The MRQ-001 aircraft is mainly used to determine the lubricity of aviation turbine fuel. The aircraft adopts a friction pair composed of standard steel balls and standard test rings. Under controlled test conditions, the size of the wear marks generated on the steel balls is used to evaluate the boundary lubrication performance of aviation fuel.
Applicable standard
SH/T0687-2000 Aviation Turbine Fuel Lubrication Determination Method (Ball Column Lubrication Evaluation Instrument Method)
ASTM D5001 Test Method for Measuring the Lubrication of Aircraft Turbine Fuel Using a BOCLE Lubrication Evaluator
1. Test load: 10N, can automatically apply load
2. Automatic temperature control: 25 ± 1 ℃, no external cooler required
3. Automatic control of air relative humidity: 10.0% ± 0.2%
4. Automatic control motor speed: 240 ± 1rpm
5. Automatic gas flow rate setting and control: 3.8 ± 0.05L/min, 30min
6. Pre treat 0.5L/min into the sample, 3.3L/min on the surface of the sample, 15 minutes
7. Sample size: 50 ± 0.5ml
8. High precision microscopic testing system with a magnification of over 100 times
9. Workpiece conditions: ambient temperature of 10-35 ℃, relative humidity of 20-80%, voltage of 220V, 50Hz
