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ASTM D2880-23 covers the grades of fuels for gas turbines, excepting those used in aircraft, and provides guidance for manufacturers, suppliers, and purchasers. The specification defines five primary grades. The sulfur content is explicitly designated by the “S” code, representing maximum parts per million (ppm): S5000 (5000 ppm), S500 (500 ppm), and S15 (15 ppm).
| 🟦 Grade | 📏 Fuel Type (per Scope) | 📐 Sulfur Options | ⚡ Key Operational Characteristics |
|---|---|---|---|
| No. 0-GT | Naphtha, Jet B, Light Hydrocarbon Liquids | S5000, S500, S15 | Characteristically low flash point and low viscosity. |
| No. 1-GT | Light Distillate Fuel Oil | S5000, S500, S15 | Suitable for use in nearly all gas turbines. |
| No. 2-GT | Heavier Distillate (than No. 1-GT) | S5000, S500, S15 | May require fuel heating depending on system design and ambient temperature. |
| No. 3-GT | Heavier Distillate, Low Ash Residual, or Blend | Per Agreement | Fuel heating required in almost every installation. |
| No. 4-GT | Most Residuals and Topped Crudes | Per Manufacturer Consultation | Wide property variation; manufacturer must agree on acceptable limits. |
Appendix X2 of D2880-23 discusses the sources of fuel contaminants and their significance in gas turbine operation. The presence of trace metals (such as vanadium, sodium, potassium, and lead) is particularly critical due to the risk of hot corrosion and fouling of turbine blades. The appendix provides recommended upper limits for these metals, but these limits do not constitute a requirement of the specification unless mutually agreed upon by the interested parties. Limitations due to the use of used or recycled oil are also explicitly noted.
The specification prescribes the required properties of gas turbine fuel oils at the time and place of delivery, unless otherwise provided by agreement between the purchaser and the supplier. Clause 1.4 clearly states that nothing in this specification shall preclude observance of federal, state, or local regulations which may be more restrictive. Appendix X1 serves as an informational resource, describing the five grades and the significance of the various test methods used in inspecting the fuels.
| 📐 Property / Contaminant | 📏 Significance in Gas Turbines | 🎯 Source of Guidance |
|---|---|---|
| Flash Point | Determines safety classification. No. 0-GT has a notably low flash point. | Appendix X1 |
| Trace Metals | Causes corrosion and fouling. Limits are recommended, not mandatory unless agreed. | Appendix X2 |
| Sulfur Content | Corrosion potential and environmental impact. Designated by the S code. | Main Specification Table |
No. Section 1.1 of the scope explicitly excludes gas turbines used in aircraft. Aircraft turbine fuels are governed by separate specifications.
These designations indicate the maximum allowable sulfur content in the fuel, measured in parts per million (ppm). S5000 corresponds to 0.5% sulfur, S500 to 0.05%, and S15 to 0.0015%.
No. The recommended upper limits for trace metals in Appendix X2 do not constitute a requirement of the specification unless they are mutually agreed upon between the purchaser and the supplier.
The standard states that fuel heating will be required by the gas turbine in almost every installation using Grade No. 3-GT, which may be a heavier distillate, a residual fuel oil, or a blend.