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Gas turbine improvement methods and reheating

Short answer

Methods: regeneration, intercooling, reheating, higher temperatures, combined cycles. Reheating splits expansion into stages with reheating between turbines; the second stage temperature drop is larger, increasing total turbine work and net work output without changing compressor work.

List the common methods used for the performance improvement of the gas turbine power plants. Explain how reheater increases net work output of the plant.

Common methods to improve gas turbine performance

  1. Reheating – expansion in stages with reheating between turbines.
  2. Intercooling – compression in stages with cooling between stages.
  3. Regeneration – exhaust gas preheats compressed air.
  4. Combination of the above (approaches the Ericsson cycle).
  5. Higher turbine inlet temperature using better materials and blade cooling.
  6. Optimum pressure ratio, high component efficiencies, low pressure losses.
  7. Combined cycle / cogeneration with waste-heat recovery.
  8. Water/steam injection, inlet air cooling.

How reheating increases net work output

      fuel            fuel
       v               v
 1->[C]-2->[CC1]-3->[HPT]-4->[CC2]-5->[LPT]-6-> exh
     ||              ||               ||
     ++=====shaft====++=====shaft=====++==> Gen
 T
 |          3       5
 |         *       *
 |        /|      /|
 |       / |     / |
 |      /  *----'  * 6
 |   2 *   4       |
 |     |          /
 |     *--------'
 |     1
 +---------------------- s
  1. Gas from the combustion chamber at T3T_3 expands in the HP turbine only to an intermediate pressure, temperature falling to T4T_4.
  2. It enters a reheater (second combustion chamber) where more fuel is burnt in the excess air, raising its temperature back to T5≈T3T_5 \approx T_3.
  3. It then expands in the LP turbine to atmospheric pressure (T6T_6).
  4. Total turbine work:
Wt=cp(T3−T4)+cp(T5−T6)W_t = c_p(T_3 - T_4) + c_p(T_5 - T_6)

On the T–s diagram, constant-pressure lines diverge as entropy increases, so the temperature drop T5−T6T_5 - T_6 is larger than the drop the gas would have had from T4T_4 without reheat. Hence turbine work increases, while compressor work is unchanged, so net work output and work ratio increase. 5. Maximum work is obtained when both turbines have equal pressure ratios: p4=p3p6p_4 = \sqrt{p_3 p_6}, with T5=T3T_5 = T_3.

Effect on efficiency: extra fuel is burnt and the exhaust is hotter, so reheat alone may slightly lower efficiency; combined with regeneration, the hot exhaust preheats the air and both output and efficiency improve. Reheating is therefore used where high specific output and a compact plant are needed.

✓ Answer checked by Claude Opus 5.5 (high effort)

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