Product Performance toetra  of the Aviation Seza lafika Fuel Combustion System

1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen fiaramanidina ahitana solika burner mpandringana, solika nozzle, igniter, solika fiarandalamby, fixer, rivotra Tube sy ny akorany, muffler, Acoustic fanoherana sy ny singa hafa.
3. Equipped with fuel pressure gauge, fuel solenoid valve, fuel temperature detection device, air pressure regulating valve, air temperature detection device;
4. Equipped with a gas and air temperature control device ice bath with a volume not less than 2 x 0.14 m3, the fuel temperature can be controlled.
5. Amin'ny alalan'ny fanovana solika sy ny rivotra nozzle tsindry torohevitra, fitsapana hafa fitsipika azo nihaona.
6. The burner covers the fuel pipeline and fuselage with insulation blanket.
7. The flame temperature provided by NexGen aviation fuel burner is not less than: 2000 +50;
8. NexGen fiaramanidina afaka manome solika burner tsy latsaky ny 10.6w / cm2 ny lelafo hafanana mikoriana.
9. Module unit of NexGen burner support system;
10. Powder coated steel frame, including an integrated digital ruler;
11. Calibrable weighing unit;
12. Movable seat cushion test device, movable drip collecting tray;
13.Seven ceramic-encapsulated, metal sheaths and grounded K-type (nickel-chromium-nickel-aluminium) thermocouples with a diameter of 1.6 mm should be used for calibration. Their conductors should have an external diameter of 0.254 mm, a cross-sectional area of 0.0507 mm2 and a resistance of 361_/km (American wire gauge 30 AWG). The thermocouple should be fixed on an angle steel bracket to form a thermocouple comb so that it can be placed on the sample bracket during calibration.
14. The heat radiation flux sensor is equipped with a cooling device and installed on a fixed bracket.