SYSTEM IDENDIFICATION
TURBO GENERATOR PARTS
THE GAS TURBINE SET CONSIST OF FOLLOWING MAIN PARTS TURBINE - REDUCTOR & COUPLING – ALTERNATOR - TURBINE RUN SYSTEM - GAS BURNING SYSTEM - LUBRICATION SYSTEM - BURNING AIR FILTER SYSTEM - CAGE AIR- CONDITIONING FILTER SYSTEM - CONTROL SYSTEM - FIRE ALARM AND EXTINCTION SYSTEM - COMPRESSOR CLEANING SYSTEM - ASSEMBLING TYPE

1- Turbine
PRODUCER : SOLAR MODEL/TYPE : TAURUS 60 POWER (kW) : 5.500 THERMAL CYCLE (kj/kWh) : 11.842 EXHAUST GAS DEBIT (kg/h) : 21.89 EXHAUST GAS TEMPERATURE : 510 °C COMPRESSION RATIO : 12:1

BASE VALUES USED AT CALCULATIONS DUE THE GEOGRAPHIC CONSTRACTION;

RELATIVE HUMIDITY(%) : 60 ALTITUDE(m) : 82 INLET AIR TEMPERATURE : 15°C LOAD (%) : 100 %O2 : 15 PRODUCER : SOLAR MODEL : TAURUS 60 DESIGN : SINGLE SHAFT COMPRESSION RATE : 12:1 COMPRESSOR FLAP AMOUNT : 12 FLAPS WEIGHT (kg) : 3.550 TURBINE STAGE NO : 3 STAGE ENTRY TEMPERATURE (kW) : 17.635 THERMAL CYCLE (kj/kWe-h) : 12.090 THERMAL CYCLE (kW/kWe-h) : 3,47 GENERATOR OUTPUT POWER (kW) : 5.251 EXHAUST TEMPERATURE (°C) : 514 EXHAUST DEBIT (kg/h) : 21,36 EXHAUST HEAT (kW) : 8.810 ELECTRICAL EFFICIENCY (%) : 29,78 STEAM GENERATION (TON/HOUR) : 11,4 HOURLY NG CONSUMPTION (m3) (according to 8076 kcal) : 1.892

IF WE EVALUATE THE EFFECT OF WEATHER TEMPERATURE ON THE ELECTRIC PRODUCTION CAPACITY ACCORDING TO OUR GEOGRAPHICAL POSITION;

1.DECEMBER-JANUARY-FEBRUARY-MARCH SEASONAL AVERAGE TEMPRATURE 6 °C
2.APRIL-MAY- OCTOBER-NOVEMBER SEASONAL AVERAGE TEMPRATURE 13,5 °C
3.JUNE-JULY-AUGUST-SEPTEMBER SEASONAL AVERAGE TEMPRATURE 22 °C
BU DURUMDA / ACCORDING TO THIS;

REDUCTOR & COUPLING
TURBOMACH SOLAR BRAND REDUCTOR WITH %98,2 EFFICIENCY AND “MAINA” BRAND PIN CONNECTED COUPLING IS USED.

ALTERNATOR
IS HAVING THE SPECIFICATIONS OF LEROY SOMMER BRAND LSA 56 BUL 85-4P CODED 1.500 RPM ALTERNATOR WITH 0,8 COFFICIENT AND 6.800 KVA.

TURBINE RUN SYSTEM
SYSTEM IS GIVING START TO THE TURBINE WITH A LEROY SOMMER BRAND 90 KWH DRIVEN 410 BAR 125 c3/rar HYDRAULIC PUMP.

GAS BURNING SYSTEM
THE GAS INLET DOES HAVE A 10MICRON FILTER AND THE PILOT AIR IS FILTERED TROUGH A 100MICRON FILTER WHICH IS PLACED TO THE INLET OF COMPRESSOR AIR. 12 PIECES GAS INJECTOR IS USED.

LUBRICATION SYSTEM
FIRST LUBRICATION IS DONE BY A DC MOTOR DRIVEN UNIT WITH A VOLUME OF 6,3 M3/MIN. MAIN PUMP IS A TWO STAGE PUMP. IN ORDER TO HEAT THE OIL A 4,5 KW HEATER IS USED. A HEAT EXCHANGER AND 2 PIECES STEAM SEPERATOR IS EXCIST. THE OIL FILTER IS 10MICRON. THE COOLING IS DONE BY A AIR COOLING HEAT EXCHANGER WHICH HAS BEEN DESIGNED FOR 55 °C.

BURNING AIR FILTER SYSTEM
TWO PIECES F06 CLASS FILTER IS USED.

1-CONTROL SYSTEM
THE CONTROL IS DONE OVER A PC. AT A WORST SENARIO THE SYSTEM IS BEING SHUTDWON BY A S5 PLC WHICH IS CONNECTED TO THE FIELDSBUS WHICH THE PC IS CONNECTED AS WELL. THE TURBINE SET CONTROL IS DONE OVER A TFT DISPLAY CONNECTED TO THE PC WHICH IS CONSIST IN THE TURBINE PACKAGE. THE SET CAN BE VISUALIZED AND CONTROLLED FROM A FAR PC CONNECTED TO THE SAME ETHERNET LINE. THE END