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Diagrama

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Cristian Ah

This document provides specifications for a gas turbine engine, including a compressor inlet temperature of 27°K and pressure of 100 kPa, a combustor outlet temperature of 1750°K and pressure of 7.5 MPa, and a turbine inlet temperature of 450°C at 500 kPa pressure. The engine has a mass flow rate of 500 MW and a compressor pressure ratio of 16.

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Wn = 500 Mw Tmax = T3 = 1750°K rp = 16/1 3 2 compresor 1 4 T5 = 723°k 5 Pa = 7.5 Mpa a Ta = 450° C b-1 b d c P = 500 Kpa combustor T1 = 27°k P1 = 100 kpa rp = 1/16 Wn = 500 Mw

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Diagrama

  • 1. Wn = 500 Mw Tmax = T3 = 1750°K rp = 16/1 3 2 compresor 1 4 T5 = 723°k 5 Pa = 7.5 Mpa a Ta = 450° C b-1 b d c P = 500 Kpa combustor T1 = 27°k P1 = 100 kpa rp = 1/16 Wn = 500 Mw