Engine Titanium Consortium - Center for Nondestructive Evaluation ...
Engine Titanium Consortium - Center for Nondestructive Evaluation ...
Engine Titanium Consortium - Center for Nondestructive Evaluation ...
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Task 2:<br />
Task 2.2<br />
Subtask 2.2.2:<br />
Inservice Inspection<br />
Inspection Development<br />
Transitions to Airline<br />
Maintenance<br />
High Speed Bolthole Eddy<br />
Current Scanning<br />
Team Members:<br />
HW: Tim Duffy, Jim Ohm, Waled Hassan<br />
ISU: Lisa Brasche<br />
GE: Tony Mellors, Shridhar Nath, Jon<br />
Bartos<br />
PW: Kevin Smith, Dave Bryson, Rob<br />
Stephan<br />
Students: None<br />
Program initiation date: June 15, 1999<br />
Objectives:<br />
To develop common fixtures to reduce inspection variables and arrive at a standardized inspection<br />
technique.<br />
To measure the process capability.<br />
To utilize this in<strong>for</strong>mation to develop an industry best practice document.<br />
Approach:<br />
<strong>Evaluation</strong> of Existing Processes: Ef<strong>for</strong>ts will concentrate on process improvements <strong>for</strong> and<br />
standardization of high speed bolt hole scanning. A detailed evaluation of existing OEM inspection<br />
processes and needs will be conducted. Current equipment and tooling will be analyzed to provide<br />
a baseline of existing inspection processes and their limitations. The data will be analyzed <strong>for</strong><br />
potential process improvements and identification of common tooling approaches. A survey of<br />
available commercial tooling will be included as part of the assessment and included in the baseline<br />
as possible.<br />
Development of Common Tooling: The ef<strong>for</strong>ts will then be focused on the detailed design and<br />
fabrication of common tooling with an emphasis placed on variability reduction and defect<br />
detectability improvements. An inspection demonstration will be conducted on a sample set of<br />
hardware from each of the industrial members <strong>for</strong> validation of process development. A<br />
comparison to the baseline data will be made. Working with task 3.1.3 an evaluation of the process<br />
POD will be conducted on existing bolt hole reliability specimens.<br />
Development of Common Process: A common inspection technique and best practices document<br />
will be developed. Currently AS4787, Eddy Current Inspection of Circular Holes in Nonferrous<br />
Metallic Aircraft <strong>Engine</strong> Hardware, serves as a standard <strong>for</strong> hole inspection. This document will be<br />
revised to reflect the results of the ETC ef<strong>for</strong>t. Recommendations <strong>for</strong> equipment improvements will<br />
be supplied to vendors and implications <strong>for</strong> further study will be provided to the FAA.<br />
Quarterly Report – January 1, 2002 –March 31, 2002<br />
print date/time: 6/6/2002 - 8:39 AM – Page 71