Patents by Inventor Manfred Moseneder

Manfred Moseneder 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).

  • Turbocharger control system and propeller control system by a motor
    Publication number: 20050254948
    Abstract: An aircraft control system includes a propeller governor in which a motor is used to apply a compression force on a speeder spring, and a turbocharger in which a motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the motor in the propeller governor and the motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
    Type: Application
    Filed: June 29, 2005
    Publication date: November 17, 2005
    Applicant: Bombardier-Rotax GmbH & Co. KG
    Inventors: Thomas Koch, Heinz Lippitsch, Johann Bayerl, Manfred Moseneder, Gerald Mayr
  • Turbocharger control system and propeller control system by stepper motor
    Patent number: 6938418
    Abstract: An aircraft control system includes a propeller governor in which a stepper motor is used to apply a compression force on a speeder spring, and a turbocharger in which a stepper motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the stepper motor in the propeller governor and the stepper motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
    Type: Grant
    Filed: August 8, 2003
    Date of Patent: September 6, 2005
    Assignee: BRP-Rotax GmbH & Co. KG
    Inventors: Thomas Koch, Heinz Lippitsch, Johann Bayerl, Manfred Moseneder, Gerald Mayr
  • Turbocharger control system and propeller control system by stepper motor
    Publication number: 20040025505
    Abstract: An aircraft control system includes a propeller governor in which a stepper motor is used to apply a compression force on a speeder spring, and a turbocharger in which a stepper motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the stepper motor in the propeller governor and the stepper motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
    Type: Application
    Filed: August 8, 2003
    Publication date: February 12, 2004
    Applicant: Bombardier-Rotax GmbH & Co. KG
    Inventors: Thomas Koch, Heinz Lippitsch, Johann Bayerl, Manfred Moseneder, Gerald Mayr
  • Turbocharger control system and propeller control system by stepper motor
    Patent number: 6637202
    Abstract: An aircraft control system includes a propeller governor in which a stepper motor is used to apply a compression force on a speeder spring, and a turbocharger in which a stepper motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the stepper motor in the propeller governor and the stepper motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
    Type: Grant
    Filed: March 16, 2002
    Date of Patent: October 28, 2003
    Assignee: Bombardier-Rotax GmbH & Co. KG
    Inventors: Thomas Koch, Heinz Lippitsch, Johann Bayerl, Manfred Moseneder, Gerald Mayr
  • Turbocharger control system and propeller control system by stepper motor
    Publication number: 20020088225
    Abstract: An aircraft control system includes a propeller governor in which a stepper motor is used to apply a compression force on a speeder spring, and a turbocharger in which a stepper motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the stepper motor in the propeller governor and the stepper motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
    Type: Application
    Filed: March 16, 2002
    Publication date: July 11, 2002
    Inventors: Thomas Koch, Heinz Lippitsch, Johann Bayerl, Manfred Moseneder, Gerald Mayr