CAT Titan 250 User Manual

Page 24

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Turbomachinery Package Specification

Titan

250 Generator Set

Customer-Furnished Pilot Air System
Fluid Clean-Dry

Air

Air Quality

See Note (d)

Minimum/Maximum Regulated Pressure Range

689 to 1379 kPag (100 to 200 psig)

Pilot Air Filter

10 micron

Construction Materials
Piping, Manifolds, and Tubing

316L Stainless Steel

Applicable Engineering Specifications
Solar’s Engineering Specification ES 9-98

Fuel, Air, and Water (or Steam) for Solar Gas
Turbine Engines

Solar’s Engineering Specification ES 1593

Guidelines for NEC Compliance of Solar Product
Lines: Class I, Group D, Division 1 and Division 2

Solar’s Engineering Specification ES 1762

Standards and Practices for Electrical Systems for
Gas Turbine Packages Installed In Hazardous
Areas (CENELEC/IEC Standards – European
ATEX Directive 94/9/EC)

Applicable Product Information Letters
Solar’s Product Information Letter PIL 148

LPG and NGL Fuels

Solar’s Product Information Letter PIL 162

Recommendations for the Sourcing, Handling,
Storage and Treatment of Fuels for Solar Gas
Turbines

Solar’s Product Information Letter PIL 176

Siloxanes in Gas Fuel

Notes

:

(a)

The gas fuel system is designed to operate with fuels that comply with Solar’s Engineering
Specification ES 9-98. Most commercially available natural gas fuels comply with ES 9-98.
The gas fuel system can be modified to operate with fuels that do not comply with ES 9-98.
Solar

gas turbines can operate on low Btu fuels. Please contact Solar Turbines for

assistance in evaluating fuel characteristics and gas turbine requirements.

(b)

Fuel pressure and flow requirements can be affected by several factors such as; fuel
temperature, fuel lower heating value, air inlet temperature, fuel composition, fuel specific
gravity, engine injector type, inlet duct loss, relative humidity, site elevation, and piping length
and diameter. Based on site conditions, minimum fuel pressure and flow requirements may
be less than stated values. Please contact Solar Turbines for site-specific fuel pressure and
flow requirements.

(c)

Fuel must have a differential temperature (

ΔT) of at least 27°C (50°F) above fuel dew point

temperature.

(d)

The particle size in the air stream should not exceed 10μ. Since it is impractical to remove
100% of all particles larger than 10μ, this is defined as ß10 > 100, or 99% efficient. Oil or
hydrocarbon content should not exceed 1 ppm. The dew point at line pressure shall be at
least 6

°C (10°F) below the minimum temperature to which any part of the air system is

exposed or between -29

°C and 93°C (-20°F and 200°F). Air should be free of all corrosive

contaminants, hazardous gases, flammables, and toxics.

© 2008 Solar Turbines Incorporated. All rights reserved.

TPS250GS/908 - Preliminary

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