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FT4000® Gas Turbine SWIFTPAC® Package
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Catalog excerpts

FT4000® Gas Turbine SWIFTPAC® Package - 1

FT4000 SWIFTP Gas T AC urbine Package ® The FT4000® SWIFTPAC® gas turbine package is available in both single- and twin-engine configuations, which offer greater than 41 percent simple cycle efficiency and a nominal 60 to 140 megawatts of power within a modular design that is built utilizing over fifty years of aero-derivative design and packaging experience. Utilizing the core technology derived from the proven Pratt & Whitney ® PW4000™ turbofan engines, the all-new SWIFTPAC® gas turbine packages are designed to provide reliable peaking and base-load power with a relatively compact footprint. This is accomplished by coupling either one or two FT4000® engines to one electric generator. The modular design includes proven features of the successful FT8® SWIFTPAC® and MOBILEPAC® gas turbine package designs. • One (1) aero-derivative engine (60-70 MW)or two (2) aero-derivative engines (120-140 MW) • Single or dual engine configuration • Modular design • Maximum factory assembly • Optimized shipping sizes • Proven industrial components • Integrated ancillary systems • Control enclosure with power distribution • Prefabricated field piping • Interconnecting quickdisconnect cables • Standard option packages • 140 MW nominal output in twinengine configuration • Wet compression for improved performance above ISO conditions • Highest power output by any aero-derivative • Single or dual engine operation • 50- or 60- hertz performance with no penalty • >41% efficiency without external cooling • Reduced transportation time and cost • Limited on-site inventory • Minimal installation time • Efficient commissioning • Low installed cost/high overall value • Operating flexibility • High part-load efficiency • <10-minute start-up time • Quick engine changeout • Design flexibility to meet customer needs

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FT4000® Gas Turbine SWIFTPAC® Package - 2

FT4000 SWIFTP AC Gas Turbine Package ® Scope of Supply GT Enclosure Assembly Electric Generator One (1) per aero-derivative engine Assembly • Gas generator, GG4000-1 • Power turbine, PT4000-1 • Exhaust diffuser and collector box • Diaphragm-type coupling • Engine base • Structural base frame with drip pan • Acoustic/weather enclosure • Combustion air inlet plenum • Engine removal system • Fuel control module • Ignition system • Synthetic lube oil system • Hydraulic start system • Hydraulic control oil system • Bleed air system • Buffer air system • Ventilation air system • Off-line water...

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