航空 发表于 2011-4-13 08:49:09

Booster Spool Forward Flange Wear

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航空 发表于 2011-4-13 08:49:27

February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 1<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 2<BR>Background<BR>• During shop visit, premature glazing/wear marks observed on the forward<BR>flange of the booster spool at each fan B=blade position<BR> Glazing/wear marks caused by contact with fan blade shank aft surface<BR>during wind milling and engine start sequence<BR>Booster Spool Forward Flange Wear<BR>FWD Flange<BR>mating surface<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 3<BR>Field Exposure - Sampling Program<BR>B20 1<BR>B20/2 15<BR>B22 1<BR>B24 2<BR>B26/2 4<BR>B20 0,000<BR>B20/2 0,053<BR>B22 0,081<BR>B24 0,086<BR>B26/2 0,018<BR>23<BR>0,049<BR>Engine Qty<BR>Wear per 10,000 EFC (millimeters)<BR>Total Engine Qty<BR>Total Wear per 10,000 EFC (millimeters)<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 4<BR>Field Exposure - Sampling Program<BR>0<BR>0,05<BR>0,1<BR>0,15<BR>0,2<BR>0,25<BR>0,3<BR>0 5000 10000 15000 20000 25000 30000<BR>OPERATING TIME (Cycles Since New)<BR>WEAR DEPTH (mm)<BR>Fleet average<BR>Projected wear at part life limit<BR>expiration: 0,005 in. (0,12 mm)<BR>9365<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 5<BR>Windmilling test<BR>• Objectives<BR> Reproduce wear seen in the field with<BR>current design<BR> Define the best improvement :<BR>– Seven new coatings tested:<BR> Baseline<BR> Two types of Teflon coating<BR> Cu-Ni-In<BR> Cu-Al<BR> Double Molydag varnish<BR> Baseline with periodic relube<BR> Molydag on # surface roughness<BR>– Low speed (33 rpm) giving full rocking<BR>of the fan blades<BR>ESN 874986 - 2.8 mils wear depth<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 6<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 7<BR>Windmilling Test<BR>• Preliminary results (1 cycle = 1 rev) :<BR> 1,686,000 cycles cumulated on 7 Jan 02<BR>– Wear initiated with current design : 0.4<BR>mils<BR> 2,231,000 cycles cumulated on Jan 21, 02<BR>– Wear increased with current design :<BR>1.2 mils<BR> Wear with new configurations not measured<BR>yet<BR>• Plan<BR> Continue current test<BR> Wear phenomenon is not linear<BR> Wear threshold with current definition now<BR>achieved, therefore final results expected by<BR>end of Feb 2002<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 8<BR>Interim Control Program<BR>• CESM No. 005 being revised to recommend lubrication in this area<BR> Benefit confirmed through engine test<BR>– Booster spool condition not directly affected by the introduction of<BR>elastomer axial buttons on Fan Retaining Flange (SB 72-318 or<BR>72-325)<BR>• Booster Spool front flange wear serviceability being extended<BR> Part installed : serviceable if not more than 0.008 in. (0,20 mm) deep<BR> Part removed : serviceable if not more than 0.003 in. (0,08 mm) deep<BR>• Repair procedure being developed to restore part condition at piece-part-level<BR>• New analysis in process to increase the 0,2 mm limit<BR>• Continue to gather data in the fleet to better appreciate the wear propagation<BR>rate<BR>Booster Spool Forward Flange Wear<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 9<BR>Long Term Action<BR>• Design improvement being reviewed to prevent occurrence of unserviceable<BR>condition<BR> Application of thermal sprayed coating (Al-Cu or Cu-Ni-In) on fan blade<BR>shank AFT surface decision based on Windmilling test results<BR>Booster Spool Forward Flange Wear

kinran 发表于 2011-6-4 23:28:00

:victory: :victory:

bocome 发表于 2011-7-31 04:39:22

Booster Spool Forward Flange Wear
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