Patents by Inventor Henri Peter-Contesse

Henri Peter-Contesse 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: 4569021
    Abstract: A Mach hold control circuit for an aircraft autothrottle system provides capture of a Mach number and control thereto while providing a low level of throttle activity also stabilizing the aircraft at maximum range cruise (MRC) Mach numbers and above. The Mach hold control law utilizes a Mach error signal, flight path acceleration signal, average engine EPR signal, and associated logic inputs and when interfaced with the autothrottle system provides a throttle rate command to the aircraft engines via. the throttle and engine control system thereby modulating engine thrust to provide control to desired flight Mach number.
    Type: Grant
    Filed: May 23, 1980
    Date of Patent: February 4, 1986
    Assignee: The Boeing Company
    Inventors: Warren R. Larson, Henri Peter-Contesse, Leonard P. Stephan
  • Patent number: 4189118
    Abstract: A system for processing signals representative of airspeed error and inertial longitudinal acceleration in first and second channels, respectively, and providing cancellation of the turbulence-induced components of the respective signals. Shear detection and compensation circuits are provided in the system for reducing speed wandering in moderate and heavy turbulence. A circuit processing the signal .DELTA.V from the shear detector circuit is utilized to provide a gust bias signal input in the system.
    Type: Grant
    Filed: November 22, 1977
    Date of Patent: February 19, 1980
    Assignee: The Boeing Company
    Inventor: Henri Peter-Contesse
  • Patent number: 4189119
    Abstract: A system for processing signals representative of airspeed and inertial longitudinal acceleration in first and second channels, respectively, and providing cancellation of the turbulence-induced components of the respective signals. Shear detection and compensation circuits are provided in the system for reducing speed wandering in moderate and heavy turbulence. A circuit processing the signal .DELTA.V from the shear detector circuit is utilized to provide a gust bias signal input in the system.
    Type: Grant
    Filed: November 22, 1977
    Date of Patent: February 19, 1980
    Assignee: The Boeing Company
    Inventors: Henri Peter-Contesse, Leonard P. Stephan
  • Patent number: 4155525
    Abstract: A maneuver detector generates a maneuver-detect signal when signals representative of elevator deflection and flight path deviation are representative of a deliberate maneuver condition and no maneuver-detect signal when the relationship of the two signals is indicative of elevator deflection such as to oppose a flight path deviation, e.g., as caused by turbulence condition or configuration change.
    Type: Grant
    Filed: October 25, 1977
    Date of Patent: May 22, 1979
    Assignee: The Boeing Company
    Inventor: Henri Peter-Contesse