Inventor Claude Nicollier

Claude Nicollier 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: 9218743
    Abstract: Navigation aid instrument for an aircraft pilot including: a first display device (R3) extending horizontally, wherein the center of the display device embodies the longitudinal axis (X) of the aircraft, a mobile marker can move on either side of the center of the first display device (R3) indicating the aircraft flight direction relative to the ground, and the mobile marker is further away from the center of the display device (R3) the further the aircraft drifts from the rectilinear flight path, and/or two left (R2) and right (R1) display devices that extend vertically at a distance from each other and have the function of indicating the angle of inclination of the aircraft wings relative to the horizontal respectively on the left side or right side of the aircraft, wherein a mobile marker can move either along the left display device (R2), or along the right display device (R1) to indicate to the pilot which way his aeroplane is inclined and the value of the inclination is higher the further the mobile
    Type: Grant
    Filed: August 5, 2014
    Date of Patent: December 22, 2015
    Assignee: Omega SA
    Inventors: Claude Nicollier, Emmanuel Fleury, Reto Galli
  • Patent number: 9171474
    Abstract: Navigation aid instrument for an aircraft pilot including: a first display device (R3) extending horizontally, wherein the center of the display device embodies the longitudinal axis (X) of the aircraft, a mobile marker can move on either side of the center of the first display device (R3) indicating the aircraft flight direction relative to the ground, and the mobile marker is further away from the center of the display device (R3) the further the aircraft drifts from the rectilinear flight path, and/or two left (R2) and right (R1) display devices that extend vertically at a distance from each other and have the function of indicating the angle of inclination of the aircraft wings relative to the horizontal respectively on the left side or right side of the aircraft, wherein a mobile marker can move either along the left display device (R2), or along the right display device (R1) to indicate to the pilot which way his aeroplane is inclined and the value of the inclination is higher the further the mobile
    Type: Grant
    Filed: November 10, 2009
    Date of Patent: October 27, 2015
    Assignee: Omega SA
    Inventors: Claude Nicollier, Emmanuel Fleury, Reto Galli
  • Publication number: 20150035688
    Abstract: Navigation aid instrument for an aircraft pilot including: a first display device (R3) extending horizontally, wherein the centre of the display device embodies the longitudinal axis (X) of the aircraft, a mobile marker can move on either side of the centre of the first display device (R3) indicating the aircraft flight direction relative to the ground, and the mobile marker is further away from the centre of the display device (R3) the further the aircraft drifts from the rectilinear flight path, and/or two left (R2) and right (R1) display devices that extend vertically at a distance from each other and have the function of indicating the angle of inclination of the aircraft wings relative to the horizontal respectively on the left side or right side of the aircraft, wherein a mobile marker can move either along the left display device (R2), or along the right display device (R1) to indicate to the pilot which way his aeroplane is inclined and the value of the inclination is higher the further the mobile
    Type: Application
    Filed: August 5, 2014
    Publication date: February 5, 2015
    Inventors: Claude Nicollier, Emmanuel Fleury, Reto Galli
  • Publication number: 20110241900
    Abstract: Navigation aid instrument for an aircraft pilot including: a first display device (R3) extending horizontally, wherein the centre of the display device embodies the longitudinal axis (X) of the aircraft, a mobile marker can move on either side of the centre of the first display device (R3) indicating the aircraft flight direction relative to the ground, and the mobile marker is further away from the centre of the display device (R3) the further the aircraft drifts from the rectilinear flight path, and/or two left (R2) and right (R1) display devices that extend vertically at a distance from each other and have the function of indicating the angle of inclination of the aircraft wings relative to the horizontal respectively on the left side or right side of the aircraft, wherein a mobile marker can move either along the left display device (R2), or along the right display device (R1) to indicate to the pilot which way his aeroplane is inclined and the value of the inclination is higher the further the mobile
    Type: Application
    Filed: November 10, 2009
    Publication date: October 6, 2011
    Applicant: OMEGA SA
    Inventors: Claude Nicollier, Emmanuel Fleury, Reto Galli