FOR SALE
Solar Titan 250S Turbine-driven C51 Centrifugal Compressors Sets:
· Used
· Located in the USA
· Two (2) T250 turbine/C51-compressor sets available
· Manufactured in 2014 by Solar Turbines
The turbine-driven compressor set consists of an axial-flow turbine and driven compressor.
Turbine and compressor are in-line on a base frame, a steel weldment with beam sections and cross members forming a rigid platform.
The turbine output shaft is aligned with the driven equipment input shaft, and the shafts are connected with a splined interconnecting drive shaft.
Auxiliary systems include start, fuel, air, lube oil, electrical control and seal systems.
Each packages components include:
· Start System
· Fuel System
· Electrical Control System
· Lube Oil System
· Enclosure and Ancillary Equipment
· Titan 250S Turbine
· Gear Unit
· Driven Equipment: C51 Centrifugal-type compressor
· Seal System
Drivers: Two (2) Solar Titan 250-30000S turbines
· UNIT 1 – 25,183 fired hours; 4,817 remaining fired hours before standard overhaul
· UNIT 2 – 13,785 fired hours; 16,215 remaining fired hours before standard overhaul
· Assembly number: 2-3R921
· Serial Numbers: KC14737, KC14738
The Titan 250-30000S gas turbine is a two-shaft, axial-flow design consisting of the following major assemblies/components:
· Air inlet assembly
· Compressor assembly
· Compressor diffuser/combustor assembly
· Turbine assembly
· Exhaust collector
· Output drives haft
Drivens: Two (2) Solar C51ML04LTN-0011 gas compressors:
The C51 gas compressor is a centrifugal-type compressor designed for efficient
gas boosting service when driven by a Solar gas-turbine engine. Included are the
compressor design characteristics particular to this installation.
Flow ranges from 2000 to 15 000 cfm (57 to 425 m3/min) are available, depending
on the selection of internal staging.
The compressor is designed to operate at ambient temperatures as low as -20°F (-29°C) and
discharge gas temperatures as high as 350°F (177°C) (375°F (191°C) with high-temperature seals).
Compression is achieved in a centrifugal-type compressor by increasing the velocity and the static pressure of the fluid gas
as it passes through each rotor/stator stage.
The gas is drawn into the eye of the impeller and leaves at the periphery through the impeller blades.
Entering a stationary diffuser at high velocity, the gas flow is
retarded, converting most of the kinetic energy into additional static pressure. (177°C) (375°F (191°C) with high-temperature seals).
Compressor Design Characteristics
· Model Number C51ML04LTN-0011
· Assembly Number 3R921-C3R921-D1
· Serial Number(s) G5110218, G5110219
· Staging E3, E2, E2, E1
· Approximate Weight 41 600 lb (18 866 kg)
· Design Point Impeller O.D. 21.18 in. (538 mm)
· Design Point Suction Pressure 461.9 psia (3184.6 kPa)
· Design Point Discharge Pressure 903.9 psia (6232.1 kPa)
· Design Point Head 37 816.0 ft-lb/lb (113.0 kJ/kg)
· Design Point Flow 14 808.26 cfm (419.32 m3/min)
· Power Required 25 993 hp (19 383 kW)
· Speed 9120 rpm
· Design Point Suction Temperature 125.0°F (51.6°C)
· Design Point Discharge Temperature 237.3°F (114.0°C)
· Design Point Efficiency 84.3%
· Design Point Surge Margin 23.6%
· Design Point Gas Specific Gravity 0.5765 Compressor Diffuser/Combustor Assembly
The compressor diffuser/combustor assembly is bolted to the aft end of the compressor case
and the forward end of the 3rd stage nozzle assembly.
The compressor diffuser/combustor assembly consists of the following components:
· Fuel manifold
· Compressor diffuser
· Compressor bearing support housing
· Fuel injectors
· Lube oil supply line
· Lube oil drain lines
· Compressor diffuser bleed air lines
· Bleed valve assembly
· Combustor liner assembly
· Torch igniter assembly
Please advise your interest for price and more details
Best regards
Woonha Jee
Korea
101-802 , Bundangro 190
Seongnam city, Kyonggido
13581, Korea
Dear Sir,
Based on the listing available at your website, we are looking for s Solar Turbine Driven Gas Compressor with all accessories for our internal usage.
Please share the detail and offer of the available equipment with you.
Looking forward to hear from you.
Replyhe Solar Gas Turbine Titan 250 operates based on the principles of the Brayton cycle, which is a thermodynamic cycle that describes the functioning of gas turbines. Here is an overview of the working principle of the Solar Titan 250 gas turbine:
Air Intake: The process begins with ambient air being drawn into the gas turbine through an inlet. The air is typically filtered to remove any contaminants that could damage the turbine components.
Compression: Once inside the turbine, the air undergoes compression in the compressor section. The compressor consists of multiple stages of rotating blades (rotors) and stationary blades (stators). As the air passes through each stage, its pressure and temperature increase due to compression. The compressor's primary function is to raise the air pressure before it enters the combustion chamber.
Fuel Injection and Combustion: In the combustion chamber, fuel (such as natural gas, diesel, or liquid fuel) is injected into the high-pressure, compressed air. The mixture of fuel and air ignites in the combustion chamber, creating a high-temperature, high-pressure gas.
Expansion and Power Generation: The hot, pressurized gas produced in the combustion chamber is directed to the turbine section. The gas expands rapidly as it passes through the turbine's rotor blades. This expansion causes the rotor blades to rotate, which is connected to a shaft that drives the generator or mechanical equipment, depending on the application. The rotation of the turbine generates mechanical energy that can be used to produce electricity, drive pumps or compressors, or perform other mechanical work.
Exhaust: After passing through the turbine, the exhaust gas exits the system through the exhaust outlet. In some cases, the exhaust gas may still have enough thermal energy to be utilized further, such as in combined heat and power (CHP) systems where the exhaust heat is captured for heating applications.
Overall, the Solar Titan 250 gas turbine utilizes the energy from compressed air and combustion to drive a turbine and generate mechanical power, which can be converted into electricity or used for various industrial purposes. The efficiency and performance of the turbine depend on factors such as fuel quality, operating conditions, and maintenance practices.
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