How AMIL Performs Catalytic Carbon Brake Disk Oxidation
Transcription
How AMIL Performs Catalytic Carbon Brake Disk Oxidation
SAE G-12 RDF Catalytic Oxidation Working Group Meeting San Francisco, May 2011 How AMIL Performs Catalytic Carbon Brake Disk Oxidation Test AIR5567A for AMS 1431C / 1435B Runway De-icer Diane Paradis Marc Mario Tremblay AMIL SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 1 AMIL vs AIR5567 Method - Background Date Actions November 2008 AMIL was contacted by Alun Williams January 2009 to April 2009 Evaluated the method, suggestions December 2009 Validation tests : Generic de-icers January 2010 Requests from RDF manufacturers Started Set-up for Testing AMIL started testing of commercial Runway De-icers SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 2 AIR5567 Test Results Typical Turn Around Time: When Runway De-icer is submitted for Testing 9 AO Coated Test Coupons in hands ¾ 2 weeks ¾ AO Coated Test Coupons not in hands delivery time : 45 days (minimum) ¾ at least 2 months SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 3 Runway De-icers Tested as per AIR5567 at AMIL - May 2011 Runway De-icer Form Total Liquid Solid 32 4 36 SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 4 AIR5567 Test Method Material and Procedure SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 5 Step 3.3 k - AO Coated Coupons Provided by Honeywell : Sets of 8 test coupons Carbon/carbon composite brake material CARBENIX® 4000 Having an average of initial weight = 19.8 ± 0.1 g Test coupons received already treated with AO coating SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 6 Contamination of Coupons – Runway Deicer Solution Step 3.4 e - Total Immersion Time = 10 ± 1 min (5 min / side) Step 3.4 a - Runway De-icer 25 % w/w Solution Glass Vessel SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 7 Deicer Contaminated Coupons Step 3.4 f - Dry Coupons Oven 150 °C, 2 hours Glass Vessel (Petri Dish) SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 8 After 2 hours at 150 °C After Drying Period Step 3.4 f - Immediately Transfer to a Desiccator Minimum of 30 minutes SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 9 Weight of Contaminated Coupons 9Step 3.4 g - Weight and Record Coupons Weights 9Step 3.4 h - Calculate the % Pick-up of Deicer To ± 0.001g Accuracy SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 10 Oxidation Testing - Alumina Disks Step 3.5 a - Place Coupons on Refractory Dish Base #1 #2 #3 #4 #5 #6 ≈ 2.5 inch High Temperature Resistance Tray #8 #7 FRONT SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 11 Oxidation Testing - Still Air Muffle Furnace Steps 3.5 b/c/d - Load Sample Tray Preheated Furnace 550 ± 5 °C 24 hours SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 12 After 24 hours Step 3.5 e - Tray with Hot Coupons Remove Hot Coupons and Tray from the Furnace SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 13 Cool to Room Temperature Step 3.5 e - Allow Coupons to Air Cool ≈ 1 hour Transfer in a Desiccator to Achieve Room Temperature at least 30 minutes SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 14 Weight Loss Determination For each Runway De-icer 9Step 3.5 f - Weight and Record Final Weights 9Step 3.5 h - Calculate the Mean % Weight Loss 9Step 3.5 k - Calculate the Mean % Normalized Oxidation Weight Loss To ± 0.001g Accuracy SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 15 For information: Marc Mario Tremblay AMIL [email protected] 1-418-545-5011 (2155) SAE G-12 RDF Cat. Oxidation WG Meeting, San Francisco May 2011 16