Patents by Inventor Peter Hakenesch

Peter Hakenesch 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).

  • Method and apparatus for determining air flow and pressure data of an aircraft or aerodynamic vehicle
    Patent number: 6568260
    Abstract: A measuring system for determining an air data for an aircraft includes a measuring device for determining measured variables which are a function of the resulting flow vector and the inertia forces acting on a front fuselage section in relation to a rear fuselage section, an acceleration transducer, and an evaluation unit for determining the air data from the measured variables. A storage unit has stored calibration curves for determining an appropriate set of air data by selecting that calibration curve which is most similar to a curve formed from the measured variables.
    Type: Grant
    Filed: January 18, 2001
    Date of Patent: May 27, 2003
    Assignee: EADS Deutschland GmbH
    Inventor: Peter Hakenesch
  • Method and apparatus for determining air flow and pressure data of an aircraft or aerodynamic vehicle
    Publication number: 20010054311
    Abstract: A measuring system for determining an air data for an aircraft includes a measuring device for determining measured variables which are a function of the resulting flow vector and the inertia forces acting on a front fuselage section in relation to a rear fuselage section, an acceleration transducer, and an evaluation unit for determining the air data from the measured variables.
    Type: Application
    Filed: January 18, 2001
    Publication date: December 27, 2001
    Inventor: Peter Hakenesch
  • Fuselage nose for controlling aerodynamic vehicles and method of utilizing same
    Patent number: 6283407
    Abstract: A control system for aerodynamic vehicles has a fuselage nose segment and at least one strake. The fuselage nose segment is rotationally adjustable with respect to the aircraft fuselage. The at least one strake is mounted on the fuselage nose segment so that the strake can swing out.
    Type: Grant
    Filed: August 20, 1999
    Date of Patent: September 4, 2001
    Assignee: DaimlerChrysler AG
    Inventor: Peter Hakenesch