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Show "Nox Reduction by Low Pressure Steam Addition" APPENDIX The hidden formulas in column F is the same as printed in column G except the letter "F" replaces "G". Column "F" is the 49 PSIG steam header pressure case. In rows 1-1 7, the temperature leaving the globe valve due to Joule-Thomson expansion is calculated. The temperature and enthalpy to the oil-gun nozzle holes are calculated in rows 18-30 based on the combined radiant and free convection heat transfer coefficients. The latter was taken equal to 2.0 Btu / Hr Sq Ft oR. 1 2 3 4 5 A I ESTIMATE OF STEAM RATES 150# Header F ALGORITHM FOR COLUMN F PSIG 150.0 150.0 PSIA 164.7 =G3+14.7 G Oeg F 365.8 =363.55+(G$4-160)*(368.42-363.55)/1 0 ~_6- +-______H --:....B, _t_u_1# _ _1 _1_9_5_.5_7_ = 1 1 95. 1 + (G $ 4 - 1 60) * (1 1 96. 1 - 1 1 95. 1 ) 11 0 7 Steam (If Saturated at Header Pressures) 8 PSIG 4 9 49 9 PSIA 63.7 =G8+14.7 1 0 Sat. Oeg. F. 296.7 =$1311OG$9*G$9+$J31*G$9+$K31 1 1 Hliq,Btu/# 266.4 =SI32*G$91OG$9+$J321OGS9+SK32 1 2 Hvap,Btu/# 1178.8 =SI33*G$91OG$9+SJ33*GS9+$K33 ~--+--------~~~-----~ 1 3 1 4 1 5 1 6 1 7 1 8 1 9 2 0 2 1 2 2 2 3 2 4 2 5 2 6 2 7 2 8 2 9 3 0 Guess Lb I H burner Header Lb/H Cp bar (300F-sat) T leaving Globe Valve,F Guess T to Gun.F Average Temp., F 156.8 9,406 156.8 =G141060 0.5709 =(SI$37*G$9"2+$J$37*G$9+$K$37) 326.1 =G10+(G6-G12)/G16 310.4 310.4 318.2 =(G17+G18)/2 Heat Losses Effect on Enthalpy to Gun h rad 1 .98 = 0.171 3E-8* «G 1 9+459.7)"4-(70+459.7) "4 )/( G 19-70) h cony 2.00 2.00 A,sq ft 85 85 Del H,Btu/Hr 84,069 =(G22+G23)*G241t(G19-70) Hmix,Btu/# 1186.6 =G6-G25/G15 X Ilq SPHTD =IF(G26<G12,(G12-G26)/(G12-G11),"SPHTO") DEL T SPHTD, F 1 3.7 =(G26-G12)/G 16 Card T to Gun,F 310.4 =IF(G28>0,G28+G1 0,G1 0) Guess I CaJ'd 1 .000 =G 18/G29 Jordan Loftus SeD Page A-l |