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Rudolf C Dankwort

age ~83

from Phoenix, AZ

Also known as:
  • Rudolf Carl Dankwort
  • Rudolf Living Dankwort

Rudolf Dankwort Phones & Addresses

  • Phoenix, AZ
  • Minneapolis, MN
  • Maricopa, AZ

Us Patents

  • Vibration Rectification Error Reducer For Fiber Optic Gyroscope

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  • US Patent:
    59460970, Aug 31, 1999
  • Filed:
    Dec 31, 1997
  • Appl. No.:
    9/001967
  • Inventors:
    Glen A. Sanders - Scottsdale AZ
    Rudolf C. Dankwort - Phoenix AZ
    Ralph A. Bergh - Phoenix AZ
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01C 1972
  • US Classification:
    356350
  • Abstract:
    An apparatus for eliminating or reducing vibration-induced errors due to vibration rectification by applying a variable weighting function at the demodulator or analog-to-digital converter by changing the size of the demodulator reference signal or the converter gain, respectively. The changing is performed within the frequency spectrum of the vibration. Sampling of the detector output may be utilized and the samples are accumulated and processed to remove the variations due to vibration, and the rotation rate is recovered by digital demodulation.
  • Fiber Optic Gyroscope Balanced Plural Serrodyne Modulators Phase Difference Control

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  • US Patent:
    50188593, May 28, 1991
  • Filed:
    Jan 26, 1989
  • Appl. No.:
    7/302484
  • Inventors:
    Chin L. Chang - Phoenix AZ
    Rudolf C. Dankwort - Phoenix AZ
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01B 902
  • US Classification:
    356350
  • Abstract:
    A phase difference controller for a rotation sensor based on a coiled optical fiber operating a dual output generator in a feedback loop to provide a pair of signals to operate a pair of frequency translating devices in the optical path with the coil. A pair of sawtooth-like signals of appropriate frequency and polarity operate the frequency translating device to provide a phase difference shift in the optical path.
  • Fiber Optic Gyroscope Bias Modulation Amplitude Determination

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  • US Patent:
    51969041, Mar 23, 1993
  • Filed:
    Dec 31, 1990
  • Appl. No.:
    7/636305
  • Inventors:
    Preston Dane - Phoenix AZ
    Rudolf C. Dankwort - Phoenix AZ
    Tamim F. El-Wailly - Peoria AZ
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01C 1972
  • US Classification:
    356350
  • Abstract:
    A bias modulation amplitude monitoring system for a rotation sensor having a pair of output signal component detectors to provide magnitudes of the corresponding frequency components in that signal which are used by a component relationship determination arrangement capable of adjusting the output signal to have a selected value in a range of values for a selected rate of rotation thereof, and to correct variations therein.
  • Vibrating Quartz Diaphragm Pressure Sensor

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  • US Patent:
    44790708, Oct 23, 1984
  • Filed:
    Jun 10, 1983
  • Appl. No.:
    6/503004
  • Inventors:
    Richard H. Frische - Phoenix AZ
    Rudolf C. Dankwort - Phoenix AZ
    Charles D. Klem - Phoenix AZ
  • Assignee:
    Sperry Corporation - New York NY
  • International Classification:
    H01L 4108
  • US Classification:
    310338
  • Abstract:
    A quartz crystal vibrating diaphragm pressure sensor includes a primary quartz crystal body having a diaphragm formed therein and electrodes on each side of the diaphragm for piezoelectrically exciting thickness shear mode oscillations of said diaphragm, said oscillations varying in frequency in accordance with variations in fluid pressures applied to the surfaces of said diaphragm. A second identical or substantially identical diaphragm similarly excited but exposed to a constant pressure provides a reference frequency for providing precision difference frequency pressure measurement and for inherently compensating for ambient conditions affecting both diaphragms.
  • Rapid Turn-On Source For Fiber Optic Gyroscope

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  • US Patent:
    54105153, Apr 25, 1995
  • Filed:
    Apr 29, 1993
  • Appl. No.:
    8/055133
  • Inventors:
    Michael S. Bielas - Phoenix AZ
    Rudolf C. Dankwort - Phoenix AZ
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01C 1964
  • US Classification:
    356350
  • Abstract:
    A light source with wavelength compensation for a fiber optic rotation sensor includes a light source to provide light for input to the fiber optic rotation sensor. A source control circuit generates a source control signal representative of the temperature of the light source. A driver generates a drive signal as a function of the source control signal to drive the light source. One of a plurality of scale factors for the fiber optic rotation sensor is generated also as a function of the source control signal over a predetermined temperature range. The source control circuit includes a temperature sensor which provides a current signal representative of the temperature of the light source and a buffer network for sinking the current signal and for generating a source control voltage as the source control signal. A method for wavelength compensation of a light source for a fiber optic rotation sensor includes sensing a temperature of the light source and generating a source control signal representative of the temperature. A drive signal is applied to the light source as a function of the source control signal and a scale factor for the fiber optic rotation sensor is generated as a function of the compensation signal.
  • Analog-To-Digital Converter

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  • US Patent:
    50972642, Mar 17, 1992
  • Filed:
    Jun 18, 1990
  • Appl. No.:
    7/539767
  • Inventors:
    Mats A. Brenner - Bloomington MN
    Rudolf C. Dankwort - Phoenix AZ
    Tamim F. El-Wailly - Peoria AZ
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    H03M 152
    H03M 118
  • US Classification:
    341167
  • Abstract:
    An integrating analog-to-digital converter system in which alternating and different combinations of signals are integrated, and which are selected for such integration both periodically and through an integrating result reaching a reference value in the periods. A digit count is provided as a system output indicating the time duration of integration of a selected signal combination in each period.
  • Fiber Optic Gyroscope Vibration Error Compensator

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  • US Patent:
    59234245, Jul 13, 1999
  • Filed:
    Jun 19, 1997
  • Appl. No.:
    8/879902
  • Inventors:
    Glen A. Sanders - Scottsdale AZ
    Rudolf C. Dankwort - Phoenix AZ
    Andrew W. Kaliszek - Phoenix AZ
    Clarence E. Laskoskie - Scottsdale AZ
    Lee K. Strandjord - Tonka Bay MN
    Daniel L. Sugarbaker - Ada MI
    Jerry L. Page - Alto MI
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01C 1972
  • US Classification:
    356350
  • Abstract:
    A rectification error reducer for a fiber optic gyroscope, which is an intensity servo or compensator for reducing vibration effects in the optical signals caused by modulation at vibration frequencies induced by the gyroscope operating environment. The vibration effects may be detected in signals from the photodiode output in amplitude form which is used in a control system to null out optical intensity variations at the frequencies of vibration.
  • Vibration Error Reduction Servo For A Fiber Optic Gyroscope

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  • US Patent:
    59262753, Jul 20, 1999
  • Filed:
    Jun 19, 1997
  • Appl. No.:
    8/879901
  • Inventors:
    Glen A. Sanders - Scottsdale AZ
    Rudolf C. Dankwort - Phoenix AZ
    Andrew W. Kaliszek - Phoenix AZ
    Clarence E. Laskoskie - Scottsdale AZ
    Lee K. Strandjord - Tonka Bay MN
    Daniel L. Sugarbaker - Ada MN
    Jerry L. Page - Alto MN
  • Assignee:
    Honeywell Inc. - Minneapolis MN
  • International Classification:
    G01C 1972
  • US Classification:
    356350
  • Abstract:
    A rectification error reducer for a fiber optic gyroscope, which is an intensity servo or compensator for reducing vibration effects in the optical signals caused by modulation at vibration frequencies induced by the gyroscope operating environment. The vibration effects may be detected in signals from the photodiode output in amplitude form which is used in a control system to null out optical intensity variations at the frequencies of vibration.

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