Patents by Inventor Conrad O. Gardner

Conrad O. Gardner 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: 6526337
    Abstract: A system and method for intervention control of an aircraft in the event of pilot command error whether voluntary or involuntary. Impending detection of a chaotic condition associated with a maneuvering aircraft enable early prediction and control of the aircraft where solutions based upon performance prediction are available. A further feature of the present intervention control of the aircraft enables an equipment malfunction detection signal substitution of a satisfactory equipment signal.
    Type: Grant
    Filed: March 29, 2000
    Date of Patent: February 25, 2003
    Inventor: Conrad O. Gardner
  • Patent number: 6480765
    Abstract: A system and method for intervention control of an aircraft in the event of pilot command error whether voluntary or involuntary. Impending detection of a chaotic condition associated with a maneuvering aircraft enable early prediction and control of the aircraft where solutions based upon performance prediction are available. A further feature of the present intervention control of the aircraft enables an equipment malfunction detection signal substitution of a satisfactory equipment signal.
    Type: Grant
    Filed: October 11, 2001
    Date of Patent: November 12, 2002
    Inventor: Conrad O. Gardner
  • Publication number: 20020035415
    Abstract: A system and method for intervention control of an aircraft in the event of pilot command error whether voluntary or involuntary. Impending detection of a chaotic condition associated with a maneuvering aircraft enable early prediction and control of the aircraft where solutions based upon performance prediction are available. A further feature of the present intervention control of the aircraft enables an equipment malfunction detection signal substitution of a satisfactory equipment signal.
    Type: Application
    Filed: March 29, 2000
    Publication date: March 21, 2002
    Inventor: Conrad O. Gardner
  • Publication number: 20020029099
    Abstract: A system and method for intervention control of an aircraft in the event of pilot command error whether voluntary or involuntary. Impending detection of a chaotic condition associated with a maneuvering aircraft enable early prediction and control of the aircraft where solutions based upon performance prediction are available. A further feature of the present intervention control of the aircraft enables an equipment malfunction detection signal substitution of a satisfactory equipment signal.
    Type: Application
    Filed: October 11, 2001
    Publication date: March 7, 2002
    Inventor: Conrad O. Gardner
  • Patent number: 5993782
    Abstract: Normal olfactory function restoration through topical application of an effective amount of fluticasone propionate to the olfactory epithelium. A patient should be started on 1 mg per day dosage and the dosage gradually inreased until the patient regains the sense of smell.
    Type: Grant
    Filed: April 28, 1998
    Date of Patent: November 30, 1999
    Inventor: Conrad O. Gardner
  • Patent number: 5346031
    Abstract: A hybrid motor vehicle utilizing electric motor propulsion prior to cruise mode detection condition and internal combustion engine propulsion during cruise mode.
    Type: Grant
    Filed: October 25, 1993
    Date of Patent: September 13, 1994
    Inventor: Conrad O. Gardner
  • Patent number: 5301764
    Abstract: A hybrid motor vehicle utilizing electric motor propulsion prior to cruise mode detection condition and internal combustion engine propulsion during cruise mode.
    Type: Grant
    Filed: April 13, 1992
    Date of Patent: April 12, 1994
    Inventor: Conrad O. Gardner
  • Patent number: 4315492
    Abstract: An EGR valve control signal developed by the EGR modulator circuit for controlling the EGR valve is combined in a feedback loop with a signal representative of an engine combustion condition, e.g. engine knock to modify ignition timing through advance or retard.
    Type: Grant
    Filed: June 12, 1980
    Date of Patent: February 16, 1982
    Inventor: Conrad O. Gardner