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Paul Ray Reismiller

from Hamilton, OH
Age ~71
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Also known as:
Paul R Reismiller
Phone and address:
7895 Jessies Way, Hamilton, OH 45011
(513) 895-2132
Related to:
Beverly J Taylor, 83Eric Taylor, 79Victoria Mapel, 73Sam HillerSam Bacon
Connected to:
Abraham I Reisner, 100Amanda Reisner, 44Anna Reisner, 30Beth C Reisner, 86Colleen B Reisner, 58Dan L Reisner, 62Dick Reisner, 71Ellen S Reisner, 83Eric J Reisner, 57Jedediah I Reisner, 39

Paul Reismiller Phones & Addresses

  • 7895 Jessies Way, Hamilton, OH 45011 (513) 895-2132
  • 7895 Jessies Way #302, Hamilton, OH 45011 (513) 895-2132
  • Fairfield, OH
  • Cincinnati, OH
  • Crescent Springs, KY
  • Middletown, OH
  • Butler, OH
  • 7895 Jessies Way APT 302, Hamilton, OH 45011

Work

Company: Ge aviation Feb 1981 Position: Engineer

Industries

Airlines/Aviation

Resumes

Resumes

Paul Reismiller Photo 1

Engineer

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Location:
Hamilton, OH
Industry:
Airlines/Aviation
Work:
Ge Aviation
Engineer

Publications

Us Patents

Apparatus For Selecting A Valid Signal From A Plurality Of Redundant Measured And Modelled Sensor Signals

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US Patent:
54694477, Nov 21, 1995
Filed:
Oct 28, 1994
Appl. No.:
8/331294
Inventors:
George A. Brunemann - Cincinnati OH
Paul R. Reismiller - West Chester OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G06F 1108
G06F 1540
US Classification:
371 36
Abstract:
The present invention provides a method and an apparatus for selecting a valid signal from a plurality of redundant sensor signals wherein the sensor signals may include a plurality of measured and modelled signals. The invention comprises a circuit for generating a plurality of first pass/fail signals by performing a series of tests on the sensor signals. The invention further comprises circuitry for assigning a plurality of weighted values to each of the measured sensor signals according to the first and second pass/fail signals wherein the second pass/fail signals are initialized as pass signals. The invention further comprises of circuitry for summing the weighted values for each measured sensor signal and generating second pass/fail signals for each measured sensor signal. The invention also includes circuitry for assigning selection flags to each sensor signal according to the first and second pass/fail signals and circuitry for selecting the valid signal from the selection flags.

Predictor Algorithm For Actuator Control

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US Patent:
54869978, Jan 23, 1996
Filed:
Aug 4, 1994
Appl. No.:
8/285836
Inventors:
Paul R. Reismiller - West Chester OH
George A. Brunemann - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G05B 1302
US Classification:
364165
Abstract:
A predictor algorithm for an actuator control is provided in a servo-actuator system. The predictor algorithm receives a signal representative of the torque motor current supplied to the servovalve controlling the actuator and uses that signal to predict the change in actuator position over a single time interval. If the measured actuator position for the previous time interval is within the maximum value and the minimum value for that time interval, then the next maximum and minimum values are calculated by adding the predicted change to the previous measured signal. If the measured actuator signal for the previous time interval is outside the maximum and minimum values for that time interval, then the next maximum and minimum values are calculated by adding the predicted change to the previous maximum and minimum values. A fault is indicated when the measured signal falls outside the maximum and minimum values for a predetermined number of time intervals. In a further embodiment of the present invention, the gain of the torque motor is tracked and used to adjust the maximum and minimum values for various operating conditions.

Redundant Actuator Control

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US Patent:
52068102, Apr 27, 1993
Filed:
Feb 7, 1991
Appl. No.:
7/652344
Inventors:
William G. Bools - Montgomery OH
Paul R. Reismiller - West Chester OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G05B 1902
US Classification:
36443102
Abstract:
A control system for operating an actuator in a mechanical system, such as an aircraft turbine engine, employs redundant electronic control channels for increased operational safety in the event of a failure of one of the control channels. In accordance with the reliability or integrity of the various components of the system, a network of triplex redundant electronic control units connects with duplex redundant input driver ports of a servo actuator, the network including a converter of triplex to duplex wherein the converter employs a duplex section of electronic circuits. The control units may include a schedule or memory addressed by a set of input parameters or variables for outputting a desired value of output parameter or variable. The converter includes a fan-in circuit by which signals of the three control units are applied to two power amplifiers for driving the two input sections of the servo actuator. Each input section of the actuator includes a torque motor for converting an electrical signal to a mechanical movement.
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Paul Ray Reismiller from Hamilton, OH, age ~71 Get Report