For a gas turbine, a combustion process adds heat. Next, heat is added at constant pressure in State 2 to State 3. This process increases the temperature, pressure, and density of the gas. The gas undergoes an isentropic, adiabatic compression in State 1 to State 2. The Brayton cycle consists of two adiabatic work transfers and two constant pressure heat transfer heat processes (Fig 2). The working of a gas turbine is based on the thermodynamic Brayton Cycle.
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |