3003 W CASINO RD PAINT HANGAR BOUNDARIES 2023-07-20

illGemnus Boeing Project Contract No.EVE-16-2929 i Technologyi Development CEI Project No. 160731 Table 1: Paint Ingredients, Flow Rates, And CFD Parameters For Baseline Clearcoat Paint Constituents & Atomization Air Total Mass Flow Ingredient Mass Rate From Gun CFD Mass Flow i %In Paint (g/s) From Gun(g/s) CFD Mass% Paint 100.0% 7.87 1.70 15.0% Inert 46.1% 3.63 0.00 0.0% Hexamethylene diisocyanate, oligomers 32.6% 2.56 0.00 0.0% Non-hazardous polymer resin 1 9.7% 0.76 0.00 0.0% Non-hazardous polymer resin 2 3.9% 0.31 0.00 0.0% Flammable 53.9% 4.24 1.70 15.0% heptan-2-one 41.8% 3.29 1.32 11.6% n-butyl acetate 8.5% 0.67 0.27 2.4% ethyl 3-ethoxypropionate 1.8% 0.14 0.06 0.5% butyl glycolate 0.5% 0.04 0.02 0.1% ethyl lactate 0.5% 0.04 0.02 0.1% dipentene 0.4% 0.03 0.01 0.1% pentane-2,4-dione 0.4% 0.03 0.01 0.1% methyl 1,2,2,6,6-pentamethyl-4- piperidyl sebacate 0.0% 0.00 0.00 0.0% bis(1,2,2,6,6-pentamethyl-4- piperidyl)sebacate 0.0% 0.00 0.00 0.0% hexamethylene-di-isocyanate 0.0% 0.00 0.00 0.0% Air 0.0% 9.63 9.63 85.0% Air 0.0% 9.63 9.63 85.0% Air 0.0% 9.63 9.63 85.0% Grand Total 100.0% 17.49 11.32 100.0% For both Case 1 (Scenario 2 only), Case 2, and Case 3 (all scenarios) stacker cranes are positioned along the aircraft to create an overspray cloud with the largest possible extents - one at the forward door, one over the wing, one at the aft door, and one at the vertical stabilizer (see Figure 11). These exact locations are adjusted slightly for each case due to the difference in aircraft dimensions, so Figure 11 and Figure 12 are used for to illustrate this for both cases. 20