3-Multi - Can Annular Combustor
3-Multi - Can-Annular Combustor The third design and the one preferred by most manufacturers, is the can-annular combustor, a combination of the single combustion chamber and the annular.
TURBINE SECTION (EXPANTION SECTION) This transition duct, located between the combustion chambers and the turbine-nozzle guide vanes, insures a final mixing of the hot gases.
Fixed Nozzles 1 st Stage Turbine Wheel 1 st Stage Turbine 2 nd Stage
Primary air Secondary air Sealing air Cooling air Bleeding air Compressor extracting air Separate HP air compressor Compressor outlet air Compressor air to exhaust Atomizing air
Diffuser Chamber
Gap = 1mm to 1.5 mm
17 IN CASE OF GAS TURBINE AIR COMPRESSOR SURGE BLEED VALVE WILL OPEN IN CASE OF GAS TURBINE AIR COMPRESSOR SURGE BLEED VALVE WILL OPEN COMPRESSOR TURBINE BLEED VALVE
Axial Compressors
Speed Controllin g System
Fly weight Governor Turbine Shaft Turbine Shaft Starts to rotate Rotating Element PIN Governor Valve Rod
Turbine Shaft Fly weight Governor Governor Valve Rod Turbine Shaft Speed Increased
Turbine Shaft Fly weight Governor Governor Valve Rod Turbine Shaft Speed Increased
Turbine Shaft Fly weight Governor Governor Valve Rod Turbine Shaft Speed Increased
Turbine Shaft Fly weight Governor Governor Valve Rod Turbine Shaft Speed Increased
To Decrease Speed Governor valve Fuel to combustion chamber Decreased Oil pressure Governor Valve Rod
Fuel to combustion chamber Increased Governor valve To increase Speed Oil pressure Governor Valve Rod
High speed Trip Valve
Turbine shaft Hydraulic oilFuel gas Or Steam Turbine OPERATING SPEED
Turbine shaft Turbine OVER SPEED Hydraulic oil out Fuel gas Or Steam Stop
Turbine Shaft OPERATING SPEED
Turbine Shaft SPEED INCREASED
Turbine Shaft SPEED MORE INCREASED
Turbine Shaft OVER SPEED