Abstract
A multi-component (NB 3 /H 2 O) Kalina-type cycle that utilizes the exhaust from a gas turbine is investigaed in this paper. The turbine-inlet pressure of 5.96 × 10 6 N/m 2 and temperature of 755.372 K were kept constant, as well as the working fluid temperature at the condenser outlet (at 290K). The HN 3 mass fraction at the turbine inlet was varied along with the seperator temperature and the effects on the cycle efficiency were studied. The relationships between turbine-inlet flow and the seperator-inlet. How are shown in addition to the upper and lower HN 3 mass-fraction bounds. The multi-component working-fluid cycle investigated is 10–20% more efficient than a Rankine cycle with the same boundary conditions.
| Original language | American English |
|---|---|
| Journal | Energy |
| Volume | 18 |
| DOIs | |
| State | Published - Sep 1 1993 |
Disciplines
- Mechanical Engineering
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