Patents by Inventor Harald Neujahr

Harald Neujahr 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: 9989378
    Abstract: A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.
    Type: Grant
    Filed: January 15, 2014
    Date of Patent: June 5, 2018
    Assignee: Airbus Defence and Space GmbH
    Inventors: Christoph Vernaleken, Marco Opitz, Harald Neujahr, Eugenio Ferreira, Lutz Broszio
  • Publication number: 20150362332
    Abstract: A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.
    Type: Application
    Filed: January 15, 2014
    Publication date: December 17, 2015
    Inventors: Christoph VERNALEKEN, Marco OPITZ, Harald NEUJAHR, Eugenio FERREIRA
  • Publication number: 20120310910
    Abstract: A method of data fusion and providing information in a computer system regarding the performance of work tasks on a technical product is provided. Product information on the technical product from a product information database, image information from an image information database and work process information from a work process database are assembled in the computer system to form a data set of a fused process instruction. This data set is processed to form a combined display file that is sent to a display unit, whereupon the fused process instruction is displayed in an optically visible manner.
    Type: Application
    Filed: June 1, 2012
    Publication date: December 6, 2012
    Applicant: EADS Deutschland GmbH
    Inventors: Claudia Haubach-Lippmann, Thomas Burger, Harald Neujahr, Milton Amador