Taurus Group 60 - Manual (Page 29)

Turbomachinery Package Specification Taurus 60 Compressor Set and Mechanical Drive
Gas Fuel System (cont.)
Response Time Less Than 100 msec From 10-to-90% Stroke
Valve Body Aluminum (Standard)
Stainless Steel (Optional)
Gas Fuel Filter (Conventional Units Only) 10 Micron
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
Solar’s Applicable Engineering Specifications
ES 9-98 Fuel, Air, and Water (or Steam) for Solar Gas Turbine Engines
ES 1593 Guidelines for NEC Compliance of Solar Product Lines: Class I, Group D, Division 1 and
Division 2
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)
ES 2201 Auxiliary Service Air
Solar’s Applicable Product Information Letters
PIL 148 LPG and NGL Fuels
PIL 162 Recommendations and Requirements for the Sourcing, Handling, Storage and Treatment
of Fuels for Solar Gas Turbines
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.
© 2009 Solar Turbines Incorporated. All rights reserved. TPS60CSMD/309
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