Origin Standard

SH/T 0687-2000 Determination of Lubricity of Aviation Turbine Fuels (Ball Cylinder Lubricity Evaluator Method)

AI-translated method card — human verification pending. This is not an official translation of the standard. Unclear source values remain unverified; check the original standard and product certificate before use.

Card type: Test method

1. Method number / full title / English name / replacement relationship

2. Scope of application and non-applicability

3. Method principle

4. Reagents and materials (purity / preparation)

7.1 Materials

7.2 Reagents

7.3 Reference liquids

5. Instruments and equipment

6. Recommended operating conditions

Table 1 Standard operating conditions:

7. Sampling and sample preparation

8. Analysis Procedure

8 Preparation of Apparatus

9 Calibration and Standardization

10 Test Procedure

11 Measurement of Wear Scar

9. Qualitative and Quantitative and Calculation Formulas

10. Precision

11. Report

12. Referenced Documents

13. Source and verification

This page is an AI translation of the available Chinese method card. Human verification is pending. It is not an official translation of the standard. Check the source standard and product certificate before use.

14. Quick Reference Q&A

Question Key Answer Points
What does this standard test? Boundary lubricity of aviation turbine fuel on rubbing steel surfaces, expressed as test ball wear scar diameter (mm) (1.1, 1.2)
What international standard is adopted? Equivalent adoption of ASTM D5001-1990 (1995) (Foreword)
What is the method principle? A fixed steel ball contacts a rotating steel ring immersed in oil under load, the cylinder rotates to transport the specimen to the ball/ring interface, measure the wear scar diameter (Chapter 4)
Specimen volume and temperature? 50 mL±1.0 mL; 25 ℃±1 ℃ (Table 1)
Relative humidity requirement? At 25 ℃±1 ℃, 10%±0.2% (Table 1)
Applied load? 1000 g (of which weights 500 g) (Table 1)
Rotation speed and test time? 240 r/min±1 r/min; 30 min±0.1 min (Table 1)
Pretreatment conditions? One air stream 0.5 L/min passed into the specimen, another stream 3.3 L/min flowing over the specimen surface 15 min (Table 1)
Air flow rate during test? 3.8 L/min flowing over the specimen surface (Table 1)
Test ring material and hardness? SAE 8720 steel or GB/T 3077 in 20CrNiMo; HRC 58~62 (7.1.1)
Test ball material and hardness? ANSI E-52100 or YB 9 GCr15; HRC 64~66; diameter 12.7 mm (7.1.3)
Reference liquid A/B average WSD? A: 0.56 mm; B: 0.85 mm (9.2.5)
How to calculate wear scar diameter? WSD = (M+N)/2, M major axis, N minor axis (12.1, denominator requires confirmation against the source standard (source-text extraction))
Repeatability formula? r = 0.109 (WSD)^1.80 (13.1, exponent requires confirmation against the source standard (source-text extraction))
Reproducibility formula? R = 0.167 (WSD)^1.80 (13.2, exponent requires confirmation against the source standard (source-text extraction))
Precision applicable range? Wear scar diameter 0.45~0.95 mm, 95% confidence level (Chapter 13)
Result reporting requirements? Take the arithmetic mean of two repeated determination results, accurate to 0.01 mm, and report the wear scar surface condition and deviations (Chapter 14)
Sampling container requirements? Comply with Appendix B; epoxy resin lined containers preferred, also gives cleaning methods for borosilicate glass bottles and tinplate containers (5.3, Appendix B)
What safety warnings are there? Compressed air, isooctane, isopropanol, acetone, isoparaffinic solvent and fuel additives, see Appendix A (A1~A5)

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