| Customization: | Available |
|---|---|
| Ambient Temperature: | 10~35ºC |
| Analytical Medium: | Jet Fuel |
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HK-9169 Apparatus for Thermal Oxidation Stability of Aviation Turbine Fuels conformsto ASTM D3241 Standard Test MethodforThermalOxidation Stability of Aviation Fuels.This apparatus is for measuring the high temperature stability of gasturbine fuels uses an instrument that subjects the test fuel to conditions that can berelated to those occurring in gasturbine engine fuel system. The fuel is pumped at a fixedvolumetric flow rate through aheater, after which it enters a precision stainless steelfilter where fuel degradation products may become trapped.
1. Apparatus pressure / flow rate accuracy meets the standard requirements.
2.Touch screen operation, do not need manual operation during the test process, dynamic display the test curve and working parameters.
3.High automation, easy operation, good applicability, safe, reliable and easy maintenance
4.Automatic fault diagnosis and alarm to ensure the system runs properly
5. Reduce 40min operation time to increase the lab efficiency
6.Sealed sample to reduce the fuel exposure
7. Accurate pump system, stable flow pressure
8. Data storage and printing function are available
9. Be able to set the test freely
| Ambient temperature | 10~35ºC | Air relative humidity | ≤85 | Power supply | 220V±10%, 50Hz±10%, 0.6kw |
| Analytical medium | Jet fuel | Coolant flow rate | 38±8L/H | Temperature control range | 100~380ºC |
| Temperature control accuracy | ≤±1ºC | Differential pressure transmitter accuracy | Level 0.075 | Differential pressure display resolution | 0.1mm Hg |
| Sample flow rate | 3ml/min±0.3ml | System operation pressure | 3.45MPa±0.345Mpa | Dimension | 470*540*860mm 45kg |
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