Eric John Jumper
Engineers at Brittany Ct, Granger, IN
License number
Colorado 15757
Issued Date
Aug 17, 1978
Renew Date
Nov 1, 2015
Expiration Date
Oct 31, 2017
Type
Professional Engineer
Address
Address
51726 Brittany Ct, Granger, IN 46530
Personal information
See more information about Eric John Jumper at radaris.comName
Address
Phone
51726 Brittany Ct, Granger, IN 46530
51726 Brittany Ct, Granger, IN 46530
Professional information
See more information about Eric John Jumper at trustoria.com
Pattern Recognition By Simulated Neural-Like Networks
Pattern Recognition By Simulated Neural-Like Networks
US Patent:
5666518, Sep 9, 1997
Filed:
Jun 26, 1995
Appl. No.:
8/494866
Inventors:
Eric J. Jumper - Granger IN
Assignee:
The United States of America as represented by the Secretary of the Air
Force - Washington DC
Force - Washington DC
International Classification:
G06F 1518
US Classification:
395500
Abstract:
Apparatus and method for replacing the traditional amplifications by rime delays in a neural network that can be trained to analyze temporally-related patterns. Time delays comprise the synapses between feeder and stimulus cells in the network. The result is a multi-temporal trainable delay neural network.
Single Dielectric Barrier Aerodynamic Plasma Actuation
Single Dielectric Barrier Aerodynamic Plasma Actuation
US Patent:
7380756, Jun 3, 2008
Filed:
Nov 16, 2004
Appl. No.:
10/994029
Inventors:
Carl L. Enloe - Colorado Springs CO, US
Thomas E. McLaughlin - Colorado Springs CO, US
Eric J. Jumper - Granger IN, US
Thomas C. Corke - Granger IN, US
Thomas E. McLaughlin - Colorado Springs CO, US
Eric J. Jumper - Granger IN, US
Thomas C. Corke - Granger IN, US
Assignee:
The United States of America as represented by the Secretary of the Air Force - Washington DC
International Classification:
B64C 13/02
US Classification:
244175, 244205, 244198, 244130
Abstract:
A single dielectric barrier aerodynamic plasma actuator apparatus based on the dielectric barrier discharge phenomenon is disclosed and suggested for application to aerodynamic uses for drag reduction, stall elimination and airfoil efficiency improvement. In the plasma actuator apparatus non-uniform in time and space, partially ionized gasses are generated by one or more electrode pairs each having one electrically encapsulated electrode and one air stream exposed electrode and energization by a high-voltage alternating current waveform. The influence of electrical waveform variation, electrode polarity, electrode size and electrode shape on the achieved plasma are considered along with theoretical verification of achieved results. Light output, generated thrust, ionizing current waveform and magnitude and other variables are considered. Misconceptions prevailing in the present day plasma generation art are addressed and are believed-to-be corrected.
Methods And Systems For Measuring An Aberated Wave Front
Methods And Systems For Measuring An Aberated Wave Front
US Patent:
7295292, Nov 13, 2007
Filed:
May 19, 2005
Appl. No.:
11/132312
Inventors:
Eric Jumper - Granger IN, US
Stanislav Gordeyev - Mishawaka IN, US
Alan Cain - St. Louis MO, US
Terry Ng - Sylvania OH, US
Stanislav Gordeyev - Mishawaka IN, US
Alan Cain - St. Louis MO, US
Terry Ng - Sylvania OH, US
Assignee:
The University of Notre Dame - Notre Dame IN
International Classification:
G01B 9/00, G01N 21/00, G01J 1/00
US Classification:
356124, 356121, 356614, 356 73, 356 27, 73 116, 2502019, 250201, 250202
Abstract:
Methods and systems are described for a system for measuring aberrations in a wave front. In the improved system multiple closely-spaced, small-aperture laser beams traverse an aberrating flow that introduces deflections of small-aperture laser beams from which aberrated wavefronts can be constructed. These beams may then be focused on position sensing devices using focusing lenses. The position sensing devices may then detect the positions of these beams and a difference between the detected position and the unaberrated position of the beams detected. This information may then be used to determine information regarding the optical aberrations introduced by the flow that may be used, for example, in improving communications systems and/or laser weapon systems.
Methods And Apparatus For Optical Propagation Improvement System
Methods And Apparatus For Optical Propagation Improvement System
US Patent:
8096507, Jan 17, 2012
Filed:
Jan 23, 2009
Appl. No.:
12/359064
Inventors:
Alan B. Cain - Chesterfield MO, US
Eric J. Jumper - Granger IN, US
Edward J. Kerschen - Tucson AZ, US
David Cavalieri - Granger IN, US
T. Terry Ng - Sylvania OH, US
Eric J. Jumper - Granger IN, US
Edward J. Kerschen - Tucson AZ, US
David Cavalieri - Granger IN, US
T. Terry Ng - Sylvania OH, US
Assignee:
Innovative Technology Applications - Chesterfield MO
University of Notre Dame Du Lac - Notre Dame IN
University of Notre Dame Du Lac - Notre Dame IN
International Classification:
B64C 1/38, B64D 7/00
US Classification:
244130, 2441294, 244 1 N, 89 3716, 343705
Abstract:
An aircraft turret and fairing assembly for facilitating transmission of a directed energy beam from a directed energy device includes a turret section for directing an energy beam. The assembly also includes a fairing section aft of and adjacent to the turret section. Each of the turret section and the aft fairing section are coupled to an aircraft. The assembly also includes at least one sensor for detecting air speed of the aircraft and air pressure. The turret section and the aft fairing section are configured and positioned relative to one another to direct airflow for generating an aeroacoustic resonance within a desired frequency range in an area aft of the turret section.