Aircraft hose and hard tube component combustion tester

Aircraft hose and hard tube component combustion testerPurpose: Used for fire testing of aircraft soft and hard pipe components, electric engine devices, and electrical connectors.

Compliant with standards: FIRE TEST HANDBOOK: Chapter 12, HB 7044 and other testing methods.

Technical features:

1. The conical cylinder of the burner is made of corrosion-resistant and high-temperature resistant alloy.

2. NexGenAviation fuel burnerIncluding components such as turbulence generator, fuel nozzle, igniter, fuel rail, fixing plate, ventilation pipe and housing, muffler, sound resistor, etc.

3. Equipped with fuel pressure gauge, fuel solenoid valve, fuel temperature detection device, air pressure regulating valve, and air temperature detection device.

4. Equipped with a gas and air temperature control device ice bath with a volume of not less than 2 x 0.14m3, which can control the fuel temperature.

By changing the fuel nozzle and air pressure input, different testing standards can be met.

6. Cover the burner with insulation blanket to cover the fuel pipeline and body.

7. The oil pressure regulator should be able to adjust the fuel flow rate to 0.126 L/min.

8. Adjustable air baffle to achieve an air flow rate of approximately 1.89 m3/min.

9. NexGenAviation fuel burnerThe flame temperature that can be provided is not less than 2000 ± 50 ℉.

10. NexGenAviation fuel burnerThe flame heat flow rate that can be provided is not less than: 10.6w/cm2.

11. UseNexGen burnerModule units supporting the system

12. Heavy duty steel frame, capable of installing test samples horizontally and vertically.

13. During calibration, seven ceramic sealed, metal sheathed, grounded K-type (nickel chromium nickel aluminum) thermocouples with a diameter of 1.6 mm should be used. The wires should have an outer diameter of 0.254 mm, a cross-sectional area of 0.0507 mm2, and a resistance of 361 Ω/km (30 AWG according to the American wire gauge). The thermocouple should be fixed on an angle steel bracket to form a thermocouple comb for placement on the sample holder during calibration.

14. Thermal radiation flux sensor, equipped with cooling device, and installed on a fixed bracket.