Research Article
Calculation and Analysis of Aircraft Pollutant Emission Based on Time Wake Separation Mode under Coastal Airport and Headwind Conditions
Table 4
Pollutant emission index of different engine models during approach.
| Engine model | Fuel flow (kg/s) | UHC (g/kg) | CO (g/kg) | Engine model | Fuel flow (kg/s) | UHC (g/kg) | CO (g/kg) |
| AE3007Al | 0.113 | 0.655 | 3.91 | V2530-A5 | 0.377 | 0.056 | 1.81 | CF6-80C2A5 | 0.687 | 0.2 | 1.93 | V2533-A5 | 0.3901 | 0.052 | 1.654 | CF6-80C2-B6 | 0.686 | 0.2 | 1.93 | V2525-D5 | 0.319 | 0.061 | 2.44 | CF34-3B | 0.116 | 0.13 | 1.88 | Trent772B/C-60 | 0.85 | 0.01 | 0.89 | CF34-8Cl | 0.1681 | 0.06 | 2.91 | Trent556-61 | 0.62 | 0 | 0.46 | CFM56-5B3/P | 0.366 | 0.5 | 1.7 | PW2037 | 0.458 | 0.11 | 1.95 | CFM56-5B4/P | 0.312 | 0.5 | 2.3 | PW306B | 0.0974 | 0 | 7.11 | CFM56-5B5/P | 0.26 | 0.7 | 3.4 | PW4052 | 0.6 | 0.17 | 2.15 | CFM56-5B/6P | 0.275 | 0.6 | 2.9 | PW4056 | 0.658 | 0.13 | 2 | CFM56-5B7/P | 0.312 | 0.5 | 2.3 | PW4060 | 0.703 | 0.14 | 1.78 | CFM56-5C4 | 0.386 | 0.065 | 1.4 | PW4062 | 0.725 | 0.14 | 1.69 | CFM56-3Bl | 0.338 | 0.1 | 1.6 | PW4062A | 0.708 | 0.15 | 1.68 | CFM56-3B2 | 0.314 | 0.073 | 3.4 | PW4077D | 0.835 | 0.07 | 0.6 | CFM56-3Cl | 0.336 | 0.07 | 3.1 | PW4158 | 0.682 | 0.14 | 1.88 | CFM56-7B22 | 0.298 | 0.1 | 2.5 | JT9D-7R4E | 0.6529 | 0.13 | 1.23 | CFM56-7B20 | 0.274 | 0.1 | 3.2 | JT8D-217A | 0.3833 | 0 | 3.54 | CFM56-7B24 | 0.316 | 0.1 | 2.2 | JT8D-217C | 0.363 | 0 | 3.79 | CFM56-7B26 | 0.338 | 0.1 | 1.6 | GE90-76B | 0.781 | 0.07 | 1.32 | CFM56-7B27 | 0.349 | 0.1 | 1.4 | GE90-90B | 0.899 | 0.07 | 0.98 | V2522-A5 | 0.311 | 0.062 | 2.6 | LF507-1H | 0.1083 | 0.12 | 4.43 | V2524-A5 | 0.328 | 0.061 | 2.37 | RB211-535E4-37 | 0.52 | 0.04 | 1.14 | V2527E-A5 | 0.319 | 0.061 | 2.44 | RB211-524H-36 | 0.77 | 0 | 1.05 |
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