Joseph J Hollkamp

age ~63

from Beavercreek, OH

Also known as:
  • Joseph Jay Hollkamp
  • Joe J Hollkamp
  • John P Hollkamp
  • Jos J Hollkamp
  • Joseph J Lkam
  • Kamp L Joseph

Joseph Hollkamp Phones & Addresses

  • Beavercreek, OH
  • 1240 Whitetail Dr, Fairborn, OH 45324 • 9374784355
  • Mishawaka, IN
  • Jeffersonville, IN
  • 1240 Whitetail Dr, Fairborn, OH 45324

Us Patents

  • Piezoelectric Strain Sensor Array

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  • US Patent:
    59111585, Jun 8, 1999
  • Filed:
    Feb 28, 1997
  • Appl. No.:
    8/808365
  • Inventors:
    Douglas A. Henderson - Dayton OH
    Robert W. Gordon - Vandalia OH
    Joseph W. Hollkamp - Fairborn OH
    Gregory S. Agnes - Christiansburg VA
  • Assignee:
    The United States of America as represented by the Secretary of the Air
    Force - Washington DC
  • International Classification:
    G01H 1108
    G01N 2912
  • US Classification:
    73583
  • Abstract:
    An apparatus and method for determining the dynamic response of a physical structure is disclosed. A single sheet of a piezoelectric polymer film, preferably polyvinylidene fluoride, or PVDF, is coated on one side with a thin layer of conductive material to serve as a ground electrode. The other side of the sheet is coated with a thin layer or conductive material in a non-contiguous pattern of individual electrodes defining an array of discrete piezoelectric transducers. Sensor leads are connected to each individual electrode and lead to a signal processor which includes associated software for determining from the processed electrical signals relative strain amplitudes of the surface area of a physical structure onto which the sheet is attached. The resulting output can be used to record strain time histories for later processing or, more simply, to show the time-averaged, steady state strain response of a structure.
  • Centrifugal Pendulum Absorber For Engine Blades

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  • US Patent:
    59248459, Jul 20, 1999
  • Filed:
    Apr 7, 1997
  • Appl. No.:
    8/840109
  • Inventors:
    Ronald L. Bagley - Boerne TX
    Joseph J. Hollkamp - Fairborn OH
    Robert W. Gordon - Vandalia OH
  • Assignee:
    The United States of America as represented by the Secretary of the Air
    Force - Washington DC
  • International Classification:
    F01D 516
    F01D 526
  • US Classification:
    416145
  • Abstract:
    A new apparatus and method for dynamically absorbing resonant vibration in jet engine blades and other rotating turbomachine components over all engine speeds is disclosed. A distributed pendulum (a pendulum having its axis of motion inside its body instead of at an end) is mounted inside a jet engine blade to function as a centrifugal pendulum. A centrifugal pendulum can be tuned so that its natural frequency linearly tracks the rotational speed of the engine or other turbomachine in which it is mounted and can absorb resonant vibrations from turbomachine components whenever the frequency of a source of vibratory excitation from a so-called speed line of the turbomachine coincides with a resonant frequency of the component. The equations of motion of a distributed pendulum are derived to show that a distributed pendulum small enough to fit inside a turbomachine component can be tuned to track a turbomachine speed line by adjusting its mass distribution about its axis of motion.

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