Patents by Inventor Herman P. Briar

Herman P. Briar 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: 4817155
    Abstract: Speech analysis is performed by synchronizing, with the initiation of glottal pulses produced during the voicing of phonemes, a pitch-independent transform that performs analysis entirely within a pitch period. Analysis is made of the three most dominant formant frequencies of the sound sets involved in the enunciation of voiced phonemes. Peaks in the transform represent formant frequencies. Three peaks are selected from the transform identifying the frequencies with the first, second and third greatest amplitudes. Correlation of the waveform between successive pitch periods detects whether a sound is a vowel, a voiced sibilant, or unvoiced. Unvoiced sound sets are similarly analyzed but the analysis is synchronized with artificially generated synch pulses. The sound sets are analyzed to determine (1) whether the sound is a vowel, a voiced sibilant or an unvoiced sound; (2) the primary formant frequency, i.e.
    Type: Grant
    Filed: January 20, 1987
    Date of Patent: March 28, 1989
    Inventors: Herman P. Briar, Robert W. Cribbs
  • Patent number: 4074563
    Abstract: This is an in-situ telemetry apparatus for the measurement of dynamic moduli, a key design parameter, of the propellant mass of solid fuel rocket engines.
    Type: Grant
    Filed: October 12, 1976
    Date of Patent: February 21, 1978
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Herman P. Briar, Kenneth W. Bills, Jr.
  • Patent number: 3937070
    Abstract: The method and sensors are capable of measuring dynamic moduli of nongaseous fluid and semi-fluid materials. When cast in a castable-type material, such as solid rocket propellant, changes due to chemical aging of the propellant or other substances being tested may be detected. The sensors include a spacer separating a pair of piezoelectric crystals with substantially no air gaps between the crystals. One of the crystals is driven while the other is connected to a recording device. The measured response of the sensor in-situ or immersed in a work sample is compared with the response in air. The elastic modulus and loss tangent of the tested material may be computed based upon the amplitude and phase of the sensor's response.
    Type: Grant
    Filed: April 29, 1974
    Date of Patent: February 10, 1976
    Assignee: Aerojet-General Corporation
    Inventor: Herman P. Briar