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Engine Titanium Consortium - Center for Nondestructive Evaluation ...

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5 MHz C-scan Image Comparisons: B1AW2-B<br />

Side 2<br />

Model Experiment Model<br />

Side 4<br />

Experiment<br />

31(H) x 31(V) @10 mils, 2dB<br />

peak amplitude @2dB=573 mv<br />

deviation=155% or 8.1 dB<br />

60(H) x 30(V) @10 mils, 2dB<br />

peak amplitude @2dB=225 mv<br />

51(H) x 31(V) @10 mils, 0dB<br />

peak amplitude @0dB=901 mv<br />

deviation=474% or 15.2 dB<br />

60(H) x 30(V) @10 mils, 0dB<br />

peak amplitude @0dB=157 mv<br />

Model<br />

Side 5<br />

Experiment<br />

Model<br />

Side 6<br />

Experiment<br />

31(H) x 31(V) @10 mils, 2dB<br />

peak amplitude @2dB=111 mv<br />

deviation=-49% or -5.8 dB<br />

60(H) x 30(V) @10 mils, 2dB<br />

peak amplitude @2dB=217 mv<br />

31(H) x 31(V) @10 mils, 0dB<br />

peak amplitude @0dB=192 mv<br />

deviation=-51% or -6.1 dB<br />

60(H) x 30(V) @10 mils, 0dB<br />

peak amplitude @0dB=384 mv<br />

Multizone Color Code<br />

0 128 255<br />

Experiment 255 = 500mv <strong>for</strong> sides 2, 5 and 6<br />

= 250mv <strong>for</strong> side 4<br />

Plans (April 1, 2002 – June 30, 2002):<br />

Figure 5. 5 MHz C-scan Image Comparisons: B1AW2-B<br />

Primary plans <strong>for</strong> this period are to complete the analysis of the CBS data. Assuming approval of<br />

the restart technical plan by the FAA, technical work will resume as directed by the agency.<br />

Milestones:<br />

Revised dates of TBD are shown <strong>for</strong> most of the tasks, given that work has been stopped while the<br />

problems with the random defect block are being addressed. Revised dates to be provided in next<br />

report.<br />

Original<br />

Revised<br />

Description<br />

Status<br />

Date<br />

Date<br />

Approach to tune flaw response model to the<br />

behavior of naturally occurring flaws<br />

4 months TBD Provide a written description of the recommended<br />

method (GE, ISU)<br />

6 months TBD A report defining a method <strong>for</strong> relating properties of<br />

naturally-occurring flaws to the parameters of the<br />

ISU model.<br />

12 month deliverable of 3.1.2 is<br />

serving as a common basis <strong>for</strong> 3.1.1,<br />

3.1.2. General procedure <strong>for</strong> tuning<br />

flaw response model is included in<br />

the 3.1.2 white-paper.<br />

Completion of full report delayed by<br />

redirection of work.<br />

Improvements and assessment of POD/PFA<br />

Quarterly Report – January 1, 2002 –March 31, 2002<br />

print date/time: 6/6/2002 - 8:39 AM – Page 93

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