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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Original<br />
Revised<br />
Description<br />
Status<br />
Date<br />
Date<br />
Sample fabrication<br />
12-30<br />
months<br />
Acquire/fabricate the necessary samples. (GE with<br />
support from PW, AS)<br />
Complete<br />
Fundamental property measurements<br />
12 - 36<br />
months<br />
Acquire velocity, attenuation, backscattered noise,<br />
and defect-echo data necessary to assess the<br />
effects of microstructural anisotropy and surface,<br />
curvature, etc., on <strong>for</strong>ging inspections. (ISU with<br />
support from GE, PW, AS)<br />
18 months 24 months Provide velocity data <strong>for</strong> incorporation into the<br />
noise model. (ISU with support from GE, PW, AS)<br />
Complete techniques <strong>for</strong> curvature correction<br />
approaches. (All)<br />
24 months Provide surface curvature data <strong>for</strong> development of<br />
curvature correction factors. Provide data to 1.3.2<br />
<strong>for</strong> transducer design optimization. (ISU with<br />
support from GE, PW, AS)<br />
24 - 39<br />
months<br />
Validate noise models in cooperation with 3.1.2.<br />
(All)<br />
45 months Report of the effects of anisotropy and surface<br />
curvature on inspection sensitivity <strong>for</strong> typical<br />
titanium <strong>for</strong>gings used in aircraft engines.<br />
45 months Initiate final report. (All)<br />
45 months Techniques used to correct <strong>for</strong> geometry effects<br />
including curvature correction factors.<br />
54 months Complete final report. (All)<br />
60 months Representative sample blocks of <strong>for</strong>ging material or<br />
fundamental property measurements.<br />
Primary measurements required to<br />
assess effects of microstructural<br />
anisotropy completed using<br />
property/flow line blocks). For<br />
surface curvature effects see below<br />
Complete<br />
Complete<br />
Work initiated using “Noise<br />
Curvature Blocks” to assess<br />
combined effects of surface<br />
curvature and microstructure on<br />
inspections, and to validate noise<br />
models.<br />
Deliverables:<br />
Techniques to correct <strong>for</strong> geometry effects including curvature correction factors.<br />
Report of effect of anisotropy and surface curvature on inspection sensitivity <strong>for</strong> typical titanium<br />
<strong>for</strong>gings used in aircraft engines.<br />
Representative sample blocks of <strong>for</strong>ging material or fundamental property measurements.<br />
Quarterly Report – January 1, 2002 –March 31, 2002<br />
print date/time: 6/6/2002 - 8:39 AM – Page 52