Table 1 should read as follows:
Table 1
Base cycle–exergy destruction data (without generator/inverter losses)
| Pressure ratio | 6.5 | 8.8 | 15 |
| Component | Exergy, % of Total Fuel Input | ||
| LP compressor | 0.83 | 0.86 | 0.87 |
| Intercooler | 1.58 | 2.09 | 2.63 |
| HP compressor | 0.82 | 0.80 | 0.80 |
| preheater | 2.53 | 2.05 | 1.43 |
| SOFC | 11.57 | 11.44 | 11.63 |
| HP combustor | 3.18 | 3.19 | 3.14 |
| HP expander | 0.81 | 0.86 | 0.84 |
| LP combustor | 9.77 | 10.14 | 10.54 |
| LP expander | 1.10 | 1.08 | 1.10 |
| Stack gas | 5.64 | 5.54 | 6.00 |
| Total | 37.83 | 38.05 | 38.98 |
| Pressure ratio | 6.5 | 8.8 | 15 |
| Component | Exergy, % of Total Fuel Input | ||
| LP compressor | 0.83 | 0.86 | 0.87 |
| Intercooler | 1.58 | 2.09 | 2.63 |
| HP compressor | 0.82 | 0.80 | 0.80 |
| preheater | 2.53 | 2.05 | 1.43 |
| SOFC | 11.57 | 11.44 | 11.63 |
| HP combustor | 3.18 | 3.19 | 3.14 |
| HP expander | 0.81 | 0.86 | 0.84 |
| LP combustor | 9.77 | 10.14 | 10.54 |
| LP expander | 1.10 | 1.08 | 1.10 |
| Stack gas | 5.64 | 5.54 | 6.00 |
| Total | 37.83 | 38.05 | 38.98 |
Copyright © 2011
by American Society of Mechanical Engineers
