A METHOD FOR DETERMINING THE OPTIMUM PARAMETERS FOR THE CYCLE OF SIMPLE GAS TURBINE EQUIPMENT,
Abstract
Dimensionless formulas are derived for determining the optimum rise in pressure and temperature during the operating cycle of a simple gas turbine installation from the standpoint of minimum cost for mechanical or electrical output energy. It was found that the optimum degree of temperature rise decreases with an increase in the cost of the installation. Proportionality is assumed between the cost of the installation and the rated power of the turbine and compressor in determining the optimum technical and economic degree of pressure rise. Application of the proposed formulas is illustrated by calculating the optimum pressure rise for the GT-6-750 gas turbine installation. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 25, 1969
- Accession Number
- AD0696544
Entities
People
- A. E. Piir
- D. D. Kalafati
Organizations
- National Air and Space Intelligence Center