Professional Aviation Fuel Testing Laboratory Equipment Supplier
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Whats/App: +86 156 1874 6768
Web: standard-groups.com
E-mail：info@standard-groups。com
Parameters
| Parameter Category | Details |
|---|---|
| Dimensions | 1500 mm (W) × 1800 mm (H) × 900 mm (D) |
| Weight | 150 kg |
| Fuel Requirement | Aviation kerosene |
| Compressed Air Requirement | ≥ 120 PSI |
| Power Supply | 220 V, 10 A |
| Operating Temperature | 10°C – 35°C |
| Sample Mounting | Horizontal and vertical installation supported |
Features
Burner cone made from corrosion-resistant, high-temperature alloy.
NexGen Aviation Fuel Burner includes diffuser, fuel nozzle, igniter, fuel rail, mounting bracket, ventilation duct, housing, silencer, and acoustic barrier.
Equipped with fuel pressure gauge, fuel solenoid valve, fuel temperature sensor, air regulator, and air temperature sensor.
Fuel and air temperature control baths (≥ 2 × 0.14 m³) maintain stable combustion conditions.
Adjustable fuel nozzle and air pressure allow compliance with multiple test standards.
Insulation blankets cover fuel lines and burner body for safety and heat containment.
Supports modular NexGen burner system units for flexibility.
Heavy-duty steel frame supports horizontal and vertical sample installation.
Calibration employs seven 1.6 mm diameter, ceramic-coated, metal-sheathed, grounded K-type thermocouples (AWG 30. 0.0507 mm² cross-section, 361 Ω/km), mounted on an angle-iron thermocouple comb.
Heat flux sensors with cooling system, mounted on fixed supports for accurate measurement.
Accessories
NexGen Aviation Fuel Burner with full assembly
Fuel and air temperature control baths
Fuel solenoid valve and pressure gauge
Igniter assembly
Adjustable fuel nozzle
Insulation blankets and acoustic silencer
Heavy-duty steel mounting frame
Thermocouple comb for calibration
Heat flux sensors with cooling system
Test Procedures
Ensure the installation area is clear and safe.
Connect the system to a 220 V, 10 A power supply.
Supply aviation kerosene fuel and compressed air ≥ 120 PSI.
Mount the test sample securely on the horizontal or vertical frame.
Apply insulation blankets to fuel lines and burner housing.
Adjust fuel nozzle and air pressure according to the selected test standard.
Activate the igniter and NexGen fuel burner.
Monitor fuel flow, air pressure, flame temperature, and heat flux using sensors.
Conduct automated combustion tests on propulsion components.
Record all data for compliance reporting and analysis.
Shut off fuel and air supply and allow the system to cool before sample removal.
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