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Engine Titanium Consortium - Center for Nondestructive Evaluation ...

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include air drying, oven drying, and flash drying. Initial studies will utilize lcf blocks with final<br />

recommendations to be based on actual engine hardware. A matrix that defines the effect of drying<br />

parameters on detectability will be generated.<br />

Development of Best Practices Document: The final stage of the work will be generation of a best<br />

practices document that provides guidance to the OEMs and airlines and will allow <strong>for</strong> any<br />

necessary specification changes. An assessment will be made of the need <strong>for</strong> further work such as<br />

a <strong>for</strong>mal POD study and recommendations provided.<br />

Objective/Approach Amendments: Objective and approach were discussed and details were<br />

added to the approach in the February 2000 kick-off meeting.<br />

Progress (January 1, 2002 – March 31, 2002):<br />

The third and final testing session <strong>for</strong> this study was held at Delta February 4-7. Honeywell<br />

completed the “baked on” contamination process which lead to oxidation/scale, soot, and<br />

coke/varnish as specified by the team. All planned cleaning methods of the baked on<br />

contamination was completed at the Delta Airlines engine shop and at Northwest Airlines (wet-glass<br />

beading) both in Atlanta.<br />

Additionally, follow-up studies identified from results of the first cleaning run which occurred in<br />

October at Delta were made. These include additional samples with penetrating oil contamination.<br />

Some specimens were involved in various other cleaning trials including the use of vapor<br />

degreasing, acidic scale conditioner, acetone and permanganate.<br />

Part two of the cleaning studies at Delta included evaluation of the cleaning methods listed below<br />

<strong>for</strong> each of the contaminate types. In cases where unsatisfactory cleaning results were found <strong>for</strong> a<br />

particular contaminate/cleaning method combination, as determined by photometer brightness<br />

numbers, the sample was then cleaned by another method.<br />

• Oxidation of nickel specimens<br />

C3 – Alkaline De-rust Solution A<br />

C7a – Ultrasonic w/Alkaline De-rust Solution B<br />

B2 – Wet Glass Bead<br />

B5 – Aluminum Oxide 500 grit<br />

• Oxidation and scale of titanium specimens<br />

C2a – Alkaline De-rust Solution A<br />

C2b – Alkaline De-rust Solution B<br />

B2 – Wet Glass Bead<br />

B5 – Aluminum Oxide 500 grit<br />

• Soot on titanium<br />

C1 – Aqueous degreaser<br />

C2a – Alkaline De-rust Solution A<br />

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

print date/time: 6/6/2002 - 8:39 AM – Page 80

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