3290 Patterson Ave southeast, Grand Rapids, MI 49512
Industry:
Airlines/Aviation
Work:
Ge Aviation Feb 1990 - May 1998
Non-Destructive Testing Project Leader
Ge Aviation Feb 1990 - May 1998
Lead Supplier Quality Engineer
Wj Schafer Associates Dec 1988 - Feb 1990
Program Engineer
Lockheed Aeronautical Systems Company Oct 1987 - Dec 1988
Low- Observables Engineer
Education:
University of Dayton 1985 - 1987
Master of Science, Masters, Engineering
Xavier University 1980 - 1985
Bachelors, Bachelor of Science, Physics
Skills:
Aerospace Continuous Improvement Engineering Manufacturing Process Improvement Project Management Program Management Six Sigma Team Leadership Dmaic Spc
George P. Egan - Union KY Karl L. Borneman - Loveland OH Douglas A. Jaeger - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G01M 326
US Classification:
73 37
Abstract:
A method and apparatus for detecting defects in a structure formed of a honeycomb matrix bonded to a support surface including providing a probe body including means defining a fluid passage forming a supply port to an exterior surface of the probe body; connecting a pressurized fluid source to the fluid passage at a location distal from the supply port; placing the supply port in close proximity to a cell of the honeycomb matrix; supplying fluid from the compressed fluid source to the cell via the fluid passage; and monitoring a fluid pressure produced at a portion of the honeycomb matrix adjacent to the supply port to detect disbonds between the honeycomb matrix and support surface.
Apparatus And Method For Inspecting An Open-Face Cell Structure Bonded To A Substrate
Karl L. Borneman - Loveland OH Douglas A. Jaeger - Cincinnati OH George P. Egan - Union KY
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G01N 2500 G01K 114
US Classification:
374153
Abstract:
An apparatus and method for inspecting the bonding between a cell structure having a multiplicity of cells which are open at one end and bonded at an opposite end to a substrate are disclosed. The apparatus includes a heater and nozzle arrangement for directing a fluid, such as heated air, having a selected temperature, substantially different from ambient, into the open ends of the cell structure to cause a change in the temperature of the cell structure and radiance therefrom. A sensor is provided for sensing the temperature of the cell structure along the extent thereof or a detector may be provided for detecting the radiance along the cell structure. The temperature sensor or radiance detector generate electrical signals representative of either the temperature sensed or the radiance detected; these electrical signals are electronically converted to an image representative of either the temperatures sensed along the cell structure or the radiance detected from the cell structure to permit detection of any disbonded or plugged cells by differences between either the temperatures sensed or radiance detected along the cell structure. In another embodiment of the present invention, the output of the temperature sensor or radiance detector may be coupled to an alarm to provide a signal if the temperature or radiance varies outside of a predetermined range.
Method And Apparatus For Inspection Of Open Face Honeycomb Structures
George P. Egan - Union KY Karl L. Borneman - Loveland OH Douglas A. Jaeger - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
G01N 3300
US Classification:
73 37
Abstract:
A method and apparatus for detecting defects in a structure formed of a honeycomb matrix bonded to a support surface including providing a probe body including means defining a fluid passage forming a supply port to an exterior surface of the probe body; connecting a pressurized fluid source to the fluid passage at a location distal from the supply port; placing the supply port in close proximity to a cell of the honeycomb matrix; supplying fluid from the compressed fluid source to the cell via the fluid passage; and monitoring a fluid pressure produced at a portion of the honeycomb matrix adjacent to the supply port to detect disbonds between the honeycomb matrix and support surface.