The combustion chamber liner.

The Liner, shown on the figure 1, is the beating heart of the combustion system, mounted inside the combustion chamber cever, figure 2, inside the liner, the air and fuel are mixed and burned inside the liner, providing, hot gases.

Inside the combustion chamber , the liner is mounted at the forward side by three liner stops and supported at the aft side by inserting the liner inside the transition piece. This configuration allows expansion of the liner

.

.

The Turbine hollow first stage nozzles received hot gases from the combustion chambers , via the transition pieces, are directed to the first stage rotor buckets.

The hollowing configuration of the turbine first stage nozzles, as shown on the above figure allows the relatively cool compressure discharge air to cool the first nozzles stage, by entring from the outer circonference side and exiting throught holes on the trailing edge.

The hot gases impact kinetic energy to the airfoil shapped rotor buckets, this energy is turned into mecanical energy in the gas turbine rotor shaft.

The Turbine first stage nozzles received hot gases from the combustion chambers , via the transition pieces, are directed to the first stage rotor buckets.

The hot gases impact kinetic energy to the airfoil rotor buckets, this energy is turned into mecanical energy in the gas turbine rotor shaft.