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Clark L Applegate

age ~75

from West Chester, OH

Also known as:
  • Clark Leonard Applegate
  • Clark Phyllis Applegate
  • Clark Janis Applegate
  • Len Applegate
  • Clare L Applegate
  • Clare M Applegate
  • Elizabeth Applegate
  • Applegate L Clark

Clark Applegate Phones & Addresses

  • West Chester, OH
  • Cincinnati, OH
  • Ft Mitchell, KY
  • Binghamton, NY
  • Butler, OH
Name / Title
Company / Classification
Phones & Addresses
Clark Applegate
Incorporator
APPLEGATE MACHINE COMPANY, (INC.)

Us Patents

  • Instability Mitigation System

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  • US Patent:
    8282336, Oct 9, 2012
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966416
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • Assignee:
    General Electric Company - Schenectady NY
  • International Classification:
    F01D 17/20
  • US Classification:
    415 1, 415914
  • Abstract:
    An instability mitigation system is disclosed, comprising a detection system for detecting an onset of an instability in a rotor during the operation of the rotor, a mitigation system that facilitates the improvement of the stability of the rotor when the onset of instability is detected by the detection system, a control system for controlling the detection system and the mitigation system.
  • Instability Mitigation System Using Stator Plasma Actuators

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  • US Patent:
    8282337, Oct 9, 2012
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966532
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • Assignee:
    General Electric Company - Schenectady NY
  • International Classification:
    F01D 17/20
  • US Classification:
    415 1, 415914
  • Abstract:
    An instability mitigation system is disclosed, comprising a stator stage located axially proximate to a rotor, the stator stage having a row of a plurality of stator vanes arranged around a centerline axis, and a mitigation system comprising at least one plasma actuator mounted on the stator vane that facilitates the improvement of the stability of the rotor, and a control system for controlling the operation of the mitigation system. An instability mitigation system further comprising a detection system for detecting an onset of an instability in a rotor and a control system for controlling the detection system and the mitigation system are disclosed.
  • Instability Mitigation System Using Rotor Plasma Actuators

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  • US Patent:
    8348592, Jan 8, 2013
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966473
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • Assignee:
    General Electric Company - Schenectady NY
  • International Classification:
    F01D 17/20
  • US Classification:
    415 1, 415914
  • Abstract:
    An instability mitigation system is disclosed, comprising a rotor having a row of blades arranged around a centerline axis, and a mitigation system comprising at least one plasma actuator mounted on a blade that facilitates the improvement of the stability of the rotor, and a control system for controlling the operation of the mitigation system. An instability mitigation system further comprising a detection system for detecting an onset of an instability in a rotor and a control system for controlling the detection system and the mitigation system are disclosed.
  • Plasma Enhanced Compression System

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  • US Patent:
    20090169356, Jul 2, 2009
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966384
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • International Classification:
    F02C 9/00
    F04D 27/00
    F01D 5/02
  • US Classification:
    415 26, 415118, 415129
  • Abstract:
    A compression system is disclosed, the compression system comprising a rotor having a circumferential row of blades each blade having a blade tip, a static component located radially outwardly and apart from the blade tips, a detection system for detecting an instability in the rotor during the operation of the rotor, and a mitigation system that facilitates the improvement of the stability of the rotor when an instability is detected by the detection system. A gas turbine engine comprising a detection system for detecting an instability during the operation of the fan section and a mitigation system that facilitates the improvement of the stability of the fan section is disclosed.
  • Plasma Enhanced Stator

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  • US Patent:
    20090169363, Jul 2, 2009
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966503
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • International Classification:
    F01B 25/16
    F02C 7/00
    F02C 9/16
  • US Classification:
    415118, 415176
  • Abstract:
    A compression system is disclosed, the compression system comprising a stator stage having a row of a plurality of stator vanes arranged around a centerline axis, each stator vane having a vane airfoil and at least one plasma actuator located on the stator stage. Exemplary embodiments of a detection system for detecting an instability in a compression system rotor and a mitigation system that facilitates the improvement of the stability of the rotor are disclosed.
  • Plasma Enhanced Rotor

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  • US Patent:
    20100047055, Feb 25, 2010
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966445
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • International Classification:
    F02C 9/16
    F01D 17/00
    F01D 7/00
  • US Classification:
    415 13, 415148, 415129
  • Abstract:
    A compression system is disclosed, the compression system comprising a rotor having a plurality of blades arranged around a centerline axis, each blade having a blade airfoil and a blade tip, and at least one plasma actuator located on a blade. Exemplary embodiments of a detection system for detecting an instability in a compression system rotor and a mitigation system comprising at least one plasma actuator mounted on a blade to facilitate the improvement of the stability of the rotor are disclosed.
  • Fan Stall Detection System

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  • US Patent:
    20100284785, Nov 11, 2010
  • Filed:
    Dec 28, 2007
  • Appl. No.:
    11/966242
  • Inventors:
    Aspi Rustom Wadia - Loveland OH, US
    Seyed Gholamali Saddoughi - Clifton Park NY, US
    Clark Leonard Applegate - West Chester OH, US
  • International Classification:
    F04D 29/00
  • US Classification:
    415118
  • Abstract:
    A system for detecting onset of a stall in a rotor is disclosed, the system comprising a sensor located on a static component spaced radially outwardly and apart from tips of a row of blades arranged circumferentially on the rotor wherein the sensor is capable of generating an input signal corresponding to a flow parameter at a location near the tip of a blade, a control system capable of generating a rotor speed signal, and a correlation processor capable of receiving the input signal and the rotor speed signal wherein the correlation processor generates a stability correlation signal.
  • Electronic Compensator For An Electrohydraulic Servovalve

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  • US Patent:
    44517696, May 29, 1984
  • Filed:
    Dec 7, 1981
  • Appl. No.:
    6/328058
  • Inventors:
    George E. Minnich - Vestal NY
    Clark L. Applegate - Binghamton NY
  • Assignee:
    The Singer Company - Binghamton NY
  • International Classification:
    G05D 1700
  • US Classification:
    318689
  • Abstract:
    Electronic compensation apparatus for modifying an input control signal, to produce a drive signal for a torque motor of an electrohydraulic servovalve. The torque motor has a frequency variable response characteristic. The apparatus includes means to determine a first voltage magnitude across the armature of the torque motor when it is not moving; means to determine a second voltage magnitude across the armature of the torque motor when it is moving; and means to determine a difference voltage of the first and second voltages. The difference voltage measures the dynamic motion of the armature and provides a feedback control signal. The apparatus further includes compensation means responsive to the feedback control signal for compensating the electrohydraulic servovalve so as to avoid resonance, and feedback means connected to the compensation means for providing a modified control signal.

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