Research Article

Alternate-Fueled Combustor-Sector Performanceโ€”Part A: Combustor Performance and Part B: Combustor Emissions

Figure 11

(a) Nitric oxide emission (ppm) variations with ๐น / ๐ด and fueling composition. (b) Nitrogen dioxide emission (ppm) variations with ๐น / ๐ด and fueling composition. (c) NOx emission variations (ppm) with ๐น / ๐ด and fueling composition. [ ( g / k g ) [ E I N O ๐‘ฅ o r K H N O ๐‘ฅ ] โ‰ˆ ( p p m N O ๐‘ฅ ) ( 1 + F A R ) / ( 6 3 0 F A R ) ] . FAR: fuelโ€‰:โ€‰air ratio ๐น / ๐ด [1]. [ ( g / k g ) [ E I N O ๐‘ฅ o r K H N O ๐‘ฅ ] โ‰ˆ ( p p m N O ๐‘ฅ ) ( 1 + F A R ) / ( 7 1 5 F A R ) ] . FAR: fuelโ€‰:โ€‰air ratio ๐น / ๐ด (herein, arp). [ ( g / k g ) [ E I N O ๐‘ฅ o r K H N O ๐‘ฅ ] โ‰ˆ ( p p m N O ๐‘ฅ ) ( 1 + F A R ) / ( 6 5 5 F A R ) ] . FAR: fuelโ€‰:โ€‰air ratio ๐น / ๐ด (herein, arpc). Aerospace-recommended practice (arp) and (arpc) corrected arp. E I ๐‘ โ‰ˆ [ 1 0 3 ๐‘š ๐‘ / ๐‘š ๐‘“ ] ร— [ ๐‘š ๐‘“ ( 1 + F A R โˆ’ 1 ) / ๐‘š g a s p r o d u c t s ] ร— [ m o l ๐‘ ๐‘€ ๐‘ / ๐‘š ๐‘ ] ร— [ ๐‘š g a s p r o d u c t s โˆ‘ / ( m o l ๐‘— M ๐‘— ) g a s p r o d u c t s ] ร— 1 0 3 / 1 0 3 ร— 1 0 โˆ’ 6 p p m . ๐‘š ๐‘‹ : mass flow rate of ๐‘‹ (g/s), ๐‘š ๐‘“ : mass flow rate of fuel (kg/s), ๐‘€ ๐‘‹ : molar mass of ๐‘‹ , m o l ๐‘‹ : moles of ๐‘‹ , and FAR: fuelโ€‰:โ€‰air ratio ๐น / ๐ด . (g/kg) [EINOx] SAE ARP 1 5 3 3 โˆผ { [ N O ๐‘ฅ ] / ( [ C O ] + [ C O 2 ] + [ C ๐‘ฅ H ๐‘ฆ ] } ร— 1 0 3 ๐‘€ N O ๐‘ฅ / ( ๐‘€ C + ๐›ผ ๐‘€ H ) . [NOx] [CO] [CO2] [CxHy] = mass fractions of NOx, CO, CO2, and total hydrocarbon THC, ๐‘€ : molar mass, ๐›ผ : ratio of H / C : ๐‘› / ๐‘š in fuel C ๐‘š H ๐‘› where NOx mol mass is assumed to be 46, contrast to Figures 11(a) and 11(b).
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684981.fig.0011b
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