Two (2) Used Solar Turbine Titan 250 / T250 C51 Compressor Sets For Sale

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